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Date:
July 27th 2010
<B> ISS TRAJECTORY DATA</B>
Lift off time (UTC) : N/A
Area (sq ft) : 8880.23
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74
ET - UTC (sec) : 66.18
UT1 - UTC (sec) : 0.00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers.
Coasting Arc #1 (Orbit 2965)
Vector Time (GMT): 2010/207/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5717102.70 A = 6739607.78 meter
Y = -3526312.96 meter E = .0018564
Z = -418678.88 I = 51.82705
XDOT = 2815.697421 Wp = 143.30493
YDOT = -3866.323319 meter/sec RA = 28.85763 deg
ZDOT = -6035.887764 TA = 41.23371
MA = 41.09364
Ha = 196.258 n.mi
Hp = 186.203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18756898.62 X = -5675212.10
Y = -11569268.23 feet Y = -3590010.75 meter
Z = -1373618.38 Z = -446350.53
XDOT = 9237.852431 XDOT = 2888.042646
YDOT = -12684.787793 feet/sec YDOT = -3834.431385 meter/sec
ZDOT = -19802.781379 ZDOT = -6022.034101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 622730.00 X = 189808.10
Y = 22021926.81 feet Y = 6712283.29 meter
Z = -1484246.41 Z = -452398.31
XDOT = -14132.740932 XDOT = -4307.659436
YDOT = -900.344301 feet/sec YDOT = -274.424943 meter/sec
ZDOT = -19747.336617 ZDOT = -6018.988201
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10207.53098269 .00016717 00000-0 10270-3 0 9009
2 25544 51.6423 29.2368 0007425 151.8329 208.3235 15.71362563 29665
Satellite: ISS
Catalog Number: 25544
Epoch time: 10207.53098269 = yrday.fracday
Element set: 900
Inclination: 51.6423 deg
RA of node: 29.2368 deg
Eccentricity: .0007425
Arg of perigee: 151.8329 deg
Mean anomaly: 208.3235 deg
Mean motion: 15.71362563 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 308
Coasting Arc #2 (Orbit 2981)
Vector Time (GMT): 2010/208/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1123075.04 A = 6727891.37 meter
Y = 4035216.39 meter E = .0009794
Z = 5260631.19 I = 51.75928
XDOT = -7190.339566 Wp = 143.68097
YDOT = -2705.907320 meter/sec RA = 23.75270 deg
ZDOT = 532.308459 TA = 301.22216
MA = 301.31810
Ha = 196.414 n.mi
Hp = 186.365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3684629.38 X = -1193668.71
Y = 13238898.91 feet Y = 4022262.35 meter
Z = 17259288.68 Z = 5255004.28
XDOT = -23590.352906 XDOT = -7162.133015
YDOT = -8877.648689 feet/sec YDOT = -2786.156327 meter/sec
ZDOT = 1746.418828 ZDOT = 497.446870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13072276.65 X = 3984429.92
Y = -4328765.63 feet Y = -1319407.76 meter
Z = 17236744.33 Z = 5253759.67
XDOT = 5642.824603 XDOT = 1719.932939
YDOT = 23547.393545 feet/sec YDOT = 7177.245553 meter/sec
ZDOT = 1607.028774 ZDOT = 489.822370
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10208.54854054 .00016717 00000-0 10270-3 0 9014
2 25544 51.6416 24.0311 0007644 155.3537 204.7991 15.71295665 29826
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208.54854054 = yrday.fracday
Element set: 901
Inclination: 51.6416 deg
RA of node: 24.0311 deg
Eccentricity: .0007644
Arg of perigee: 155.3537 deg
Mean anomaly: 204.7991 deg
Mean motion: 15.71295665 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 2982
Checksum: 304
Coasting Arc #3 (Orbit 2996)
Vector Time (GMT): 2010/209/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6517634.00 A = 6738981.46 meter
Y = 1098314.22 meter E = .0008177
Z = -1321691.16 I = 51.76954
XDOT = 341.100511 Wp = 90.28639
YDOT = 4978.381138 meter/sec RA = 18.62891 deg
ZDOT = 5850.071472 TA = 255.25843
MA = 255.34906
Ha = 196.238 n.mi
Hp = 186.432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21383313.65 X = 6511288.45
Y = 3603393.10 feet Y = 1171162.90 meter
Z = -4336257.10 Z = -1290044.49
