Date:
July 5th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 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 2588)
---------------------------------------
Vector Time (GMT): 2010/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6062241
52 A = 6737233
36 meter
Y = 2864903
84 meter E =
0022593
Z = 517799
26 I = 51
82447
XDOT = -1610
672023 Wp = 42
65293
YDOT = -4522
244671 meter/sec RA = 151
22451 deg
ZDOT = 6027
678262 TA = 322
96782
MA = 323
12354
Ha = 195
885 n
mi
Hp = 184
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19889243
82 X = -6096342
19
Y = 9399290
80 feet Y = 2796921
51 meter
Z = 1698816
45 Z = 488266
62
XDOT = -5284
357030 XDOT = -1589
264879
YDOT = -14836
760731 feet/sec YDOT = -4540
137152 meter/sec
ZDOT = 19775
847316 ZDOT = 6019
905169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12599792
73 X = 3840416
82
Y = 18043298
20 feet Y = 5499597
29 meter
Z = 1580910
45 Z = 481861
50
XDOT = -12406
006844 XDOT = -3781
350886
YDOT = 6891
246096 feet/sec YDOT = 2100
451810 meter/sec
ZDOT = 19744
747805 ZDOT = 6018
199131
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 10183
56264152
00016717 00000-0 10270-3 0 9001
2 25544 51
6437 151
9092 0009789 32
0679 328
1077 15
72193407 25896
Satellite: ISS
Catalog Number: 25544
Epoch time: 10183
56264152 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 151
9092 deg
Eccentricity:
0009789
Arg of perigee: 32
0679 deg
Mean anomaly: 328
1077 deg
Mean motion: 15
72193407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2589
Checksum: 321
Coasting Arc #2 (Orbit 2603)
---------------------------------------
Vector Time (GMT): 2010/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2390492
02 A = 6725325
20 meter
Y = 3413304
14 meter E =
0022289
Z = -5296529
38 I = 51
81072
XDOT = -6347
318492 Wp = 68
26798
YDOT = 4327
763212 meter/sec RA = 146
11129 deg
ZDOT = -67
916250 TA = 201
04163
MA = 201
13347
Ha = 196
019 n
mi
Hp = 184
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7842821
59 X = 2377875
62
Y = 11198504
40 feet Y = 3439966
09 meter
Z = -17377064
89 Z = -5284946
69
XDOT = -20824
535735 XDOT = -6394
910655
YDOT = 14198
698202 feet/sec YDOT = 4256
517615 meter/sec
ZDOT = -222
822343 ZDOT = -98
866507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9540345
95 X = 2907897
45
Y = -9874470
04 feet Y = -3009738
47 meter
Z = -17330763
86 Z = -5282416
82
XDOT = 17075
652750 XDOT = 5204
658958
YDOT = 17151
062339 feet/sec YDOT = 5227
643801 meter/sec
ZDOT = -346
382927 ZDOT = -105
577516
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 10184
51609218
00016717 00000-0 10270-3 0 9014
2 25544 51
6442 147
0262 0009909 34
6243 325
5563 15
72172655 26047
Satellite: ISS
Catalog Number: 25544
Epoch time: 10184
51609218 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 147
0262 deg
Eccentricity:
0009909
Arg of perigee: 34
6243 deg
Mean anomaly: 325
5563 deg
Mean motion: 15
72172655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2604
Checksum: 295
Coasting Arc #3 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2010/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4892055
27 A = 6737099
53 meter
Y = -4588001
69 meter E =
0016589
Z = 619972
49 I = 51
87555
XDOT = 3677
604358 Wp = 91
65743
YDOT = 3090
704291 meter/sec RA = 140
99718 deg
ZDOT = -6009
718588 TA = 81
62316
MA = 81
43513
Ha = 196
033 n
mi
Hp = 183
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16050050
10 X = 4939983
84
Y = -15052499
00 feet Y = -4533027
90 meter
Z = 2034030
49 Z = 643853
96
XDOT = 12065
631096 XDOT = 3671
964299
YDOT = 10140
105942 feet/sec YDOT = 3131
798609 meter/sec
