Date:
July 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6081 61 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 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
202/01:19:29
697 -0
9 3
4 3
4
N/A 3
3 0
1 186
9
000/00:04:59
394 0
1 0
2 172
7
204/22:30:58
068 2
1 11
1 11
1
N/A -10
7 -0
0 187
3
000/00:19:56
136 1
9 0
5 179
6
Coasting Arc #1 (Orbit 1492)
---------------------------------------
Vector Time (GMT): 2007/194/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 309310
73 A = 6707336
34 meter
Y = 4492512
78 meter E =
0014185
Z = 4962690
29 I = 51
44337
XDOT = -6992
769195 Wp = 58
50552
YDOT = 2627
828221 meter/sec RA = 327
51006 deg
ZDOT = -1931
671978 TA = 50
22839
MA = 50
10354
Ha = 185
409 n
mi
Hp = 173
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1014798
98 X = 234944
32
Y = 14739215
17 feet Y = 4495554
80 meter
Z = 16281792
30 Z = 4964013
24
XDOT = -22942
156152 XDOT = -7012
250673
YDOT = 8621
483665 feet/sec YDOT = 2549
522638 meter/sec
ZDOT = -6337
506490 ZDOT = -1965
689095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14481540
50 X = 4413973
54
Y = -2894998
41 feet Y = -882395
51 meter
Z = 16287265
29 Z = 4964358
46
XDOT = 11409
109921 XDOT = 3477
496704
YDOT = 20484
621834 feet/sec YDOT = 6243
712735 meter/sec
ZDOT = -6465
927592 ZDOT = -1970
814730
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 07194
50944623
00020000 00000-0 20000-3 0 9003
2 25544 51
6327 327
8197 0008345 61
2598 298
9405 15
78942328 14937
Satellite: ISS
Catalog Number: 25544
Epoch time: 07194
50944623 = yrday
fracday
Element set: 900
Inclination: 51
6327 deg
RA of node: 327
8197 deg
Eccentricity:
0008345
Arg of perigee: 61
2598 deg
Mean anomaly: 298
9405 deg
Mean motion: 15
78942328 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1493
Checksum: 322
Coasting Arc #2 (Orbit 1508)
---------------------------------------
Vector Time (GMT): 2007/195/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5779430
16 A = 6713475
09 meter
Y = -1299485
74 meter E =
0020800
Z = 3136615
33 I = 51
44273
XDOT = -1312
865898 Wp = 77
58916
YDOT = 5874
130940 meter/sec RA = 322
36397 deg
ZDOT = 4830
277748 TA = 319
16706
MA = 319
32272
Ha = 185
142 n
mi
Hp = 173
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18961385
03 X = 5778294
86
Y = -4263404
67 feet Y = -1234863
88 meter
Z = 10290732
70 Z = 3164688
22
XDOT = -4307
302815 XDOT = -1401
917857
YDOT = 19272
083138 feet/sec YDOT = 5858
950868 meter/sec
ZDOT = 15847
367939 ZDOT = 4823
684830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7075333
39 X = -2156561
62
Y = -18040397
03 feet Y = -5498713
01 meter
Z = 10396809
78 Z = 3168947
62
XDOT = 18399
837370 XDOT = 5608
270430
YDOT = 1944
539284 feet/sec YDOT = 592
695574 meter/sec
ZDOT = 15823
041787 ZDOT = 4822
863137
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 07195
52205768
00020000 00000-0 20000-3 0 9017
2 25544 51
6339 322
5804 0008180 64
4950 295
7061 15
79042165 15093
Satellite: ISS
Catalog Number: 25544
Epoch time: 07195
52205768 = yrday
fracday
Element set: 901
Inclination: 51
6339 deg
RA of node: 322
5804 deg
Eccentricity:
0008180
Arg of perigee: 64
4950 deg
Mean anomaly: 295
7061 deg
Mean motion: 15
79042165 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1509
Checksum: 292
Coasting Arc #3 (Orbit 1523)
---------------------------------------
Vector Time (GMT): 2007/196/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2407640
56 A = 6713958
83 meter
Y = -5503574
34 meter E =
0012829
Z = -3002759
96 I = 51
42268
XDOT = 5906
007272 Wp = 67
86457
YDOT = -102
055410 meter/sec RA = 317
12551 deg
ZDOT = 4944
105895 TA = 257
25058
MA = 257
39400
Ha = 185
305 n
mi
Hp = 173
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7899083
21 X = 2483589
93
Y = -18056346
26 feet Y = -5476225
58 meter
Z = -9851574
67 Z = -2990880
39
XDOT = 19376
664278 XDOT = 5882
692512
YDOT = -334
827462 feet/sec YDOT = -36
142334 meter/sec