XDOT = 1119.096165 XDOT = 256.987990
YDOT = 16333.271451 feet/sec YDOT = 4981.724853 meter/sec
ZDOT = 19193.147874 ZDOT = 5851.524520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9419779.08 X = -2871148.66
Y = -19559646.42 feet Y = -5961780.23 meter
Z = -4209710.65 Z = -1283119.81
XDOT = 11328.936970 XDOT = 3453.059988
YDOT = -9565.443565 feet/sec YDOT = -2915.547199 meter/sec
ZDOT = 19198.909115 ZDOT = 5851.827498
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10209.50248946 .00016717 00000-0 10270-3 0 9029
2 25544 51.6422 19.1509 0007736 159.5539 200.5934 15.71358465 29972
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209.50248946 = yrday.fracday
Element set: 902
Inclination: 51.6422 deg
RA of node: 19.1509 deg
Eccentricity: .0007736
Arg of perigee: 159.5539 deg
Mean anomaly: 200.5934 deg
Mean motion: 15.71358465 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 325
Coasting Arc #4 (Orbit 3012)
Vector Time (GMT): 2010/210/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1718202.59 A = 6729422.56 meter
Y = -4351186.72 meter E = .0014425
Z = -4847961.29 I = 51.70932
XDOT = 7295.871754 Wp = 104.67117
YDOT = -201.893970 meter/sec RA = 13.55218 deg
ZDOT = -2414.120677 TA = 141.79554
MA = 141.69323
Ha = 196.109 n.mi
Hp = 186.416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5637147.59 X = -1645869.01
Y = -14275546.98 feet Y = -4369996.01 meter
Z = -15905384.81 Z = -4856132.70
XDOT = 23936.587121 XDOT = 7309.314282
YDOT = -662.381790 feet/sec YDOT = -120.231887 meter/sec
ZDOT = -7920.343428 ZDOT = -2378.645306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8234257.24 X = -2509801.61
Y = 12912261.24 feet Y = 3935657.23 meter
Z = -15938019.26 Z = -4857908.27
XDOT = -13775.723376 XDOT = -4198.840485
YDOT = -18347.559987 feet/sec YDOT = -5592.336284 meter/sec
ZDOT = -7778.478224 ZDOT = -2370.880163
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10210.52002812 .00016717 00000-0 10270-3 0 9034
2 25544 51.6428 13.9464 0007696 162.2144 197.9288 15.71383182 30133
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210.52002812 = yrday.fracday
Element set: 903
Inclination: 51.6428 deg
RA of node: 13.9464 deg
Eccentricity: .0007696
Arg of perigee: 162.2144 deg
Mean anomaly: 197.9288 deg
Mean motion: 15.71383182 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 291
Coasting Arc #5 (Orbit 3028)
Vector Time (GMT): 2010/211/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5920550.09 A = 6736212.59 meter
Y = 1410107.92 meter E = .0017867
Z = 2861476.45 I = 51.70158
XDOT = -3551.465572 Wp = 122.42921
YDOT = -4578.343086 meter/sec RA = 8.39855 deg
ZDOT = -5078.493356 TA = 24.74023
MA = 24.65466
Ha = 196.106 n.mi
Hp = 186.705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19424376.95 X = -5949778.50
Y = 4626338.30 feet Y = 1343737.24 meter
Z = 9388046.10 Z = 2832643.88
XDOT = -11651.789934 XDOT = -3475.335684
YDOT = -15020.810649 feet/sec YDOT = -4617.631818 meter/sec
ZDOT = -16661.723610 ZDOT = -5095.561418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15471528.13 X = 4715721.77
Y = 12707988.60 feet Y = 3873394.92 meter
Z = 9272738.47 Z = 2826330.68
XDOT = -4040.545496 XDOT = -1231.558267
YDOT = 17159.447071 feet/sec YDOT = 5230.199467 meter/sec
ZDOT = -16729.930024 ZDOT = -5099.282671
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10211.53755768 .00016717 00000-0 10270-3 0 9042
2 25544 51.6423 8.7406 0007692 167.3042 192.8315 15.71368007 30296
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211.53755768 = yrday.fracday
Element set: 904
Inclination: 51.6423 deg
RA of node: 8.7406 deg
Eccentricity: .0007692
Arg of perigee: 167.3042 deg
Mean anomaly: 192.8315 deg
