Date:
April 8th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 1688)
---------------------------------------
Vector Time (GMT): 2008/095/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1839877
42 A = 6717045
02 meter
Y = -5150377
66 meter E =
0006822
Z = -3907252
28 I = 51
82805
XDOT = 6485
219398 Wp = 62
71809
YDOT = 773
126576 meter/sec RA = 36
17341 deg
ZDOT = -4075
259062 TA = 164
96472
MA = 164
94443
Ha = 185
438 n
mi
Hp = 179
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6036343
24 X = -1763167
60
Y = -16897564
51 feet Y = -5170523
68 meter
Z = -12819069
15 Z = -3916003
61
XDOT = 21276
966530 XDOT = 6495
889079
YDOT = 2536
504514 feet/sec YDOT = 845
707292 meter/sec
ZDOT = -13370
272512 ZDOT = -4043
727986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -557640
17 X = -169968
72
Y = -17910291
05 feet Y = -5459056
71 meter
Z = -12853177
50 Z = -3917648
50
XDOT = 18271
417946 XDOT = 5569
128190
YDOT = 8933
819371 feet/sec YDOT = 2723
028144 meter/sec
ZDOT = -13249
238015 ZDOT = -4038
367747
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 08095
43992638
00020000 00000-0 20000-3 0 9005
2 25544 51
6387 36
5664 0001170 340
7826 19
3295 15
76971058 16893
Satellite: ISS
Catalog Number: 25544
Epoch time: 08095
43992638 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 36
5664 deg
Eccentricity:
0001170
Arg of perigee: 340
7826 deg
Mean anomaly: 19
3295 deg
Mean motion: 15
76971058 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1689
Checksum: 320
Coasting Arc #2 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2008/096/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6030828
06 A = 6720354
85 meter
Y = -1110653
01 meter E =
0013033
Z = 2736239
49 I = 51
81548
XDOT = -1335
574451 Wp = 96
26922
YDOT = -5551
312577 meter/sec RA = 30
97925 deg
ZDOT = -5177
443183 TA = 52
50530
MA = 52
38687
Ha = 185
373 n
mi
Hp = 179
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19786181
30 X = -6031252
60
Y = -3643874
72 feet Y = -1178095
31 meter
Z = 8977163
69 Z = 2706940
58
XDOT = -4381
805941 XDOT = -1248
248266
YDOT = -18212
967773 feet/sec YDOT = -5565
759932 meter/sec
ZDOT = -16986
362149 ZDOT = -5183
718840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17957874
46 X = -5473560
13
Y = -9181109
32 feet Y = -2798402
12 meter
Z = 8864662
32 Z = 2701949
07
XDOT = 449
840807 XDOT = 137
111478
YDOT = -17367
255588 feet/sec YDOT = -5293
539503 meter/sec
ZDOT = -17011
010231 ZDOT = -5184
955918
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 08096
45382081
00020000 00000-0 20000-3 0 9014
2 25544 51
6389 31
3365 0001255 338
7871 21
3241 15
77041112 17050
Satellite: ISS
Catalog Number: 25544
Epoch time: 08096
45382081 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 31
3365 deg
Eccentricity:
0001255
Arg of perigee: 338
7871 deg
Mean anomaly: 21
3241 deg
Mean motion: 15
77041112 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1705
Checksum: 266
Coasting Arc #3 (Orbit 1720)
---------------------------------------
Vector Time (GMT): 2008/097/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 370392
60 A = 6712554
38 meter
Y = 4514677
79 meter E =
0004969
Z = 4950581
56 I = 51
76544
XDOT = -7229
253101 Wp = 116
79303
YDOT = -1687
805911 meter/sec RA = 25
87176 deg
ZDOT = 2076
283337 TA = 313
13209
MA = 313
17364
Ha = 185
139 n
mi
Hp = 179
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1215198
81 X = 295831
88
Y = 14811935
02 feet Y = 4518403
20 meter
Z = 16242065
49 Z = 4952199
52
XDOT = -23718
