Date:
February 9th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8234 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 2540)
---------------------------------------
Vector Time (GMT): 2009/037/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1458907
18 A = 6735733
46 meter
Y = 5535334
47 meter E =
0010304
Z = -3562453
55 I = 51
31965
XDOT = -4769
360533 Wp = 25
31211
YDOT = -4101
357619 meter/sec RA = 254
88218 deg
ZDOT = -4415
062008 TA = 197
28483
MA = 197
31994
Ha = 196
665 n
mi
Hp = 188
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4786440
88 X = -1503390
45
Y = 18160546
17 feet Y = 5518771
69 meter
Z = -11687839
72 Z = -3569648
35
XDOT = -15647
508310 XDOT = -4701
696963
YDOT = -13455
897699 feet/sec YDOT = -4154
312702 meter/sec
ZDOT = -14485
111575 ZDOT = -4438
066965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9080772
11 X = -2767819
34
Y = 16419767
88 feet Y = 5004745
25 meter
Z = -11715453
53 Z = -3570870
24
XDOT = -10537
354864 XDOT = -3211
785762
YDOT = -16237
213401 feet/sec YDOT = -4949
102645 meter/sec
ZDOT = -14575
026137 ZDOT = -4442
467966
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 09037
60638838
00010596 00000-0 82463-4 0 9001
2 25544 51
6373 255
5573 0008679 354
0385 6
0671 15
70818705 25411
Satellite: ISS
Catalog Number: 25544
Epoch time: 09037
60638838 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 255
5573 deg
Eccentricity:
0008679
Arg of perigee: 354
0385 deg
Mean anomaly: 6
0671 deg
Mean motion: 15
70818705 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2541
Checksum: 322
Coasting Arc #2 (Orbit 2556)
---------------------------------------
Vector Time (GMT): 2009/038/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4585234
81 A = 6732472
93 meter
Y = 2058112
20 meter E =
0014253
Z = 4479190
76 I = 51
31714
XDOT = -76
166752 Wp = 32
71248
YDOT = 7027
046529 meter/sec RA = 249
69837 deg
ZDOT = -3134
358463 TA = 88
82313
MA = 88
65983
Ha = 196
669 n
mi
Hp = 188
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15043421
30 X = 4540121
44
Y = 6752336
60 feet Y = 2109134
44 meter
Z = 14695507
75 Z = 4501355
70
XDOT = -249
890917 XDOT = -139
513006
YDOT = 23054
614597 feet/sec YDOT = 7025
840790 meter/sec
ZDOT = -10283
328292 ZDOT = -3134
881910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12987530
99 X = 3958599
45
Y = 10033578
52 feet Y = 3058234
73 meter
Z = 14782011
46 Z = 4505557
09
XDOT = -4793
690100 XDOT = -1461
116742
YDOT = 21436
349030 feet/sec YDOT = 6533
799184 meter/sec
ZDOT = -10284
833009 ZDOT = -3134
817101
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 09038
62428281
00010596 00000-0 82463-4 0 9014
2 25544 51
6369 250
3535 0008578 357
0208 3
0901 15
70811771 25578
Satellite: ISS
Catalog Number: 25544
Epoch time: 09038
62428281 = yrday
fracday
Element set: 901
Inclination: 51
6369 deg
RA of node: 250
3535 deg
Eccentricity:
0008578
Arg of perigee: 357
0208 deg
Mean anomaly: 3
0901 deg
Mean motion: 15
70811771 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2557
Checksum: 302
Coasting Arc #3 (Orbit 2572)
---------------------------------------
Vector Time (GMT): 2009/039/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1400018
88 A = 6739789
55 meter
Y = -6326216
89 meter E =
0019395
Z = 1811304
18 I = 51
35261
XDOT = 5220
249119 Wp = 42
51339
YDOT = 467
495658 meter/sec RA = 244
60409 deg
ZDOT = 5646
633839 TA = 337
65157
MA = 337
73596
Ha = 196
790 n
mi
Hp = 187
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4593237
79 X = -1337972
71
