Date:
November 7th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6768 35 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 3308)
---------------------------------------
Vector Time (GMT): 2007/309/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3163522
77 A = 6718619
83 meter
Y = -3978813
32 meter E =
0009907
Z = 4385338
49 I = 51
95271
XDOT = 3088
580108 Wp = 85
27166
YDOT = -6197
246486 meter/sec RA = 93
97967 deg
ZDOT = -3387
395193 TA = 38
68270
MA = 38
61178
Ha = 187
908 n
mi
Hp = 180
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10379011
72 X = -3140099
60
Y = -13053849
46 feet Y = -4014058
58 meter
Z = 14387593
48 Z = 4370026
73
XDOT = 10133
136836 XDOT = 3174
104809
YDOT = -20332
173509 feet/sec YDOT = -6162
230098 meter/sec
ZDOT = -11113
501288 ZDOT = -3372
182699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15000676
25 X = 4572206
12
Y = -7402253
32 feet Y = -2256206
81 meter
Z = 14328854
59 Z = 4367434
88
XDOT = 17118
672180 XDOT = 5217
771281
YDOT = 13242
253043 feet/sec YDOT = 4036
238727 meter/sec
ZDOT = -11056
326864 ZDOT = -3369
968428
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 07309
63569468
00020000 00000-0 20000-3 0 9005
2 25544 51
6384 94
5480 0002619 157
6137 202
5142 15
75839916 33092
Satellite: ISS
Catalog Number: 25544
Epoch time: 07309
63569468 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 94
5480 deg
Eccentricity:
0002619
Arg of perigee: 157
6137 deg
Mean anomaly: 202
5142 deg
Mean motion: 15
75839916 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3309
Checksum: 309
Coasting Arc #2 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2007/310/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2605248
57 A = 6721515
47 meter
Y = 5137163
38 meter E =
0013421
Z = 3455616
34 I = 51
96467
XDOT = -3687
570050 Wp = 101
33628
YDOT = -4970
241900 meter/sec RA = 88
90149 deg
ZDOT = 4591
207353 TA = 299
44436
MA = 299
57822
Ha = 187
606 n
mi
Hp = 180
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8547403
44 X = -2679286
67
Y = 16854210
57 feet Y = 5107616
09 meter
Z = 11337323
96 Z = 3442779
82
XDOT = -12098
326936 XDOT = -3654
021821
YDOT = -16306
567915 feet/sec YDOT = -5011
290769 meter/sec
ZDOT = 15063
016251 ZDOT = 4573
374219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14808403
74 X = -4513601
46
Y = -11786674
79 feet Y = -3592578
48 meter
Z = 11289061
53 Z = 3440905
95
XDOT = 17541
752165 XDOT = 5346
726060
YDOT = -7622
163169 feet/sec YDOT = -2323
235334 meter/sec
ZDOT = 14994
571202 ZDOT = 4570
345302
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 07310
65030714
00020000 00000-0 20000-3 0 9017
2 25544 51
6389 89
3221 0002503 163
3322 196
7925 15
75936895 33259
Satellite: ISS
Catalog Number: 25544
Epoch time: 07310
65030714 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 89
3221 deg
Eccentricity:
0002503
Arg of perigee: 163
3322 deg
Mean anomaly: 196
7925 deg
Mean motion: 15
75936895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3325
Checksum: 288
Coasting Arc #3 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2007/311/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3303413
06 A = 6721247
73 meter
Y = 4663210
22 meter E =
0006329
Z = -3545435
34 I = 51
96219
XDOT = -2939
858978 Wp = 115
92791
YDOT = 5504
712130 meter/sec RA = 83
72314 deg
ZDOT = 4504
487478 TA = 202
05473
MA = 202
08198
Ha = 187
451 n
mi
Hp = 180
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10837969
35 X = 3268246
42
Y = 15299246
14 feet Y = 4699954
24 meter
