Date: March 10th 2010
<B> ISS TRAJECTORY DATA</B>
Lift off time (UTC) : N/A
Area (sq ft) : 18836.84
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 763)
Vector Time (GMT): 2010/067/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6234802.97 A = 6730671.74 meter
Y = 1045767.73 meter E = .0013586
Z = -2295663.59 I = 51.81059
XDOT = 1106.466435 Wp = 32.18011
YDOT = 5321.865514 meter/sec RA = 26.11907 deg
ZDOT = 5455.335592 TA = 302.08120
MA = 302.21303
Ha = 192.727 n.mi
Hp = 182.606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20455390.31 X = 6233797.35
Y = 3430996.50 feet Y = 1115483.32 meter
Z = -7531704.71 Z = -2265377.91
XDOT = 3630.139224 XDOT = 1020.373567
YDOT = 17460.188693 feet/sec YDOT = 5333.757445 meter/sec
ZDOT = 17898.082651 ZDOT = 5460.501464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16820256.55 X = 5126814.20
Y = -12209495.86 feet Y = -3721454.34 meter
Z = -7411375.44 Z = -2258987.23
XDOT = 14030.020551 XDOT = 4276.350264
YDOT = 8503.839446 feet/sec YDOT = 2591.970263 meter/sec
ZDOT = 17918.706991 ZDOT = 5461.621891
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 10067.67113940 .00016717 00000-0 10270-3 0 9002
2 25544 51.6488 26.6488 0007819 24.1633 335.9895 15.73746945 7642
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067.67113940 = yrday.fracday
Element set: 900
Inclination: 51.6488 deg
RA of node: 26.6488 deg
Eccentricity: .0007819
Arg of perigee: 24.1633 deg
Mean anomaly: 335.9895 deg
Mean motion: 15.73746945 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 764
Checksum: 338
Coasting Arc #2 (Orbit 779)
Vector Time (GMT): 2010/068/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1443844.14 A = 6723017.77 meter
Y = -4559344.27 meter E = .0017924
Z = -4741953.17 I = 51.75796
XDOT = 7188.652573 Wp = 53.22008
YDOT = 507.495855 meter/sec RA = 21.03651 deg
ZDOT = -2673.210459 TA = 190.47779
MA = 190.51519
Ha = 192.674 n.mi
Hp = 182.361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4737021.46 X = -1369718.34
Y = -14958478.58 feet Y = -4575075.90 meter
Z = -15557589.14 Z = -4748787.02
XDOT = 23584.818152 XDOT = 7195.429101
YDOT = 1665.012649 feet/sec YDOT = 587.921434 meter/sec
ZDOT = -8770.375521 ZDOT = -2638.272246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14043872.28 X = -4280572.27
Y = -6936637.72 feet Y = -2114287.18 meter
Z = -15584824.09 Z = -4750254.38
XDOT = 16982.356658 XDOT = 5176.222309
YDOT = -14963.235532 feet/sec YDOT = -4560.794190 meter/sec
ZDOT = -8631.573660 ZDOT = -2630.903652
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 10068.68713421 .00016717 00000-0 10270-3 0 9015
2 25544 51.6491 21.4339 0007864 27.3490 332.8086 15.73783857 7809
Satellite: ISS
Catalog Number: 25544
Epoch time: 10068.68713421 = yrday.fracday
Element set: 901
Inclination: 51.6491 deg
RA of node: 21.4339 deg
Eccentricity: .0007864
Arg of perigee: 27.3490 deg
Mean anomaly: 332.8086 deg
Mean motion: 15.73783857 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 780
Checksum: 318
Coasting Arc #3 (Orbit 795)
Vector Time (GMT): 2010/069/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6292390.47 A = 6730441.09 meter
Y = 155696.46 meter E = .0017698
Z = 2372968.72 I = 51.75390
XDOT = -2174.373279 Wp = 81.17621
YDOT = -5041.776060 meter/sec RA = 15.86985 deg
ZDOT = -5398.225279 TA = 72.13291
MA = 71.93996
Ha = 192.794 n.mi
Hp = 182.311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20644325.69 X = -6305191.03
Y = 510815.15 feet Y = 85259.76 meter
Z = 7785330.45 Z = 2342369.86
XDOT = -7133.770601 XDOT = -2091.610609
YDOT = -16541.260041 feet/sec YDOT = -5065.628714 meter/sec