Y = -20755304
76 feet Y = -6341525
85 meter
Z = 5942599
02 Z = 1804653
63
XDOT = 17126
801572 XDOT = 5187
204132
YDOT = 1533
778404 feet/sec YDOT = 525
686581 meter/sec
ZDOT = 18525
701573 ZDOT = 5671
912701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -59982
43 X = -18282
64
Y = -21264760
46 feet Y = -6481498
99 meter
Z = 5916194
46 Z = 1803256
07
XDOT = 14741
879115 XDOT = 4493
324754
YDOT = 5159
285994 feet/sec YDOT = 1572
550371 meter/sec
ZDOT = 18624
225558 ZDOT = 5676
663950
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 09039
64216565
00010596 00000-0 82463-4 0 9028
2 25544 51
6362 245
1495 0008551 1
6206 358
4982 15
70837469 25735
Satellite: ISS
Catalog Number: 25544
Epoch time: 09039
64216565 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 245
1495 deg
Eccentricity:
0008551
Arg of perigee: 1
6206 deg
Mean anomaly: 358
4982 deg
Mean motion: 15
70837469 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2573
Checksum: 323
Coasting Arc #4 (Orbit 2587)
---------------------------------------
Vector Time (GMT): 2009/040/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4118846
49 A = 6729349
12 meter
Y = 1202547
69 meter E =
0016731
Z = -5196280
23 I = 51
33180
XDOT = -3204
807040 Wp = 66
80933
YDOT = -6920
776899 meter/sec RA = 239
44658 deg
ZDOT = 947
565547 TA = 212
22518
MA = 212
32752
Ha = 196
855 n
mi
Hp = 187
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13513275
89 X = -4106745
72
Y = 3945366
44 feet Y = 1156556
00 meter
Z = -17048163
48 Z = -5216259
52
XDOT = -10514
458794 XDOT = -3131
782527
YDOT = -22705
960956 feet/sec YDOT = -6956
206610 meter/sec
ZDOT = 3108
810849 ZDOT = 932
174516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13930250
42 X = -4245940
33
Y = 1210634
63 feet Y = 369001
44 meter
Z = -17125913
31 Z = -5219978
38
XDOT = -5739
024979 XDOT = -1749
254814
YDOT = -23326
122220 feet/sec YDOT = -7109
802053 meter/sec
ZDOT = 3048
287832 ZDOT = 929
118131
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 09040
59641957
00010596 00000-0 82463-4 0 9032
2 25544 51
6364 240
2714 0008505 6
0537 354
0726 15
70860935 25880
Satellite: ISS
Catalog Number: 25544
Epoch time: 09040
59641957 = yrday
fracday
Element set: 903
Inclination: 51
6364 deg
RA of node: 240
2714 deg
Eccentricity:
0008505
Arg of perigee: 6
0537 deg
Mean anomaly: 354
0726 deg
Mean motion: 15
70860935 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2588
Checksum: 312
Coasting Arc #5 (Orbit 2603)
---------------------------------------
Vector Time (GMT): 2009/041/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4034665
80 A = 6740926
98 meter
Y = 5397485
84 meter E =
0010539
Z = 161763
54 I = 51
38720
XDOT = -3753
667150 Wp = 89
70387
YDOT = 2996
007519 meter/sec RA = 234
32010 deg
ZDOT = -6005
719391 TA = 88
53617
MA = 88
41545
Ha = 196
963 n
mi
Hp = 187
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13237092
51 X = 3973224
56
Y = 17708286
89 feet Y = 5442260
29 meter
Z = 530720
27 Z = 181213
93
XDOT = -12315
180937 XDOT = -3757
716216
YDOT = 9829
420993 feet/sec YDOT = 2954
008998 meter/sec
ZDOT = -19703
803777 ZDOT = -6023
964077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9807299
04 X = 2989264
75
Y = 19812475
90 feet Y = 6038842
66 meter
Z = 606952
02 Z = 184998
98
XDOT = -12335
088642 XDOT = -3759
735018
YDOT = 6741
407639 feet/sec YDOT = 2054
781048 meter/sec
ZDOT = -19774
649796 ZDOT = -6027
313258
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 09041
61427677
00010596 00000-0 82463-4 0 9048
2 25544 51
6361 235
