Date:
February 9th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
040/21:39:35
884 0
3 1
6 1
6
N/A 1
5 0
1 191
4
000/00:04:11
769 -0
6 -0
0 188
2
Coasting Arc #1 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2011/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1549312
23 A = 6730515
73 meter
Y = 5402135
75 meter E =
0001888
Z = -3705123
60 I = 51
97372
XDOT = -4669
685705 Wp = 88
09176
YDOT = 4312
246382 meter/sec RA = 105
03332 deg
ZDOT = 4336
632603 TA = 227
58134
MA = 227
59731
Ha = 191
178 n
mi
Hp = 187
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5083045
36 X = 1506787
82
Y = 17723542
48 feet Y = 5419223
17 meter
Z = -12155917
32 Z = -3697700
72
XDOT = -15320
491158 XDOT = -4738
625128
YDOT = 14147
789966 feet/sec YDOT = 4259
641857 meter/sec
ZDOT = 14227
797254 ZDOT = 4313
780120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8466417
64 X = -2580564
10
Y = 16401413
97 feet Y = 4999150
98 meter
Z = -12126047
41 Z = -3696019
25
XDOT = -19717
466270 XDOT = -6009
883719
YDOT = 267
876578 feet/sec YDOT = 81
648781 meter/sec
ZDOT = 14135
486631 ZDOT = 4308
496325
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 11038
50785149
00016717 00000-0 10270-3 0 9009
2 25544 51
6434 105
8736 0003997 288
2056 71
8671 15
72501055 20490
Satellite: ISS
Catalog Number: 25544
Epoch time: 11038
50785149 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 105
8736 deg
Eccentricity:
0003997
Arg of perigee: 288
2056 deg
Mean anomaly: 71
8671 deg
Mean motion: 15
72501055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 313
Coasting Arc #2 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2011/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3539313
98 A = 6731358
61 meter
Y = -4576447
42 meter E =
0002187
Z = -3443887
04 I = 51
98320
XDOT = 2683
198614 Wp = 37
03556
YDOT = 5544
300830 meter/sec RA = 99
98396 deg
ZDOT = -4609
859972 TA = 183
45028
MA = 183
45179
Ha = 191
269 n
mi
Hp = 187
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11611922
49 X = 3606955
11
Y = -15014591
26 feet Y = -4536490
59 meter
Z = -11298841
98 Z = -3426528
89
XDOT = 8803
145058 XDOT = 2643
395239
YDOT = 18189
963353 feet/sec YDOT = 5574
083254 meter/sec
ZDOT = -15124
212505 ZDOT = -4596
922116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18756847
42 X = 5717087
09
Y = -3167901
76 feet Y = -965576
46 meter
Z = -11228695
30 Z = -3422506
33
XDOT = -5975
144192 XDOT = -1821
223950
YDOT = 18047
400629 feet/sec YDOT = 5500
847712 meter/sec
ZDOT = -15072
091297 ZDOT = -4593
973427
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 11039
52465884
00016717 00000-0 10270-3 0 9014
2 25544 51
6433 100
6634 0003979 293
8720 66
2025 15
72502815 20653
Satellite: ISS
Catalog Number: 25544
Epoch time: 11039
52465884 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 100
6634 deg
Eccentricity:
0003979
Arg of perigee: 293
8720 deg
Mean anomaly: 66
2025 deg
Mean motion: 15
72502815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 301
Coasting Arc #3 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2011/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3037263
49 A = 6728205
26 meter
Y = -4167573
01 meter E =
0007582
Z = 4319748
84 I = 51
97778
XDOT = 3263
263589 Wp = 47
87910
YDOT = -6024
841584 meter/sec RA = 94
83398 deg
ZDOT = -3509
289011 TA = 77
52007
MA = 77
43526
Ha = 191
315 n
mi
Hp = 187
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9964775
23 X = -3011419
40
Y = -13673139
79 feet Y = -4201392
90 meter
Z = 14172404
33 Z = 4305056
93
XDOT = 10706
245371 XDOT = 3347
439199
YDOT = -19766
540630 feet/sec YDOT = -5987
879243 meter/sec
ZDOT = -11513
415389 ZDOT = -3493
231699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1548339
45 X = 471933
86
Y = -16897610
82 feet Y = -5150391
78 meter
Z = 14113183
03 Z = 4301698
19
XDOT = 19942
494096 XDOT = 6078
472200
YDOT = -7759
