Date:
October 13th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 ET - UTC (sec) : 66 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 2420)
---------------------------------------
Vector Time (GMT): 2009/284/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3062884
84 A = 6729359
75 meter
Y = 5858029
73 meter E =
0004500
Z = -1264615
79 I = 51
97491
XDOT = -3756
626912 Wp = 94
44680
YDOT = 3231
356748 meter/sec RA = 71
00080 deg
ZDOT = 5887
485811 TA = 251
75349
MA = 251
80248
Ha = 190
237 n
mi
Hp = 182
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10048834
79 X = 3003295
04
Y = 19219257
64 feet Y = 5891947
53 meter
Z = -4149001
94 Z = -1249880
86
XDOT = -12324
891443 XDOT = -3821
081981
YDOT = 10601
564135 feet/sec YDOT = 3188
987536 meter/sec
ZDOT = 19315
898331 ZDOT = 5869
079345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21455469
05 X = 6539626
97
Y = 3240802
70 feet Y = 987796
66 meter
Z = -4090624
38 Z = -1246822
31
XDOT = 1432
167206 XDOT = 436
524564
YDOT = 14734
504744 feet/sec YDOT = 4491
077046 meter/sec
ZDOT = 19243
455148 ZDOT = 5865
405129
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 09284
09882633
00020000 00000-0 20000-3 0 9001
2 25544 51
6403 71
6811 0007679 187
9432 172
1611 15
74749400 24217
Satellite: ISS
Catalog Number: 25544
Epoch time: 09284
09882633 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 71
6811 deg
Eccentricity:
0007679
Arg of perigee: 187
9432 deg
Mean anomaly: 172
1611 deg
Mean motion: 15
74749400 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2421
Checksum: 290
Coasting Arc #2 (Orbit 2436)
---------------------------------------
Vector Time (GMT): 2009/285/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3211691
60 A = 6718249
01 meter
Y = -2801889
71 meter E =
0013806
Z = -5203229
04 I = 51
92773
XDOT = 3892
255605 Wp = 112
53891
YDOT = 6540
234089 meter/sec RA = 65
90234 deg
ZDOT = -1126
891532 TA = 146
78189
MA = 146
69514
Ha = 190
087 n
mi
Hp = 182
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10537045
95 X = 3268060
68
Y = -9192551
54 feet Y = -2765659
60 meter
Z = -17070961
41 Z = -5187489
54
XDOT = 12769
867470 XDOT = 3824
306572
YDOT = 21457
460922 feet/sec YDOT = 6583
379640 meter/sec
ZDOT = -3697
150695 ZDOT = -1108
147966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1365251
28 X = -416128
59
Y = -13992128
78 feet Y = -4264800
85 meter
Z = -17009011
89 Z = -5184346
83
XDOT = 23884
631094 XDOT = 7280
035558
YDOT = 2043
449912 feet/sec YDOT = 622
843533 meter/sec
ZDOT = -3622
933511 ZDOT = -1104
270134
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 09285
11416059
00020000 00000-0 20000-3 0 9011
2 25544 51
6412 66
4605 0007615 191
7092 168
3896 15
74790336 24378
Satellite: ISS
Catalog Number: 25544
Epoch time: 09285
11416059 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 66
4605 deg
Eccentricity:
0007615
Arg of perigee: 191
7092 deg
Mean anomaly: 168
3896 deg
Mean motion: 15
74790336 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2437
Checksum: 301
Coasting Arc #3 (Orbit 2452)
---------------------------------------
Vector Time (GMT): 2009/286/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3732617
67 A = 6729721
49 meter
Y = -5541848
94 meter E =
0017728
Z = 703665
56 I = 51
95342
XDOT = 3605
555826 Wp = 151
01757
YDOT = -3198
390541 meter/sec RA = 60
76598 deg
ZDOT = -6016
322091 TA = 21
33980
MA = 21
26597
Ha = 189
936 n
mi
Hp = 182
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12246120
97 X = -3673788
64
Y = -18181919
10 feet Y = -5583260
31 meter
Z = 2308614
04 Z = 685675
51
XDOT = 11829
251399 XDOT = 3670
279234
YDOT = -10493
407288 feet/sec YDOT = -3157