Mean motion: 15.71368007 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 302
Coasting Arc #6 (Orbit 3044)
Vector Time (GMT): 2010/212/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4337835.94 A = 6732834.31 meter
Y = 3348907.03 meter E = .0015483
Z = 3908350.50 I = 51.66173
XDOT = -5882.049451 Wp = 128.05631
YDOT = 2866.879436 meter/sec RA = 3.33521 deg
ZDOT = 4051.686861 TA = 279.69856
MA = 279.87341
Ha = 195.814 n.mi
Hp = 186.738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14231745.20 X = 4281079.57
Y = 10987227.80 feet Y = 3397097.81 meter
Z = 12822672.23 Z = 3929285.78
XDOT = -19298.062504 XDOT = -5933.352423
YDOT = 9405.772428 feet/sec YDOT = 2800.815824 meter/sec
ZDOT = 13292.935896 ZDOT = 4022.987648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -127284.93 X = -38796.45
Y = -17919056.55 feet Y = -5461728.44 meter
Z = 12906350.39 Z = 3933855.60
XDOT = 18072.021443 XDOT = 5508.352136
YDOT = 9410.782346 feet/sec YDOT = 2868.406459 meter/sec
ZDOT = 13178.152437 ZDOT = 4016.700863
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10212.55507786 .00016717 00000-0 10270-3 0 9051
2 25544 51.6432 3.5357 0007722 171.2386 188.8912 15.71416642 30458
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212.55507786 = yrday.fracday
Element set: 905
Inclination: 51.6432 deg
RA of node: 3.5357 deg
Eccentricity: .0007722
Arg of perigee: 171.2386 deg
Mean anomaly: 188.8912 deg
Mean motion: 15.71416642 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 303
Coasting Arc #7 (Orbit 3059)
Vector Time (GMT): 2010/213/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4115211.54 A = 6732322.12 meter
Y = -3395199.69 meter E = .0012864
Z = -4120154.45 I = 51.63041
XDOT = 6084.912859 Wp = 141.38263
YDOT = 2793.534815 meter/sec RA = 358.16976 deg
ZDOT = 3772.075210 TA = 167.39289
MA = 167.36068
Ha = 195.789 n.mi
Hp = 187.003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13501350.20 X = 4172886.27
Y = -11139106.59 feet Y = -3348858.26 meter
Z = -13517567.10 Z = -4100022.95
XDOT = 19963.624867 XDOT = 6034.898856
YDOT = 9165.140469 feet/sec YDOT = 2861.300125 meter/sec
ZDOT = 12375.574837 ZDOT = 3801.514179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17216897.16 X = -5247710.26
Y = -3480688.69 feet Y = -1060913.91 meter
Z = -13437039.53 Z = -4095609.65
XDOT = -5726.319508 XDOT = -1745.382186
YDOT = -19949.977308 feet/sec YDOT = -6080.753084 meter/sec
ZDOT = 12493.255185 ZDOT = 3807.944180
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10213.50899645 .00016717 00000-0 10270-3 0 9066
2 25544 51.6443 358.6566 0007655 173.9550 186.1705 15.71404052 30603
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213.50899645 = yrday.fracday
Element set: 906
Inclination: 51.6443 deg
RA of node: 358.6566 deg
Eccentricity: .0007655
Arg of perigee: 173.9550 deg
Mean anomaly: 186.1705 deg
Mean motion: 15.71404052 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 313
Coasting Arc #8 (Orbit 3075)
Vector Time (GMT): 2010/214/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6049016.24 A = 6736444.56 meter
Y = -1360457.74 meter E = .0011284
Z = -2622243.02 I = 51.61443
XDOT = 3293.031267 Wp = 157.07799
YDOT = -4578.700180 meter/sec RA = 353.10025 deg
ZDOT = -5238.631389 TA = 52.71996
MA = 52.61713
Ha = 195.541 n.mi
Hp = 187.031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19845853.80 X = -6020615.45
Y = -4463444.01 feet Y = -1427942.50 meter
Z = -8603159.53 Z = -2651560.12
XDOT = 10803.908355 XDOT = 3369.434599
YDOT = -15021.982217 feet/sec YDOT = -4541.448026 meter/sec
ZDOT = -17187.110856 ZDOT = -5222.448602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9366246.25 X = 2854831.86