ZDOT = 16220
819864 ZDOT = 4972
739973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19137585
78 X = -5833136
14
Y = -4801256
65 feet Y = -1463423
03 meter
Z = -9807212
87 Z = -2989238
48
XDOT = -3926
528896 XDOT = -1196
806008
YDOT = -17558
363837 feet/sec YDOT = -5351
789297 meter/sec
ZDOT = 16329
151917 ZDOT = 4977
125504
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 07196
47136465
00020000 00000-0 20000-3 0 9020
2 25544 51
6345 317
6688 0008301 67
1556 293
0486 15
79039244 15245
Satellite: ISS
Catalog Number: 25544
Epoch time: 07196
47136465 = yrday
fracday
Element set: 902
Inclination: 51
6345 deg
RA of node: 317
6688 deg
Eccentricity:
0008301
Arg of perigee: 67
1556 deg
Mean anomaly: 293
0486 deg
Mean motion: 15
79039244 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1524
Checksum: 307
Coasting Arc #4 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2007/197/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4249039
00 A = 6706570
15 meter
Y = -1300539
73 meter E =
0021892
Z = -5042765
51 I = 51
37801
XDOT = 3944
593605 Wp = 74
47100
YDOT = -6387
805570 meter/sec RA = 311
97329 deg
ZDOT = -1676
552086 TA = 179
33233
MA = 179
32940
Ha = 185
242 n
mi
Hp = 172
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13940416
67 X = -4209684
11
Y = -4266862
62 feet Y = -1347834
09 meter
Z = -16544506
26 Z = -5063311
46
XDOT = 12941
580069 XDOT = 4023
874013
YDOT = -20957
367355 feet/sec YDOT = -6343
251382 meter/sec
ZDOT = -5500
498969 ZDOT = -1657
198066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1627551
39 X = -496077
66
Y = 14398238
01 feet Y = 4388582
94 meter
Z = -16622389
71 Z = -5066504
38
XDOT = -21947
865828 XDOT = -6689
709504
YDOT = -8746
395255 feet/sec YDOT = -2665
901274 meter/sec
ZDOT = -5427
957784 ZDOT = -1654
441533
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 07197
48393695
00020000 00000-0 20000-3 0 9033
2 25544 51
6346 312
4295 0008280 70
3330 289
8729 15
79082127 15404
Satellite: ISS
Catalog Number: 25544
Epoch time: 07197
48393695 = yrday
fracday
Element set: 903
Inclination: 51
6346 deg
RA of node: 312
4295 deg
Eccentricity:
0008280
Arg of perigee: 70
3330 deg
Mean anomaly: 289
8729 deg
Mean motion: 15
79082127 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1540
Checksum: 309
Coasting Arc #5 (Orbit 1555)
---------------------------------------
Vector Time (GMT): 2007/198/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4167229
91 A = 6717613
52 meter
Y = 5258690
08 meter E =
0017173
Z = -238545
28 I = 51
39712
XDOT = -3646
120973 Wp = 111
26082
YDOT = -3146
314247 meter/sec RA = 306
76843 deg
ZDOT = -6017
365699 TA = 71
34500
MA = 71
15864
Ha = 185
194 n
mi
Hp = 172
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13672014
14 X = -4224564
86
Y = 17252920
20 feet Y = 5211769
22 meter
Z = -782628
87 Z = -258927
87
XDOT = -11962
339151 XDOT = -3581
436804
YDOT = -10322
553304 feet/sec YDOT = -3186
724820 meter/sec
ZDOT = -19742
013449 ZDOT = -6034
921440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19659462
62 X = 5992204
21
Y = 9897831
96 feet Y = 3016859
18 meter
Z = -859177
53 Z = -261877
31
XDOT = -6992
008369 XDOT = -2131
164151
YDOT = 12259
817426 feet/sec YDOT = 3736
792351 meter/sec
ZDOT = -19808
788261 ZDOT = -6037
718662
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 07198
49648812
00020000 00000-0 20000-3 0 9040
2 25544 51
6344 307
1889 0008292 73
9995 286
2083 15
79121047 15567
Satellite: ISS
Catalog Number: 25544
Epoch time: 07198
49648812 = yrday
fracday
Element set: 904
Inclination: 51
6344 deg
RA of node: 307
1889 deg
Eccentricity:
0008292
Arg of perigee: 73
9995 deg
Mean anomaly: 286
2083 deg
Mean motion: 15
79121047 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1556
Checksum: 329
Coasting Arc #6 (Orbit 1571)
---------------------------------------
Vector Time (GMT): 2007/199/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2051862