709474 meter/sec
ZDOT = -19738
589538 ZDOT = -5998
648814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21928548
97 X = -6683821
73
Y = -109901
16 feet Y = -33497
88 meter
Z = 2237413
98 Z = 681963
78
XDOT = -1952
173138 XDOT = -595
022372
YDOT = -14180
814442 feet/sec YDOT = -4322
312242 meter/sec
ZDOT = -19669
028113 ZDOT = -5995
119769
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 09286
12947791
00020000 00000-0 20000-3 0 9026
2 25544 51
6416 61
2404 0007606 195
6244 164
4686 15
74795457 24535
Satellite: ISS
Catalog Number: 25544
Epoch time: 09286
12947791 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 61
2404 deg
Eccentricity:
0007606
Arg of perigee: 195
6244 deg
Mean anomaly: 164
4686 deg
Mean motion: 15
74795457 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2453
Checksum: 313
Coasting Arc #4 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2009/287/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3105239
40 A = 6717680
54 meter
Y = 2779556
40 meter E =
0008008
Z = 5269321
36 I = 51
89774
XDOT = -4645
631967 Wp = 180
93568
YDOT = -6124
511314 meter/sec RA = 55
65526 deg
ZDOT = 485
143808 TA = 264
42766
MA = 264
51900
Ha = 189
662 n
mi
Hp = 182
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10187793
29 X = -3161687
74
Y = 9119279
54 feet Y = 2744516
53 meter
Z = 17287799
73 Z = 5254098
66
XDOT = -15241
574695 XDOT = -4579
158106
YDOT = -20093
541056 feet/sec YDOT = -6176
089800 meter/sec
ZDOT = 1591
679161 ZDOT = 462
737013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1975495
16 X = 602130
92
Y = 13605802
00 feet Y = 4147048
45 meter
Z = 17227883
85 Z = 5251059
00
XDOT = -24174
845090 XDOT = -7368
492783
YDOT = 1574
268746 feet/sec YDOT = 479
837114 meter/sec
ZDOT = 1503
035777 ZDOT = 458
125305
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 09287
14477551
00020000 00000-0 20000-3 0 9032
2 25544 51
6414 56
0201 0007560 200
9157 159
1698 15
74873472 24697
Satellite: ISS
Catalog Number: 25544
Epoch time: 09287
14477551 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 56
0201 deg
Eccentricity:
0007560
Arg of perigee: 200
9157 deg
Mean anomaly: 159
1698 deg
Mean motion: 15
74873472 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2469
Checksum: 301
Coasting Arc #5 (Orbit 2483)
---------------------------------------
Vector Time (GMT): 2009/288/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4351832
19 A = 6729732
97 meter
Y = 5130211
33 meter E =
0005727
Z = -124911
68 I = 51
92072
XDOT = -3550
901002 Wp = 70
49016
YDOT = 3154
139305 meter/sec RA = 50
52645 deg
ZDOT = 6057
513800 TA = 288
15844
MA = 288
22078
Ha = 189
448 n
mi
Hp = 183
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14277664
66 X = 4294748
64
Y = 16831402
01 feet Y = 5178556
91 meter
Z = -409815
23 Z = -103909
29
XDOT = -11649
937670 XDOT = -3615
333932
YDOT = 10348
226067 feet/sec YDOT = 3114
071287 meter/sec
ZDOT = 19873
732939 ZDOT = 6040
106514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21857726
79 X = 6662235
13
Y = -3073883
20 feet Y = -936919
60 meter
Z = -326759
69 Z = -99596
35
XDOT = 2234
345172 XDOT = 681
028408
YDOT = 13881
291439 feet/sec YDOT = 4231
017631 meter/sec
ZDOT = 19805
217194 ZDOT = 6036
630201
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 09288
09660394
00020000 00000-0 20000-3 0 9047
2 25544 51
6419 51
1253 0007387 204
3164 155
7652 15
74854852 24848
Satellite: ISS
Catalog Number: 25544
Epoch time: 09288
09660394 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 51
1253 deg
Eccentricity:
0007387
Arg of perigee: 204
3164 deg
Mean anomaly: 155
7652 deg
Mean motion: 15
74854852 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2484