Z = -11632005
70 Z = -3529472
29
XDOT = -9645
206621 XDOT = -3023
077641
YDOT = 18060
079166 feet/sec YDOT = 5471
371654 meter/sec
ZDOT = 14778
502224 ZDOT = 4490
003083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17025756
77 X = -5189450
66
Y = 7941921
17 feet Y = 2420697
57 meter
Z = -11570720
08 Z = -3526755
48
XDOT = -15412
620180 XDOT = -4697
766631
YDOT = -11606
348550 feet/sec YDOT = -3537
615038 meter/sec
ZDOT = 14724
001220 ZDOT = 4487
875572
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 07311
60148377
00020000 00000-0 20000-3 0 9029
2 25544 51
6392 84
4240 0002262 167
9961 192
1257 15
75938407 33407
Satellite: ISS
Catalog Number: 25544
Epoch time: 07311
60148377 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 84
4240 deg
Eccentricity:
0002262
Arg of perigee: 167
9961 deg
Mean anomaly: 192
1257 deg
Mean motion: 15
75938407 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3340
Checksum: 288
Coasting Arc #4 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2007/312/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2592776
04 A = 6718332
13 meter
Y = -4414780
76 meter E =
0008807
Z = -4358111
50 I = 51
94854
XDOT = 3889
692902 Wp = 83
82711
YDOT = 5678
916859 meter/sec RA = 78
64503 deg
ZDOT = -3443
643399 TA = 151
57323
MA = 151
52516
Ha = 187
369 n
mi
Hp = 180
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8506483
07 X = 2663121
69
Y = -14484188
84 feet Y = -4385393
46 meter
Z = -14298266
07 Z = -4345344
59
XDOT = 12761
459653 XDOT = 3842
630444
YDOT = 18631
616992 feet/sec YDOT = 5722
150537 meter/sec
ZDOT = -11298
042646 ZDOT = -3424
860862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12871430
46 X = 3923212
01
Y = 10855936
18 feet Y = 3308889
35 meter
Z = -14250169
14 Z = -4343451
55
XDOT = -19698
422786 XDOT = -6004
079265
YDOT = 8641
293687 feet/sec YDOT = 2633
866316 meter/sec
ZDOT = -11225
919230 ZDOT = -3421
660181
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 07312
61604378
00020000 00000-0 20000-3 0 9030
2 25544 51
6394 79
1984 0002277 171
2175 188
9030 15
75980881 33568
Satellite: ISS
Catalog Number: 25544
Epoch time: 07312
61604378 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 79
1984 deg
Eccentricity:
0002277
Arg of perigee: 171
2175 deg
Mean anomaly: 188
9030 deg
Mean motion: 15
75980881 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3356
Checksum: 310
Coasting Arc #5 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2007/313/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3509336
00 A = 6723924
01 meter
Y = -5193813
94 meter E =
0015018
Z = 2411493
58 I = 51
96070
XDOT = 3049
254835 Wp = 113
31294
YDOT = -4577
400018 meter/sec RA = 73
47156 deg
ZDOT = -5400
735592 TA = 39
56434
MA = 39
45482
Ha = 187
321 n
mi
Hp = 180
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11513569
57 X = -3462712
16
Y = -17040071
99 feet Y = -5232796
73 meter
Z = 7911724
34 Z = 2394557
70
XDOT = 10004
116913 XDOT = 3126
450064
YDOT = -15017
716596 feet/sec YDOT = -4542
869689 meter/sec
ZDOT = -17718
948792 ZDOT = -5385
734480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18560931
11 X = 5657371
80
Y = -8913079
48 feet Y = -2716706
63 meter
Z = 7846691
66 Z = 2391671
62
XDOT = 12709
828146 XDOT = 3873
955619
YDOT = 10858
507750 feet/sec YDOT = 3309
673162 meter/sec
ZDOT = -17662
356391 ZDOT = -5383
486228
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 07313
63057578
00020000 00000-0 20000-3 0 9048
2 25544 51
6393 73
9731 0002165 170
1022 190
0186 15
76027778 33726
Satellite: ISS
