Date:
November 6th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22873 31 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2805)
---------------------------------------
Vector Time (GMT): 2009/308/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3334850
02 A = 6726534
26 meter
Y = -5779937
98 meter E =
0010176
Z = -792525
18 I = 51
38887
XDOT = 4546
559023 Wp = 5
44380
YDOT = 1809
286043 meter/sec RA = 305
42619 deg
ZDOT = 5952
336555 TA = 345
87533
MA = 345
90377
Ha = 185
685 n
mi
Hp = 183
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10941108
98 X = 3403084
50
Y = -18963051
12 feet Y = -5742264
15 meter
Z = -2600148
24 Z = -776158
55
XDOT = 14916
532228 XDOT = 4497
073020
YDOT = 5935
977831 feet/sec YDOT = 1859
851294 meter/sec
ZDOT = 19528
663238 ZDOT = 5974
304379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7705197
42 X = 2348544
17
Y = 20500379
41 feet Y = 6248515
65 meter
Z = -2535807
73 Z = -772914
20
XDOT = -12485
514331 XDOT = -3805
584768
YDOT = 7112
347139 feet/sec YDOT = 2167
843408 meter/sec
ZDOT = 19615
338818 ZDOT = 5978
755272
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 09308
52232161
00016717 00000-0 10270-3 0 9009
2 25544 51
6418 306
0381 0005992 289
7971 70
2547 15
75892579 28065
Satellite: ISS
Catalog Number: 25544
Epoch time: 09308
52232161 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 306
0381 deg
Eccentricity:
0005992
Arg of perigee: 289
7971 deg
Mean anomaly: 70
2547 deg
Mean motion: 15
75892579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 328
Coasting Arc #2 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2009/309/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3722207
81 A = 6714709
60 meter
Y = -1949993
57 meter E =
0009952
Z = -5245616
59 I = 51
33228
XDOT = 3760
468921 Wp = 72
77493
YDOT = -6714
062637 meter/sec RA = 300
26476 deg
ZDOT = -169
859428 TA = 195
59015
MA = 195
62082
Ha = 185
902 n
mi
Hp = 182
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12211967
89 X = -3674643
02
Y = -6397616
71 feet Y = -1991351
14 meter
Z = -17210028
18 Z = -5263584
20
XDOT = 12337
496459 XDOT = 3836
092418
YDOT = -22027
764558 feet/sec YDOT = -6671
588012 meter/sec
ZDOT = -557
281587 ZDOT = -151
407372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12536695
23 X = 3821184
70
Y = -5517889
57 feet Y = -1681852
74 meter
Z = -17280940
28 Z = -5267230
60
XDOT = 9196
263837 XDOT = 2803
021218
YDOT = 22439
139853 feet/sec YDOT = 6839
449827 meter/sec
ZDOT = -484
745313 ZDOT = -147
750371
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 09309
53694057
00016717 00000-0 10270-3 0 9018
2 25544 51
6414 300
8123 0006126 295
2336 64
8193 15
75894676 28228
Satellite: ISS
Catalog Number: 25544
Epoch time: 09309
53694057 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 300
8123 deg
Eccentricity:
0006126
Arg of perigee: 295
2336 deg
Mean anomaly: 64
8193 deg
Mean motion: 15
75894676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 320
Coasting Arc #3 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2009/310/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3213951
78 A = 6726430
39 meter
Y = 5882118
59 meter E =
0005625
Z = -519842
19 I = 51
35881
XDOT = -4011
426854 Wp = 159
89806
YDOT = -2718
715967 meter/sec RA = 295
09714 deg
ZDOT = -5986
315098 TA = 25
78328
MA = 25
75525
Ha = 186
064 n
mi
Hp = 182
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10544461
24 X = -3276962
43
Y = 19298289
33 feet Y = 5845826
02 meter
Z = -1705519
01 Z = -535608
51
XDOT = -13160
849257 XDOT = -3951
646464
YDOT = -8919
671809 feet/sec YDOT = -2763