021986 XDOT = -7219
928842
YDOT = -5537
420967 feet/sec YDOT = -1768
595268 meter/sec
ZDOT = 6811
953204 ZDOT = 2041
185925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2923066
31 X = -890950
61
Y = 14563967
14 feet Y = 4439097
18 meter
Z = 16248734
20 Z = 4952614
18
XDOT = -20312
773413 XDOT = -6191
333336
YDOT = -11540
315509 feet/sec YDOT = -3517
488167 meter/sec
ZDOT = 6677
157089 ZDOT = 2035
197481
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 08097
46767141
00020000 00000-0 20000-3 0 9021
2 25544 51
6399 26
1068 0001231 332
9376 27
1725 15
77132940 17212
Satellite: ISS
Catalog Number: 25544
Epoch time: 08097
46767141 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 26
1068 deg
Eccentricity:
0001231
Arg of perigee: 332
9376 deg
Mean anomaly: 27
1725 deg
Mean motion: 15
77132940 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1721
Checksum: 285
Coasting Arc #4 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2008/098/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6433045
74 A = 6722918
02 meter
Y = 1764473
11 meter E =
0011183
Z = -790989
57 I = 51
77360
XDOT = -591
264829 Wp = 33
90810
YDOT = 4817
037323 meter/sec RA = 20
69727 deg
ZDOT = 5986
172254 TA = 317
47110
MA = 317
55767
Ha = 185
168 n
mi
Hp = 179
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21105793
10 X = 6416679
55
Y = 5788953
78 feet Y = 1836319
57 meter
Z = -2595110
14 Z = -759777
14
XDOT = -1939
845238 XDOT = -674
165981
YDOT = 15803
928225 feet/sec YDOT = 4809
962192 meter/sec
ZDOT = 19639
672750 ZDOT = 5983
098267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18960128
03 X = 5779047
02
Y = 10958464
76 feet Y = 3340140
06 meter
Z = -2475213
16 Z = -754444
97
XDOT = -5195
119377 XDOT = -1583
472386
YDOT = 13383
594469 feet/sec YDOT = 4079
319594 meter/sec
ZDOT = 19628
368437 ZDOT = 5982
726700
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 08098
41811899
00020000 00000-0 20000-3 0 9038
2 25544 51
6397 21
2030 0001177 340
3492 19
7627 15
77170309 17361
Satellite: ISS
Catalog Number: 25544
Epoch time: 08098
41811899 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 21
2030 deg
Eccentricity:
0001177
Arg of perigee: 340
3492 deg
Mean anomaly: 19
7627 deg
Mean motion: 15
77170309 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1736
Checksum: 291
Coasting Arc #5 (Orbit 1751)
---------------------------------------
Vector Time (GMT): 2008/099/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1477677
01 A = 6710965
62 meter
Y = -3904974
46 meter E =
0014536
Z = -5266421
77 I = 51
70671
XDOT = 7330
480174 Wp = 88
03702
YDOT = 2317
873969 meter/sec RA = 15
54906 deg
ZDOT = 339
440590 TA = 185
17713
MA = 185
19218
Ha = 185
028 n
mi
Hp = 179
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4848021
69 X = 1546816
97
Y = -12811596
00 feet Y = -3888063
70 meter
Z = -17278286
66 Z = -5259075
12
XDOT = 24050
131803 XDOT = 7302
367556
YDOT = 7604
573389 feet/sec YDOT = 2399
690404 meter/sec
ZDOT = 1113
650229 ZDOT = 374
984351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7842188
19 X = 2390298
96
Y = -11273862
48 feet Y = -3436273
28 meter
Z = -17250495
80 Z = -5257951
12
XDOT = 20733
214297 XDOT = 6319
483718
YDOT = 12515
684422 feet/sec YDOT = 3814
780612 meter/sec
ZDOT = 1250
212913 ZDOT = 381
064896
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 08099
43188691
00020000 00000-0 20000-3 0 9049
2 25544 51
6405 15
9721 0001254 338
6824 21
4288 15
77227664 17521
Satellite: ISS
Catalog Number: 25544
Epoch time: 08099