ZDOT = -19716
924501 ZDOT = -5991
866153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17972981
04 X = -5478164
62
Y = -12678992
99 feet Y = -3864557
06 meter
Z = 2129366
95 Z = 649031
05
XDOT = 6554
796508 XDOT = 1997
901976
YDOT = -12663
238686 feet/sec YDOT = -3859
755152 meter/sec
ZDOT = -19645
584204 ZDOT = -5987
974065
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 10185
53309212
00016717 00000-0 10270-3 0 9029
2 25544 51
6446 141
8178 0009947 38
0471 322
1392 15
72206787 26207
Satellite: ISS
Catalog Number: 25544
Epoch time: 10185
53309212 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 141
8178 deg
Eccentricity:
0009947
Arg of perigee: 38
0471 deg
Mean anomaly: 322
1392 deg
Mean motion: 15
72206787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 300
Coasting Arc #4 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2010/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3905226
51 A = 6725708
09 meter
Y = -1843317
87 meter E =
0011175
Z = 5146620
78 I = 51
86075
XDOT = 4639
974353 Wp = 64
86518
YDOT = -5997
933192 meter/sec RA = 135
91014 deg
ZDOT = 1374
903660 TA = 12
03790
MA = 12
01122
Ha = 196
083 n
mi
Hp = 183
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12812422
94 X = -3909325
34
Y = -6047630
80 feet Y = -1887012
00 meter
Z = 16885238
79 Z = 5127638
98
XDOT = 15223
012969 XDOT = 4700
020435
YDOT = -19678
258505 feet/sec YDOT = -5945
710667 meter/sec
ZDOT = 4510
838778 ZDOT = 1397
589791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3084806
64 X = -940249
06
Y = 13920180
12 feet Y = 4242870
90 meter
Z = 16809398
04 Z = 5123504
52
XDOT = -21504
019084 XDOT = -6554
425017
YDOT = -10312
563769 feet/sec YDOT = -3143
269437 meter/sec
ZDOT = 4601
399512 ZDOT = 1402
506571
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 10186
55007762
00016717 00000-0 10270-3 0 9038
2 25544 51
6449 136
6103 0009818 41
2951 318
8952 15
72256337 26363
Satellite: ISS
Catalog Number: 25544
Epoch time: 10186
55007762 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 136
6103 deg
Eccentricity:
0009818
Arg of perigee: 41
2951 deg
Mean anomaly: 318
8952 deg
Mean motion: 15
72256337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 315
Coasting Arc #5 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2010/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3095527
74 A = 6735815
46 meter
Y = 5708993
66 meter E =
0017348
Z = -1766832
54 I = 51
91523
XDOT = -5061
891358 Wp = 42
29950
YDOT = -989
541382 meter/sec RA = 130
77779 deg
ZDOT = 5715
925015 TA = 298
21741
MA = 298
39247
Ha = 196
079 n
mi
Hp = 183
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10155930
91 X = -3150553
70
Y = 18730294
15 feet Y = 5674070
20 meter
Z = -5796694
68 Z = -1782003
50
XDOT = -16607
255112 XDOT = -5078
216918
YDOT = -3246
526844 feet/sec YDOT = -1046
238565 meter/sec
ZDOT = 18753
034826 ZDOT = 5691
294479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20583538
04 X = 6273862
39
Y = 5438664
73 feet Y = 1657705
01 meter
Z = -5857252
66 Z = -1785290
61
XDOT = 1168
451736 XDOT = 356
144089
YDOT = 15511
553064 feet/sec YDOT = 4727
921374 meter/sec
ZDOT = 18654
631813 ZDOT = 5685
931777
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 10187
50349131
00016717 00000-0 10270-3 0 9044
2 25544 51
6446 131
7272 0009940 44
9169 315
2796 15
72234851 26511
Satellite: ISS
Catalog Number: 25544
Epoch time: 10187
50349131 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 131
7272 deg
Eccentricity:
0009940
Arg of perigee: 44
9169 deg
Mean anomaly: 315
2796 deg
Mean motion: 15
72234851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 309