239372 meter/sec
ZDOT = -19640
141397 ZDOT = -6005
658063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8928263
43 X = -2721334
69
Y = -20091801
95 feet Y = -6123981
23 meter
Z = -1767494
09 Z = -538732
20
XDOT = 13545
929490 XDOT = 4128
799309
YDOT = -4291
755765 feet/sec YDOT = -1308
127157 meter/sec
ZDOT = -19716
508450 ZDOT = -6009
591775
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 09310
55152094
00016717 00000-0 10270-3 0 9023
2 25544 51
6417 295
5869 0006163 300
1523 59
9030 15
75976006 28383
Satellite: ISS
Catalog Number: 25544
Epoch time: 09310
55152094 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 295
5869 deg
Eccentricity:
0006163
Arg of perigee: 300
1523 deg
Mean anomaly: 59
9030 deg
Mean motion: 15
75976006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 310
Coasting Arc #4 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2009/311/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3322988
38 A = 6714980
04 meter
Y = 2831219
04 meter E =
0006179
Z = 5104815
59 I = 51
30864
XDOT = -3583
187222 Wp = 345
05277
YDOT = 6679
698403 meter/sec RA = 289
90783 deg
ZDOT = -1366
669944 TA = 118
11839
MA = 118
05593
Ha = 186
076 n
mi
Hp = 182
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10902192
85 X = 3266283
52
Y = 9288776
37 feet Y = 2868061
23 meter
Z = 16748082
63 Z = 5120821
41
XDOT = -11755
863588 XDOT = -3650
975308
YDOT = 21915
021006 feet/sec YDOT = 6639
250166 meter/sec
ZDOT = -4483
825275 ZDOT = -1384
241552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13889622
26 X = -4233556
86
Y = 3177419
66 feet Y = 968477
51 meter
Z = 16811301
11 Z = 5124084
58
XDOT = -10436
603076 XDOT = -3181
076618
YDOT = -21437
801590 feet/sec YDOT = -6534
241925 meter/sec
ZDOT = -4552
890975 ZDOT = -1387
721169
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 09311
56606290
00016717 00000-0 10270-3 0 9038
2 25544 51
6414 290
3617 0006208 303
2589 56
7980 15
76021607 28546
Satellite: ISS
Catalog Number: 25544
Epoch time: 09311
56606290 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 290
3617 deg
Eccentricity:
0006208
Arg of perigee: 303
2589 deg
Mean anomaly: 56
7980 deg
Mean motion: 15
76021607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2854
Checksum: 308
Coasting Arc #5 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2009/312/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3039647
19 A = 6724602
72 meter
Y = -5693698
66 meter E =
0012158
Z = 1860019
84 I = 51
33322
XDOT = 3655
972590 Wp = 41
28406
YDOT = 3793
582228 meter/sec RA = 284
76336 deg
ZDOT = 5626
077389 TA = 339
48844
MA = 339
53722
Ha = 185
990 n
mi
Hp = 182
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9972595
77 X = 3094053
44
Y = -18680113
71 feet Y = -5659403
43 meter
Z = 6102427
30 Z = 1874918
51
XDOT = 11994
660728 XDOT = 3585
949521
YDOT = 12446
135917 feet/sec YDOT = 3834
073655 meter/sec
ZDOT = 18458
259151 ZDOT = 5643
668463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9456875
33 X = 2882455
60
Y = 18927460
04 feet Y = 5769089
82 meter
Z = 6160982
00 Z = 1877867
31
XDOT = -15652
744327 XDOT = -4770
956471
YDOT = 1777
292774 feet/sec YDOT = 541
718837 meter/sec
ZDOT = 18527
771534 ZDOT = 5647
264763
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 09312
58056393
00016717 00000-0 10270-3 0 9045
2 25544 51
6415 285
1363 0006091 305
8102 54
2496 15
76125168 28706
Satellite: ISS
Catalog Number: 25544
Epoch time: 09312
58056393 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 285
1363 deg
Eccentricity:
0006091
Arg of perigee: 305
8102 deg
Mean anomaly: 54
2496 deg
Mean motion: 15