045527 feet/sec YDOT = -2364
957077 meter/sec
ZDOT = -11448
481542 ZDOT = -3489
497174
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 11040
54144320
00016717 00000-0 10270-3 0 9028
2 25544 51
6436 95
4534 0004158 299
1912 60
8834 15
72573250 20815
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
54144320 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 95
4534 deg
Eccentricity:
0004158
Arg of perigee: 299
1912 deg
Mean anomaly: 60
8834 deg
Mean motion: 15
72573250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 287
Coasting Arc #4 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2011/040/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4069054
79 A = 6725986
88 meter
Y = -1691431
31 meter E =
0009929
Z = -5090033
84 I = 51
96938
XDOT = 964
625997 Wp = 61
04871
YDOT = 7438
590270 meter/sec RA = 92
81270 deg
ZDOT = -1698
510047 TA = 192
65593
MA = 192
68087
Ha = 191
433 n
mi
Hp = 188
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13349917
30 X = 4112392
37
Y = -5549315
33 feet Y = -1645686
48 meter
Z = -16699586
07 Z = -5070161
36
XDOT = 3164
783456 XDOT = 889
625515
YDOT = 24404
823720 feet/sec YDOT = 7448
957912 meter/sec
ZDOT = -5572
539524 ZDOT = -1694
006306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8694135
03 X = -2649972
36
Y = -11666236
07 feet Y = -3555868
76 meter
Z = -16619335
71 Z = -5065573
53
XDOT = 22012
416114 XDOT = 6709
384432
YDOT = -8481
335365 feet/sec YDOT = -2585
111019 meter/sec
ZDOT = -5554
511768 ZDOT = -1693
015187
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 11040
92273596
00016717 00000-0 10270-3 0 9039
2 25544 51
6447 93
5004 0004870 291
9441 68
1203 15
72269565 20874
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
92273596 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 93
5004 deg
Eccentricity:
0004870
Arg of perigee: 291
9441 deg
Mean anomaly: 68
1203 deg
Mean motion: 15
72269565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 307
Coasting Arc #5 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2011/041/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1822388
61 A = 6735397
54 meter
Y = -6159550
28 meter E =
0009273
Z = 2011967
78 I = 52
00116
XDOT = 4261
805833 Wp = 109
78341
YDOT = -3099
501292 meter/sec RA = 87
68279 deg
ZDOT = -5611
036069 TA = 47
92593
MA = 47
84708
Ha = 191
554 n
mi
Hp = 188
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5978965
26 X = -1763149
55
Y = -20208498
30 feet Y = -6179598
09 meter
Z = 6600944
15 Z = 2003258
69
XDOT = 13982
302602 XDOT = 4323
405299
YDOT = -10168
967493 feet/sec YDOT = -3051
498834 meter/sec
ZDOT = -18408
910987 ZDOT = -5590
182866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17912340
63 X = -5459681
42
Y = 11123874
43 feet Y = 3390556
93 meter
Z = 6565924
43 Z = 2001293
77
XDOT = -12708
357655 XDOT = -3873
507413
YDOT = -9613
053620 feet/sec YDOT = -2930
058743 meter/sec
ZDOT = -18324
664485 ZDOT = -5585
357735
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 11041
93969138
00016717 00000-0 10270-3 0 9046
2 25544 51
6446 88
2917 0004830 295
1432 64
9229 15
72259638 21030
Satellite: ISS
Catalog Number: 25544
Epoch time: 11041
93969138 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 88
2917 deg
Eccentricity:
0004830
Arg of perigee: 295
1432 deg
Mean anomaly: 64
9229 deg
Mean motion: 15
72259638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 320
Coasting Arc #6 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2011/042/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3207787
07 A = 6727623
69 meter
Y = 3632623
71 meter E =
0003239
Z = 4664311
24 I = 51
97376
XDOT = -3100
423151 Wp = 110
60494
YDOT = -6433
637978 meter/sec RA = 82
62398 deg
ZDOT = 2875
633000 TA = 311
07631
MA = 311
10428
Ha = 191
769 n
mi
Hp = 187
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10524235
78 X = -3270827
37
Y = 11918056
80 feet Y = 3596399