Y = 18000647.31 feet Y = 5486597.30 meter
Z = -8720362.78 Z = -2657966.58
XDOT = -17200.618449 XDOT = -5242.748503
YDOT = 682.891107 feet/sec YDOT = 208.145210 meter/sec
ZDOT = -17122.360293 ZDOT = -5218.895417
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10214.52649983 .00016717 00000-0 10270-3 0 9078
2 25544 51.6441 353.4514 0007580 178.0177 182.1017 15.71425866 30760
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214.52649983 = yrday.fracday
Element set: 907
Inclination: 51.6441 deg
RA of node: 353.4514 deg
Eccentricity: .0007580
Arg of perigee: 178.0177 deg
Mean anomaly: 182.1017 deg
Mean motion: 15.71425866 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 312
Coasting Arc #9 (Orbit 3091)
Vector Time (GMT): 2010/215/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1496167.34 A = 6729061.38 meter
Y = 4321425.33 meter E = .0006638
Z = 4930487.39 I = 51.55963
XDOT = -7401.477532 Wp = 128.06011
YDOT = -142.308443 meter/sec RA = 347.94169 deg
ZDOT = -2123.356482 TA = 342.53867
MA = 342.56148
Ha = 195.599 n.mi
Hp = 187.246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4908685.49 X = -1568330.44
Y = 14177904.63 feet Y = 4304290.43 meter
Z = 16176139.73 Z = 4923044.08
XDOT = -24283.062770 XDOT = -7389.021273
YDOT = -466.891218 feet/sec YDOT = -225.006382 meter/sec
ZDOT = -6966.392656 ZDOT = -2159.282488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13966078.23 X = 4256860.65
Y = -5569581.68 feet Y = -1697608.50 meter
Z = 16146333.58 Z = 4921402.48
XDOT = 15204.316387 XDOT = 4634.275635
YDOT = 17533.581828 feet/sec YDOT = 5344.235741 meter/sec
ZDOT = -7110.030131 ZDOT = -2167.137184
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10215.54399600 .00016717 00000-0 10270-3 0 9080
2 25544 51.6445 348.2467 0007580 180.9853 179.1295 15.71400042 30927
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215.54399600 = yrday.fracday
Element set: 908
Inclination: 51.6445 deg
RA of node: 348.2467 deg
Eccentricity: .0007580
Arg of perigee: 180.9853 deg
Mean anomaly: 179.1295 deg
Mean motion: 15.71400042 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 311
Coasting Arc #10 (Orbit 3107)
Vector Time (GMT): 2010/216/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6554646.76 A = 6738885.65 meter
Y = -1146125.32 meter E = .0010852
Z = 1055822.22 I = 51.56506
XDOT = -96.766025 Wp = 89.40371
YDOT = 4932.133879 meter/sec RA = 342.84783 deg
ZDOT = 5902.640220 TA = 282.13692
MA = 282.25847
Ha = 195.339 n.mi
Hp = 187.313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21504746.57 X = 6561846.81
Y = -3760253.68 feet Y = -1072787.18 meter
Z = 3463983.66 Z = 1087681.93
XDOT = -317.473834 XDOT = -180.584674
YDOT = 16181.541598 feet/sec YDOT = 4930.582581 meter/sec
ZDOT = 19365.617520 ZDOT = 5901.966996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17209253.56 X = -5245380.48
Y = -13399119.96 feet Y = -4084051.76 meter
Z = 3591377.45 Z = 1094651.85
XDOT = 11306.866546 XDOT = 3446.332923
YDOT = -9288.045795 feet/sec YDOT = -2830.996358 meter/sec
ZDOT = 19362.871628 ZDOT = 5901.803272
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10216.56147967 .00016717 00000-0 10270-3 0 9091
2 25544 51.6455 343.0416 0007534 185.5420 174.5660 15.71463538 31087
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216.56147967 = yrday.fracday
Element set: 909
Inclination: 51.6455 deg
RA of node: 343.0416 deg
Eccentricity: .0007534
Arg of perigee: 185.5420 deg
Mean anomaly: 174.5660 deg
Mean motion: 15.71463538 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 312
Coasting Arc #11 (Orbit 3122)
Vector Time (GMT): 2010/217/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1284284.09 A = 6727320.82 meter