Checksum: 307
Coasting Arc #6 (Orbit 2499)
---------------------------------------
Vector Time (GMT): 2009/289/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3132083
39 A = 6717544
81 meter
Y = -2735061
77 meter E =
0013503
Z = -5286001
28 I = 51
86105
XDOT = 5274
177578 Wp = 120
85438
YDOT = 5597
359943 meter/sec RA = 45
40075 deg
ZDOT = 222
556566 TA = 151
29051
MA = 151
21611
Ha = 189
261 n
mi
Hp = 183
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10275864
14 X = 3188113
47
Y = -8973299
76 feet Y = -2699724
14 meter
Z = -17342523
90 Z = -5270648
99
XDOT = 17303
732211 XDOT = 5210
113775
YDOT = 18364
041807 feet/sec YDOT = 5655
980726 meter/sec
ZDOT = 730
172459 ZDOT = 248
022904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2271678
91 X = -692407
73
Y = -13529423
96 feet Y = -4123768
42 meter
Z = -17282094
49 Z = -5267582
40
XDOT = 23693
891389 XDOT = 7221
898095
YDOT = -5066
392297 feet/sec YDOT = -1544
236372 meter/sec
ZDOT = 830
844882 ZDOT = 253
241520
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 09289
11186878
00020000 00000-0 20000-3 0 9052
2 25544 51
6429 45
9044 0007337 208
2526 151
8229 15
74904771 25000
Satellite: ISS
Catalog Number: 25544
Epoch time: 09289
11186878 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 45
9044 deg
Eccentricity:
0007337
Arg of perigee: 208
2526 deg
Mean anomaly: 151
8229 deg
Mean motion: 15
74904771 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2500
Checksum: 304
Coasting Arc #7 (Orbit 2515)
---------------------------------------
Vector Time (GMT): 2009/290/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4840720
55 A = 6729531
80 meter
Y = -4632464
41 meter E =
0015022
Z = -515124
90 I = 51
87987
XDOT = 3631
727893 Wp = 167
07671
YDOT = -3129
257080 meter/sec RA = 40
28204 deg
ZDOT = -6034
804649 TA = 18
51494
MA = 18
46033
Ha = 189
123 n
mi
Hp = 183
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15881629
11 X = -4786057
31
Y = -15198374
05 feet Y = -4686290
60 meter
Z = -1690042
33 Z = -538508
56
XDOT = 11915
117758 XDOT = 3695
766583
YDOT = -10266
591471 feet/sec YDOT = -3088
287370 meter/sec
ZDOT = -19799
227850 ZDOT = -6017
005484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21133532
72 X = -6441500
77
Y = 6022426
96 feet Y = 1835635
74 meter
Z = -1782450
08 Z = -543290
79
XDOT = -2346
023020 XDOT = -715
067816
YDOT = -14027
642922 feet/sec YDOT = -4275
625563 meter/sec
ZDOT = -19729
164108 ZDOT = -6013
449220
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 09290
12711718
00020000 00000-0 20000-3 0 9063
2 25544 51
6434 40
6839 0007438 212
2719 147
7990 15
74887123 25168
Satellite: ISS
Catalog Number: 25544
Epoch time: 09290
12711718 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 40
6839 deg
Eccentricity:
0007438
Arg of perigee: 212
2719 deg
Mean anomaly: 147
7990 deg
Mean motion: 15
74887123 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2516
Checksum: 303
Coasting Arc #8 (Orbit 2531)
---------------------------------------
Vector Time (GMT): 2009/291/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3223830
37 A = 6717608
00 meter
Y = 2746350
70 meter E =
0004116
Z = 5215178
45 I = 51
81722
XDOT = -5788
261258 Wp = 200
47767
YDOT = -4991
361863 meter/sec RA = 35
14107 deg
ZDOT = -953
605242 TA = 258
56136
MA = 258
60760
Ha = 188
788 n
mi
Hp = 183
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10576871
30 X = -3279636
06
Y = 9010336
96 feet Y = 2709988
22 meter
Z = 17110165
51 Z = 5199380
91
XDOT = -18990
358458 XDOT = -5727
384206
YDOT = -16375
859130 feet/sec YDOT = -5055
749288 meter/sec
ZDOT = -3128
626121 ZDOT = -981
577244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2621132
