Date:
February 17th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3171)
---------------------------------------
Vector Time (GMT): 2007/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5585221
11 A = 6716824
59 meter
Y = 2741938
20 meter E =
0014461
Z = 2551245
53 I = 51
68316
XDOT = -4222
643134 Wp = 173
27438
YDOT = 3670
911635 meter/sec RA = 7
24121 deg
ZDOT = 5281
862221 TA = 215
64256
MA = 215
73921
Ha = 187
713 n
mi
Hp = 174
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18324216
25 X = 5541752
19
Y = 8995860
24 feet Y = 2804152
20 meter
Z = 8370228
13 Z = 2578272
06
XDOT = -13853
816056 XDOT = -4289
035432
YDOT = 12043
673344 feet/sec YDOT = 3623
320449 meter/sec
ZDOT = 17328
944294 ZDOT = 5261
188057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9926865
87 X = 3025708
72
Y = 17788884
87 feet Y = 5422052
11 meter
Z = 8472073
57 Z = 2582288
02
XDOT = -17025
462057 XDOT = -5189
360835
YDOT = 1258
175678 feet/sec YDOT = 383
491947 meter/sec
ZDOT = 17251
742750 ZDOT = 5258
331190
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 07047
55813942
00020000 00000-0 20000-3 0 9004
2 25544 51
6336 7
4001 0021150 214
3143 145
6658 15
78384820 31729
Satellite: ISS
Catalog Number: 25544
Epoch time: 07047
55813942 = yrday
fracday
Element set: 900
Inclination: 51
6336 deg
RA of node: 7
4001 deg
Eccentricity:
0021150
Arg of perigee: 214
3143 deg
Mean anomaly: 145
6658 deg
Mean motion: 15
78384820 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3172
Checksum: 265
Coasting Arc #2 (Orbit 3186)
---------------------------------------
Vector Time (GMT): 2007/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4864038
25 A = 6713837
88 meter
Y = -2770450
44 meter E =
0019083
Z = -3715992
82 I = 51
64422
XDOT = 5317
064345 Wp = 202
04535
YDOT = 3571
278291 meter/sec RA = 2
02498 deg
ZDOT = 4272
743489 TA = 113
10156
MA = 112
90031
Ha = 187
438 n
mi
Hp = 175
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15958130
75 X = 4912707
35
Y = -9089404
33 feet Y = -2715786
03 meter
Z = -12191577
50 Z = -3692245
81
XDOT = 17444
436829 XDOT = 5255
979097
YDOT = 11716
792293 feet/sec YDOT = 3630
395254 meter/sec
ZDOT = 14018
187299 ZDOT = 4298
424460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18377029
32 X = 5601318
54
Y = 1312463
23 feet Y = 400038
79 meter
Z = -12102727
12 Z = -3688911
23
XDOT = 8061
042373 XDOT = 2457
005715
YDOT = 18035
657176 feet/sec YDOT = 5497
268307 meter/sec
ZDOT = 14115
085222 ZDOT = 4302
277976
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 07048
50784269
00020000 00000-0 20000-3 0 9010
2 25544 51
6338 2
4903 0020954 218
2779 141
6900 15
78368391 31873
Satellite: ISS
Catalog Number: 25544
Epoch time: 07048
50784269 = yrday
fracday
Element set: 901
Inclination: 51
6338 deg
RA of node: 2
4903 deg
Eccentricity:
0020954
Arg of perigee: 218
2779 deg
Mean anomaly: 141
6900 deg
Mean motion: 15
78368391 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3187
Checksum: 305
Coasting Arc #3 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2007/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3423273
07 A = 6710223
56 meter
Y = -3468491
80 meter E =
0012514
Z = -4603930
19 I = 51
60508
XDOT = 6621
327530 Wp = 197
63016
YDOT = -2674
214691 meter/sec RA = 356
90315 deg
ZDOT = -2918
305871 TA = 43
55861
MA = 43
45986
Ha = 187
000 n
mi
Hp = 175
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11231210
86 X = -3361869
06
Y = -11379566
27 feet Y = -3506429
69 meter
Z = -15104757
84 Z = -4620410
62
XDOT = 21723
515517 XDOT = 6664
