Date:
May 25th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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 159)
---------------------------------------
Vector Time (GMT): 2009/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3161814
57 A = 6728835
91 meter
Y = -4515230
77 meter E =
0018343
Z = 3854764
25 I = 51
96926
XDOT = 3065
955507 Wp = 54
90348
YDOT = -5712
838205 meter/sec RA = 88
15747 deg
ZDOT = -4152
724604 TA = 78
41422
MA = 78
20837
Ha = 194
539 n
mi
Hp = 183
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10373407
39 X = -3129815
58
Y = -14813749
24 feet Y = -4550409
36 meter
Z = 12646864
33 Z = 3839481
32
XDOT = 10058
909145 XDOT = 3149
783098
YDOT = -18742
907498 feet/sec YDOT = -5678
083931 meter/sec
ZDOT = -13624
424553 ZDOT = -4137
626673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18106348
54 X = -5518815
04
Y = 855360
94 feet Y = 260714
02 meter
Z = 12586755
94 Z = 3836443
21
XDOT = -10302
721454 XDOT = -3140
269499
YDOT = -17297
976021 feet/sec YDOT = -5272
423091 meter/sec
ZDOT = -13565
634625 ZDOT = -4134
805434
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 09140
54006321
00010596 00000-0 82463-4 0 9005
2 25544 51
6385 88
7309 0009612 23
0422 337
1170 15
72929224 1608
Satellite: ISS
Catalog Number: 25544
Epoch time: 09140
54006321 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 88
7309 deg
Eccentricity:
0009612
Arg of perigee: 23
0422 deg
Mean anomaly: 337
1170 deg
Mean motion: 15
72929224 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 160
Checksum: 273
Coasting Arc #2 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2009/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1986064
68 A = 6730260
61 meter
Y = 5468138
06 meter E =
0018977
Z = 3360643
44 I = 51
97274
XDOT = -4228
222823 Wp = 62
98486
YDOT = -4424
238455 meter/sec RA = 83
10449 deg
ZDOT = 4688
267671 TA = 336
43540
MA = 336
52222
Ha = 194
572 n
mi
Hp = 183
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6515960
25 X = -2063388
47
Y = 17940085
49 feet Y = 5445496
11 meter
Z = 11025733
06 Z = 3350807
54
XDOT = -13872
122122 XDOT = -4201
211239
YDOT = -14515
218027 feet/sec YDOT = -4471
370257 meter/sec
ZDOT = 15381
455612 ZDOT = 4667
791774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11858365
57 X = 3614429
82
Y = 14984147
94 feet Y = 4567168
29 meter
Z = 10987523
45 Z = 3348997
15
XDOT = -18578
105873 XDOT = -5662
606670
YDOT = 3454
542477 feet/sec YDOT = 1052
944547 meter/sec
ZDOT = 15301
024277 ZDOT = 4663
752200
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 09141
55658394
00010596 00000-0 82463-4 0 9011
2 25544 51
6390 83
5188 0009514 27
0994 333
0664 15
72958903 1767
Satellite: ISS
Catalog Number: 25544
Epoch time: 09141
55658394 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 83
5188 deg
Eccentricity:
0009514
Arg of perigee: 27
0994 deg
Mean anomaly: 333
0664 deg
Mean motion: 15
72958903 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 176
Checksum: 328
Coasting Arc #3 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2009/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4113009
85 A = 6727150
62 meter
Y = 3147399
85 meter E =
0013863
Z = -4300887
79 I = 51
95798
XDOT = -1413
674747 Wp = 67
60685
YDOT = 6676
641383 meter/sec RA = 77
94984 deg
ZDOT = 3548
254759 TA = 238
17996
MA = 238
31502
Ha = 194
615 n
mi
Hp = 183
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13494126
79 X = 4098402
84
Y = 10326114
99 feet Y = 3193312
71 meter
Z = -14110524