73 A = 6707122
00 meter
Y = 4111380
21 meter E =
0014647
Z = 4876013
04 I = 51
34598
XDOT = -5250
890861 Wp = 68
24787
YDOT = 5218
512857 meter/sec RA = 301
55446 deg
ZDOT = -2179
972222 TA = 43
01512
MA = 42
90071
Ha = 185
194 n
mi
Hp = 172
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6731833
10 X = 1982049
82
Y = 13488780
22 feet Y = 4133934
45 meter
Z = 15997418
10 Z = 4885811
66
XDOT = -17227
332220 XDOT = -5298
265071
YDOT = 17121
105175 feet/sec YDOT = 5159
529786 meter/sec
ZDOT = -7152
139836 ZDOT = -2205
595109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11707116
95 X = 3568329
25
Y = -9434292
05 feet Y = -2875572
22 meter
Z = 16034952
48 Z = 4887453
52
XDOT = 19780
877930 XDOT = 6029
211593
YDOT = 12167
518760 feet/sec YDOT = 3708
659718 meter/sec
ZDOT = -7248
515250 ZDOT = -2209
347448
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 07199
50901909
00020000 00000-0 20000-3 0 9053
2 25544 51
6349 301
9495 0008413 77
2251 282
9855 15
79133522 15723
Satellite: ISS
Catalog Number: 25544
Epoch time: 07199
50901909 = yrday
fracday
Element set: 905
Inclination: 51
6349 deg
RA of node: 301
9495 deg
Eccentricity:
0008413
Arg of perigee: 77
2251 deg
Mean anomaly: 282
9855 deg
Mean motion: 15
79133522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1572
Checksum: 308
Coasting Arc #7 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2007/200/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4691383
69 A = 6712390
94 meter
Y = -3413483
14 meter E =
0020821
Z = 3356466
31 I = 51
35072
XDOT = 1104
344983 Wp = 86
33236
YDOT = 6082
581858 meter/sec RA = 296
40235 deg
ZDOT = 4619
124971 TA = 313
54834
MA = 313
72109
Ha = 185
038 n
mi
Hp = 172
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15391678
76 X = 4712900
22
Y = -11199091
66 feet Y = -3360901
45 meter
Z = 11012028
58 Z = 3379308
67
XDOT = 3623
179078 XDOT = 1013
808034
YDOT = 19955
977224 feet/sec YDOT = 6094
424617 meter/sec
ZDOT = 15154
609484 ZDOT = 4624
270456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14496883
44 X = -4418650
07
Y = -12258107
62 feet Y = -3736271
20 meter
Z = 11098079
59 Z = 3382694
66
XDOT = 17665
810510 XDOT = 5384
539044
YDOT = -7085
062398 feet/sec YDOT = -2159
527019 meter/sec
ZDOT = 15174
762476 ZDOT = 4625
267603
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 07200
52152630
00020000 00000-0 20000-3 0 9068
2 25544 51
6351 296
7092 0008318 81
1494 279
0614 15
79207831 15889
Satellite: ISS
Catalog Number: 25544
Epoch time: 07200
52152630 = yrday
fracday
Element set: 906
Inclination: 51
6351 deg
RA of node: 296
7092 deg
Eccentricity:
0008318
Arg of perigee: 81
1494 deg
Mean anomaly: 279
0614 deg
Mean motion: 15
79207831 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1588
Checksum: 289
Coasting Arc #8 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2007/201/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 50812
87 A = 6714248
40 meter
Y = -6143794
68 meter E =
0012787
Z = -2713051
17 I = 51
34494
XDOT = 5277
980347 Wp = 73
13430
YDOT = -2220
853676 meter/sec RA = 291
15713 deg
ZDOT = 5151
684356 TA = 255
71638
MA = 255
85841
Ha = 185
130 n
mi
Hp = 172
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 166708
88 X = 132689
28
Y = -20156806
68 feet Y = -6142768
42 meter
Z = -8901086
52 Z = -2712606
01
XDOT = 17316
208489 XDOT = 5277
396303
YDOT = -7286
265340 feet/sec YDOT = -2161
836069 meter/sec
ZDOT = 16901
851561 ZDOT = 5177
322896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19558891
27 X = -5961550
06
Y = 4877708
33 feet Y = 1486725
50 meter
Z = -8900096
78 Z = -2712749
50
XDOT = -11041
160954 XDOT = -3365
345859
YDOT = -13398
460053 feet/sec YDOT = -4083
850624 meter/sec
ZDOT = 16998
615378 ZDOT = 5181
177967
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 07201
47073580
00020000 00000-0 20000-3 0 9070
2 25544 51
6350 291
7971 0008254 82
7671 277
4433 15
79180195 16034
Satellite: ISS
Catalog Number: 25544