915065
YDOT = -8773
670247 feet/sec YDOT = -2599
927766 meter/sec
ZDOT = -9574
494326 ZDOT = -2886
034376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3243596
15 X = -988648
11
Y = -15595731
31 feet Y = -4753578
90 meter
Z = -15167088
85 Z = -4622928
68
XDOT = 21930
728427 XDOT = 6684
486025
YDOT = 4601
891419 feet/sec YDOT = 1402
656504 meter/sec
ZDOT = -9453
619395 ZDOT = -2881
463191
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 07049
52083616
00020000 00000-0 20000-3 0 9022
2 25544 51
6347 357
2534 0020921 222
1704 137
7853 15
78430306 32038
Satellite: ISS
Catalog Number: 25544
Epoch time: 07049
52083616 = yrday
fracday
Element set: 902
Inclination: 51
6347 deg
RA of node: 357
2534 deg
Eccentricity:
0020921
Arg of perigee: 222
1704 deg
Mean anomaly: 137
7853 deg
Mean motion: 15
78430306 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3203
Checksum: 272
Coasting Arc #4 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2007/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6336781
64 A = 6719016
87 meter
Y = 1856679
06 meter E =
0022363
Z = 1163964
13 I = 51
60666
XDOT = -2360
672294 Wp = 188
24592
YDOT = -4380
369445 meter/sec RA = 351
69867 deg
ZDOT = -5900
176237 TA = 338
95748
MA = 339
04935
Ha = 186
824 n
mi
Hp = 175
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20789966
01 X = -6362726
53
Y = 6091466
72 feet Y = 1785672
64 meter
Z = 3818779
94 Z = 1133117
60
XDOT = -7744
987842 XDOT = -2282
853599
YDOT = -14371
290829 feet/sec YDOT = -4406
333120 meter/sec
ZDOT = -19357
533587 ZDOT = -5911
454784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20909566
24 X = -6373235
79
Y = -5743550
87 feet Y = -1750634
30 meter
Z = 3703160
38 Z = 1128723
28
XDOT = 627
715721 XDOT = 191
327752
YDOT = -14715
956598 feet/sec YDOT = -4485
423571 meter/sec
ZDOT = -19400
442101 ZDOT = -5913
254752
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 07050
53380745
00020000 00000-0 20000-3 0 9039
2 25544 51
6353 352
0171 0020950 225
9584 133
9856 15
78442711 32195
Satellite: ISS
Catalog Number: 25544
Epoch time: 07050
53380745 = yrday
fracday
Element set: 903
Inclination: 51
6353 deg
RA of node: 352
0171 deg
Eccentricity:
0020950
Arg of perigee: 225
9584 deg
Mean anomaly: 133
9856 deg
Mean motion: 15
78442711 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3219
Checksum: 286
Coasting Arc #5 (Orbit 3234)
---------------------------------------
Vector Time (GMT): 2007/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 570884
64 A = 6707338
73 meter
Y = 4150393
94 meter E =
0018562
Z = 5248901
62 I = 51
53974
XDOT = -7542
580046 Wp = 226
71905
YDOT = 1497
968705 meter/sec RA = 346
53266 deg
ZDOT = -377
462598 TA = 226
79300
MA = 226
94819
Ha = 186
397 n
mi
Hp = 175
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1872981
10 X = 498934
12
Y = 13616778
01 feet Y = 4156375
96 meter
Z = 17220805
84 Z = 5251499
87
XDOT = -24745
997525 XDOT = -7556
936354
YDOT = 4914
595489 feet/sec YDOT = 1413
543065 meter/sec
ZDOT = -1238
394350 ZDOT = -414
138805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5421296
44 X = -1652411
16
Y = 12616660
02 feet Y = 3845557
97 meter
Z = 17231085
01 Z = 5252034
71
XDOT = -22862
383795 XDOT = -6968
454581
YDOT = -8004
389088 feet/sec YDOT = -2439
737794 meter/sec
ZDOT = -1375
948334 ZDOT = -419
389052
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 07051
54675409
00020000 00000-0 20000-3 0 9046
2 25544 51
6354 346
7807 0020978 230
2317 129
7001 15
78510099 32353
Satellite: ISS
Catalog Number: 25544