23 Z = -4280941
44
XDOT = -4638
040508 XDOT = -1505
466206
YDOT = 21904
991414 feet/sec YDOT = 6660
319237 meter/sec
ZDOT = 11641
255770 ZDOT = 3541
164702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15789025
26 X = 4812494
90
Y = -6452118
97 feet Y = -1966605
86 meter
Z = -14032243
04 Z = -4277027
68
XDOT = 16011
332873 XDOT = 4880
254260
YDOT = 14025
163563 feet/sec YDOT = 4274
869854 meter/sec
ZDOT = 11613
851254 ZDOT = 3539
901862
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 09142
50955447
00010596 00000-0 82463-4 0 9027
2 25544 51
6394 78
6322 0009563 30
1563 330
0148 15
72976498 1917
Satellite: ISS
Catalog Number: 25544
Epoch time: 09142
50955447 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 78
6322 deg
Eccentricity:
0009563
Arg of perigee: 30
1563 deg
Mean anomaly: 330
0148 deg
Mean motion: 15
72976498 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 191
Checksum: 314
Coasting Arc #4 (Orbit 206)
---------------------------------------
Vector Time (GMT): 2009/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 467008
12 A = 6731422
61 meter
Y = -6083900
99 meter E =
0011156
Z = -2858547
68 I = 51
96661
XDOT = 5032
333918 Wp = 58
20018
YDOT = 2779
969772 meter/sec RA = 72
89242 deg
ZDOT = -5103
264540 TA = 154
38832
MA = 154
33302
Ha = 194
578 n
mi
Hp = 182
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1532178
87 X = 548891
26
Y = -19960305
07 feet Y = -6078220
40 meter
Z = -9378437
28 Z = -2856080
84
XDOT = 16510
281884 XDOT = 5025
665141
YDOT = 9120
635736 feet/sec YDOT = 2836
207685 meter/sec
ZDOT = -16742
993898 ZDOT = -5078
832683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16585599
39 X = -5055290
69
Y = -11218487
42 feet Y = -3419394
97 meter
Z = -9369091
17 Z = -2855698
99
XDOT = 15302
808225 XDOT = 4664
295947
YDOT = -8745
078683 feet/sec YDOT = -2665
499983 meter/sec
ZDOT = -16647
168899 ZDOT = -5074
057080
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 09143
52603663
00010596 00000-0 82463-4 0 9031
2 25544 51
6405 73
4197 0009596 34
0834 326
0943 15
73021302 2075
Satellite: ISS
Catalog Number: 25544
Epoch time: 09143
52603663 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 73
4197 deg
Eccentricity:
0009596
Arg of perigee: 34
0834 deg
Mean anomaly: 326
0943 deg
Mean motion: 15
73021302 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 207
Checksum: 286
Coasting Arc #5 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2009/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4590865
40 A = 6725763
04 meter
Y = -1681826
12 meter E =
0017447
Z = 4612456
53 I = 51
93778
XDOT = -396
755215 Wp = 50
26613
YDOT = -7098
624851 meter/sec RA = 67
74146 deg
ZDOT = -2964
964199 TA = 69
09302
MA = 68
90635
Ha = 194
698 n
mi
Hp = 182
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15061894
36 X = -4594124
67
Y = -5517802
24 feet Y = -1733182
86 meter
Z = 15132731
40 Z = 4590145
44
XDOT = -1301
690337 XDOT = -302
944149
YDOT = -23289
451612 feet/sec YDOT = -7102
536576 meter/sec
ZDOT = -9727
572831 ZDOT = -2966
664997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12085833
93 X = -3683762
18
Y = 10671407
32 feet Y = 3252644
95 meter
Z = 15045266
59 Z = 4585797
26
XDOT = -20275
576106 XDOT = -6179
995597
YDOT = -9153
436163 feet/sec YDOT = -2789
967342 meter/sec
ZDOT = -9734
585650 ZDOT = -2967
101706
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 09144
54249911
00010596 00000-0 82463-4 0 9047
2 25544 51
6406 68
2079 0009543 37
8333 322
3499 15
73039794 2231