ZDOT = -17710.712859 ZDOT = -5408.586872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13615335.18 X = -4149954.16
Y = 15586841.02 feet Y = 4750869.14 meter
Z = 7663779.78 Z = 2335920.08
XDOT = -15802.752564 XDOT = -4816.678981
YDOT = -5015.382351 feet/sec YDOT = -1528.688541 meter/sec
ZDOT = -17751.971505 ZDOT = -5410.800915
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 10069.70311080 .00016717 00000-0 10270-3 0 9025
2 25544 51.6489 16.2186 0007818 32.0999 328.0639 15.73777997 7960
Satellite: ISS
Catalog Number: 25544
Epoch time: 10069.70311080 = yrday.fracday
Element set: 902
Inclination: 51.6489 deg
RA of node: 16.2186 deg
Eccentricity: .0007818
Arg of perigee: 32.0999 deg
Mean anomaly: 328.0639 deg
Mean motion: 15.73777997 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 796
Checksum: 339
Coasting Arc #4 (Orbit 811)
Vector Time (GMT): 2010/070/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2338546.40 A = 6723080.11 meter
Y = 4208781.83 meter E = .0011717
Z = 4681242.07 I = 51.70083
XDOT = -7137.687762 Wp = 75.69427
YDOT = 873.419526 meter/sec RA = 10.78367 deg
ZDOT = 2777.492044 TA = 346.96060
MA = 346.99087
Ha = 192.728 n.mi
Hp = 182.088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7672396.34 X = 2268569.13
Y = 13808339.35 feet Y = 4234541.90 meter
Z = 15358405.76 Z = 4692432.22
XDOT = -23417.610768 XDOT = -7160.416261
YDOT = 2865.549627 feet/sec YDOT = 793.474767 meter/sec
ZDOT = 9112.506706 ZDOT = 2742.762672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15361986.40 X = 4682333.46
Y = 3489315.47 feet Y = 1063543.35 meter
Z = 15402940.63 Z = 4694816.30
XDOT = -13174.175798 XDOT = -4015.488783
YDOT = 18341.620608 feet/sec YDOT = 5590.525961 meter/sec
ZDOT = 8974.563903 ZDOT = 2735.447078
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 10070.71906562 .00016717 00000-0 10270-3 0 9034
2 25544 51.6493 11.0031 0007861 35.0501 325.1178 15.73818058 8126
Satellite: ISS
Catalog Number: 25544
Epoch time: 10070.71906562 = yrday.fracday
Element set: 903
Inclination: 51.6493 deg
RA of node: 11.0031 deg
Eccentricity: .0007861
Arg of perigee: 35.0501 deg
Mean anomaly: 325.1178 deg
Mean motion: 15.73818058 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 812
Checksum: 274
Coasting Arc #5 (Orbit 826)
Vector Time (GMT): 2010/071/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6109723.10 A = 6730023.22 meter
Y = -1356839.95 meter E = .0013233
Z = -2465751.95 I = 51.69434
XDOT = 3158.186131 Wp = 40.91449
YDOT = 4553.317582 meter/sec RA = 5.61118 deg
ZDOT = 5345.781298 TA = 291.23791
MA = 291.37920
Ha = 192.788 n.mi
Hp = 182.027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20045023.30 X = 6136419.37
Y = -4451574.65 feet Y = -1288368.34 meter
Z = -8089737.37 Z = -2436006.59
XDOT = 10361.503055 XDOT = 3081.067110
YDOT = 14938.705977 feet/sec YDOT = 4588.203554 meter/sec
ZDOT = 17538.652553 ZDOT = 5360.935733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9689492.84 X = 2953357.42
Y = -18155730.17 feet Y = -5533866.56 meter
Z = -7971606.93 Z = -2429745.79
XDOT = 16695.289911 XDOT = 5088.724365
YDOT = 1220.789683 feet/sec YDOT = 372.096695 meter/sec
ZDOT = 17598.942421 ZDOT = 5364.157650
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 10071.67150478 .00016717 00000-0 10270-3 0 9048
2 25544 51.6491 6.1136 0007803 37.0306 323.1395 15.73852144 8275
Satellite: ISS
Catalog Number: 25544
Epoch time: 10071.67150478 = yrday.fracday
Element set: 904
Inclination: 51.6491 deg
RA of node: 6.1136 deg
Eccentricity: .0007803
Arg of perigee: 37.0306 deg
Mean anomaly: 323.1395 deg
Mean motion: 15.73852144 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 827