80 meter
Z = 15302858
40 Z = 4648574
95
XDOT = -10171
991965 XDOT = -3042
219651
YDOT = -21107
736148 feet/sec YDOT = -6467
983363 meter/sec
ZDOT = 9434
491471 ZDOT = 2860
712729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14412114
09 X = 4392812
37
Y = 6858091
88 feet Y = 2090346
40 meter
Z = 15239246
53 Z = 4644922
34
XDOT = -16903
974627 XDOT = -5152
331466
YDOT = 14672
733071 feet/sec YDOT = 4472
249040 meter/sec
ZDOT = 9374
412943 ZDOT = 2857
321065
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 11042
95662477
00016717 00000-0 10270-3 0 9056
2 25544 51
6452 83
0825 0004896 300
4658 59
6020 15
72308560 21196
Satellite: ISS
Catalog Number: 25544
Epoch time: 11042
95662477 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 83
0825 deg
Eccentricity:
0004896
Arg of perigee: 300
4658 deg
Mean anomaly: 59
6020 deg
Mean motion: 15
72308560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 306
Coasting Arc #7 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2011/043/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3481267
42 A = 6733072
40 meter
Y = 4929100
24 meter E =
0004508
Z = -2980856
66 I = 51
98777
XDOT = -2890
139474 Wp =
74078
YDOT = 5072
162738 meter/sec RA = 77
47972 deg
ZDOT = 5016
417635 TA = 325
05672
MA = 325
08630
Ha = 191
802 n
mi
Hp = 187
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11421481
02 X = 3440370
74
Y = 16171588
71 feet Y = 4967801
26 meter
Z = -9779713
46 Z = -2964044
24
XDOT = -9482
084890 XDOT = -2971
010952
YDOT = 16640
953866 feet/sec YDOT = 5039
391197 meter/sec
ZDOT = 16458
063107 ZDOT = 5002
181245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12045664
32 X = 3671518
49
Y = -15754143
07 feet Y = -4801862
81 meter
Z = -9711964
41 Z = -2960206
75
XDOT = 17583
576363 XDOT = 5359
474075
YDOT = 3343
190114 feet/sec YDOT = 1019
004347 meter/sec
ZDOT = 16400
461175 ZDOT = 4998
860566
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 11043
90998095
00016717 00000-0 10270-3 0 9061
2 25544 51
6456 78
1991 0005032 304
2615 55
8071 15
72348904 21344
Satellite: ISS
Catalog Number: 25544
Epoch time: 11043
90998095 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 78
1991 deg
Eccentricity:
0005032
Arg of perigee: 304
2615 deg
Mean anomaly: 55
8071 deg
Mean motion: 15
72348904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 309
Coasting Arc #8 (Orbit 2149)
---------------------------------------
Vector Time (GMT): 2011/044/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1731420
38 A = 6729668
68 meter
Y = -5077277
54 meter E =
0006246
Z = -4069914
46 I = 51
96881
XDOT = 4678
120465 Wp = 27
73958
YDOT = 4710
966007 meter/sec RA = 72
42992 deg
ZDOT = -3883
807818 TA = 202
37693
MA = 202
40420
Ha = 191
799 n
mi
Hp = 187
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5680513
07 X = 1807837
24
Y = -16657734
70 feet Y = -5057488
39 meter
Z = -13352737
73 Z = -4061317
90
XDOT = 15348
164255 XDOT = 4643
960273
YDOT = 15455
925220 feet/sec YDOT = 4763
088659 meter/sec
ZDOT = -12742
151634 ZDOT = -3861
164900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17624058
68 X = -5371813
09
Y = -264865
89 feet Y = -80731
12 meter
Z = -13317896
24 Z = -4059294
78
XDOT = 9840
819938 XDOT = 2999
481917
YDOT = -18196
817838 feet/sec YDOT = -5546
390077 meter/sec
ZDOT = -12650
858915 ZDOT = -3855
981797
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 11044
92687421
00016717 00000-0 10270-3 0 9073
2 25544 51
6456 72
9901 0005138 307
4071 52
6623 15
72372770 21509
Satellite: ISS
Catalog Number: 25544
Epoch time: 11044
92687421 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 72
9901 deg
Eccentricity:
0005138
Arg of perigee: 307
4071 deg
Mean anomaly: 52
6623 deg
Mean motion: 15
72372770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2150
Checksum: 296
Coasting Arc #9 (Orbit 2165)
---------------------------------------