Y = -4000825.73 meter E = .0015906
Z = -5265866.71 I = 51.49772
XDOT = 7191.381002 Wp = 119.64434
YDOT = -2698.776336 meter/sec RA = 337.71199 deg
ZDOT = 289.469965 TA = 153.15511
MA = 153.07271
Ha = 195.133 n.mi
Hp = 187.459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4213530.47 X = -1213870.25
Y = -13126068.67 feet Y = -4014793.10 meter
Z = -17276465.59 Z = -5271935.11
XDOT = 23593.769690 XDOT = 7219.618549
YDOT = -8854.253070 feet/sec YDOT = -2618.200161 meter/sec
ZDOT = 949.704609 ZDOT = 324.473725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6764273.74 X = -2061750.64
Y = 11977257.12 feet Y = 3650667.97 meter
Z = -17300684.78 Z = -5273248.72
XDOT = -21718.991687 XDOT = -6619.948666
YDOT = -10658.527337 feet/sec YDOT = -3248.719132 meter/sec
ZDOT = 1089.688393 ZDOT = 332.137022
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10217.51536466 .00016717 00000-0 10270-3 0 9105
2 25544 51.6455 338.1627 0007382 189.3638 170.7388 15.71484010 31230
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217.51536466 = yrday.fracday
Element set: 910
Inclination: 51.6455 deg
RA of node: 338.1627 deg
Eccentricity: .0007382
Arg of perigee: 189.3638 deg
Mean anomaly: 170.7388 deg
Mean motion: 15.71484010 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 309
Coasting Arc #12 (Orbit 3138)
Vector Time (GMT): 2010/218/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5734380.41 A = 6739269.09 meter
Y = 3474821.86 meter E = .0017705
Z = 558498.45 I = 51.51050
XDOT = -2924.758820 Wp = 151.24239
YDOT = -3852.901734 meter/sec RA = 332.58324 deg
ZDOT = -5995.042757 TA = 22.66993
MA = 22.59183
Ha = 195.022 n.mi
Hp = 187.745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18813584.01 X = -5775523.36
Y = 11400334.17 feet Y = 3410466.48 meter
Z = 1832343.98 Z = 530541.62
XDOT = -9595.665419 XDOT = -2852.335122
YDOT = -12640.753720 feet/sec YDOT = -3885.202517 meter/sec
ZDOT = -19668.775448 ZDOT = -6009.075580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21290697.82 X = 6489404.70
Y = 5569742.07 feet Y = 1697657.38 meter
Z = 1720525.08 Z = 524416.04
XDOT = -2064.648018 XDOT = -629.304716
YDOT = 14053.606487 feet/sec YDOT = 4283.539257 meter/sec
ZDOT = -19724.843408 ZDOT = -6012.132271
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10218.53283329 .00016717 00000-0 10270-3 0 9116
2 25544 51.6458 332.9571 0007425 193.5613 166.5350 15.71471717 31390
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218.53283329 = yrday.fracday
Element set: 911
Inclination: 51.6458 deg
RA of node: 332.9571 deg
Eccentricity: .0007425
Arg of perigee: 193.5613 deg
Mean anomaly: 166.5350 deg
Mean motion: 15.71471717 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 310
Coasting Arc #13 (Orbit 3154)
Vector Time (GMT): 2010/219/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3654135.45 A = 6727936.54 meter
Y = 2471708.16 meter E = .0009891
Z = 5080459.37 I = 51.44753
XDOT = -5597.960108 Wp = 170.07917
YDOT = 5045.769099 meter/sec RA = 327.47390 deg
ZDOT = 1561.476271 TA = 264.82822
MA = 264.94111
Ha = 194.701 n.mi
Hp = 187.856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11988633.37 X = 3601545.26
Y = 8109278.74 feet Y = 2512276.30 meter
Z = 16668173.79 Z = 5098083.38
XDOT = -18366.010854 XDOT = -5661.552003
YDOT = 16554.360560 feet/sec YDOT = 4982.813634 meter/sec
ZDOT = 5122.953646 ZDOT = 1534.127934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2703646.39 X = -824071.42
Y = -14135934.19 feet Y = -4308632.74 meter
Z = 16738620.32 Z = 5101931.47
XDOT = 23685.748538 XDOT = 7219.416154
YDOT = 1445.338570 feet/sec YDOT = 440.539196 meter/sec
ZDOT = 5013.551478 ZDOT = 1528.130490
