Date:
October 26th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4305 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 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 3115)
---------------------------------------
Vector Time (GMT): 2007/297/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4362066
31 A = 6723233
75 meter
Y = 4286708
90 meter E =
0006252
Z = -2796530
29 I = 51
77453
XDOT = -5341
452488 Wp = 81
20324
YDOT = -2094
040942 meter/sec RA = 156
60908 deg
ZDOT = 5132
426880 TA = 246
83519
MA = 246
90107
Ha = 187
913 n
mi
Hp = 180
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14311241
17 X = -4396091
33
Y = 14064005
59 feet Y = 4237739
39 meter
Z = -9174968
14 Z = -2817804
68
XDOT = -17524
450419 XDOT = -5342
572679
YDOT = -6870
213064 feet/sec YDOT = -2153
778033 meter/sec
ZDOT = 16838
670867 ZDOT = 5106
474830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15970712
94 X = 4867873
31
Y = -12085675
96 feet Y = -3683714
03 meter
Z = -9255305
61 Z = -2821017
15
XDOT = 15691
971745 XDOT = 4782
912988
YDOT = 7943
374865 feet/sec YDOT = 2421
140659 meter/sec
ZDOT = 16739
724814 ZDOT = 5102
268123
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 07297
39694683
00020000 00000-0 20000-3 0 9002
2 25544 51
6382 157
5777 0002396 120
7477 239
3923 15
75924388 31168
Satellite: ISS
Catalog Number: 25544
Epoch time: 07297
39694683 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 157
5777 deg
Eccentricity:
0002396
Arg of perigee: 120
7477 deg
Mean anomaly: 239
3923 deg
Mean motion: 15
75924388 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3116
Checksum: 332
Coasting Arc #2 (Orbit 3131)
---------------------------------------
Vector Time (GMT): 2007/298/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4270686
16 A = 6716683
34 meter
Y = 1984427
77 meter E =
0013199
Z = -4801296
71 I = 51
77849
XDOT = -5195
648793 Wp = 79
89837
YDOT = 5081
799179 meter/sec RA = 151
51178 deg
ZDOT = -2524
676835 TA = 165
43185
MA = 165
39377
Ha = 187
835 n
mi
Hp = 180
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14011437
52 X = 4271503
17
Y = 6510589
80 feet Y = 2032189
36 meter
Z = -15752285
78 Z = -4780547
14
XDOT = -17046
091841 XDOT = -5239
823259
YDOT = 16672
569485 feet/sec YDOT = 5023
451390 meter/sec
ZDOT = -8283
060481 ZDOT = -2550
025636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13271791
98 X = -4045242
20
Y = -8065673
26 feet Y = -2458417
21 meter
Z = -15673133
73 Z = -4777171
16
XDOT = 18189
935452 XDOT = 5544
292326
YDOT = -13672
282697 feet/sec YDOT = -4167
311766 meter/sec
ZDOT = -8378
797925 ZDOT = -2553
857608
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 07298
41153680
00020000 00000-0 20000-3 0 9014
2 25544 51
6381 152
3520 0002276 123
1484 236
9899 15
75958745 31325
Satellite: ISS
Catalog Number: 25544
Epoch time: 07298
41153680 = yrday
fracday
Element set: 901
Inclination: 51
6381 deg
RA of node: 152
3520 deg
Eccentricity:
0002276
Arg of perigee: 123
1484 deg
Mean anomaly: 236
9899 deg
Mean motion: 15
75958745 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3132
Checksum: 301
Coasting Arc #3 (Orbit 3147)
---------------------------------------
Vector Time (GMT): 2007/299/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4649560
69 A = 6725560
97 meter
Y = -4585020
45 meter E =
0016434
Z = 1576324
83 I = 51
83252
XDOT = 4440
559693 Wp = 118
93675
YDOT = 2502
572374 meter/sec RA = 146
33801 deg
ZDOT = -5781
543721 TA = 43
69768
MA = 43
56769
Ha = 187
845 n
mi
Hp = 180
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15254464