Coasting Arc #6 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2010/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4737696
83 A = 6727280
26 meter
Y = -152858
44 meter E =
0021001
Z = -4793443
69 I = 51
90649
XDOT = -2402
220344 Wp = 61
19821
YDOT = 6820
738801 meter/sec RA = 125
71078 deg
ZDOT = -2590
433011 TA = 183
42186
MA = 183
43625
Ha = 196
089 n
mi
Hp = 183
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15543624
76 X = 4762339
73
Y = -501504
07 feet Y = -99740
12 meter
Z = -15726521
28 Z = -4770368
06
XDOT = -7881
300342 XDOT = -2465
728663
YDOT = 22377
751973 feet/sec YDOT = 6793
521068 meter/sec
ZDOT = -8498
795967 ZDOT = -2602
256180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4419683
79 X = -1347119
62
Y = -15007110
25 feet Y = -4574167
20 meter
Z = -15634330
36 Z = -4765343
89
XDOT = 22533
499261 XDOT = 6868
210575
YDOT = 2271
579844 feet/sec YDOT = 692
377536 meter/sec
ZDOT = -8545
986575 ZDOT = -2604
816708
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 10188
52045182
00016717 00000-0 10270-3 0 9057
2 25544 51
6455 126
5182 0009943 48
7593 311
4424 15
72275047 26674
Satellite: ISS
Catalog Number: 25544
Epoch time: 10188
52045182 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 126
5182 deg
Eccentricity:
0009943
Arg of perigee: 48
7593 deg
Mean anomaly: 311
4424 deg
Mean motion: 15
72275047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 315
Coasting Arc #7 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2010/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1077408
78 A = 6733758
48 meter
Y = -6048190
83 meter E =
0021502
Z = 2743972
96 I = 51
94589
XDOT = 5526
389072 Wp = 80
59010
YDOT = -1382
881373 meter/sec RA = 120
56610 deg
ZDOT = -5180
352641 TA = 68
21734
MA = 67
98867
Ha = 196
102 n
mi
Hp = 183
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3534805
72 X = 1131630
96
Y = -19843145
78 feet Y = -6035839
93 meter
Z = 9002535
95 Z = 2749337
61
XDOT = 18131
197744 XDOT = 5566
607178
YDOT = -4537
012378 feet/sec YDOT = -1320
856177 meter/sec
ZDOT = -16995
907614 ZDOT = -5153
408003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20049625
79 X = -6111125
94
Y = 1967723
77 feet Y = 599762
20 meter
Z = 9023940
84 Z = 2750497
17
XDOT = -9117
365067 XDOT = -2778
972872
YDOT = -14884
492363 feet/sec YDOT = -4536
793272 meter/sec
ZDOT = -16888
253234 ZDOT = -5147
539586
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 10189
53739880
00016717 00000-0 10270-3 0 9065
2 25544 51
6460 121
3098 0009932 52
3105 307
8957 15
72294006 26831
Satellite: ISS
Catalog Number: 25544
Epoch time: 10189
53739880 = yrday
fracday
Element set: 906
Inclination: 51
6460 deg
RA of node: 121
3098 deg
Eccentricity:
0009932
Arg of perigee: 52
3105 deg
Mean anomaly: 307
8957 deg
Mean motion: 15
72294006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 320
Coasting Arc #8 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2010/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4726836
39 A = 6729393
87 meter
Y = 2268395
98 meter E =
0018272
Z = 4201364
74 I = 51
94600
XDOT = 35
437215 Wp = 81
59127
YDOT = -6770
849931 meter/sec RA = 115
51342 deg
ZDOT = 3684
670170 TA = 330
98286
MA = 331
08431
Ha = 196
227 n
mi
Hp = 183
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15507993
40 X = -4772260
07
Y = 7442244
03 feet Y = 2215282
87 meter
Z = 13784005
04 Z = 4178291
98
XDOT = 116
263828 XDOT = 93
248079
YDOT = -22214
074578 feet/sec YDOT = -6770
131137 meter/sec
ZDOT = 12088
812895 ZDOT = 3684
981417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11573267
91 X = 3527532