Vector Time (GMT): 2011/045/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4548337
82 A = 6730522
79 meter
Y = -3216813
83 meter E =
0009206
Z = 3774306
80 I = 51
96192
XDOT = 949
290085 Wp = 57
90260
YDOT = -6345
617588 meter/sec RA = 67
27849 deg
ZDOT = -4252
061907 TA = 76
68690
MA = 76
58426
Ha = 191
938 n
mi
Hp = 187
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14922368
19 X = -4530363
16
Y = -10553851
16 feet Y = -3267575
66 meter
Z = 12382896
32 Z = 3752255
19
XDOT = 3114
468783 XDOT = 1040
832609
YDOT = -20818
955342 feet/sec YDOT = -6334
490143 meter/sec
ZDOT = -13950
334342 ZDOT = -4247
228133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5034874
98 X = -1534629
89
Y = 17632521
65 feet Y = 5374392
60 meter
Z = 12293949
01 Z = 3747195
66
XDOT = -19427
360717 XDOT = -5921
459546
YDOT = 4193
822425 feet/sec YDOT = 1278
277075 meter/sec
ZDOT = -13930
644642 ZDOT = -4246
060487
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 11045
94374629
00016717 00000-0 10270-3 0 9080
2 25544 51
6456 67
7808 0005139 313
0851 46
9881 15
72441604 21669
Satellite: ISS
Catalog Number: 25544
Epoch time: 11045
94374629 = yrday
fracday
Element set: 908
Inclination: 51
6456 deg
RA of node: 67
7808 deg
Eccentricity:
0005139
Arg of perigee: 313
0851 deg
Mean anomaly: 46
9881 deg
Mean motion: 15
72441604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2166
Checksum: 323
Coasting Arc #10 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2011/046/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 128243
30 A = 6731843
59 meter
Y = 5840802
40 meter E =
0009959
Z = 3332590
96 I = 51
95280
XDOT = -5522
375743 Wp = 66
36891
YDOT = -2571
553361 meter/sec RA = 62
22742 deg
ZDOT = 4712
381425 TA = 332
62128
MA = 332
67373
Ha = 192
107 n
mi
Hp = 187
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 420745
72 X = 46732
19
Y = 19162737
53 feet Y = 5841780
75 meter
Z = 10933697
37 Z = 3333015
95
XDOT = -18118
030652 XDOT = -5516
100888
YDOT = -8436
854860 feet/sec YDOT = -2633
272815 meter/sec
ZDOT = 15460
568981 ZDOT = 4685
569817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17863621
64 X = 5444831
88
Y = -6945830
74 feet Y = -2117089
21 meter
Z = 10935251
81 Z = 3333064
75
XDOT = -2141
244304 XDOT = -652
651264
YDOT = 18699
982535 feet/sec YDOT = 5699
754677 meter/sec
ZDOT = 15352
381238 ZDOT = 4679
405801
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 11046
96059840
00016717 00000-0 10270-3 0 9099
2 25544 51
6449 62
5704 0005149 317
2251 42
8510 15
72423190 21822
Satellite: ISS
Catalog Number: 25544
Epoch time: 11046
96059840 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 62
5704 deg
Eccentricity:
0005149
Arg of perigee: 317
2251 deg
Mean anomaly: 42
8510 deg
Mean motion: 15
72423190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 295
Coasting Arc #11 (Orbit 2196)
---------------------------------------
Vector Time (GMT): 2011/047/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4926411
97 A = 6728148
33 meter
Y = 1246348
55 meter E =
0005251
Z = -4413723
09 I = 51
92488
XDOT = 1278
223144 Wp = 82
61431
YDOT = 6806
079392 meter/sec RA = 57
07504 deg
ZDOT = 3352
643770 TA = 220
97640
MA = 221
01587
Ha = 192
131 n
mi
Hp = 187
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16162768
94 X = 4933549
27
Y = 4089070
03 feet Y = 1301478
44 meter
Z = -14480718
81 Z = -4389774
10
XDOT = 4193
645486 XDOT = 1185
735293
YDOT = 22329
656798 feet/sec YDOT = 6819
856225 meter/sec
ZDOT = 10999
487435 ZDOT = 3358
628327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2055651
99 X = -626562
73
Y = -16628896
38 feet Y = -5068487
62 meter
Z = -14384050
58 Z = -4384258
62
XDOT = 18119
697883 XDOT = 5522
883915
YDOT = -11763
727987 feet/sec YDOT = -3585
584291 meter/sec
ZDOT = 11023
463177 ZDOT = 3359
951576
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 11047
91387517