43188691 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 15
9721 deg
Eccentricity:
0001254
Arg of perigee: 338
6824 deg
Mean anomaly: 21
4288 deg
Mean motion: 15
77227664 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1752
Checksum: 302
Coasting Arc #6 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2008/100/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6175080
66 A = 6721901
47 meter
Y = -2252536
94 meter E =
0007386
Z = -1393150
61 I = 51
71645
XDOT = 2828
936403 Wp = 139
52078
YDOT = -4161
459124 meter/sec RA = 10
41075 deg
ZDOT = -5833
307462 TA = 55
79537
MA = 55
72539
Ha = 184
906 n
mi
Hp = 178
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20259451
00 X = -6142665
73
Y = -7390213
06 feet Y = -2321408
95 meter
Z = -4570704
09 Z = -1423070
86
XDOT = 9281
287413 XDOT = 2903
597766
YDOT = -13653
081114 feet/sec YDOT = -4129
406767 meter/sec
ZDOT = -19138
147840 ZDOT = -5819
383036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18107848
11 X = -5519272
10
Y = -11666279
67 feet Y = -3555882
04 meter
Z = -4685690
45 Z = -1428198
45
XDOT = 11316
350820 XDOT = 3449
223730
YDOT = -9928
433234 feet/sec YDOT = -3026
186450 meter/sec
ZDOT = -19085
145563 ZDOT = -5817
152368
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 08100
44561166
00020000 00000-0 20000-3 0 9056
2 25544 51
6410 10
7411 0001255 340
5042 19
6075 15
77303232 17687
Satellite: ISS
Catalog Number: 25544
Epoch time: 08100
44561166 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 10
7411 deg
Eccentricity:
0001255
Arg of perigee: 340
5042 deg
Mean anomaly: 19
6075 deg
Mean motion: 15
77303232 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1768
Checksum: 245
Coasting Arc #7 (Orbit 1783)
---------------------------------------
Vector Time (GMT): 2008/101/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3426149
58 A = 6713178
39 meter
Y = 3393511
68 meter E =
0008323
Z = 4666738
99 I = 51
65831
XDOT = -6608
162877 Wp = 54
36373
YDOT = -2820
986011 meter/sec RA = 5
21882 deg
ZDOT = -2791
906257 TA = 63
18093
MA = 63
09584
Ha = 184
928 n
mi
Hp = 178
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11240648
22 X = -3486512
07
Y = 11133568
49 feet Y = 3354860
84 meter
Z = 15310823
44 Z = 4649948
12
XDOT = -21680
324399 XDOT = -6562
564351
YDOT = -9255
203449 feet/sec YDOT = -2894
627204 meter/sec
ZDOT = -9159
797430 ZDOT = -2823
898318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13356102
00 X = -4070939
89
Y = 8595413
26 feet Y = 2619881
96 meter
Z = 15246745
38 Z = 4647207
99
XDOT = -18665
124503 XDOT = -5689
129948
YDOT = -12488
936683 feet/sec YDOT = -3806
627901 meter/sec
ZDOT = -9282
788821 ZDOT = -2829
394033
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 08101
45929349
00020000 00000-0 20000-3 0 9060
2 25544 51
6409 5
5102 0001234 342
0372 18
0749 15
77365014 17849
Satellite: ISS
Catalog Number: 25544
Epoch time: 08101
45929349 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 5
5102 deg
Eccentricity:
0001234
Arg of perigee: 342
0372 deg
Mean anomaly: 18
0749 deg
Mean motion: 15
77365014 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1784
Checksum: 271
Coasting Arc #8 (Orbit 1799)
---------------------------------------
Vector Time (GMT): 2008/102/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5144797
13 A = 6717369
76 meter
Y = 2680338
56 meter E =
0012198
Z = 3375138
21 I = 51
64407
XDOT = -4956
106322 Wp = 84
53609
YDOT = 3659
238160 meter/sec RA =
10532 deg
ZDOT = 4635
617139 TA = 315
35248
MA = 315