Checksum: 287
Coasting Arc #6 (Orbit 842)
Vector Time (GMT): 2010/072/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3120438.55 A = 6722985.26 meter
Y = -3721617.91 meter E = .0018085
Z = -4666277.13 I = 51.64053
XDOT = 6811.628399 Wp = 57.85520
YDOT = -2171.393973 meter/sec RA = .52129 deg
ZDOT = -2821.792968 TA = 184.21967
MA = 184.23494
Ha = 192.692 n.mi
Hp = 181.776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10237659.29 X = -3055923.33
Y = -12210032.50 feet Y = -3756152.25 meter
Z = -15309308.18 Z = -4681278.86
XDOT = 22347.862201 XDOT = 6849.110565
YDOT = -7123.995975 feet/sec YDOT = -2095.013004 meter/sec
ZDOT = -9257.850946 ZDOT = -2788.611442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15876484.58 X = -4839152.50
Y = 36752.11 feet Y = 11202.04 meter
Z = -15368974.10 Z = -4684463.31
XDOT = 8791.255935 XDOT = 2679.574809
YDOT = -20645.052828 feet/sec YDOT = -6292.612102 meter/sec
ZDOT = -9126.094171 ZDOT = -2781.633503
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 10072.68742080 .00016717 00000-0 10270-3 0 9057
2 25544 51.6486 .8978 0007714 40.4919 319.6817 15.73889526 8434
Satellite: ISS
Catalog Number: 25544
Epoch time: 10072.68742080 = yrday.fracday
Element set: 905
Inclination: 51.6486 deg
RA of node: .8978 deg
Eccentricity: .0007714
Arg of perigee: 40.4919 deg
Mean anomaly: 319.6817 deg
Mean motion: 15.73889526 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 843
Checksum: 335
Coasting Arc #7 (Orbit 858)
Vector Time (GMT): 2010/073/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5766808.96 A = 6729781.61 meter
Y = 2427568.83 meter E = .0018960
Z = 2465135.99 I = 51.63396
XDOT = -3943.299644 Wp = 83.87323
YDOT = -3914.510462 meter/sec RA = 355.34416 deg
ZDOT = -5332.916136 TA = 68.25361
MA = 68.05191
Ha = 192.745 n.mi
Hp = 181.686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18919976.90 X = -5805500.87
Y = 7964464.67 feet Y = 2362864.88 meter
Z = 8087716.51 Z = 2437027.00
XDOT = -12937.334791 XDOT = -3873.327855
YDOT = -12842.882094 feet/sec YDOT = -3958.216145 meter/sec
ZDOT = -17496.444016 ZDOT = -5351.902002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5612193.97 X = -1710596.72
Y = 19791264.60 feet Y = 6032377.45 meter
Z = 7976121.00 Z = 2431121.68
XDOT = -16601.441082 XDOT = -5060.119242
YDOT = 2423.619977 feet/sec YDOT = 738.719369 meter/sec
ZDOT = -17571.937071 ZDOT = -5355.926419
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 10073.70331694 .00016717 00000-0 10270-3 0 9067
2 25544 51.6491 355.6825 0007811 44.5357 315.6432 15.73940294 8597
Satellite: ISS
Catalog Number: 25544
Epoch time: 10073.70331694 = yrday.fracday
Element set: 906
Inclination: 51.6491 deg
RA of node: 355.6825 deg
Eccentricity: .0007811
Arg of perigee: 44.5357 deg
Mean anomaly: 315.6432 deg
Mean motion: 15.73940294 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 859
Checksum: 318
Coasting Arc #8 (Orbit 874)
Vector Time (GMT): 2010/074/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3740454.70 A = 6722920.02 meter
Y = 3092012.70 meter E = .0012991
Z = 4640728.30 I = 51.58007
XDOT = -6322.177728 Wp = 82.67773
YDOT = 3374.032627 meter/sec RA = 350.24947 deg
ZDOT = 2842.536419 TA = 339.22194
MA = 339.27470
Ha = 192.700 n.mi
Hp = 181.582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12271833.02 X = 3683057.68
Y = 10144398.62 feet Y = 3133520.31 meter
Z = 15225486.55 Z = 4658759.46
XDOT = -20742.052914 XDOT = -6373.245272
YDOT = 11069.660850 feet/sec YDOT = 3303.049078 meter/sec
ZDOT = 9325.906888 ZDOT = 2811.699161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15471886.63 X = 4715831.04
Y = -3455366.83 feet Y = -1053195.81 meter