Satellite: ISS
Catalog Number: 25544
Epoch time: 09144
54249911 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 68
2079 deg
Eccentricity:
0009543
Arg of perigee: 37
8333 deg
Mean anomaly: 322
3499 deg
Mean motion: 15
73039794 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 223
Checksum: 318
Coasting Arc #6 (Orbit 238)
---------------------------------------
Vector Time (GMT): 2009/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1170988
58 A = 6732528
55 meter
Y = 6201628
39 meter E =
0022668
Z = 2307654
00 I = 51
94889
XDOT = -5343
663141 Wp = 59
89617
YDOT = -1033
098031 meter/sec RA = 62
67687 deg
ZDOT = 5459
504468 TA = 325
95878
MA = 326
10398
Ha = 194
640 n
mi
Hp = 182
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3841826
06 X = 1090343
57
Y = 20346549
82 feet Y = 6214271
72 meter
Z = 7571043
31 Z = 2313148
02
XDOT = -17531
703218 XDOT = -5358
235379
YDOT = -3389
429237 feet/sec YDOT = -1092
936494 meter/sec
ZDOT = 17911
760065 ZDOT = 5433
508975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19795196
61 X = 6033575
93
Y = 6046577
97 feet Y = 1842996
97 meter
Z = 7592858
48 Z = 2314303
27
XDOT = -10722
748044 XDOT = -3268
293604
YDOT = 12622
791032 feet/sec YDOT = 3847
426706 meter/sec
ZDOT = 17809
890945 ZDOT = 5428
454760
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 09145
55894169
00010596 00000-0 82463-4 0 9051
2 25544 51
6411 62
9952 0009557 41
4220 318
7666 15
73060986 2398
Satellite: ISS
Catalog Number: 25544
Epoch time: 09145
55894169 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 62
9952 deg
Eccentricity:
0009557
Arg of perigee: 41
4220 deg
Mean anomaly: 318
7666 deg
Mean motion: 15
73060986 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 239
Checksum: 329
Coasting Arc #7 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2009/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4631010
23 A = 6724498
69 meter
Y = 140390
67 meter E =
0018565
Z = -4888142
75 I = 51
90806
XDOT = 2253
120913 Wp = 79
87112
YDOT = 6965
220866 meter/sec RA = 57
52993 deg
ZDOT = 2345
336624 TA = 212
88030
MA = 212
99593
Ha = 194
633 n
mi
Hp = 182
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15193603
12 X = 4652842
06
Y = 460599
31 feet Y = 192300
34 meter
Z = -16037213
75 Z = -4865592
07
XDOT = 7392
128981 XDOT = 2163
673874
YDOT = 22851
774494 feet/sec YDOT = 6989
916002 meter/sec
ZDOT = 7694
673963 ZDOT = 2356
066444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7249882
30 X = 2209764
12
Y = -13465608
78 feet Y = -4104317
55 meter
Z = -15948872
66 Z = -4861216
39
XDOT = 22742
776282 XDOT = 6931
998211
YDOT = 3122
630638 feet/sec YDOT = 951
777819 meter/sec
ZDOT = 7737
027998 ZDOT = 2358
246134
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 09146
51183754
00010596 00000-0 82463-4 0 9060
2 25544 51
6417 58
1085 0009501 44
6937 315
4990 15
73100914 2544
Satellite: ISS
Catalog Number: 25544
Epoch time: 09146
51183754 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 58
1085 deg
Eccentricity:
0009501
Arg of perigee: 44
6937 deg
Mean anomaly: 315
4990 deg
Mean motion: 15
73100914 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 254
Checksum: 304
Coasting Arc #8 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2009/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2728175
68 A = 6733226
87 meter
Y = -5885113
08 meter E =
0011551
Z = -1816386
27 I = 51
92107
XDOT = 5135
304720 Wp = 87
28052
YDOT = -633
880259 meter/sec RA = 52
45539 deg
ZDOT = -5689