45064
Ha = 184
680 n
mi
Hp = 178
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16879255
67 X = 5098046
94
Y = 8793761
69 feet Y = 2737609
10 meter
Z = 11073288
10 Z = 3400018
25
XDOT = -16260
191345 XDOT = -5019
175187
YDOT = 12005
374540 feet/sec YDOT = 3603
463330 meter/sec
ZDOT = 15208
717648 ZDOT = 4611
387265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14879437
05 X = 4535252
41
Y = 11777660
07 feet Y = 3589830
79 meter
Z = 11168988
41 Z = 3404307
67
XDOT = -17440
847313 XDOT = -5315
970261
YDOT = 7658
665218 feet/sec YDOT = 2334
361159 meter/sec
ZDOT = 15116
124737 ZDOT = 4607
394820
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 08102
47293199
00020000 00000-0 20000-3 0 9071
2 25544 51
6409
2780 0001243 342
9791 17
1332 15
77432123 18000
Satellite: ISS
Catalog Number: 25544
Epoch time: 08102
47293199 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node:
2780 deg
Eccentricity:
0001243
Arg of perigee: 342
9791 deg
Mean anomaly: 17
1332 deg
Mean motion: 15
77432123 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1800
Checksum: 263
Coasting Arc #9 (Orbit 1814)
---------------------------------------
Vector Time (GMT): 2008/103/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5091614
46 A = 6717843
69 meter
Y = -2998038
45 meter E =
0004581
Z = -3197511
26 I = 51
61706
XDOT = 4993
603788 Wp = 62
98899
YDOT = 3370
119543 meter/sec RA = 354
89155 deg
ZDOT = 4799
068960 TA = 259
62712
MA = 259
67876
Ha = 184
670 n
mi
Hp = 178
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16704771
86 X = 5140293
47
Y = -9836084
16 feet Y = -2940828
84 meter
Z = -10490522
50 Z = -3172658
09
XDOT = 16383
214528 XDOT = 4932
234496
YDOT = 11056
822649 feet/sec YDOT = 3425
617610 meter/sec
ZDOT = 15744
976903 ZDOT = 4823
178856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18190157
90 X = 5544360
13
Y = -6848455
52 feet Y = -2087409
24 meter
Z = -10395471
57 Z = -3168539
74
XDOT = 13681
382868 XDOT = 4170
085498
YDOT = 12335
071978 feet/sec YDOT = 3759
729939 meter/sec
ZDOT = 15837
793724 ZDOT = 4827
359527
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 08103
42317911
00020000 00000-0 20000-3 0 9087
2 25544 51
6412 355
3728 0001280 341
9561 18
1558 15
77501226 18153
Satellite: ISS
Catalog Number: 25544
Epoch time: 08103
42317911 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 355
3728 deg
Eccentricity:
0001280
Arg of perigee: 341
9561 deg
Mean anomaly: 18
1558 deg
Mean motion: 15
77501226 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1815
Checksum: 272
Coasting Arc #10 (Orbit 1830)
---------------------------------------
Vector Time (GMT): 2008/104/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3400335
72 A = 6711892
11 meter
Y = -3253852
78 meter E =
0012112
Z = -4796753
74 I = 51
56965
XDOT = 6551
972308 Wp = 65
75159
YDOT = -3185
123853 meter/sec RA = 349
77055 deg
ZDOT = -2483
985976 TA = 179
91991
MA = 179
91971
Ha = 184
546 n
mi
Hp = 178
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11155957
08 X = -3340396
27
Y = -10675370
03 feet Y = -3291542
11 meter
Z = -15737381
03 Z = -4813126
91
XDOT = 21495
972140 XDOT = 6599
168595
YDOT = -10449
881407 feet/sec YDOT = -3111
592049 meter/sec
ZDOT = -8149
560290 ZDOT = -2452
042044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9306124
51 X = -2836506
75
Y = -12240260
88 feet Y = -3730831
52 meter
Z = -15800510
29 Z = -4815995
54
XDOT = 21992
610557 XDOT = 6703
347698
YDOT = -6358
613311 feet/sec YDOT = -1938
105337 meter/sec
ZDOT = -8027