00016717 00000-0 10270-3 0 9102
2 25544 51
6443 57
6858 0005164 319
1102 40
9673 15
72485584 21974
Satellite: ISS
Catalog Number: 25544
Epoch time: 11047
91387517 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 57
6858 deg
Eccentricity:
0005164
Arg of perigee: 319
1102 deg
Mean anomaly: 40
9673 deg
Mean motion: 15
72485584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2197
Checksum: 320
Coasting Arc #12 (Orbit 2212)
---------------------------------------
Vector Time (GMT): 2011/048/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2086512
11 A = 6733679
45 meter
Y = -5884669
11 meter E =
0001135
Z = -2523731
33 I = 51
92557
XDOT = 5542
191802 Wp = 48
83764
YDOT = 318
658873 meter/sec RA = 52
01674 deg
ZDOT = -5325
884905 TA = 159
59018
MA = 159
58564
Ha = 192
131 n
mi
Hp = 187
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6845512
17 X = -2008294
13
Y = -19306657
17 feet Y = -5907564
56 meter
Z = -8279958
42 Z = -2533676
93
XDOT = 18183
043971 XDOT = 5564
087917
YDOT = 1045
468743 feet/sec YDOT = 380
757127 meter/sec
ZDOT = -17473
375673 ZDOT = -5298
908674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15318413
47 X = -4669052
43
Y = 13575357
58 feet Y = 4137768
99 meter
Z = -8319954
01 Z = -2535921
98
XDOT = -4939
062171 XDOT = -1505
426150
YDOT = -16213
791599 feet/sec YDOT = -4941
963679 meter/sec
ZDOT = -17364
457850 ZDOT = -5292
686753
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 11048
93068384
00016717 00000-0 10270-3 0 9114
2 25544 51
6437 52
4760 0005148 322
1605 37
9195 15
72491960 22135
Satellite: ISS
Catalog Number: 25544
Epoch time: 11048
93068384 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 52
4760 deg
Eccentricity:
0005148
Arg of perigee: 322
1605 deg
Mean anomaly: 37
9195 deg
Mean motion: 15
72491960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2213
Checksum: 303
Coasting Arc #13 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2011/049/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4605355
31 A = 6726141
23 meter
Y = 659301
80 meter E =
0008469
Z = 4857971
24 I = 51
88114
XDOT = -3460
536559 Wp = 21
15669
YDOT = -6444
939332 meter/sec RA = 46
86944 deg
ZDOT = -2396
889365 TA = 92
20616
MA = 92
10918
Ha = 192
253 n
mi
Hp = 186
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15109433
44 X = -4635983
92
Y = 2163063
66 feet Y = 607631
09 meter
Z = 15938225
87 Z = 4835524
65
XDOT = -11353
466400 XDOT = -3376
567524
YDOT = -21144
814083 feet/sec YDOT = -6483
167852 meter/sec
ZDOT = -7863
810252 ZDOT = -2413
495653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7965002
57 X = 2427732
78
Y = 13130652
22 feet Y = 4002222
80 meter
Z = 15847573
10 Z = 4830340
28
XDOT = -14042
768930 XDOT = -4280
235970
YDOT = 18125
866360 feet/sec YDOT = 5524
764067 meter/sec
ZDOT = -7930
682753 ZDOT = -2417
272103
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 11049
94746899
00016717 00000-0 10270-3 0 9121
2 25544 51
6439 47
2649 0005179 326
2011 33
8821 15
72561532 22296
Satellite: ISS
Catalog Number: 25544
Epoch time: 11049
94746899 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 47
2649 deg
Eccentricity:
0005179
Arg of perigee: 326
2011 deg
Mean anomaly: 33
8821 deg
Mean motion: 15
72561532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 321
Coasting Arc #14 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2011/050/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3897342
80 A = 6734949
08 meter
Y = 5225904
65 meter E =
0014579
Z = 1655474
93 I = 51
88863
XDOT = -4808
930309 Wp = 43
47825
YDOT = 1756
923522 meter/sec RA = 41
79545 deg
ZDOT = 5755
663123 TA = 334
75082
MA = 334
82201
Ha = 192
185 n
mi
Hp = 186
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12786557
75 X = 3830574
28
Y = 17145356
45 feet Y = 5269113
93 meter
Z = 5431348
20 Z = 1674245
09
XDOT = -15777
330411 XDOT = -4856
178449
YDOT = 5764