741331 TA = 112
75196
MA = 112
62985
Ha = 194
579 n
mi
Hp = 182
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8950707
63 X = -2653340
90
Y = -19308113
78 feet Y = -5915202
38 meter
Z = -5959272
55 Z = -1829459
07
XDOT = 16848
112600 XDOT = 5169
650982
YDOT = -2079
659642 feet/sec YDOT = -576
261212 meter/sec
ZDOT = -18667
130351 ZDOT = -5664
710664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21265317
71 X = -6481668
84
Y = -297413
40 feet Y = -90651
61 meter
Z = -6010753
87 Z = -1832077
78
XDOT = 5425
471097 XDOT = 1653
683590
YDOT = -14640
742134 feet/sec YDOT = -4462
498203 meter/sec
ZDOT = -18569
102753 ZDOT = -5659
862519
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 09147
52824120
00010596 00000-0 82463-4 0 9072
2 25544 51
6420 52
8954 0009369 48
5729 311
6237 15
73116329 2705
Satellite: ISS
Catalog Number: 25544
Epoch time: 09147
52824120 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 52
8954 deg
Eccentricity:
0009369
Arg of perigee: 48
5729 deg
Mean anomaly: 311
6237 deg
Mean motion: 15
73116329 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 270
Checksum: 307
Coasting Arc #9 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2009/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4256021
45 A = 6723445
18 meter
Y = 1231793
62 meter E =
0014804
Z = 5049415
72 I = 51
86933
XDOT = -3967
601842 Wp = 52
25418
YDOT = -6362
155729 meter/sec RA = 47
31298 deg
ZDOT = -1779
749558 TA = 54
88887
MA = 54
75019
Ha = 194
614 n
mi
Hp = 182
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13963324
95 X = -4294008
35
Y = 4041317
65 feet Y = 1183987
10 meter
Z = 16566324
54 Z = 5028647
93
XDOT = -13017
066411 XDOT = -3887
518578
YDOT = -20873
214333 feet/sec YDOT = -6406
075716 meter/sec
ZDOT = -5839
073353 ZDOT = -1798
830624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2178272
93 X = -663937
59
Y = 14465444
07 feet Y = 4409067
35 meter
Z = 16485019
13 Z = 5024633
83
XDOT = -23328
601560 XDOT = -7110
557755
YDOT = 3273
491253 feet/sec YDOT = 997
760134 meter/sec
ZDOT = -5914
115752 ZDOT = -1802
622481
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 09148
54462344
00010596 00000-0 82463-4 0 9082
2 25544 51
6416 47
6823 0009374 51
3057 308
8943 15
73202871 2866
Satellite: ISS
Catalog Number: 25544
Epoch time: 09148
54462344 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 47
6823 deg
Eccentricity:
0009374
Arg of perigee: 51
3057 deg
Mean anomaly: 308
8943 deg
Mean motion: 15
73202871 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 286
Checksum: 318
Coasting Arc #10 (Orbit 301)
---------------------------------------
Vector Time (GMT): 2009/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149877
99 A = 6733773
03 meter
Y = 5129572
29 meter E =
0023381
Z = 1286536
44 I = 51
88330
XDOT = -4496
979737 Wp = 57
33476
YDOT = 2147
463246 meter/sec RA = 42
22701 deg
ZDOT = 5878
951076 TA = 316
74409
MA = 316
92745
Ha = 194
588 n
mi
Hp = 182
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13615085
27 X = 4085960
07
Y = 16829305
41 feet Y = 5175621
09 meter
Z = 4220920
07 Z = 1306541
92
XDOT = -14753
870529 XDOT = -4549
217607
YDOT = 7045
483091 feet/sec YDOT = 2096
882532 meter/sec
ZDOT = 19287
897232 ZDOT = 5856
978207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20864328
38 X = 6359447
29
Y = -5710173
34 feet Y = -1740460
84 meter
Z = 4299529
67 Z = 1310496
64
XDOT = 84
063873 XDOT = 25
622668
YDOT = 14921
624372 feet/sec YDOT = 4548
111109 meter/sec
ZDOT = 19201
909487 ZDOT = 5852