06
Y = 12824875
06 feet Y = 3909021
92 meter
Z = 13691811
43 Z = 4173264
12
XDOT = -20371
783118 XDOT = -6209
319494
YDOT = 5437
895886 feet/sec YDOT = 1657
470666 meter/sec
ZDOT = 12090
032410 ZDOT = 3685
041879
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 10190
55433211
00016717 00000-0 10270-3 0 9079
2 25544 51
6464 116
1016 0009875 56
4211 303
7893 15
72315209 26996
Satellite: ISS
Catalog Number: 25544
Epoch time: 10190
55433211 = yrday
fracday
Element set: 907
Inclination: 51
6464 deg
RA of node: 116
1016 deg
Eccentricity:
0009875
Arg of perigee: 56
4211 deg
Mean anomaly: 303
7893 deg
Mean motion: 15
72315209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 299
Coasting Arc #9 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2010/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 969856
55 A = 6731176
17 meter
Y = 5580786
41 meter E =
0014614
Z = -3644701
26 I = 51
96496
XDOT = -5067
636051 Wp = 74
05752
YDOT = 3746
604763 meter/sec RA = 110
36263 deg
ZDOT = 4406
764369 TA = 242
54963
MA = 242
69831
Ha = 196
126 n
mi
Hp = 183
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3181944
06 X = 925084
21
Y = 18309666
72 feet Y = 5591382
32 meter
Z = -11957681
30 Z = -3640097
39
XDOT = -16626
102529 XDOT = -5130
561665
YDOT = 12292
010378 feet/sec YDOT = 3689
582724 meter/sec
ZDOT = 14457
888351 ZDOT = 4381
993943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16479582
01 X = 5022976
60
Y = -8615803
68 feet Y = -2626096
96 meter
Z = -11939267
53 Z = -3639088
74
XDOT = 16126
438919 XDOT = 4915
338582
YDOT = 11031
561574 feet/sec YDOT = 3362
419968 meter/sec
ZDOT = 14358
899275 ZDOT = 4376
592499
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 10191
50769539
00016717 00000-0 10270-3 0 9081
2 25544 51
6470 111
2186 0009897 59
5828 300
6311 15
72333874 27146
Satellite: ISS
Catalog Number: 25544
Epoch time: 10191
50769539 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 111
2186 deg
Eccentricity:
0009897
Arg of perigee: 59
5828 deg
Mean anomaly: 300
6311 deg
Mean motion: 15
72333874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 321
Coasting Arc #10 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2010/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3973331
19 A = 6731644
50 meter
Y = -4179452
70 meter E =
0014687
Z = -3489292
46 I = 51
97711
XDOT = 2110
950058 Wp = 71
07605
YDOT = 5809
963087 meter/sec RA = 105
31445 deg
ZDOT = -4566
267345 TA = 150
00721
MA = 149
92299
Ha = 196
119 n
mi
Hp = 183
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13035863
48 X = 4036721
35
Y = -13712115
15 feet Y = -4134665
45 meter
Z = -11447809
89 Z = -3469837
13
XDOT = 6925
689167 XDOT = 2068
006839
YDOT = 19061
558686 feet/sec YDOT = 5833
329734 meter/sec
ZDOT = -14981
192076 ZDOT = -4556
115738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17163544
02 X = -5231448
22
Y = -8071112
67 feet Y = -2460075
14 meter
Z = -11370052
18 Z = -3465591
90
XDOT = 15258
865484 XDOT = 4650
902199
YDOT = -11452
032586 feet/sec YDOT = -3490
579532 meter/sec
ZDOT = -14940
604595 ZDOT = -4553
896280
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 10192
52460270
00016717 00000-0 10270-3 0 9095
2 25544 51
6480 106
0099 0009915 63
1408 297
0767 15
72360052 27308
Satellite: ISS
Catalog Number: 25544
Epoch time: 10192
52460270 = yrday
fracday
Element set: 909
Inclination: 51
6480 deg
RA of node: 106
0099 deg
Eccentricity:
0009915
Arg of perigee: 63
1408 deg
Mean anomaly: 297
0767 deg
Mean motion: 15
72360052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 297