76125168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 305
Coasting Arc #6 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2009/313/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3100973
97 A = 6716815
67 meter
Y = -3789841
84 meter E =
0005377
Z = -4601853
22 I = 51
30055
XDOT = 3398
943800 Wp = 84
99792
YDOT = -6278
677347 meter/sec RA = 279
54899 deg
ZDOT = 2883
748152 TA = 213
66214
MA = 213
69630
Ha = 186
211 n
mi
Hp = 182
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10173799
10 X = -3036009
56
Y = -12433864
30 feet Y = -3824155
40 meter
Z = -15097943
64 Z = -4616760
25
XDOT = 11151
390420 XDOT = 3454
891534
YDOT = -20599
335128 feet/sec YDOT = -6240
355612 meter/sec
ZDOT = 9461
115983 ZDOT = 2900
396163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15958771
30 X = 4864233
49
Y = -1281294
79 feet Y = -390538
65 meter
Z = -15156878
77 Z = -4619816
65
XDOT = 10614
288889 XDOT = 3235
235253
YDOT = 19639
837400 feet/sec YDOT = 5986
222440 meter/sec
ZDOT = 9526
542613 ZDOT = 2903
690189
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 09313
53162554
00016717 00000-0 10270-3 0 9059
2 25544 51
6415 280
2369 0006209 310
9783 49
0843 15
76130513 28855
Satellite: ISS
Catalog Number: 25544
Epoch time: 09313
53162554 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 280
2369 deg
Eccentricity:
0006209
Arg of perigee: 310
9783 deg
Mean anomaly: 49
0843 deg
Mean motion: 15
76130513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 308
Coasting Arc #7 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2009/314/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2926872
42 A = 6721504
82 meter
Y = 5170775
63 meter E =
0003539
Z = -3146607
03 I = 51
31396
XDOT = -3483
317765 Wp = 1
26917
YDOT = -4900
062383 meter/sec RA = 274
42023 deg
ZDOT = -4808
747161 TA = 215
56917
MA = 215
59277
Ha = 186
323 n
mi
Hp = 181
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9602599
80 X = -2969189
52
Y = 16964486
97 feet Y = 5137809
03 meter
Z = -10323513
89 Z = -3160928
75
XDOT = -11428
207891 XDOT = -3404
905151
YDOT = -16076
320153 feet/sec YDOT = -4938
576441 meter/sec
ZDOT = -15776
729530 ZDOT = -4825
478931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8888782
03 X = -2709300
76
Y = -17315541
01 feet Y = -5277776
90 meter
Z = -10379801
23 Z = -3163763
41
XDOT = 18399
766817 XDOT = 5608
248926
YDOT = 58
299549 feet/sec YDOT = 17
769703 meter/sec
ZDOT = -15842
911697 ZDOT = -4828
919485
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 09314
54605096
00016717 00000-0 10270-3 0 9065
2 25544 51
6420 275
0106 0006219 315
0926 44
9734 15
76219780 29014
Satellite: ISS
Catalog Number: 25544
Epoch time: 09314
54605096 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 275
0106 deg
Eccentricity:
0006219
Arg of perigee: 315
0926 deg
Mean anomaly: 44
9734 deg
Mean motion: 15
76219780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 303
Coasting Arc #8 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2009/315/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3022628
64 A = 6719696
65 meter
Y = 4731779
66 meter E =
0009596
Z = 3690266
56 I = 51
30745
XDOT = -3341
319909 Wp = 52
00390
YDOT = 5473
098053 meter/sec RA = 269
19286 deg
ZDOT = -4267
607455 TA = 83
27275
MA = 83
16355
Ha = 186
338 n
mi
Hp = 181
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9916760
64 X = 2951565
42
Y = 15524211
47 feet Y = 4765183
16 meter
Z = 12107173
76 Z = 3704778
12
XDOT = -10962
335658 XDOT = -3381
541053
YDOT = 17956
358443 feet/sec YDOT = 5435
508525 meter/sec
ZDOT = -14001
336796 ZDOT = -4283