742012
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 09149
56098898
00010596 00000-0 82463-4 0 9095
2 25544 51
6420 42
4688 0009433 55
1779 305
0270 15
73180636 3027
Satellite: ISS
Catalog Number: 25544
Epoch time: 09149
56098898 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 42
4688 deg
Eccentricity:
0009433
Arg of perigee: 55
1779 deg
Mean anomaly: 305
0270 deg
Mean motion: 15
73180636 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 302
Checksum: 322
Coasting Arc #11 (Orbit 316)
---------------------------------------
Vector Time (GMT): 2009/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3532552
95 A = 6722796
59 meter
Y = -2444411
16 meter E =
0022117
Z = -5189584
56 I = 51
82424
XDOT = 5432
139871 Wp = 83
11710
YDOT = 5298
379218 meter/sec RA = 37
08971 deg
ZDOT = 1208
978807 TA = 198
38836
MA = 198
46844
Ha = 194
505 n
mi
Hp = 181
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11589740
66 X = 3584834
26
Y = -8019721
65 feet Y = -2404615
19 meter
Z = -17026196
05 Z = -5172296
71
XDOT = 17821
981204 XDOT = 5366
615775
YDOT = 17383
133918 feet/sec YDOT = 5358
758080 meter/sec
ZDOT = 3966
465902 ZDOT = 1235
209551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2904963
81 X = -885432
97
Y = -13874338
10 feet Y = -4228898
25 meter
Z = -16958576
10 Z = -5168974
00
XDOT = 21881
776494 XDOT = 6669
565475
YDOT = -9527
563304 feet/sec YDOT = -2904
001295 meter/sec
ZDOT = 4069
471787 ZDOT = 1240
375001
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 09150
51381134
00010596 00000-0 82463-4 0 9102
2 25544 51
6423 37
5811 0009300 58
4686 301
7383 15
73234124 3175
Satellite: ISS
Catalog Number: 25544
Epoch time: 09150
51381134 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 37
5811 deg
Eccentricity:
0009300
Arg of perigee: 58
4686 deg
Mean anomaly: 301
7383 deg
Mean motion: 15
73234124 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 317
Checksum: 277
Coasting Arc #12 (Orbit 332)
---------------------------------------
Vector Time (GMT): 2009/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5283377
85 A = 6734062
61 meter
Y = -4086744
12 meter E =
0014997
Z = -848675
64 I = 51
83792
XDOT = 3523
440569 Wp = 104
11207
YDOT = -3333
644667 meter/sec RA = 31
99189 deg
ZDOT = -5973
213192 TA = 85
11262
MA = 84
94141
Ha = 194
496 n
mi
Hp = 181
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17333916
83 X = -5233163
79
Y = -13407953
15 feet Y = -4145545
09 meter
Z = -2784368
91 Z = -874220
79
XDOT = 11559
844386 XDOT = 3589
472943
YDOT = -10937
154418 feet/sec YDOT = -3293
873706 meter/sec
ZDOT = -19597
156142 ZDOT = -5955
936202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18850201
91 X = -5745541
54
Y = 11150757
07 feet Y = 3398750
76 meter
Z = -2884630
90 Z = -879235
50
XDOT = -5047
344164 XDOT = -1538
430501
YDOT = -13509
935850 feet/sec YDOT = -4117
828447 meter/sec
ZDOT = -19529
618569 ZDOT = -5952
627740
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 09151
53013816
00010596 00000-0 82463-4 0 9115
2 25544 51
6425 32
3675 0009144 62
9481 297
2614 15
73217089 3332
Satellite: ISS
Catalog Number: 25544
Epoch time: 09151
53013816 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 32
3675 deg
Eccentricity:
0009144
Arg of perigee: 62
9481 deg
Mean anomaly: 297
2614 deg
Mean motion: 15
73217089 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 333
Checksum: 297
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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