41 X = 798921
16
Y = 13722618
88 feet Y = 4182654
23 meter
Z = 17047977
54 Z = 5196223
56
XDOT = -22572
072092 XDOT = -6879
967574
YDOT = 8319
132780 feet/sec YDOT = 2535
671671 meter/sec
ZDOT = -3239
131496 ZDOT = -987
287280
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 09291
14234506
00020000 00000-0 20000-3 0 9072
2 25544 51
6437 35
4633 0007295 217
9323 142
1328 15
74986039 25327
Satellite: ISS
Catalog Number: 25544
Epoch time: 09291
14234506 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 35
4633 deg
Eccentricity:
0007295
Arg of perigee: 217
9323 deg
Mean anomaly: 142
1328 deg
Mean motion: 15
74986039 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2532
Checksum: 291
Coasting Arc #9 (Orbit 2547)
---------------------------------------
Vector Time (GMT): 2009/292/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5224093
94 A = 6728791
58 meter
Y = 4074735
24 meter E =
0007285
Z = 1161818
78 I = 51
82998
XDOT = -3791
396168 Wp = 73
51880
YDOT = 3169
260025 meter/sec RA = 30
03056 deg
ZDOT = 5904
347093 TA = 299
17272
MA = 299
24560
Ha = 188
547 n
mi
Hp = 183
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17139415
80 X = 5172497
19
Y = 13368553
93 feet Y = 4132865
69 meter
Z = 3811741
41 Z = 1187072
72
XDOT = -12438
963807 XDOT = -3855
236730
YDOT = 10397
834728 feet/sec YDOT = 3126
505675 meter/sec
ZDOT = 19371
217498 ZDOT = 5885
772730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19895398
27 X = 6064117
39
Y = -8710947
94 feet Y = -2655096
93 meter
Z = 3911482
40 Z = 1192219
83
XDOT = 2551
667818 XDOT = 777
748351
YDOT = 14534
018908 feet/sec YDOT = 4429
968963 meter/sec
ZDOT = 19298
092208 ZDOT = 5882
058505
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 09292
15755830
00020000 00000-0 20000-3 0 9083
2 25544 51
6440 30
2423 0007171 222
1266 137
9347 15
74974789 25487
Satellite: ISS
Catalog Number: 25544
Epoch time: 09292
15755830 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 30
2423 deg
Eccentricity:
0007171
Arg of perigee: 222
1266 deg
Mean anomaly: 137
9347 deg
Mean motion: 15
74974789 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2548
Checksum: 302
Coasting Arc #10 (Orbit 2562)
---------------------------------------
Vector Time (GMT): 2009/293/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3417324
78 A = 6718229
33 meter
Y = -2812428
83 meter E =
0011263
Z = -5063207
66 I = 51
76811
XDOT = 6122
509505 Wp = 135
11299
YDOT = 4332
364463 meter/sec RA = 24
87323 deg
ZDOT = 1720
303792 TA = 151
45302
MA = 151
39130
Ha = 188
334 n
mi
Hp = 183
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11211695
48 X = 3473116
76
Y = -9227128
71 feet Y = -2773902
42 meter
Z = -16611573
68 Z = -5046470
22
XDOT = 20086
973440 XDOT = 6065
252029
YDOT = 14213
794171 feet/sec YDOT = 4400
509857 meter/sec
ZDOT = 5644
041311 ZDOT = 1749
908695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2993525
29 X = -912426
51
Y = -14285162
31 feet Y = -4354117
47 meter
Z = -16545674
48 Z = -5043121
58
XDOT = 20802
049498 XDOT = 6340
464687
YDOT = -11052
743542 feet/sec YDOT = -3368
876231 meter/sec
ZDOT = 5760
941415 ZDOT = 1755
934943
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 09293
10930313
00020000 00000-0 20000-3 0 9091
2 25544 51
6441 25
3477 0007182 226
3755 133
6813 15
75016191 25636
Satellite: ISS
Catalog Number: 25544
Epoch time: 09293
10930313 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 25
3477 deg
Eccentricity:
0007182
Arg of perigee: 226
3755 deg
Mean anomaly: 133
6813 deg
Mean motion: 15
75016191 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2563
Checksum: 279
Coasting Arc #11 (Orbit 2578)
---------------------------------------