Epoch time: 07051
54675409 = yrday
fracday
Element set: 904
Inclination: 51
6354 deg
RA of node: 346
7807 deg
Eccentricity:
0020978
Arg of perigee: 230
2317 deg
Mean anomaly: 129
7001 deg
Mean motion: 15
78510099 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3235
Checksum: 291
Coasting Arc #6 (Orbit 3250)
---------------------------------------
Vector Time (GMT): 2007/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6440093
17 A = 6717821
01 meter
Y = -647099
29 meter E =
0007762
Z = 1817860
19 I = 51
54757
XDOT = -1082
821273 Wp = 210
11875
YDOT = 5105
542341 meter/sec RA = 341
37547 deg
ZDOT = 5657
303766 TA = 170
08003
MA = 170
06470
Ha = 186
120 n
mi
Hp = 175
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21128914
60 X = 6438019
76
Y = -2123029
17 feet Y = -575094
07 meter
Z = 5964108
24 Z = 1849140
78
XDOT = -3552
563232 XDOT = -1167
313526
YDOT = 16750
466997 feet/sec YDOT = 5092
961512 meter/sec
ZDOT = 18560
707894 ZDOT = 5651
837982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19375561
17 X = 5905671
05
Y = 8608823
01 feet Y = 2623969
25 meter
Z = 6081502
10 Z = 1853641
84
XDOT = -10847
515636 XDOT = -3306
322766
YDOT = 11325
032116 feet/sec YDOT = 3451
869789 meter/sec
ZDOT = 18540
820927 ZDOT = 5651
242219
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 07052
55967923
00020000 00000-0 20000-3 0 9054
2 25544 51
6351 341
5425 0020944 234
0934 125
8288 15
78528643 32515
Satellite: ISS
Catalog Number: 25544
Epoch time: 07052
55967923 = yrday
fracday
Element set: 905
Inclination: 51
6351 deg
RA of node: 341
5425 deg
Eccentricity:
0020944
Arg of perigee: 234
0934 deg
Mean anomaly: 125
8288 deg
Mean motion: 15
78528643 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3251
Checksum: 301
Coasting Arc #7 (Orbit 3265)
---------------------------------------
Vector Time (GMT): 2007/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2342693
71 A = 6711547
68 meter
Y = -4685105
30 meter E =
0017216
Z = -4196525
66 I = 51
50008
XDOT = 6802
058897 Wp = 215
25616
YDOT = 140
695402 meter/sec RA = 336
15397 deg
ZDOT = 3618
935706 TA = 91
71711
MA = 91
51991
Ha = 185
805 n
mi
Hp = 175
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7686002
97 X = 2415294
87
Y = -15371080
39 feet Y = -4658502
18 meter
Z = -13768128
80 Z = -4184968
49
XDOT = 22316
466196 XDOT = 6782
400119
YDOT = 461
599089 feet/sec YDOT = 216
650009 meter/sec
ZDOT = 11873
148643 ZDOT = 3651
932020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14193302
12 X = 4326118
49
Y = -9750494
16 feet Y = -2971950
62 meter
Z = -13725311
04 Z = -4183474
80
XDOT = 18580
532056 XDOT = 5663
346171
YDOT = 10060
750581 feet/sec YDOT = 3066
516777 meter/sec
ZDOT = 11997
083765 ZDOT = 3656
711132
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 07053
50927507
00020000 00000-0 20000-3 0 9065
2 25544 51
6354 336
6321 0020915 237
7039 122
2101 15
78571580 32661
Satellite: ISS
Catalog Number: 25544
Epoch time: 07053
50927507 = yrday
fracday
Element set: 906
Inclination: 51
6354 deg
RA of node: 336
6321 deg
Eccentricity:
0020915
Arg of perigee: 237
7039 deg
Mean anomaly: 122
2101 deg
Mean motion: 15
78571580 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3266
Checksum: 278
Coasting Arc #8 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2007/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5109218
33 A = 6711153
58 meter
Y = -1010568
25 meter E =
0012456
Z = -4219264
59 I = 51
47425
XDOT = 4049
211781 Wp = 235
99723
YDOT = -5504
420263 meter/sec RA = 331
02318 deg