0670 0008768 8
7772 351
3541 15
70922764 26044
Satellite: ISS
Catalog Number: 25544
Epoch time: 09041
61427677 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 235
0670 deg
Eccentricity:
0008768
Arg of perigee: 8
7772 deg
Mean anomaly: 351
3541 deg
Mean motion: 15
70922764 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2604
Checksum: 312
Coasting Arc #6 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2009/042/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2127604
05 A = 6729586
29 meter
Y = -3801642
51 meter E =
0008063
Z = 5123208
77 I = 51
36719
XDOT = 5713
656494 Wp = 43
69821
YDOT = 4988
658732 meter/sec RA = 229
20186 deg
ZDOT = 1333
489164 TA = 33
52092
MA = 33
46992
Ha = 196
997 n
mi
Hp = 187
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6980328
25 X = 2145069
53
Y = -12472580
43 feet Y = -3777752
50 meter
Z = 16808427
72 Z = 5133587
02
XDOT = 18745
592173 XDOT = 5650
970152
YDOT = 16366
990592 feet/sec YDOT = 5052
201731 meter/sec
ZDOT = 4374
964448 ZDOT = 1361
092886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8837646
53 X = 2693714
66
Y = -11172993
36 feet Y = -3405528
37 meter
Z = 16848552
19 Z = 5135438
71
XDOT = 14963
887423 XDOT = 4560
992887
YDOT = 18574
128464 feet/sec YDOT = 5661
394356 meter/sec
ZDOT = 4482
944240 ZDOT = 1366
401404
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 09042
63212508
00010596 00000-0 82463-4 0 9057
2 25544 51
6364 229
8630 0008621 13
3511 346
7877 15
70889329 26202
Satellite: ISS
Catalog Number: 25544
Epoch time: 09042
63212508 = yrday
fracday
Element set: 905
Inclination: 51
6364 deg
RA of node: 229
8630 deg
Eccentricity:
0008621
Arg of perigee: 13
3511 deg
Mean anomaly: 346
7877 deg
Mean motion: 15
70889329 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2620
Checksum: 309
Coasting Arc #7 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2009/043/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5607155
25 A = 6738939
36 meter
Y = -3057902
46 meter E =
0014473
Z = -2131021
18 I = 51
42079
XDOT = 818
332602 Wp = 28
06976
YDOT = -5317
729966 meter/sec RA = 224
04206 deg
ZDOT = 5505
153305 TA = 308
04710
MA = 308
17762
Ha = 197
042 n
mi
Hp = 186
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18396178
65 X = -5562192
64
Y = -10032488
39 feet Y = -3120353
65 meter
Z = -6991539
31 Z = -2158150
81
XDOT = 2684
818248 XDOT = 850
993018
YDOT = -17446
620622 feet/sec YDOT = -5308
395980 meter/sec
ZDOT = 18061
526592 ZDOT = 5509
208305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16678777
86 X = -5083691
49
Y = -12625190
81 feet Y = -3848158
16 meter
Z = -7097517
87 Z = -2163323
45
XDOT = 4199
877717 XDOT = 1280
122728
YDOT = -15660
322501 feet/sec YDOT = -4773
266298 meter/sec
ZDOT = 18076
880530 ZDOT = 5509
833186
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 09043
58634458
00010596 00000-0 82463-4 0 9065
2 25544 51
6380 224
9850 0008555 17
4521 342
6933 15
70914169 26357
Satellite: ISS
Catalog Number: 25544
Epoch time: 09043
58634458 = yrday
fracday
Element set: 906
Inclination: 51
6380 deg
RA of node: 224
9850 deg
Eccentricity:
0008555
Arg of perigee: 17
4521 deg
Mean anomaly: 342
6933 deg
Mean motion: 15
70914169 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2635
Checksum: 322
Coasting Arc #8 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2009/044/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 798569
31 A = 6732777
27 meter
Y = 5098341
93 meter E =
0015964
Z = -4340768
29 I = 51
42252
XDOT = -6628
238525 Wp = 45
76183
YDOT = -1864