324932 ZDOT = -2446
728639
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 08104
43673480
00020000 00000-0 20000-3 0 9096
2 25544 51
6419 350
1403 0001315 346
5500 13
5629 15
77582580 18314
Satellite: ISS
Catalog Number: 25544
Epoch time: 08104
43673480 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 350
1403 deg
Eccentricity:
0001315
Arg of perigee: 346
5500 deg
Mean anomaly: 13
5629 deg
Mean motion: 15
77582580 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1831
Checksum: 272
Coasting Arc #11 (Orbit 1846)
---------------------------------------
Vector Time (GMT): 2008/105/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6141404
62 A = 6721500
86 meter
Y = 2523856
27 meter E =
0012788
Z = 1007522
97 I = 51
57365
XDOT = -2680
131101 Wp = 120
56394
YDOT = -4136
766053 meter/sec RA = 344
57355 deg
ZDOT = -5925
140443 TA = 48
39569
MA = 48
28619
Ha = 184
485 n
mi
Hp = 178
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20148965
28 X = -6174064
67
Y = 8280368
35 feet Y = 2454996
98 meter
Z = 3305521
55 Z = 977608
82
XDOT = -8793
081040 XDOT = -2604
890844
YDOT = -13572
067103 feet/sec YDOT = -4166
316220 meter/sec
ZDOT = -19439
437149 ZDOT = -5937
977620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21104547
20 X = -6432665
99
Y = 5466929
35 feet Y = 1666320
07 meter
Z = 3191010
13 Z = 972619
89
XDOT = -6361
723018 XDOT = -1939
053176
YDOT = -13085
793190 feet/sec YDOT = -3988
549764 meter/sec
ZDOT = -19489
090585 ZDOT = -5940
274810
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 08105
45024857
00020000 00000-0 20000-3 0 9109
2 25544 51
6419 344
9076 0001263 344
5398 15
5728 15
77615028 18479
Satellite: ISS
Catalog Number: 25544
Epoch time: 08105
45024857 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 344
9076 deg
Eccentricity:
0001263
Arg of perigee: 344
5398 deg
Mean anomaly: 15
5728 deg
Mean motion: 15
77615028 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1847
Checksum: 300
Coasting Arc #12 (Orbit 1862)
---------------------------------------
Vector Time (GMT): 2008/106/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1212886
09 A = 6709496
14 meter
Y = 4001010
54 meter E =
0002715
Z = 5246104
93 I = 51
50644
XDOT = -7278
808738 Wp = 44
90277
YDOT = 2527
867788 meter/sec RA = 339
41062 deg
ZDOT = -243
098998 TA = 47
41775
MA = 47
39485
Ha = 184
225 n
mi
Hp = 178
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3979285
08 X = 1142571
48
Y = 13126675
01 feet Y = 4014180
77 meter
Z = 17211630
34 Z = 5251826
16
XDOT = -23880
606097 XDOT = -7305
353847
YDOT = 8293
529489 feet/sec YDOT = 2446
323557 meter/sec
ZDOT = -797
568891 ZDOT = -278
523894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2296631
03 X = 700013
14
Y = 13494448
45 feet Y = 4113107
89 meter
Z = 17233974
36 Z = 5252915
39
XDOT = -23706
996430 XDOT = -7225
892512
YDOT = 5234
783955 feet/sec YDOT = 1595
562149 meter/sec
ZDOT = -933
216703 ZDOT = -284
444451
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 08106
46371760
00020000 00000-0 20000-3 0 9110
2 25544 51
6419 339
6749 0001418 340
0453 20
0656 15
77735104 18639
Satellite: ISS
Catalog Number: 25544
Epoch time: 08106
46371760 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 339
6749 deg
Eccentricity:
0001418
Arg of perigee: 340
0453 deg
Mean anomaly: 20
0656 deg
Mean motion: 15
77735104 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1863
Checksum: 281
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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