937629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18383373
63 X = -5603252
28
Y = -32285
63 feet Y = -9840
66 meter
Z = 12164599
11 Z = 3707769
81
XDOT = -9305
580593 XDOT = -2836
340965
YDOT = -17481
044386 feet/sec YDOT = -5328
222329 meter/sec
ZDOT = -14065
529034 ZDOT = -4287
173250
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 09315
56043632
00016717 00000-0 10270-3 0 9071
2 25544 51
6421 269
7843 0006235 318
4863 41
5827 15
76282569 29176
Satellite: ISS
Catalog Number: 25544
Epoch time: 09315
56043632 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 269
7843 deg
Eccentricity:
0006235
Arg of perigee: 318
4863 deg
Mean anomaly: 41
5827 deg
Mean motion: 15
76282569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 331
Coasting Arc #9 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2009/316/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2957254
80 A = 6717600
32 meter
Y = -4297396
85 meter E =
0005919
Z = 4226417
12 I = 51
30325
XDOT = 3475
068712 Wp = 72
49683
YDOT = 5889
824037 meter/sec RA = 264
06716 deg
ZDOT = 3554
882608 TA = 341
26635
MA = 341
28813
Ha = 186
201 n
mi
Hp = 181
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9702279
53 X = 2984557
59
Y = -14099071
02 feet Y = -4264174
39 meter
Z = 13866197
90 Z = 4240850
15
XDOT = 11401
144067 XDOT = 3391
680008
YDOT = 19323
569676 feet/sec YDOT = 5928
218079 meter/sec
ZDOT = 11663
000681 ZDOT = 3571
562294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6994601
56 X = 2131954
56
Y = 15569728
21 feet Y = 4745653
16 meter
Z = 13922951
86 Z = 4243715
73
XDOT = -21262
274933 XDOT = -6480
741400
YDOT = -943
329647 feet/sec YDOT = -287
526877 meter/sec
ZDOT = 11729
029181 ZDOT = 3575
008094
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 09316
57478045
00016717 00000-0 10270-3 0 9084
2 25544 51
6425 264
5575 0006131 320
9522 39
1199 15
76361405 29330
Satellite: ISS
Catalog Number: 25544
Epoch time: 09316
57478045 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 264
5575 deg
Eccentricity:
0006131
Arg of perigee: 320
9522 deg
Mean anomaly: 39
1199 deg
Mean motion: 15
76361405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 318
Coasting Arc #10 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2009/317/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3055287
81 A = 6722805
76 meter
Y = -5470293
63 meter E =
0008813
Z = -2422559
79 I = 51
32517
XDOT = 3503
022777 Wp = 3
28359
YDOT = -4315
782470 meter/sec RA = 258
84335 deg
ZDOT = 5336
996863 TA = 329
20540
MA = 329
25707
Ha = 186
389 n
mi
Hp = 181
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10023910
13 X = -2982122
26
Y = -17947157
58 feet Y = -5504050
56 meter
Z = -7948030
80 Z = -2437225
10
XDOT = 11492
856881 XDOT = 3525
095355
YDOT = -14159
391306 feet/sec YDOT = -4276
486216 meter/sec
ZDOT = 17509
832228 ZDOT = 5354
068622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20527680
55 X = 6256837
03
Y = 516840
48 feet Y = 157532
98 meter
Z = -8006100
19 Z = -2440259
34
XDOT = 6452
668565 XDOT = 1966
773379
YDOT = 15505
029707 feet/sec YDOT = 4725
933055 meter/sec
ZDOT = 17576
993285 ZDOT = 5357
467553
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 09317
52569312
00016717 00000-0 10270-3 0 9099
2 25544 51
6423 259
6569 0006240 325
4144 34
6614 15
76381387 29486
Satellite: ISS
Catalog Number: 25544
Epoch time: 09317
52569312 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 259
6569 deg
Eccentricity:
0006240
Arg of perigee: 325
4144 deg
Mean anomaly: 34
6614 deg
Mean motion: 15
76381387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 329