976428 meter/sec RA = 218
95812 deg
ZDOT = -3406
652425 TA = 189
66517
MA = 189
69592
Ha = 197
195 n
mi
Hp = 186
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2619978
04 X = 762585
78
Y = 16726843
60 feet Y = 5107070
59 meter
Z = -14241365
78 Z = -4336976
55
XDOT = -21746
189388 XDOT = -6590
342786
YDOT = -6118
689069 feet/sec YDOT = -1938
885522 meter/sec
ZDOT = -11176
681183 ZDOT = -3438
759757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 501936
44 X = 152990
23
Y = 16936132
56 feet Y = 5162133
21 meter
Z = -14226157
40 Z = -4336132
78
XDOT = -19465
410761 XDOT = -5933
057200
YDOT = -8925
461691 feet/sec YDOT = -2720
480723 meter/sec
ZDOT = -11301
963556 ZDOT = -3444
838492
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 09044
60416657
00010596 00000-0 82463-4 0 9079
2 25544 51
6383 219
7818 0008650 21
0210 339
1305 15
70941365 26518
Satellite: ISS
Catalog Number: 25544
Epoch time: 09044
60416657 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 219
7818 deg
Eccentricity:
0008650
Arg of perigee: 21
0210 deg
Mean anomaly: 339
1305 deg
Mean motion: 15
70941365 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2651
Checksum: 297
Coasting Arc #9 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2009/045/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5599766
32 A = 6734768
54 meter
Y = 167899
22 meter E =
0017720
Z = 3732558
99 I = 51
45303
XDOT = 2665
468568 Wp = 58
99458
YDOT = 5845
678449 meter/sec RA = 213
78077 deg
ZDOT = -4237
976625 TA = 75
85630
MA = 75
65946
Ha = 197
203 n
mi
Hp = 186
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18371936
75 X = 5579340
80
Y = 550850
47 feet Y = 230404
98 meter
Z = 12245928
44 Z = 3759712
67
XDOT = 8744
975618 XDOT = 2620
490173
YDOT = 19178
735069 feet/sec YDOT = 5875
233643 meter/sec
ZDOT = -13904
122787 ZDOT = -4225
137393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18121229
93 X = 5523350
88
Y = 2617076
56 feet Y = 797684
94 meter
Z = 12351768
93 Z = 3764819
17
XDOT = 6790
413428 XDOT = 2069
718013
YDOT = 18732
177844 feet/sec YDOT = 5709
567807 meter/sec
ZDOT = -13853
588593 ZDOT = -4222
573803
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 09045
62197646
00010596 00000-0 82463-4 0 9087
2 25544 51
6382 214
5775 0008596 25
0384 335
1193 15
70937233 26674
Satellite: ISS
Catalog Number: 25544
Epoch time: 09045
62197646 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 214
5775 deg
Eccentricity:
0008596
Arg of perigee: 25
0384 deg
Mean anomaly: 335
1193 deg
Mean motion: 15
70937233 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2667
Checksum: 331
Coasting Arc #10 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2009/046/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3774150
12 A = 6737027
48 meter
Y = -4729809
52 meter E =
0019685
Z = 2935027
63 I = 51
48751
XDOT = 5686
170326 Wp = 61
80866
YDOT = -1423
741254 meter/sec RA = 208
70644 deg
ZDOT = 5001
238030 TA = 332
09095
MA = 332
19640
Ha = 197
252 n
mi
Hp = 186
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12382382
27 X = -3735237
76
Y = -15517747
76 feet Y = -4771796
65 meter
Z = 9629355
74 Z = 2916787
62
XDOT = 18655
414455 XDOT = 5677
373419
YDOT = -4671
067106 feet/sec YDOT = -1360
204308 meter/sec
ZDOT = 16408
261253 ZDOT = 5028
839753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10890923
28 X = -3319553
42
Y = -16639814
70 feet Y = -5071815
52 meter
Z = 9557862
47 Z = 2913236
48
XDOT = 17709
622650 XDOT = 5397
892984
YDOT = -2073
707099 feet/sec YDOT = -632
065924 meter/sec