184782 feet/sec YDOT = 1702
883522 meter/sec
ZDOT = 18883
409196 ZDOT = 5732
186977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10434392
86 X = 3180402
94
Y = -18648200
90 feet Y = -5683971
64 meter
Z = 5506986
36 Z = 1678529
44
XDOT = 10396
671910 XDOT = 3168
905598
YDOT = 11384
355085 feet/sec YDOT = 3469
951430 meter/sec
ZDOT = 18788
571759 ZDOT = 5726
756672
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 11050
96423217
00016717 00000-0 10270-3 0 9132
2 25544 51
6430 42
0535 0005079 329
5340 30
5527 15
72599092 22451
Satellite: ISS
Catalog Number: 25544
Epoch time: 11050
96423217 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 42
0535 deg
Eccentricity:
0005079
Arg of perigee: 329
5340 deg
Mean anomaly: 30
5527 deg
Mean motion: 15
72599092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 287
Coasting Arc #15 (Orbit 2259)
---------------------------------------
Vector Time (GMT): 2011/051/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3664255
08 A = 6724709
61 meter
Y = -2318716
62 meter E =
0011706
Z = -5149372
63 I = 51
82994
XDOT = 5345
252178 Wp = 80
41375
YDOT = 5349
415323 meter/sec RA = 36
65793 deg
ZDOT = 1399
440303 TA = 202
94288
MA = 202
99521
Ha = 192
332 n
mi
Hp = 186
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12021834
26 X = 3714925
33
Y = -7607337
98 feet Y = -2277457
85 meter
Z = -16894267
14 Z = -5131448
72
XDOT = 17536
916593 XDOT = 5278
238630
YDOT = 17550
575207 feet/sec YDOT = 5408
814603 meter/sec
ZDOT = 4591
339577 ZDOT = 1425
243791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12033692
44 X = -3667869
46
Y = -7747808
06 feet Y = -2361531
90 meter
Z = -16821833
10 Z = -5127294
73
XDOT = 7895
821373 XDOT = 2406
646354
YDOT = -22425
170693 feet/sec YDOT = -6835
192027 meter/sec
ZDOT = 4695
362379 ZDOT = 1431
146453
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 11051
91742789
00016717 00000-0 10270-3 0 9147
2 25544 51
6423 37
1678 0005014 334
3825 25
7089 15
72620521 22605
Satellite: ISS
Catalog Number: 25544
Epoch time: 11051
91742789 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 37
1678 deg
Eccentricity:
0005014
Arg of perigee: 334
3825 deg
Mean anomaly: 25
7089 deg
Mean motion: 15
72620521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2260
Checksum: 296
Coasting Arc #16 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2011/052/21:41:41
769
Vector Time (MET): N/A
Weight (LBS) : 863319
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5339558
24 A = 6735680
25 meter
Y = -4023357
81 meter E =
0005637
Z = -805323
76 I = 51
84277
XDOT = 3453
716597 Wp = 124
88548
YDOT = -3393
013342 meter/sec RA = 31
56724 deg
ZDOT = -5980
486352 TA = 63
86254
MA = 63
80457
Ha = 192
363 n
mi
Hp = 186
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17518235
68 X = -5290259
38
Y = -13199992
81 feet Y = -4082792
39 meter
Z = -2642138
32 Z = -831142
90
XDOT = 11331
091197 XDOT = 3520
452922
YDOT = -11131
933537 feet/sec YDOT = -3354
019093 meter/sec
ZDOT = -19621
018214 ZDOT = -5963
546094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4154744
44 X = -1266366
10
Y = 21524531
92 feet Y = 6560677
33 meter
Z = -2746253
92 Z = -837058
19
XDOT = -13464
218959 XDOT = -4103
893939
YDOT = -5080
455237 feet/sec YDOT = -1548
522756 meter/sec
ZDOT = -19552
522914 ZDOT = -5959
608984
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 11052
93414622
00016717 00000-0 10270-3 0 9153
2 25544 51
6429 31
9580 0005090 338
4213 21
6735 15
72661311 22767
Satellite: ISS
Catalog Number: 25544
Epoch time: 11052
93414622 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 31
9580 deg
Eccentricity:
0005090
Arg of perigee: 338
4213 deg
Mean anomaly: 21
6735 deg
Mean motion: 15
72661311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 284
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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