Coasting Arc #11 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2009/318/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3228484
91 A = 6714293
97 meter
Y = 3162308
95 meter E =
0012864
Z = -4976461
60 I = 51
30521
XDOT = -3509
222073 Wp = 48
44401
YDOT = -6580
438664 meter/sec RA = 253
70316 deg
ZDOT = -1899
699032 TA = 203
08929
MA = 203
14715
Ha = 186
439 n
mi
Hp = 180
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10592142
11 X = -3239430
94
Y = 10375029
38 feet Y = 3126145
05 meter
Z = -16326973
77 Z = -4992172
59
XDOT = -11513
195778 XDOT = -3426
148959
YDOT = -21589
365696 feet/sec YDOT = -6619
216322 meter/sec
ZDOT = -6232
608372 ZDOT = -1916
545741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3854142
78 X = -1174742
72
Y = -14246299
39 feet Y = -4342272
05 meter
Z = -16388816
87 Z = -4995311
38
XDOT = 23402
714373 XDOT = 7133
147341
YDOT = 935
149915 feet/sec YDOT = 285
033694 meter/sec
ZDOT = -6299
329904 ZDOT = -1920
035755
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 09318
53995979
00016717 00000-0 10270-3 0 9105
2 25544 51
6433 254
4293 0006147 329
5641 30
5166 15
76469925 29647
Satellite: ISS
Catalog Number: 25544
Epoch time: 09318
53995979 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 254
4293 deg
Eccentricity:
0006147
Arg of perigee: 329
5641 deg
Mean anomaly: 30
5166 deg
Mean motion: 15
76469925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 346
Coasting Arc #12 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2009/319/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3050205
49 A = 6724720
58 meter
Y = 5932422
18 meter E =
0008610
Z = 830327
31 I = 51
35103
XDOT = -3970
167148 Wp = 107
60012
YDOT = 2879
207710 meter/sec RA = 248
50241 deg
ZDOT = -5938
671586 TA = 63
29971
MA = 63
21159
Ha = 186
487 n
mi
Hp = 180
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10007235
86 X = 2979607
70
Y = 19463327
36 feet Y = 5966136
60 meter
Z = 2724170
98 Z = 844974
49
XDOT = -13025
482768 XDOT = -3973
217944
YDOT = 9446
219521 feet/sec YDOT = 2834
794187 meter/sec
ZDOT = -19483
830662 ZDOT = -5957
966558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21871745
49 X = -6666508
03
Y = -522633
18 feet Y = -159298
59 meter
Z = 2782192
05 Z = 848012
14
XDOT = -2166
935714 XDOT = -660
482006
YDOT = -14260
533656 feet/sec YDOT = -4346
610658 meter/sec
ZDOT = -19559
827270 ZDOT = -5961
835352
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 09319
55418630
00016717 00000-0 10270-3 0 9113
2 25544 51
6438 249
2019 0006083 332
9078 27
1769 15
76512627 29808
Satellite: ISS
Catalog Number: 25544
Epoch time: 09319
55418630 = yrday
fracday
Element set: 911
Inclination: 51
6438 deg
RA of node: 249
2019 deg
Eccentricity:
0006083
Arg of perigee: 332
9078 deg
Mean anomaly: 27
1769 deg
Mean motion: 15
76512627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 325
Coasting Arc #13 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2009/320/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3766961
22 A = 6712634
20 meter
Y = -1846342
53 meter E =
0005611
Z = 5240477
15 I = 51
32329
XDOT = 3434
543565 Wp = 357
91106
YDOT = 6897
875445 meter/sec RA = 243
33424 deg
ZDOT = -33
003174 TA = 92
43540
MA = 92
37115
Ha = 186
301 n
mi
Hp = 180
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12358796
67 X = 3761869
28
Y = -6057554
24 feet Y = -1804246
99 meter
Z = 17193166
49 Z = 5258765
12
XDOT = 11268
187548 XDOT = 3357
315380
YDOT = 22630
824951 feet/sec YDOT = 6935
850733 meter/sec
ZDOT = -108
278130 ZDOT = -16
504742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -300744
75 X = -91667
00
Y = 13669669