Z = 15297166.86 Z = 4662576.46
XDOT = -4180.241053 XDOT = -1274.137473
YDOT = 22101.212564 feet/sec YDOT = 6736.449589 meter/sec
ZDOT = 9203.503241 ZDOT = 2805.227788
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 10074.71919381 .00016717 00000-0 10270-3 0 9075
2 25544 51.6482 350.4662 0007785 48.3978 311.7851 15.73919911 8752
Satellite: ISS
Catalog Number: 25544
Epoch time: 10074.71919381 = yrday.fracday
Element set: 907
Inclination: 51.6482 deg
RA of node: 350.4662 deg
Eccentricity: .0007785
Arg of perigee: 48.3978 deg
Mean anomaly: 311.7851 deg
Mean motion: 15.73919911 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 875
Checksum: 341
Coasting Arc #9 (Orbit 889)
Vector Time (GMT): 2010/075/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5224968.39 A = 6729620.35 meter
Y = -3433574.60 meter E = .0012995
Z = -2484530.20 I = 51.57247
XDOT = 4586.245047 Wp = 49.59766
YDOT = 3146.977679 meter/sec RA = 345.06663 deg
ZDOT = 5322.273779 TA = 282.27684
MA = 282.42232
Ha = 192.703 n.mi
Hp = 181.525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17142284.74 X = 5275044.23
Y = -11265008.53 feet Y = -3374866.20 meter
Z = -8151345.80 Z = -2459025.41
XDOT = 15046.735718 XDOT = 4524.859615
YDOT = 10324.729919 feet/sec YDOT = 3197.921199 meter/sec
ZDOT = 17461.528145 ZDOT = 5344.404157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1219070.30 X = 371572.63
Y = -20516141.79 feet Y = -6253320.02 meter
Z = -8050128.91 Z = -2453679.29
XDOT = 15706.940197 XDOT = 4787.475372
YDOT = -5918.269578 feet/sec YDOT = -1803.888567 meter/sec
ZDOT = 17549.485273 ZDOT = 5349.083111
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 10075.67155720 .00016717 00000-0 10270-3 0 9081
2 25544 51.6472 345.5759 0007578 51.3717 308.8123 15.73975688 8907
Satellite: ISS
Catalog Number: 25544
Epoch time: 10075.67155720 = yrday.fracday
Element set: 908
Inclination: 51.6472 deg
RA of node: 345.5759 deg
Eccentricity: .0007578
Arg of perigee: 51.3717 deg
Mean anomaly: 308.8123 deg
Mean motion: 15.73975688 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 890
Checksum: 342
Coasting Arc #10 (Orbit 905)
Vector Time (GMT): 2010/076/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213715.23 A = 6722614.97 meter
Y = -2412583.27 meter E = .0018469
Z = -4667396.76 I = 51.51933
XDOT = 5630.228963 Wp = 64.20757
YDOT = -4420.681376 meter/sec RA = 339.96740 deg
ZDOT = -2798.590827 TA = 178.07694
MA = 178.06983
Ha = 192.657 n.mi
Hp = 181.235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13824525.03 X = -4163750.77
Y = -7915299.44 feet Y = -2459424.68 meter
Z = -15312981.50 Z = -4687745.34
XDOT = 18471.879800 XDOT = 5692.838392
YDOT = -14503.547823 feet/sec YDOT = -4357.371045 meter/sec
ZDOT = -9181.728434 ZDOT = -2771.086653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14437315.92 X = -4400493.89
Y = 6546021.96 feet Y = 1995227.49 meter
Z = -15393841.80 Z = -4692042.98
XDOT = -509.688022 XDOT = -155.352909
YDOT = -22454.258244 feet/sec YDOT = -6844.057913 meter/sec
ZDOT = -9072.597954 ZDOT = -2765.327857
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 10076.68739319 .00016717 00000-0 10270-3 0 9096
2 25544 51.6460 340.3596 0007576 55.6688 304.5191 15.74008429 9065
Satellite: ISS
Catalog Number: 25544
Epoch time: 10076.68739319 = yrday.fracday
Element set: 909
Inclination: 51.6460 deg
RA of node: 340.3596 deg
Eccentricity: .0007576
Arg of perigee: 55.6688 deg
Mean anomaly: 304.5191 deg
Mean motion: 15.74008429 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 906
Checksum: 335
Coasting Arc #11 (Orbit 921)