Vector Time (GMT): 2009/294/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5436347
53 A = 6727819
35 meter
Y = -3496352
71 meter E =
0010336
Z = -1842450
34 I = 51
77260
XDOT = 4039
969997 Wp = 185
98100
YDOT = -3296
094971 meter/sec RA = 19
77145 deg
ZDOT = -5672
721094 TA = 14
44275
MA = 14
41323
Ha = 188
149 n
mi
Hp = 184
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17835785
85 X = -5387896
11
Y = -11470973
47 feet Y = -3556874
24 meter
Z = -6044784
59 Z = -1868743
19
XDOT = 13254
494741 XDOT = 4104
085074
YDOT = -10813
959878 feet/sec YDOT = -3250
559140 meter/sec
ZDOT = -18611
289679 ZDOT = -5652
938636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18187984
27 X = -5543697
61
Y = 10845736
01 feet Y = 3305780
34 meter
Z = -6148589
14 Z = -1874089
97
XDOT = -2956
153326 XDOT = -901
035534
YDOT = -15450
970698 feet/sec YDOT = -4709
455869 meter/sec
ZDOT = -18533
395329 ZDOT = -5648
978896
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 09294
12448154
00020000 00000-0 20000-3 0 9103
2 25544 51
6440 20
1273 0007311 230
2484 129
8036 15
74994918 25791
Satellite: ISS
Catalog Number: 25544
Epoch time: 09294
12448154 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 20
1273 deg
Eccentricity:
0007311
Arg of perigee: 230
2484 deg
Mean anomaly: 129
8036 deg
Mean motion: 15
74994918 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2579
Checksum: 286
Coasting Arc #12 (Orbit 2594)
---------------------------------------
Vector Time (GMT): 2009/295/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3633981
05 A = 6719089
30 meter
Y = 2973337
73 meter E =
0000552
Z = 4805730
60 I = 51
71523
XDOT = -6296
814621 Wp = 138
06283
YDOT = -3671
244624 meter/sec RA = 14
59838 deg
ZDOT = -2490
319375 TA = 336
25957
MA = 336
26212
Ha = 187
836 n
mi
Hp = 184
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11922510
00 X = -3690305
29
Y = 9755045
05 feet Y = 2932385
41 meter
Z = 15766832
67 Z = 4787939
51
XDOT = -20658
840620 XDOT = -6243
196304
YDOT = -12044
765828 feet/sec YDOT = -3741
359477 meter/sec
ZDOT = -8170
339158 ZDOT = -2520
779885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3657124
14 X = 1114691
44
Y = 15037846
88 feet Y = 4583535
73 meter
Z = 15696775
64 Z = 4784377
21
XDOT = -18626
363126 XDOT = -5677
315481
YDOT = 13182
868493 feet/sec YDOT = 4018
138317 meter/sec
ZDOT = -8290
581979 ZDOT = -2526
969387
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 09295
13964007
00020000 00000-0 20000-3 0 9116
2 25544 51
6439 14
9058 0007163 235
8471 124
2014 15
75095141 25957
Satellite: ISS
Catalog Number: 25544
Epoch time: 09295
13964007 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 14
9058 deg
Eccentricity:
0007163
Arg of perigee: 235
8471 deg
Mean anomaly: 124
2014 deg
Mean motion: 15
75095141 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2595
Checksum: 285
Coasting Arc #13 (Orbit 2610)
---------------------------------------
Vector Time (GMT): 2009/296/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5509875
20 A = 6726280
69 meter
Y = 2928176
71 meter E =
0007247
Z = 2506122
14 I = 51
70929
XDOT = -4303
767635 Wp = 91
88225
YDOT = 3536
006916 meter/sec RA = 9
50068 deg
ZDOT = 5317
214388 TA = 296
46803
MA = 296
54235
Ha = 187
577 n
mi
Hp = 184
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18077018
36 X = 5464547
76
Y = 9606878
99 feet Y = 2989537
89 meter
Z = 8222185
51 Z = 2532779
65
XDOT = -14119
972556 XDOT = -4368
818626
YDOT = 11601
072560 feet/sec YDOT = 3487
515812 meter/sec
ZDOT = 17444
929096 ZDOT = 5296
148307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16201357
72 X = 4938173
83
Y = -12443687
91 feet Y = -3792836