20 X = 4692827
73
Y = -15042718
00 feet Y = -4532784
49 meter
Z = 5171669
39 Z = 1599018
35
XDOT = 14568
765398 XDOT = 4440
332219
YDOT = 8210
539284 feet/sec YDOT = 2552
227897 meter/sec
ZDOT = -18968
319295 ZDOT = -5759
971286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16600910
15 X = -5059957
41
Y = 13509177
25 feet Y = 4117597
22 meter
Z = 5257387
15 Z = 1602451
60
XDOT = -12832
774607 XDOT = -3911
429700
YDOT = -8373
039145 feet/sec YDOT = -2552
102331 meter/sec
ZDOT = -18885
971060 ZDOT = -5756
443979
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 07299
42611072
00020000 00000-0 20000-3 0 9021
2 25544 51
6374 147
1260 0002370 129
0030 231
1345 15
75936108 31486
Satellite: ISS
Catalog Number: 25544
Epoch time: 07299
42611072 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 147
1260 deg
Eccentricity:
0002370
Arg of perigee: 129
0030 deg
Mean anomaly: 231
1345 deg
Mean motion: 15
75936108 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3148
Checksum: 259
Coasting Arc #4 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2007/300/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3482572
71 A = 6714796
67 meter
Y = -2440392
06 meter E =
0005962
Z = 5193074
83 I = 51
82022
XDOT = 5388
564794 Wp = 126
86367
YDOT = -5406
596170 meter/sec RA = 141
22431 deg
ZDOT = 1068
594134 TA = 312
95307
MA = 313
00305
Ha = 187
784 n
mi
Hp = 180
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11425763
47 X = -3480252
95
Y = -8006535
63 feet Y = -2479323
33 meter
Z = 17037647
09 Z = 5176161
46
XDOT = 17679
018352 XDOT = 5443
430450
YDOT = -17738
176412 feet/sec YDOT = -5346
031449 meter/sec
ZDOT = 3505
886266 ZDOT = 1094
905833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10852850
67 X = 3307948
88
Y = 8891919
96 feet Y = 2710257
20 meter
Z = 16973022
53 Z = 5173377
27
XDOT = -18356
926056 XDOT = -5595
191062
YDOT = 15496
047895 feet/sec YDOT = 4723
195399 meter/sec
ZDOT = 3605
278427 ZDOT = 1098
888865
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 07300
44066421
00020000 00000-0 20000-3 0 9039
2 25544 51
6375 141
8996 0002165 131
3794 228
7556 15
76002054 31648
Satellite: ISS
Catalog Number: 25544
Epoch time: 07300
44066421 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 141
8996 deg
Eccentricity:
0002165
Arg of perigee: 131
3794 deg
Mean anomaly: 228
7556 deg
Mean motion: 15
76002054 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3164
Checksum: 279
Coasting Arc #5 (Orbit 3178)
---------------------------------------
Vector Time (GMT): 2007/301/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4694038
07 A = 6726343
39 meter
Y = 4804403
04 meter E =
0011749
Z = -260161
88 I = 51
88122
XDOT = -3562
352865 Wp = 53
04160
YDOT = -3163
206278 meter/sec RA = 136
07583 deg
ZDOT = 6053
239724 TA = 304
13858
MA = 304
24996
Ha = 187
533 n
mi
Hp = 180
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15400387
37 X = -4746148
90
Y = 15762477
17 feet Y = 4751620
30 meter
Z = -853549
46 Z = -283092
53
XDOT = -11687
509401 XDOT = -3556
123118
YDOT = -10377
973354 feet/sec YDOT = -3203
008043 meter/sec
ZDOT = 19859
710380 ZDOT = 6035
948219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16340823
12 X = 4980682
89
Y = -14780045
04 feet Y = -4504957
73 meter
Z = -940176
89 Z = -286565
92
XDOT = 10056
843324 XDOT = 3065
325845
YDOT = 9896
403847 feet/sec YDOT = 3016
423893 meter/sec
ZDOT = 19793
556264 ZDOT = 6033
075949
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 07301
39179313
00020000 00000-0 20000-3 0 9040
2 25544 51
6374 136
9997 0002026 135
7411 224
3915 15