Epoch time: 07201
47073580 = yrday
fracday
Element set: 907
Inclination: 51
6350 deg
RA of node: 291
7971 deg
Eccentricity:
0008254
Arg of perigee: 82
7671 deg
Mean anomaly: 277
4433 deg
Mean motion: 15
79180195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1603
Checksum: 296
Coasting Arc #9 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2007/202/01:21:59
394
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3781551
87 A = 6707036
38 meter
Y = 1855430
63 meter E =
0013714
Z = 5207939
32 I = 51
30972
XDOT = -2790
766154 Wp = 79
74374
YDOT = 7177
834823 meter/sec RA = 288
10318 deg
ZDOT = -527
245863 TA = 15
29716
MA = 15
25574
Ha = 186
883 n
mi
Hp = 172
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12406666
23 X = 3735224
10
Y = 6087370
84 feet Y = 1897458
55 meter
Z = 17086415
09 Z = 5226197
60
XDOT = -9156
056937 XDOT = -2868
261102
YDOT = 23549
326847 feet/sec YDOT = 7146
193660 meter/sec
ZDOT = -1729
809261 ZDOT = -540
990846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5119812
53 X = 1560518
86
Y = 12743469
63 feet Y = 3884209
54 meter
Z = 17155714
30 Z = 5229061
72
XDOT = -21585
534021 XDOT = -6579
270770
YDOT = 11085
632065 feet/sec YDOT = 3378
900653 meter/sec
ZDOT = -1781
005641 ZDOT = -542
850519
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 07202
10355541
00020000 00000-0 20000-3 0 9082
2 25544 51
6352 288
5246 0011023 83
3142 276
9277 15
78624522 16130
Satellite: ISS
Catalog Number: 25544
Epoch time: 07202
10355541 = yrday
fracday
Element set: 908
Inclination: 51
6352 deg
RA of node: 288
5246 deg
Eccentricity:
0011023
Arg of perigee: 83
3142 deg
Mean anomaly: 276
9277 deg
Mean motion: 15
78624522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1613
Checksum: 274
Coasting Arc #10 (Orbit 1628)
---------------------------------------
Vector Time (GMT): 2007/203/01:21:59
394
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2901411
23 A = 6717444
80 meter
Y = -5730933
37 meter E =
0024914
Z = 1931362
29 I = 51
33681
XDOT = 3722
876576 Wp = 75
73596
YDOT = 3788
422354 meter/sec RA = 282
93193 deg
ZDOT = 5594
667124 TA = 305
90295
MA = 306
13394
Ha = 187
013 n
mi
Hp = 172
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9519065
72 X = 2955897
58
Y = -18802274
84 feet Y = -5698183
71 meter
Z = 6336490
46 Z = 1945589
02
XDOT = 12214
161995 XDOT = 3653
059449
YDOT = 12429
207199 feet/sec YDOT = 3829
662694 meter/sec
ZDOT = 18355
207101 ZDOT = 5612
583583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19466798
35 X = 5933480
14
Y = -8031507
49 feet Y = -2448003
48 meter
Z = 6389672
31 Z = 1947572
12
XDOT = 456
378191 XDOT = 139
104073
YDOT = 15903
153689 feet/sec YDOT = 4847
281244 meter/sec
ZDOT = 18423
434843 ZDOT = 5615
462940
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 07203
11642519
00020000 00000-0 20000-3 0 9099
2 25544 51
6351 283
2864 0011076 86
4091 273
8341 15
78610599 16296
Satellite: ISS
Catalog Number: 25544
Epoch time: 07203
11642519 = yrday
fracday
Element set: 909
Inclination: 51
6351 deg
RA of node: 283
2864 deg
Eccentricity:
0011076
Arg of perigee: 86
4091 deg
Mean anomaly: 273
8341 deg
Mean motion: 15
78610599 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1629
Checksum: 297
Coasting Arc #11 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2007/204/01:21:59
394
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2687957
07 A = 6711604
33 meter
Y = -4602905
76 meter E =
0018386
Z = -4095880
45 I = 51
31217
XDOT = 3786
048776 Wp = 97
98192
YDOT = -5544
677595 meter/sec RA = 277
69379 deg
ZDOT = 3758
294446 TA = 210
70276
MA = 210
81047
Ha = 186
914 n
mi
Hp = 172
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8818756
81 X = -2616389
95
Y = -15101396
84 feet Y = -4632563
36 meter
Z = -13437928
00 Z = -4108765
23
XDOT = 12421
419870 XDOT = 3829
511740
YDOT = -18191
199459 feet/sec YDOT = -5502
097311 meter/sec
ZDOT = 12330
362355 ZDOT = 3776