69 feet Y = 4166515
32 meter
Z = 17265238
94 Z = 5262444
83
XDOT = -24279
794950 XDOT = -7400
481501
YDOT = -457
143387 feet/sec YDOT = -139
337304 meter/sec
ZDOT = -42
911467 ZDOT = -13
079415
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 09320
56837045
00016717 00000-0 10270-3 0 9122
2 25544 51
6436 243
9745 0006149 335
2678 24
8191 15
76619978 29965
Satellite: ISS
Catalog Number: 25544
Epoch time: 09320
56837045 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 243
9745 deg
Eccentricity:
0006149
Arg of perigee: 335
2678 deg
Mean anomaly: 24
8191 deg
Mean motion: 15
76619978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 351
Coasting Arc #14 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2009/321/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2876592
04 A = 6724363
93 meter
Y = -5999435
81 meter E =
0016404
Z = 901767
01 I = 51
37767
XDOT = 4729
444815 Wp = 33
50007
YDOT = -1370
089576 meter/sec RA = 238
16705 deg
ZDOT = 5933
869753 TA = 336
39859
MA = 336
47377
Ha = 186
526 n
mi
Hp = 180
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9437637
93 X = -2813672
25
Y = -19683188
34 feet Y = -6031251
83 meter
Z = 2958553
19 Z = 887944
43
XDOT = 15516
551229 XDOT = 4715
587391
YDOT = -4495
044541 feet/sec YDOT = -1317
280145 meter/sec
ZDOT = 19468
076617 ZDOT = 5956
812279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21833390
42 X = 6654817
40
Y = 348001
66 feet Y = 106070
91 meter
Z = 2903774
65 Z = 885070
51
XDOT = -2844
203129 XDOT = -866
913114
YDOT = 14194
075159 feet/sec YDOT = 4326
354109 meter/sec
ZDOT = 19558
539720 ZDOT = 5961
442907
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 09321
58251787
00016717 00000-0 10270-3 0 9139
2 25544 51
6437 238
7463 0006146 340
3371 19
7556 15
76632073 30128
Satellite: ISS
Catalog Number: 25544
Epoch time: 09321
58251787 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 238
7463 deg
Eccentricity:
0006146
Arg of perigee: 340
3371 deg
Mean anomaly: 19
7556 deg
Mean motion: 15
76632073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 311
Coasting Arc #15 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2009/322/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4522112
37 A = 6713734
00 meter
Y = 561853
87 meter E =
0011037
Z = -4938910
95 I = 51
36001
XDOT = -3060
420369 Wp = 77
15689
YDOT = -6762
903811 meter/sec RA = 232
96665 deg
ZDOT = 2039
036029 TA = 212
63176
MA = 212
70001
Ha = 186
462 n
mi
Hp = 179
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14836326
69 X = -4504066
09
Y = 1843352
58 feet Y = 511386
35 meter
Z = -16203776
09 Z = -4960836
03
XDOT = -10040
749242 XDOT = -2994
474455
YDOT = -22188
004630 feet/sec YDOT = -6796
758720 meter/sec
ZDOT = 6689
750751 ZDOT = 2024
327631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4703724
63 X = 1433695
27
Y = -14091808
43 feet Y = -4295183
21 meter
Z = -16290267
27 Z = -4965273
46
XDOT = 23337
557846 XDOT = 7113
287631
YDOT = 147
406973 feet/sec YDOT = 44
929645 meter/sec
ZDOT = 6631
439260 ZDOT = 2021
262687
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 09322
53324203
00016717 00000-0 10270-3 0 9140
2 25544 51
6442 233
8452 0006108 343
3083 16
7880 15
76708408 30278
Satellite: ISS
Catalog Number: 25544
Epoch time: 09322
53324203 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 233
8452 deg
Eccentricity:
0006108
Arg of perigee: 343
3083 deg
Mean anomaly: 16
7880 deg
Mean motion: 15
76708408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 292
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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