Catalog Number: 25544
Epoch time: 07313
63057578 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 73
9731 deg
Eccentricity:
0002165
Arg of perigee: 170
1022 deg
Mean anomaly: 190
0186 deg
Mean motion: 15
76027778 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3372
Checksum: 286
Coasting Arc #6 (Orbit 3387)
---------------------------------------
Vector Time (GMT): 2007/314/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2792231
57 A = 6715446
22 meter
Y = 3536454
18 meter E =
0007365
Z = 4976696
34 I = 51
92417
XDOT = -4158
447573 Wp = 136
72360
YDOT = -6160
170123 meter/sec RA = 68
37889 deg
ZDOT = 2037
277111 TA = 293
61528
MA = 293
69259
Ha = 187
118 n
mi
Hp = 180
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9160864
74 X = -2855745
90
Y = 11602539
97 feet Y = 3504874
44 meter
Z = 16327743
89 Z = 4962977
16
XDOT = -13643
200700 XDOT = -4099
151605
YDOT = -20210
531899 feet/sec YDOT = -6206
340820 meter/sec
ZDOT = 6683
980023 ZDOT = 2017
218366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10293273
44 X = -3137389
74
Y = -10690133
44 feet Y = -3258352
67 meter
Z = 16275907
53 Z = 4960896
62
XDOT = 21046
082445 XDOT = 6414
845929
YDOT = -10170
414234 feet/sec YDOT = -3099
942258 meter/sec
ZDOT = 6606
963200 ZDOT = 2013
802383
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 07314
64507709
00020000 00000-0 20000-3 0 9057
2 25544 51
6401 68
7468 0002035 177
4858 182
6316 15
76106782 33880
Satellite: ISS
Catalog Number: 25544
Epoch time: 07314
64507709 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 68
7468 deg
Eccentricity:
0002035
Arg of perigee: 177
4858 deg
Mean anomaly: 182
6316 deg
Mean motion: 15
76106782 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3388
Checksum: 309
Coasting Arc #7 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2007/315/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3727281
95 A = 6725741
84 meter
Y = 5486999
85 meter E =
0008367
Z = -1092888
72 I = 51
94660
XDOT = -3433
609380 Wp = 44
96372
YDOT = 3507
933499 meter/sec RA = 63
22218 deg
ZDOT = 5934
975867 TA = 303
12177
MA = 303
20205
Ha = 187
011 n
mi
Hp = 180
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12228615
32 X = 3670957
69
Y = 18001968
02 feet Y = 5528365
59 meter
Z = -3585592
92 Z = -1074917
40
XDOT = -11265
122638 XDOT = -3501
412363
YDOT = 11508
968174 feet/sec YDOT = 3469
157360 meter/sec
ZDOT = 19471
705601 ZDOT = 5918
130451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19277509
08 X = -5875784
77
Y = 10123118
45 feet Y = 3085526
50 meter
Z = -3516600
42 Z = -1071859
81
XDOT = -9403
294716 XDOT = -2866
124230
YDOT = -11203
311749 feet/sec YDOT = -3414
769421 meter/sec
ZDOT = 19407
957510 ZDOT = 5915
545449
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 07315
59614852
00020000 00000-0 20000-3 0 9061
2 25544 51
6399 63
8482 0001706 179
9432 180
1733 15
76085460 34030
Satellite: ISS
Catalog Number: 25544
Epoch time: 07315
59614852 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 63
8482 deg
Eccentricity:
0001706
Arg of perigee: 179
9432 deg
Mean anomaly: 180
1733 deg
Mean motion: 15
76085460 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3403
Checksum: 303
Coasting Arc #8 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2007/316/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3275244
40 A = 6714043
18 meter
Y = -2572794
56 meter E =
0014876
Z = -5278730
56 I = 51
89283
XDOT = 4328
662857 Wp = 93
44438
YDOT = 6347
290579 meter/sec RA = 58
10420 deg
ZDOT = -409
692677 TA = 172