Vector Time (GMT): 2010/077/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4593711.53 A = 6729459.98 meter
Y = 4278889.34 meter E = .0019749
Z = 2407230.75 I = 51.51563
XDOT = -5013.036343 Wp = 89.18570
YDOT = -2346.613406 meter/sec RA = 334.78063 deg
ZDOT = -5357.197410 TA = 63.59581
MA = 63.39324
Ha = 192.565 n.mi
Hp = 181.233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15071232.05 X = -4652911.33
Y = 14038350.85 feet Y = 4227188.95 meter
Z = 7897738.68 Z = 2384770.27
XDOT = -16446.969630 XDOT = -4960.399160
YDOT = -7698.862880 feet/sec YDOT = -2402.378345 meter/sec
ZDOT = -17576.106989 ZDOT = -5381.422712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2947205.85 X = 898308.34
Y = 20418882.50 feet Y = 6223675.38 meter
Z = 7808637.64 Z = 2380072.75
XDOT = -14139.732025 XDOT = -4309.790321
YDOT = 8847.447189 feet/sec YDOT = 2696.701903 meter/sec
ZDOT = -17672.356237 ZDOT = -5386.534181
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 10077.70320686 .00016717 00000-0 10270-3 0 9105
2 25544 51.6466 335.1430 0007529 57.7814 302.4078 15.74090682 9223
Satellite: ISS
Catalog Number: 25544
Epoch time: 10077.70320686 = yrday.fracday
Element set: 910
Inclination: 51.6466 deg
RA of node: 335.1430 deg
Eccentricity: .0007529
Arg of perigee: 57.7814 deg
Mean anomaly: 302.4078 deg
Mean motion: 15.74090682 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 922
Checksum: 302
Coasting Arc #12 (Orbit 937)
Vector Time (GMT): 2010/078/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4513326.48 A = 6722380.74 meter
Y = 1677830.16 meter E = .0013540
Z = 4679378.09 I = 51.46338
XDOT = -4831.274276 Wp = 90.42168
YDOT = 5349.457863 meter/sec RA = 329.67553 deg
ZDOT = 2734.848744 TA = 332.57396
MA = 332.64536
Ha = 192.552 n.mi
Hp = 181.162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14807501.59 X = 4471497.59
Y = 5504692.12 feet Y = 1728067.32 meter
Z = 15352290.32 Z = 4701202.18
XDOT = -15850.637389 XDOT = -4904.019245
YDOT = 17550.714773 feet/sec YDOT = 5295.025141 meter/sec
ZDOT = 8972.600867 ZDOT = 2711.201248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12742678.54 X = 3883968.42
Y = -9193387.47 feet Y = -2802144.50 meter
Z = 15438987.24 Z = 4705803.31
XDOT = 5114.626118 XDOT = 1558.938041
YDOT = 22037.681922 feet/sec YDOT = 6717.085450 meter/sec
ZDOT = 8878.809651 ZDOT = 2706.261182
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 10078.71900396 .00016717 00000-0 10270-3 0 9110
2 25544 51.6452 329.9257 0007570 63.0621 297.1315 15.74046819 9382
Satellite: ISS
Catalog Number: 25544
Epoch time: 10078.71900396 = yrday.fracday
Element set: 911
Inclination: 51.6452 deg
RA of node: 329.9257 deg
Eccentricity: .0007570
Arg of perigee: 63.0621 deg
Mean anomaly: 297.1315 deg
Mean motion: 15.74046819 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 938
Checksum: 316
Coasting Arc #13 (Orbit 952)
Vector Time (GMT): 2010/079/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3810942.92 A = 6729507.54 meter
Y = -5021749.77 meter E = .0012996
Z = -2352242.01 I = 51.46182
XDOT = 5286.680172 Wp = 57.68895
YDOT = 1500.867087 meter/sec RA = 324.48439 deg
ZDOT = 5389.419528 TA = 275.76399
MA = 275.91215
Ha = 192.608 n.mi
Hp = 181.046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12503093.57 X = 3878240.59
Y = -16475556.98 feet Y = -4978757.38 meter
Z = -7717329.43 Z = -2333564.67
XDOT = 17344.751219 XDOT = 5243.323378
YDOT = 4924.104616 feet/sec YDOT = 1559.743743 meter/sec
ZDOT = 17681.822600 ZDOT = 5414.996908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7086662.86 X = -2160014.84
Y = -19459912.12 feet Y = -5931381.22 meter
Z = -7643266.96 Z = -2329667.77
XDOT = 12038.236664 XDOT = 3669.254535