76037940 31792
Satellite: ISS
Catalog Number: 25544
Epoch time: 07301
39179313 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 136
9997 deg
Eccentricity:
0002026
Arg of perigee: 135
7411 deg
Mean anomaly: 224
3915 deg
Mean motion: 15
76037940 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3179
Checksum: 294
Coasting Arc #6 (Orbit 3194)
---------------------------------------
Vector Time (GMT): 2007/302/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2754900
63 A = 6714298
40 meter
Y = 3140029
65 meter E =
0016338
Z = -5270637
86 I = 51
86042
XDOT = -5324
645363 Wp = 98
73438
YDOT = 5528
246638 meter/sec RA = 130
93878 deg
ZDOT = 509
280381 TA = 176
10069
MA = 176
08794
Ha = 187
434 n
mi
Hp = 180
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9038387
89 X = 2745188
04
Y = 10301934
53 feet Y = 3170782
58 meter
Z = -17292118
97 Z = -5257277
58
XDOT = -17469
308935 XDOT = -5388
541362
YDOT = 18137
292121 feet/sec YDOT = 5468
346144 meter/sec
ZDOT = 1670
867393 ZDOT = 483
257794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8666233
41 X = -2641467
94
Y = -10699852
10 feet Y = -3261314
92 meter
Z = -17240917
97 Z = -5255031
80
XDOT = 17491
041795 XDOT = 5331
269539
YDOT = -16706
360503 feet/sec YDOT = -5092
098681 meter/sec
ZDOT = 1572
547796 ZDOT = 479
312568
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 07302
40631307
00020000 00000-0 20000-3 0 9050
2 25544 51
6370 131
7727 0001899 139
2060 220
9246 15
76066315 31953
Satellite: ISS
Catalog Number: 25544
Epoch time: 07302
40631307 = yrday
fracday
Element set: 905
Inclination: 51
6370 deg
RA of node: 131
7727 deg
Eccentricity:
0001899
Arg of perigee: 139
2060 deg
Mean anomaly: 220
9246 deg
Mean motion: 15
76066315 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3195
Checksum: 275
Coasting Arc #7 (Orbit 3210)
---------------------------------------
Vector Time (GMT): 2007/303/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4570229
38 A = 6725827
77 meter
Y = -4791499
19 meter E =
0011435
Z = -1150495
25 I = 51
91723
XDOT = 2784
779975 Wp = 143
37341
YDOT = 4068
304507 meter/sec RA = 125
82078 deg
ZDOT = -5920
034921 TA = 49
18776
MA = 49
08864
Ha = 187
465 n
mi
Hp = 180
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14994190
86 X = 4629057
97
Y = -15720141
70 feet Y = -4740063
29 meter
Z = -3774590
71 Z = -1128150
09
XDOT = 9136
417240 XDOT = 2767
839618
YDOT = 13347
455730 feet/sec YDOT = 4099
351194 meter/sec
ZDOT = -19422
686748 ZDOT = -5906
547060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15441604
59 X = -4706601
08
Y = 15301495
15 feet Y = 4663895
72 meter
Z = -3690154
94 Z = -1124759
22
XDOT = -7759
486129 XDOT = -2365
091372
YDOT = -12470
579011 feet/sec YDOT = -3801
032482 meter/sec
ZDOT = -19370
885645 ZDOT = -5904
245945
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 07303
42081638
00020000 00000-0 20000-3 0 9060
2 25544 51
6372 126
5470 0001954 147
4267 212
7018 15
76039678 32111
Satellite: ISS
Catalog Number: 25544
Epoch time: 07303
42081638 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 126
5470 deg
Eccentricity:
0001954
Arg of perigee: 147
4267 deg
Mean anomaly: 212
7018 deg
Mean motion: 15
76039678 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3211
Checksum: 283
Coasting Arc #8 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2007/304/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2161122
76 A = 6715443
96 meter
Y = -3976444
36 meter E =
0006235
Z = 4956826
22 I = 51
89913
XDOT = 5101
030129 Wp = 72
51682
YDOT = -5386
372479 meter/sec RA = 120
65990 deg
ZDOT = -2093