ZDOT = -3584
272475 TA = 357
57643
MA = 357
58246
Ha = 185
303 n
mi
Hp = 175
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16762527
33 X = -5077042
08
Y = -3315512
62 feet Y = -1067522
48 meter
Z = -13842731
60 Z = -4244006
75
XDOT = 13284
815555 XDOT = 4127
873612
YDOT = -18059
121598 feet/sec YDOT = -5458
699907 meter/sec
ZDOT = -11759
424129 ZDOT = -3564
410528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13225930
86 X = -4031263
73
Y = -10698832
04 feet Y = -3261004
01 meter
Z = -13935778
07 Z = -4247625
16
XDOT = 19439
899636 XDOT = 5925
281409
YDOT = -8807
944478 feet/sec YDOT = -2684
661477 meter/sec
ZDOT = -11685
516440 ZDOT = -3561
745411
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 07054
52215497
00020000 00000-0 20000-3 0 9077
2 25544 51
6359 331
3948 0020856 241
7542 118
1518 15
78617174 32825
Satellite: ISS
Catalog Number: 25544
Epoch time: 07054
52215497 = yrday
fracday
Element set: 907
Inclination: 51
6359 deg
RA of node: 331
3948 deg
Eccentricity:
0020856
Arg of perigee: 241
7542 deg
Mean anomaly: 118
1518 deg
Mean motion: 15
78617174 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3282
Checksum: 304
Coasting Arc #9 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2007/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4433616
80 A = 6717734
88 meter
Y = 4715638
09 meter E =
0015970
Z = 1768295
52 I = 51
47158
XDOT = -4685
738966 Wp = 202
46865
YDOT = -2286
328845 meter/sec RA = 325
79862 deg
ZDOT = -5682
685790 TA = 317
84450
MA = 317
96721
Ha = 185
215 n
mi
Hp = 175
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14545986
88 X = -4494608
17
Y = 15471253
58 feet Y = 4665717
87 meter
Z = 5801494
50 Z = 1746609
23
XDOT = -15373
159336 XDOT = -4632
219572
YDOT = -7501
078888 feet/sec YDOT = -2338
428064 meter/sec
ZDOT = -18643
982250 ZDOT = -5705
318839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19980983
31 X = -6090203
71
Y = 7255165
16 feet Y = 2211374
34 meter
Z = 5720633
24 Z = 1743649
01
XDOT = -9730
739704 XDOT = -2965
929462
YDOT = -12113
128418 feet/sec YDOT = -3692
081542 meter/sec
ZDOT = -18729
269300 ZDOT = -5708
681283
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 07055
53501268
00020000 00000-0 20000-3 0 9084
2 25544 51
6357 326
1570 0020917 245
4622 114
4363 15
78619728 32985
Satellite: ISS
Catalog Number: 25544
Epoch time: 07055
53501268 = yrday
fracday
Element set: 908
Inclination: 51
6357 deg
RA of node: 326
1570 deg
Eccentricity:
0020917
Arg of perigee: 245
4622 deg
Mean anomaly: 114
4363 deg
Mean motion: 15
78619728 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3298
Checksum: 301
Coasting Arc #10 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2007/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2891527
61 A = 6706768
57 meter
Y = 3042328
26 meter E =
0018978
Z = 5246165
59 I = 51
41253
XDOT = -5807
156018 Wp = 245
22175
YDOT = 5042
668549 meter/sec RA = 320
63171 deg
ZDOT = 269
340307 TA = 202
17087
MA = 202
25304
Ha = 184
832 n
mi
Hp = 175
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9486639
13 X = 2831808
49
Y = 9981391
91 feet Y = 3074328
90 meter
Z = 17211829
35 Z = 5260067
39
XDOT = -19052
349139 XDOT = -5864
420643
YDOT = 16544
188154 feet/sec YDOT = 4977
409500 meter/sec
ZDOT = 883
662426 ZDOT = 240
990680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4119467
35 X = 1255613
65
Y = 13070627
66 feet Y = 3983927
31 meter
Z = 17264421
73 Z = 5262195
74
XDOT = -23400
241425 XDOT = -7132
393586
YDOT = 6317
123666 feet/sec YDOT = 1925
459293 meter/sec