68605
MA = 172
66433
Ha = 186
866 n
mi
Hp = 180
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10745552
50 X = 3329414
19
Y = -8440927
04 feet Y = -2535865
55 meter
Z = -17318669
82 Z = -5262687
64
XDOT = 14201
649792 XDOT = 4259
355044
YDOT = 20824
444156 feet/sec YDOT = 6395
308657 meter/sec
ZDOT = -1344
136080 ZDOT = -388
831198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7354515
05 X = 2241656
19
Y = 11607304
60 feet Y = 3537906
44 meter
Z = -17257869
52 Z = -5260198
63
XDOT = -21252
674191 XDOT = -6477
815094
YDOT = 11595
613613 feet/sec YDOT = 3534
343029 meter/sec
ZDOT = -1264
055304 ZDOT = -385
284057
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 07316
61059646
00020000 00000-0 20000-3 0 9070
2 25544 51
6393 58
6220 0001739 184
3490 175
7659 15
76145709 34193
Satellite: ISS
Catalog Number: 25544
Epoch time: 07316
61059646 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 58
6220 deg
Eccentricity:
0001739
Arg of perigee: 184
3490 deg
Mean anomaly: 175
7659 deg
Mean motion: 15
76145709 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3419
Checksum: 315
Coasting Arc #9 (Orbit 3434)
---------------------------------------
Vector Time (GMT): 2007/317/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3787422
13 A = 6725804
40 meter
Y = -5536210
12 meter E =
0012577
Z = -396014
79 I = 51
91691
XDOT = 4127
568226 Wp = 142
93399
YDOT = -2398
845206 meter/sec RA = 52
97159 deg
ZDOT = -6048
568636 TA = 41
36007
MA = 41
26490
Ha = 186
764 n
mi
Hp = 180
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12425925
64 X = -3723310
09
Y = -18163419
02 feet Y = -5578204
71 meter
Z = -1299261
13 Z = -414259
37
XDOT = 13541
890504 XDOT = 4183
469260
YDOT = -7870
227054 feet/sec YDOT = -2352
375223 meter/sec
ZDOT = -19844
385290 ZDOT = -6028
380885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19092304
97 X = 5819334
56
Y = -10936655
17 feet Y = -3333492
50 meter
Z = -1369292
71 Z = -417360
42
XDOT = 5963
463997 XDOT = 1817
663826
YDOT = 12843
177722 feet/sec YDOT = 3914
600570 meter/sec
ZDOT = -19767
781079 ZDOT = -6025
219673
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 07317
62501599
00020000 00000-0 20000-3 0 9082
2 25544 51
6394 53
3957 0001588 181
5466 178
5694 15
76216314 34356
Satellite: ISS
Catalog Number: 25544
Epoch time: 07317
62501599 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 53
3957 deg
Eccentricity:
0001588
Arg of perigee: 181
5466 deg
Mean anomaly: 178
5694 deg
Mean motion: 15
76216314 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3435
Checksum: 320
Coasting Arc #10 (Orbit 3450)
---------------------------------------
Vector Time (GMT): 2007/318/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3971801
13 A = 6714174
28 meter
Y = 1644886
87 meter E =
0003366
Z = 5154904
46 I = 51
85996
XDOT = -4293
020677 Wp = 72
31420
YDOT = -6266
137593 meter/sec RA = 47
82173 deg
ZDOT = -1306
560881 TA = 30
14275
MA = 30
12339
Ha = 186
681 n
mi
Hp = 180
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13030843
59 X = -4014941
40
Y = 5396610
47 feet Y = 1600230
21 meter
Z = 16912416
21 Z = 5135504
44
XDOT = -14084
713507 XDOT = -4216
285548
YDOT = -20558
194204 feet/sec YDOT = -6313
715400 meter/sec
ZDOT = -4286
617064 ZDOT = -1327
231039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4568879
86 X = -1392594
58
Y = -13436469
94 feet Y = -4095436
04 meter
Z = 16838726
90 Z = 5132443
96
XDOT = 20413
903084 XDOT = 6222
157660
YDOT = -12419
923568 feet/sec YDOT = -3785
592704 meter/sec