062367 TA = 37
69085
MA = 37
64718
Ha = 187
298 n
mi
Hp = 180
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7090297
76 X = -2140576
65
Y = -13046077
31 feet Y = -4000496
66 meter
Z = 16262553
20 Z = 4946377
01
XDOT = 16735
663152 XDOT = 5171
050101
YDOT = -17671
825717 feet/sec YDOT = -5328
938252 meter/sec
ZDOT = -6867
002517 ZDOT = -2068
111431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7047191
12 X = 2147983
85
Y = 13119317
26 feet Y = 3998767
90 meter
Z = 16222321
16 Z = 4944563
49
XDOT = -15998
281566 XDOT = -4876
276221
YDOT = 16984
436001 feet/sec YDOT = 5176
856093 meter/sec
ZDOT = -6772
710258 ZDOT = -2064
322087
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 07304
43529917
00020000 00000-0 20000-3 0 9070
2 25544 51
6373 121
3199 0001728 149
3850 210
7416 15
76129809 32274
Satellite: ISS
Catalog Number: 25544
Epoch time: 07304
43529917 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 121
3199 deg
Eccentricity:
0001728
Arg of perigee: 149
3850 deg
Mean anomaly: 210
7416 deg
Mean motion: 15
76129809 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3227
Checksum: 296
Coasting Arc #9 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2007/305/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4309860
39 A = 6723454
49 meter
Y = 4520227
89 meter E =
0014284
Z = 2474102
54 I = 51
93895
XDOT = -2226
718836 Wp = 81
72172
YDOT = -5069
766727 meter/sec RA = 115
56542 deg
ZDOT = 5359
522045 TA = 306
16718
MA = 306
29924
Ha = 187
166 n
mi
Hp = 180
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14139961
90 X = -4372104
82
Y = 14830144
00 feet Y = 4471684
47 meter
Z = 8117134
32 Z = 2453013
97
XDOT = -7305
507993 XDOT = -2195
898340
YDOT = -16633
092935 feet/sec YDOT = -5094
495033 meter/sec
ZDOT = 17583
733745 ZDOT = 5348
779191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14082551
68 X = 4292361
75
Y = -14927863
10 feet Y = -4550012
67 meter
Z = 8037425
23 Z = 2449807
21
XDOT = 6430
716882 XDOT = 1960
082506
YDOT = 15554
635493 feet/sec YDOT = 4741
052898 meter/sec
ZDOT = 17542
251702 ZDOT = 5346
878319
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 07305
44976528
00020000 00000-0 20000-3 0 9087
2 25544 51
6364 116
0927 0001681 155
4231 204
7014 15
76151414 32435
Satellite: ISS
Catalog Number: 25544
Epoch time: 07305
44976528 = yrday
fracday
Element set: 908
Inclination: 51
6364 deg
RA of node: 116
0927 deg
Eccentricity:
0001681
Arg of perigee: 155
4231 deg
Mean anomaly: 204
7014 deg
Mean motion: 15
76151414 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3243
Checksum: 274
Coasting Arc #10 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2007/306/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1775434
55 A = 6718048
48 meter
Y = 4865496
46 meter E =
0009860
Z = -4288951
54 I = 51
93142
XDOT = -4779
467270 Wp = 117
80704
YDOT = 4873
915956 meter/sec RA = 110
38710 deg
ZDOT = 3552
283303 TA = 188
08359
MA = 188
09949
Ha = 187
088 n
mi
Hp = 180
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5824916
50 X = 1741731
06
Y = 15962914
90 feet Y = 4885162
00 meter
Z = -14071363
33 Z = -4280408
17
XDOT = -15680
666896 XDOT = -4850
869455
YDOT = 15990
537914 feet/sec YDOT = 4820
069955 meter/sec
ZDOT = 11654
472778 ZDOT = 3528
891036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6287315
70 X = -1916373
82
Y = -15815944
24 feet Y = -4820699
81 meter
Z = -14038274
08 Z = -4278865
94
XDOT = 14202
540794 XDOT = 4328
934434
YDOT = -15907
092139 feet/sec YDOT = -4848
481684 meter/sec
ZDOT = 11566
031841 ZDOT = 3525
326505