ZDOT = 777
811810 ZDOT = 237
077040
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 07056
54784526
00020000 00000-0 20000-3 0 9097
2 25544 51
6358 320
9187 0021017 249
6696 110
2211 15
78699902 33148
Satellite: ISS
Catalog Number: 25544
Epoch time: 07056
54784526 = yrday
fracday
Element set: 909
Inclination: 51
6358 deg
RA of node: 320
9187 deg
Eccentricity:
0021017
Arg of perigee: 249
6696 deg
Mean anomaly: 110
2211 deg
Mean motion: 15
78699902 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3314
Checksum: 307
Coasting Arc #11 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2007/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5378113
07 A = 6718024
33 meter
Y = -3799093
77 meter E =
0007983
Z = 1335523
24 I = 51
42956
XDOT = 1867
107101 Wp = 277
52027
YDOT = 4680
088509 meter/sec RA = 315
45466 deg
ZDOT = 5825
108350 TA = 97
20841
MA = 97
11765
Ha = 184
591 n
mi
Hp = 175
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17644727
92 X = 5413707
79
Y = -12464218
41 feet Y = -3738753
72 meter
Z = 4381637
93 Z = 1361735
89
XDOT = 6125
679466 XDOT = 1786
338243
YDOT = 15354
621094 feet/sec YDOT = 4700
515822 meter/sec
ZDOT = 19111
247869 ZDOT = 5833
982462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21221567
87 X = 6468333
89
Y = -3933189
00 feet Y = -1198836
01 meter
Z = 4479620
12 Z = 1365388
21
XDOT = -1255
981895 XDOT = -382
823282
YDOT = 14916
140106 feet/sec YDOT = 4546
439504 meter/sec
ZDOT = 19145
165449 ZDOT = 5835
446429
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 07057
56065778
00020000 00000-0 20000-3 0 9103
2 25544 51
6361 315
6799 0020925 253
8307 106
0555 15
78699282 33308
Satellite: ISS
Catalog Number: 25544
Epoch time: 07057
56065778 = yrday
fracday
Element set: 910
Inclination: 51
6361 deg
RA of node: 315
6799 deg
Eccentricity:
0020925
Arg of perigee: 253
8307 deg
Mean anomaly: 106
0555 deg
Mean motion: 15
78699282 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3330
Checksum: 313
Coasting Arc #12 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2007/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -411172
96 A = 6710047
41 meter
Y = -5007539
59 meter E =
0013961
Z = -4441951
78 I = 51
38370
XDOT = 6170
566147 Wp = 235
05004
YDOT = -3349
388001 meter/sec RA = 310
22940 deg
ZDOT = 3189
724314 TA = 66
98711
MA = 66
83992
Ha = 184
363 n
mi
Hp = 175
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1348992
64 X = -333569
76
Y = -16428935
67 feet Y = -5011703
63 meter
Z = -14573332
61 Z = -4443760
75
XDOT = 20244
639590 XDOT = 6192
066192
YDOT = -10988
805778 feet/sec YDOT = -3280
265094 meter/sec
ZDOT = 10464
974783 ZDOT = 3219
752311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5466865
00 X = 1666300
45
Y = -15544342
10 feet Y = -4737915
47 meter
Z = -14580759
50 Z = -4444215
50
XDOT = 21770
130687 XDOT = 6635
535833
YDOT = -2311
216053 feet/sec YDOT = -704
458653 meter/sec
ZDOT = 10577
346350 ZDOT = 3223
975167
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 07058
51014692
00020000 00000-0 20000-3 0 9119
2 25544 51
6364 310
7692 0021021 257
5490 102
3324 15
78747508 33455
Satellite: ISS
Catalog Number: 25544
Epoch time: 07058
51014692 = yrday
fracday
Element set: 911
Inclination: 51
6364 deg
RA of node: 310
7692 deg
Eccentricity:
0021021
Arg of perigee: 257
5490 deg
Mean anomaly: 102
3324 deg
Mean motion: 15
78747508 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3345
Checksum: 276
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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