Coasting Arc #11 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2010/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2634191
23 A = 6728771
04 meter
Y = -4429153
38 meter E =
0019621
Z = 4315213
84 I = 51
97394
XDOT = 3810
572854 Wp = 69
17296
YDOT = -5703
963333 meter/sec RA = 100
16588 deg
ZDOT = -3508
879335 TA = 56
23853
MA = 56
05176
Ha = 196
181 n
mi
Hp = 182
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8642359
68 X = -2605429
94
Y = -14531343
11 feet Y = -4458450
37 meter
Z = 14157525
71 Z = 4302486
34
XDOT = 12501
879441 XDOT = 3891
117547
YDOT = -18713
790461 feet/sec YDOT = -5660
900313 meter/sec
ZDOT = -11512
071309 ZDOT = -3490
173240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10784815
17 X = -3287211
66
Y = 13075790
27 feet Y = 3985500
88 meter
Z = 14106640
92 Z = 4299704
15
XDOT = -20883
039520 XDOT = -6365
150446
YDOT = -4815
731374 feet/sec YDOT = -1467
834923 meter/sec
ZDOT = -11437
301264 ZDOT = -3486
089425
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 10193
54149693
00016717 00000-0 10270-3 0 9103
2 25544 51
6475 100
8015 0009898 66
7693 293
4510 15
72373151 27464
Satellite: ISS
Catalog Number: 25544
Epoch time: 10193
54149693 = yrday
fracday
Element set: 910
Inclination: 51
6475 deg
RA of node: 100
8015 deg
Eccentricity:
0009898
Arg of perigee: 66
7693 deg
Mean anomaly: 293
4510 deg
Mean motion: 15
72373151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 321
Coasting Arc #12 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2010/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2546998
69 A = 6733894
79 meter
Y = 5651146
65 meter E =
0023614
Z = 2601985
38 I = 51
99584
XDOT = -3774
536514 Wp = 74
11727
YDOT = -4149
588999 meter/sec RA = 95
11333 deg
ZDOT = 5284
538091 TA = 315
30248
MA = 315
49256
Ha = 196
176 n
mi
Hp = 182
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8356294
93 X = -2622641
24
Y = 18540507
37 feet Y = 5622241
30 meter
Z = 8536697
46 Z = 2589429
36
XDOT = -12383
649981 XDOT = -3753
525285
YDOT = -13614
137137 feet/sec YDOT = -4191
681343 meter/sec
ZDOT = 17337
723397 ZDOT = 5266
252277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20310341
12 X = 6190591
97
Y = 1386548
41 feet Y = 422619
96 meter
Z = 8486507
47 Z = 2586687
48
XDOT = -8282
030432 XDOT = -2524
362876
YDOT = 14979
573225 feet/sec YDOT = 4565
773919 meter/sec
ZDOT = 17264
614584 ZDOT = 5262
254525
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 10194
55837774
00016717 00000-0 10270-3 0 9110
2 25544 51
6480 95
5925 0009897 70
3330 289
8899 15
72378954 27621
Satellite: ISS
Catalog Number: 25544
Epoch time: 10194
55837774 = yrday
fracday
Element set: 911
Inclination: 51
6480 deg
RA of node: 95
5925 deg
Eccentricity:
0009897
Arg of perigee: 70
3330 deg
Mean anomaly: 289
8899 deg
Mean motion: 15
72378954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 365
Coasting Arc #13 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2010/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3796937
09 A = 6726603
72 meter
Y = 2729070
33 meter E =
0020743
Z = -4853585
49 I = 51
97345
XDOT = -1917
800818 Wp = 92
30486
YDOT = 7022
589527 meter/sec RA = 89
97319 deg
ZDOT = 2456
531532 TA = 201
59854
MA = 201
68616
Ha = 196
061 n
mi
Hp = 182
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12457142
69 X = 3789715
29
Y = 8953642
83 feet Y = 2771490
09 meter
Z = -15923836
89 Z = -4835157
59
XDOT = -6291
997433 XDOT = -2008
119299
YDOT = 23039
991885 feet/sec YDOT = 7000
638275 meter/sec
ZDOT = 8059
486653 ZDOT = 2446
996408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3737873
20 X = 1139303
75
Y = -14957187
80 feet Y = -4558950
84 meter
Z = -15850159