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 07306
40081109
00020000 00000-0 20000-3 0 9097
2 25544 51
6355 111
1916 0001685 156
8047 203
3193 15
76166455 32583
Satellite: ISS
Catalog Number: 25544
Epoch time: 07306
40081109 = yrday
fracday
Element set: 909
Inclination: 51
6355 deg
RA of node: 111
1916 deg
Eccentricity:
0001685
Arg of perigee: 156
8047 deg
Mean anomaly: 203
3193 deg
Mean motion: 15
76166455 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3258
Checksum: 282
Coasting Arc #11 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2007/307/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4054018
32 A = 6720124
79 meter
Y = -3901554
31 meter E =
0006158
Z = -3679457
60 I = 51
94663
XDOT = 1880
276265 Wp = 94
31920
YDOT = 6059
648265 meter/sec RA = 105
30696 deg
ZDOT = -4360
397506 TA = 129
71251
MA = 129
65821
Ha = 187
044 n
mi
Hp = 180
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13300585
05 X = 4115219
16
Y = -12800375
03 feet Y = -3855877
79 meter
Z = -12071711
30 Z = -3659614
27
XDOT = 6168
885385 XDOT = 1833
558913
YDOT = 19880
735777 feet/sec YDOT = 6080
413368 meter/sec
ZDOT = -14305
766095 ZDOT = -4351
376486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12828194
59 X = -3910033
71
Y = 13341628
96 feet Y = 4066528
51 meter
Z = -11996655
26 Z = -3656580
52
XDOT = -6092
384695 XDOT = -1856
958855
YDOT = -18670
223186 feet/sec YDOT = -5690
684027 meter/sec
ZDOT = -14270
717909 ZDOT = -4349
714819
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 07307
41524127
00020000 00000-0 20000-3 0 9103
2 25544 51
6347 105
9649 0001611 159
6379 200
4850 15
76190202 32749
Satellite: ISS
Catalog Number: 25544
Epoch time: 07307
41524127 = yrday
fracday
Element set: 910
Inclination: 51
6347 deg
RA of node: 105
9649 deg
Eccentricity:
0001611
Arg of perigee: 159
6379 deg
Mean anomaly: 200
4850 deg
Mean motion: 15
76190202 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3274
Checksum: 274
Coasting Arc #12 (Orbit 3289)
---------------------------------------
Vector Time (GMT): 2007/308/09:23:23
224
Vector Time (MET): N/A
Weight (LBS) : 509051
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1566098
42 A = 6721214
78 meter
Y = -5667006
57 meter E =
0013274
Z = 3243447
11 I = 51
95782
XDOT = 4522
883955 Wp = 98
75349
YDOT = -4000
587892 meter/sec RA = 100
12455 deg
ZDOT = -4791
476284 TA = 43
41563
MA = 43
31116
Ha = 186
855 n
mi
Hp = 180
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5138118
18 X = -1518369
04
Y = -18592541
25 feet Y = -5684252
66 meter
Z = 10641230
67 Z = 3235954
89
XDOT = 14838
858120 XDOT = 4590
559483
YDOT = -13125
288358 feet/sec YDOT = -3949
632108 meter/sec
ZDOT = -15720
066550 ZDOT = -4769
339323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6276534
65 X = 1913087
76
Y = 18256729
05 feet Y = 5564651
01 meter
Z = 10612049
57 Z = 3234552
71
XDOT = -12802
629221 XDOT = -3902
241386
YDOT = 13518
139883 feet/sec YDOT = 4120
329036 meter/sec
ZDOT = -15636
288344 ZDOT = -4765
940687
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 07308
42965104
00020000 00000-0 20000-3 0 9110
2 25544 51
6352 100
7370 0001463 169
2412 190
8784 15
76251836 32906
Satellite: ISS
Catalog Number: 25544
Epoch time: 07308
42965104 = yrday
fracday
Element set: 911
Inclination: 51
6352 deg
RA of node: 100
7370 deg
Eccentricity:
0001463
Arg of perigee: 169
2412 deg
Mean anomaly: 190
8784 deg
Mean motion: 15
76251836 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3290
Checksum: 278
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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