07 meter
Z = 8327405
99 Z = 2538193
35
XDOT = 3776
172292 XDOT = 1150
977315
YDOT = 16564
283320 feet/sec YDOT = 5048
793556 meter/sec
ZDOT = 17361
972544 ZDOT = 5291
929231
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 09296
15478356
00020000 00000-0 20000-3 0 9127
2 25544 51
6429 9
6836 0007149 240
0594 119
9861 15
75089663 26111
Satellite: ISS
Catalog Number: 25544
Epoch time: 09296
15478356 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 9
6836 deg
Eccentricity:
0007149
Arg of perigee: 240
0594 deg
Mean anomaly: 119
9861 deg
Mean motion: 15
75089663 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2611
Checksum: 320
Coasting Arc #14 (Orbit 2625)
---------------------------------------
Vector Time (GMT): 2009/297/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3876506
69 A = 6720493
85 meter
Y = -3231862
49 meter E =
0006957
Z = -4443349
06 I = 51
65922
XDOT = 6274
694913 Wp = 159
04107
YDOT = 3051
170150 meter/sec RA = 4
31364 deg
ZDOT = 3250
145638 TA = 143
55494
MA = 143
50756
Ha = 187
374 n
mi
Hp = 184
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12718197
80 X = 3933943
20
Y = -10603223
38 feet Y = -3188191
87 meter
Z = -14577916
87 Z = -4424377
20
XDOT = 20586
269399 XDOT = 6224
320940
YDOT = 10010
400753 feet/sec YDOT = 3121
055765 meter/sec
ZDOT = 10663
207474 ZDOT = 3280
506354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4636716
31 X = -1413271
13
Y = -15964160
34 feet Y = -4865876
07 meter
Z = -14503206
81 Z = -4420577
44
XDOT = 16183
359772 XDOT = 4932
688058
YDOT = -14511
043843 feet/sec YDOT = -4422
966163 meter/sec
ZDOT = 10783
036174 ZDOT = 3286
669426
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 09297
10646407
00020000 00000-0 20000-3 0 9138
2 25544 51
6421 4
7876 0007136 243
5305 116
5127 15
75118379 26268
Satellite: ISS
Catalog Number: 25544
Epoch time: 09297
10646407 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 4
7876 deg
Eccentricity:
0007136
Arg of perigee: 243
5305 deg
Mean anomaly: 116
5127 deg
Mean motion: 15
75118379 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2626
Checksum: 288
Coasting Arc #15 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2009/298/02:18:49
834
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5411917
30 A = 6724528
73 meter
Y = -2428616
43 meter E =
0004028
Z = -3161651
93 I = 51
64248
XDOT = 4567
178894 Wp = 210
72415
YDOT = -3887
054073 meter/sec RA = 359
21983 deg
ZDOT = -4832
682046 TA = 6
13326
MA = 6
12833
Ha = 187
023 n
mi
Hp = 184
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17755634
19 X = -5368998
89
Y = -7967901
68 feet Y = -2488895
68 meter
Z = -10372873
78 Z = -3187839
21
XDOT = 14984
182724 XDOT = 4633
781827
YDOT = -12752
802076 feet/sec YDOT = -3835
608740 meter/sec
ZDOT = -15855
256058 ZDOT = -4810
332603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14121487
12 X = -4304229
27
Y = 13310853
86 feet Y = 4057148
26 meter
Z = -10476224
70 Z = -3193153
29
XDOT = -5058
511355 XDOT = -1541
834261
YDOT = -17774
288279 feet/sec YDOT = -5417
603067 meter/sec
ZDOT = -15767
247388 ZDOT = -4805
857004
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 09298
12157334
00020000 00000-0 20000-3 0 9148
2 25544 51
6414 359
5665 0007142 247
8096 112
2310 15
75127589 26426
Satellite: ISS
Catalog Number: 25544
Epoch time: 09298
12157334 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 359
5665 deg
Eccentricity:
0007142
Arg of perigee: 247
8096 deg
Mean anomaly: 112
2310 deg
Mean motion: 15
75127589 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2642
Checksum: 296
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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