ZDOT = -4365
958234 ZDOT = -1330
744070
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 07318
63940522
00020000 00000-0 20000-3 0 9098
2 25544 51
6396 48
1690 0001518 191
7881 168
3248 15
76285789 34513
Satellite: ISS
Catalog Number: 25544
Epoch time: 07318
63940522 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 48
1690 deg
Eccentricity:
0001518
Arg of perigee: 191
7881 deg
Mean anomaly: 168
3248 deg
Mean motion: 15
76285789 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3451
Checksum: 323
Coasting Arc #11 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2007/319/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3619245
93 A = 6724161
22 meter
Y = 5341450
17 meter E =
0013637
Z = 1872463
21 I = 51
87260
XDOT = -5028
397030 Wp = 71
43867
YDOT = 1410
567546 meter/sec RA = 42
71311 deg
ZDOT = 5666
307270 TA = 309
31208
MA = 309
43291
Ha = 186
636 n
mi
Hp = 180
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11874166
44 X = 3550151
80
Y = 17524442
80 feet Y = 5381536
13 meter
Z = 6143251
99 Z = 1889878
46
XDOT = -16497
365585 XDOT = -5071
322833
YDOT = 4627
846281 feet/sec YDOT = 1354
096629 meter/sec
ZDOT = 18590
246949 ZDOT = 5641
774775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18040370
83 X = -5498705
03
Y = 11037257
96 feet Y = 3364156
23 meter
Z = 6210106
79 Z = 1892840
55
XDOT = -3069
786476 XDOT = -935
670918
YDOT = -15478
103611 feet/sec YDOT = -4717
725981 meter/sec
ZDOT = 18496
987882 ZDOT = 5637
881907
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 07319
65377007
00020000 00000-0 20000-3 0 9105
2 25544 51
6390 42
9418 0001261 183
1815 176
9342 15
76274075 34677
Satellite: ISS
Catalog Number: 25544
Epoch time: 07319
65377007 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 42
9418 deg
Eccentricity:
0001261
Arg of perigee: 183
1815 deg
Mean anomaly: 176
9342 deg
Mean motion: 15
76274075 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3467
Checksum: 294
Coasting Arc #12 (Orbit 3481)
---------------------------------------
Vector Time (GMT): 2007/320/14:15:28
336
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4822720
27 A = 6716404
42 meter
Y = -860575
41 meter E =
0010706
Z = -4605141
74 I = 51
82507
XDOT = 3894
184540 Wp = 115
94155
YDOT = 5936
111651 meter/sec RA = 37
53473 deg
ZDOT = 2969
600360 TA = 183
45268
MA = 183
46008
Ha = 186
500 n
mi
Hp = 180
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15822573
06 X = 4854356
18
Y = -2823410
13 feet Y = -806467
78 meter
Z = -15108732
74 Z = -4581635
85
XDOT = 12776
195997 XDOT = 3813
090630
YDOT = 19475
431927 feet/sec YDOT = 5979
204981 meter/sec
ZDOT = 9742
783334 ZDOT = 2988
322055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2378575
57 X = 724989
83
Y = 15980037
57 feet Y = 4870715
45 meter
Z = -15019322
41 Z = -4577889
47
XDOT = -18657
379426 XDOT = -5686
769249
YDOT = 11999
459147 feet/sec YDOT = 3657
435148 meter/sec
ZDOT = 9814
674971 ZDOT = 2991
512931
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 07320
60470845
00020000 00000-0 20000-3 0 9117
2 25544 51
6393 38
0411 0001184 188
0133 172
1013 15
76339298 34829
Satellite: ISS
Catalog Number: 25544
Epoch time: 07320
60470845 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 38
0411 deg
Eccentricity:
0001184
Arg of perigee: 188
0133 deg
Mean anomaly: 172
1013 deg
Mean motion: 15
76339298 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3482
Checksum: 268
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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