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10219.55029146 .00016717 00000-0 10270-3 0 9125
2 25544 51.6466 327.7521 0007325 198.0553 162.0350 15.71525668 31552
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219.55029146 = yrday.fracday
Element set: 912
Inclination: 51.6466 deg
RA of node: 327.7521 deg
Eccentricity: .0007325
Arg of perigee: 198.0553 deg
Mean anomaly: 162.0350 deg
Mean motion: 15.71525668 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 301
Coasting Arc #14 (Orbit 3169)
Vector Time (GMT): 2010/220/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3843956.98 A = 6737441.30 meter
Y = -5110363.73 meter E = .0002324
Z = -2126341.96 I = 51.45423
XDOT = 5135.368494 Wp = 137.96150
YDOT = 1573.616602 meter/sec RA = 322.31289 deg
ZDOT = 5503.420279 TA = 198.24538
MA = 198.25371
Ha = 194.656 n.mi
Hp = 188.181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12611407.42 X = 3911145.47
Y = -16766285.20 feet Y = -5067002.45 meter
Z = -6976187.55 Z = -2107505.68
XDOT = 16848.321832 XDOT = 5090.656335
YDOT = 5162.784126 feet/sec YDOT = 1630.792887 meter/sec
ZDOT = 18055.840812 ZDOT = 5528.258875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20742087.28 X = -6322188.20
Y = 3311727.17 feet Y = 1009414.44 meter
Z = -6900825.13 Z = -2103371.50
XDOT = -8243.879593 XDOT = -2512.734500
YDOT = -13814.649438 feet/sec YDOT = -4210.705149 meter/sec
ZDOT = 18155.149517 ZDOT = 5533.689573
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10220.50415291 .00016717 00000-0 10270-3 0 9133
2 25544 51.6468 322.8728 0007111 202.1638 157.9217 15.71477871 31707
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220.50415291 = yrday.fracday
Element set: 913
Inclination: 51.6468 deg
RA of node: 322.8728 deg
Eccentricity: .0007111
Arg of perigee: 202.1638 deg
Mean anomaly: 157.9217 deg
Mean motion: 15.71477871 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 294
Coasting Arc #15 (Orbit 3185)
Vector Time (GMT): 2010/221/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5056720.53 A = 6730618.35 meter
Y = -151789.49 meter E = .0006710
Z = -4442785.75 I = 51.40838
XDOT = 3017.216952 Wp = 117.35900
YDOT = -6298.662667 meter/sec RA = 317.22464 deg
ZDOT = -3225.721929 TA = 120.23095
MA = 120.16450
Ha = 194.432 n.mi
Hp = 188.174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16590290.45 X = -5033065.66
Y = -497997.01 feet Y = -208204.25 meter
Z = -14576068.74 Z = -4467293.24
XDOT = 9899.005747 XDOT = 3103.095084
YDOT = -20664.903763 feet/sec YDOT = -6264.441989 meter/sec
ZDOT = -10583.077195 ZDOT = -3210.856420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11749573.49 X = 3581270.00
Y = 11600292.18 feet Y = 3535769.06 meter
Z = -14674067.67 Z = -4472655.83
XDOT = -20519.133678 XDOT = -6254.231945
YDOT = 7498.992019 feet/sec YDOT = 2285.692767 meter/sec
ZDOT = -10523.592672 ZDOT = -3207.591046
The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10221.52159565 .00016717 00000-0 10270-3 0 9146
2 25544 51.6467 317.6682 0007238 205.7480 154.3322 15.71503628 31866
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221.52159565 = yrday.fracday
Element set: 914
Inclination: 51.6467 deg
RA of node: 317.6682 deg
Eccentricity: .0007238
Arg of perigee: 205.7480 deg
Mean anomaly: 154.3322 deg
Mean motion: 15.71503628 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 306
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics
DOD C-Band Radar Network
Goddard Space Flight Center (GSFC)
NASA Johnson Space Center (JSC)
DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command.
David Cottle
Director Of Engineering
IDB Communications
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