YDOT = -11331.683826 feet/sec YDOT = -3453.897230 meter/sec
ZDOT = 17783.418579 ZDOT = 5420.385983
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 10079.67129162 .00016717 00000-0 10270-3 0 9121
2 25544 51.6446 325.0343 0007496 68.0002 292.1957 15.74105805 9538
Satellite: ISS
Catalog Number: 25544
Epoch time: 10079.67129162 = yrday.fracday
Element set: 912
Inclination: 51.6446 deg
RA of node: 325.0343 deg
Eccentricity: .0007496
Arg of perigee: 68.0002 deg
Mean anomaly: 292.1957 deg
Mean motion: 15.74105805 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 953
Checksum: 303
Coasting Arc #14 (Orbit 968)
Vector Time (GMT): 2010/080/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4678125.65 A = 6721888.81 meter
Y = -975719.28 meter E = .0019203
Z = -4745445.55 I = 51.41266
XDOT = 3906.199790 Wp = 71.46812
YDOT = -6086.449033 meter/sec RA = 319.37477 deg
ZDOT = -2601.940972 TA = 172.88130
MA = 172.85400
Ha = 192.593 n.mi
Hp = 180.730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15348181.28 X = -4643814.76
Y = -3201178.74 feet Y = -1027841.18 meter
Z = -15569047.09 Z = -4768088.53
XDOT = 12815.616108 XDOT = 3986.608999
YDOT = -19968.664806 feet/sec YDOT = -6042.318082 meter/sec
ZDOT = -8536.551747 ZDOT = -2582.769121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10742808.90 X = -3274408.15
Y = 11295920.05 feet Y = 3442996.43 meter
Z = -15658981.07 Z = -4772857.43
XDOT = -9401.484389 XDOT = -2865.572442
YDOT = -20657.816657 feet/sec YDOT = -6296.502517 meter/sec
ZDOT = -8460.546498 ZDOT = -2578.774573
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 10080.68704624 .00016717 00000-0 10270-3 0 9137
2 25544 51.6444 319.8174 0007630 72.0513 288.1481 15.74146795 9698
Satellite: ISS
Catalog Number: 25544
Epoch time: 10080.68704624 = yrday.fracday
Element set: 913
Inclination: 51.6444 deg
RA of node: 319.8174 deg
Eccentricity: .0007630
Arg of perigee: 72.0513 deg
Mean anomaly: 288.1481 deg
Mean motion: 15.74146795 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 969
Checksum: 319
Coasting Arc #15 (Orbit 984)
Vector Time (GMT): 2010/081/16:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 798335.7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2999609.32 A = 6729569.44 meter
Y = 5600697.04 meter E = .0020565
Z = 2196221.83 I = 51.41665
XDOT = -5380.595470 Wp = 97.04970
YDOT = -721.777313 meter/sec RA = 314.18140 deg
ZDOT = -5467.007144 TA = 58.24537
MA = 58.04515
Ha = 192.461 n.mi
Hp = 180.877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9841237.94 X = -3072683.19
Y = 18374990.30 feet Y = 5566745.10 meter
Z = 7205452.20 Z = 2181472.15
XDOT = -17652.872278 XDOT = -5345.566881
YDOT = -2368.035805 feet/sec YDOT = -781.750603 meter/sec
ZDOT = -17936.375145 ZDOT = -5493.060889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10746149.18 X = 3275426.27
Y = 17884336.16 feet Y = 5451145.66 meter
Z = 7146997.43 Z = 2178404.82
XDOT = -9697.000545 XDOT = -2955.645766
YDOT = 13090.224175 feet/sec YDOT = 3989.900329 meter/sec
ZDOT = -18039.850803 ZDOT = -5498.546525
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 10081.70277822 .00016717 00000-0 10270-3 0 9147
2 25544 51.6444 314.5995 0007381 74.7162 285.4817 15.74192747 9852
Satellite: ISS
Catalog Number: 25544
Epoch time: 10081.70277822 = yrday.fracday
Element set: 914
Inclination: 51.6444 deg
RA of node: 314.5995 deg
Eccentricity: .0007381
Arg of perigee: 74.7162 deg
Mean anomaly: 285.4817 deg
Mean motion: 15.74192747 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 985
Checksum: 333
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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