791908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2958009
93 X = 901601
43
Y = -17197263
57 feet Y = -5241725
94 meter
Z = -13487211
35 Z = -4110902
02
XDOT = 19883
378813 XDOT = 6060
453862
YDOT = -6274
197137 feet/sec YDOT = -1912
375287 meter/sec
ZDOT = 12399
726667 ZDOT = 3779
436688
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 07204
06597083
00020000 00000-0 20000-3 0 9101
2 25544 51
6349 278
3756 0010930 89
9206 270
3212 15
78649673 16443
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
06597083 = yrday
fracday
Element set: 910
Inclination: 51
6349 deg
RA of node: 278
3756 deg
Eccentricity:
0010930
Arg of perigee: 89
9206 deg
Mean anomaly: 270
3212 deg
Mean motion: 15
78649673 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1644
Checksum: 306
Coasting Arc #12 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2007/204/22:40:56
136
Vector Time (MET): N/A
Weight (LBS) : 508148
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2440744
72 A = 6720726
41 meter
Y = -5263274
85 meter E =
0006800
Z = -3397138
56 I = 51
31700
XDOT = 3931
654954 Wp = 80
73608
YDOT = -4775
552932 meter/sec RA = 273
07945 deg
ZDOT = 4582
986191 TA = 238
92538
MA = 238
99214
Ha = 187
313 n
mi
Hp = 179
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8007692
65 X = -2365205
97
Y = -17267962
11 feet Y = -5290145
81 meter
Z = -11145467
70 Z = -3408812
90
XDOT = 12899
130425 XDOT = 3962
500435
YDOT = -15667
824581 feet/sec YDOT = -4731
415119 meter/sec
ZDOT = 15036
043933 ZDOT = 4602
160382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15476682
57 X = 4717292
85
Y = -11035294
80 feet Y = -3363557
85 meter
Z = -11190249
01 Z = -3410787
90
XDOT = 16983
916281 XDOT = 5176
697682
YDOT = 8528
666684 feet/sec YDOT = 2599
537605 meter/sec
ZDOT = 15108
059025 ZDOT = 4604
936391
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 07204
95220270
00020000 00000-0 20000-3 0 9111
2 25544 51
6344 273
7920 0002141 55
7247 304
4120 15
76243397 16584
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
95220270 = yrday
fracday
Element set: 911
Inclination: 51
6344 deg
RA of node: 273
7920 deg
Eccentricity:
0002141
Arg of perigee: 55
7247 deg
Mean anomaly: 304
4120 deg
Mean motion: 15
76243397 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1658
Checksum: 267
Coasting Arc #13 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2007/205/22:40:56
136
Vector Time (MET): N/A
Weight (LBS) : 508148
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3442216
09 A = 6716982
81 meter
Y = 3673866
10 meter E =
0011920
Z = -4458476
29 I = 51
30490
XDOT = -2770
903803 Wp = 67
14671
YDOT = -6440
286387 meter/sec RA = 267
95237 deg
ZDOT = -3169
772307 TA = 171
00508
MA = 170
98370
Ha = 187
301 n
mi
Hp = 179
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11293359
89 X = -3461383
60
Y = 12053366
49 feet Y = 3635266
83 meter
Z = -14627546
88 Z = -4475244
50
XDOT = -9090
891742 XDOT = -2683
283520
YDOT = -21129
548515 feet/sec YDOT = -6470
781794 meter/sec
ZDOT = -10399
515444 ZDOT = -3183
021465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14086592
19 X = -4293593
30
Y = -8517238
31 feet Y = -2596054
24 meter
Z = -14690586
14 Z = -4477690
65
XDOT = 18222
142263 XDOT = 5554
108962
YDOT = -12124
747182 feet/sec YDOT = -3695
622941 meter/sec
ZDOT = -10450
396196 ZDOT = -3185
280761
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 07205
96658640
00020000 00000-0 20000-3 0 9120
2 25544 51
6349 268
5646 0002189 56
9356 303
2019 15
76276452 16742
Satellite: ISS
Catalog Number: 25544
Epoch time: 07205
96658640 = yrday
fracday
Element set: 912
Inclination: 51
6349 deg
RA of node: 268
5646 deg
Eccentricity:
0002189
Arg of perigee: 56
9356 deg
Mean anomaly: 303
2019 deg
Mean motion: 15
76276452 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1674
Checksum: 314
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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