ZDOT = 16515
721264 ZDOT = 5033
991841
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 09046
63977091
00010596 00000-0 82463-4 0 9090
2 25544 51
6395 209
3744 0008578 28
4425 331
7203 15
71007314 26830
Satellite: ISS
Catalog Number: 25544
Epoch time: 09046
63977091 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 209
3744 deg
Eccentricity:
0008578
Arg of perigee: 28
4425 deg
Mean anomaly: 331
7203 deg
Mean motion: 15
71007314 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2683
Checksum: 320
Coasting Arc #11 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2009/047/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3977388
94 A = 6730461
03 meter
Y = 2473091
00 meter E =
0016679
Z = -4846147
09 I = 51
49201
XDOT = -5715
906317 Wp = 76
97112
YDOT = -4554
007509 meter/sec RA = 203
54199 deg
ZDOT = 2377
780603 TA = 216
26184
MA = 216
37500
Ha = 197
308 n
mi
Hp = 186
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13049176
33 X = -3981206
46
Y = 8113815
61 feet Y = 2428592
19 meter
Z = -15899432
70 Z = -4865478
25
XDOT = -18752
973482 XDOT = -5676
108507
YDOT = -14940
969519 feet/sec YDOT = -4617
703584 meter/sec
ZDOT = 7801
117463 ZDOT = 2350
109752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13556564
40 X = -4132040
83
Y = 7066785
67 feet Y = 2153956
27 meter
Z = -15974575
70 Z = -4869050
67
XDOT = -17045
829926 XDOT = -5195
568961
YDOT = -15387
941864 feet/sec YDOT = -4690
244680 meter/sec
ZDOT = 7692
871630 ZDOT = 2344
787273
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 09047
59394387
00010596 00000-0 82463-4 0 9109
2 25544 51
6394 204
4972 0008729 31
7821 328
3866 15
71006220 26981
Satellite: ISS
Catalog Number: 25544
Epoch time: 09047
59394387 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 204
4972 deg
Eccentricity:
0008729
Arg of perigee: 31
7821 deg
Mean anomaly: 328
3866 deg
Mean motion: 15
71006220 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2698
Checksum: 330
Coasting Arc #12 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2009/048/13:58:10
944
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5935398
79 A = 6740064
46 meter
Y = 2969913
43 meter E =
0010842
Z = -1182521
99 I = 51
55201
XDOT = -3100
871237 Wp = 91
62334
YDOT = 3878
463809 meter/sec RA = 198
44978 deg
ZDOT = -5869
930187 TA = 101
31915
MA = 101
19731
Ha = 197
411 n
mi
Hp = 186
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19473093
15 X = 5907491
99
Y = 9743810
48 feet Y = 3036130
50 meter
Z = -3879665
31 Z = -1153756
01
XDOT = -10173
462064 XDOT = -3115
495783
YDOT = 12724
618797 feet/sec YDOT = 3843
706385 meter/sec
ZDOT = -19258
301140 ZDOT = -5885
029448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18856981
73 X = 5747608
03
Y = 10927803
89 feet Y = 3330794
63 meter
Z = -3767272
83 Z = -1148264
76
XDOT = -10031
004536 XDOT = -3057
450182
YDOT = 10704
432745 feet/sec YDOT = 3262
711101 meter/sec
ZDOT = -19316
835595 ZDOT = -5887
771489
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 09048
61171380
00010596 00000-0 82463-4 0 9110
2 25544 51
6395 199
2926 0008812 35
3225 324
8519 15
71029209 27140
Satellite: ISS
Catalog Number: 25544
Epoch time: 09048
61171380 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 199
2926 deg
Eccentricity:
0008812
Arg of perigee: 35
3225 deg
Mean anomaly: 324
8519 deg
Mean motion: 15
71029209 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2714
Checksum: 310
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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