07 Z = -4831128
48
XDOT = 22671
132452 XDOT = 6910
161171
YDOT = -2806
128746 feet/sec YDOT = -855
308042 meter/sec
ZDOT = 8021
371591 ZDOT = 2444
914061
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 10195
51169001
00016717 00000-0 10270-3 0 9129
2 25544 51
6483 90
7090 0009762 73
5764 286
6470 15
72413283 27772
Satellite: ISS
Catalog Number: 25544
Epoch time: 10195
51169001 = yrday
fracday
Element set: 912
Inclination: 51
6483 deg
RA of node: 90
7090 deg
Eccentricity:
0009762
Arg of perigee: 73
5764 deg
Mean anomaly: 286
6470 deg
Mean motion: 15
72413283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 315
Coasting Arc #14 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2010/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 756685
33 A = 6735474
55 meter
Y = -6473731
79 meter E =
0014724
Z = -1700176
34 I = 52
00204
XDOT = 4688
383721 Wp = 106
12634
YDOT = 2045
099572 meter/sec RA = 84
90845 deg
ZDOT = -5745
294667 TA = 92
55460
MA = 92
38604
Ha = 196
046 n
mi
Hp = 182
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2482563
42 X = 837278
55
Y = -21239277
53 feet Y = -6464819
32 meter
Z = -5578006
38 Z = -1696305
24
XDOT = 15381
836354 XDOT = 4693
075736
YDOT = 6709
644265 feet/sec YDOT = 2097
554617 meter/sec
ZDOT = -18849
391953 ZDOT = -5722
507296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20589799
25 X = -6275770
81
Y = 5788142
65 feet Y = 1764225
88 meter
Z = -5562531
60 Z = -1695459
63
XDOT = 704
437489 XDOT = 214
712547
YDOT = -15379
528847 feet/sec YDOT = -4687
680393 meter/sec
ZDOT = -18758
284335 ZDOT = -5717
525065
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 10196
52854459
00016717 00000-0 10270-3 0 9130
2 25544 51
6482 85
4994 0009628 78
0490 282
1751 15
72401553 27930
Satellite: ISS
Catalog Number: 25544
Epoch time: 10196
52854459 = yrday
fracday
Element set: 913
Inclination: 51
6482 deg
RA of node: 85
4994 deg
Eccentricity:
0009628
Arg of perigee: 78
0490 deg
Mean anomaly: 282
1751 deg
Mean motion: 15
72401553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2793
Checksum: 334
Coasting Arc #15 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2010/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4237377
00 A = 6725008
36 meter
Y = -786956
27 meter E =
0013692
Z = 5152160
74 I = 51
96373
XDOT = -273
051149 Wp = 72
29301
YDOT = -7579
263189 meter/sec RA = 79
78173 deg
ZDOT = -1375
204093 TA = 30
83975
MA = 30
75939
Ha = 196
033 n
mi
Hp = 182
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13902155
51 X = -4253290
15
Y = -2581877
52 feet Y = -834430
55 meter
Z = 16903414
49 Z = 5131537
08
XDOT = -895
837102 XDOT = -181
597740
YDOT = -24866
349046 feet/sec YDOT = -7581
805154 meter/sec
ZDOT = -4511
824452 ZDOT = -1376
309045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3201877
64 X = 975932
30
Y = 13873167
83 feet Y = 4228541
55 meter
Z = 16820958
21 Z = 5127028
06
XDOT = -21456
763515 XDOT = -6540
021519
YDOT = 10456
160399 feet/sec YDOT = 3187
037690 meter/sec
ZDOT = -4516
237454 ZDOT = -1376
549176
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 10197
54538350
00016717 00000-0 10270-3 0 9143
2 25544 51
6482 80
2899 0009583 80
6405 279
5840 15
72494578 28098
Satellite: ISS
Catalog Number: 25544
Epoch time: 10197
54538350 = yrday
fracday
Element set: 914
Inclination: 51
6482 deg
RA of node: 80
2899 deg
Eccentricity:
0009583
Arg of perigee: 80
6405 deg
Mean anomaly: 279
5840 deg
Mean motion: 15
72494578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 345
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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