Date:
March 24th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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
080/15:37:31
822 1
4 -1
4 6
4
N/A -4
0 -0
2 197
0
000/02:29:03
644 -4
8 -6
3 185
5
Coasting Arc #1 (Orbit 3203)
---------------------------------------
Vector Time (GMT): 2009/079/18:27:19
449
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5655208
13 A = 6734128
05 meter
Y = 1075888
98 meter E =
0012913
Z = -3510474
49 I = 51
85413
XDOT = 1672
322178 Wp = 124
89010
YDOT = 5976
822289 meter/sec RA = 39
38806 deg
ZDOT = 4530
310956 TA = 193
65547
MA = 193
69043
Ha = 196
807 n
mi
Hp = 185
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18553832
45 X = 5659810
08
Y = 3529819
49 feet Y = 1139154
41 meter
Z = -11517304
74 Z = -3482990
71
XDOT = 5486
621320 XDOT = 1583
356918
YDOT = 19608
997010 feet/sec YDOT = 5995
025914 meter/sec
ZDOT = 14863
224920 ZDOT = 4538
218665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2062185
97 X = 628554
28
Y = -18839169
29 feet Y = -5742178
80 meter
Z = -11409895
81 Z = -3477736
24
XDOT = 17752
751611 XDOT = 5411
038691
YDOT = -7068
524795 feet/sec YDOT = -2154
486358 meter/sec
ZDOT = 14894
511883 ZDOT = 4539
847222
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 09079
77626166
00010596 00000-0 82463-4 0 9006
2 25544 51
6413 39
9332 0008975 142
4108 217
7683 15
71478567 32044
Satellite: ISS
Catalog Number: 25544
Epoch time: 09079
77626166 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 39
9332 deg
Eccentricity:
0008975
Arg of perigee: 142
4108 deg
Mean anomaly: 217
7683 deg
Mean motion: 15
71478567 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3204
Checksum: 330
Coasting Arc #2 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2009/080/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3991038
67 A = 6737498
20 meter
Y = -4926131
04 meter E =
0015021
Z = -2267119
99 I = 51
84335
XDOT = 5148
756306 Wp = 140
86937
YDOT = -1667
024753 meter/sec RA = 34
66894 deg
ZDOT = -5472
630677 TA = 64
48459
MA = 64
32932
Ha = 197
034 n
mi
Hp = 185
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13093958
88 X = -3924644
12
Y = -16161847
24 feet Y = -4970390
05 meter
Z = -7438057
70 Z = -2286346
65
XDOT = 16892
245097 XDOT = 5193
599267
YDOT = -5469
241317 feet/sec YDOT = -1609
197922 meter/sec
ZDOT = -17954
825056 ZDOT = -5447
509362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19456178
66 X = -5930243
25
Y = 7279183
36 feet Y = 2218695
09 meter
Z = -7513479
18 Z = -2290108
45
XDOT = 708
340087 XDOT = 215
902059
YDOT = -16434
481615 feet/sec YDOT = -5009
229996 meter/sec
ZDOT = -17856
827412 ZDOT = -5442
760995
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 09080
73014015
00010596 00000-0 82463-4 0 9019
2 25544 51
6424 35
0527 0009194 144
8075 215
3696 15
71332956 32197
Satellite: ISS
Catalog Number: 25544
Epoch time: 09080
73014015 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 35
0527 deg
Eccentricity:
0009194
Arg of perigee: 144
8075 deg
Mean anomaly: 215
3696 deg
Mean motion: 15
71332956 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3219
Checksum: 296
Coasting Arc #3 (Orbit 3234)
---------------------------------------
Vector Time (GMT): 2009/081/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3571819
17 A = 6728383
46 meter
Y = 2572722
29 meter E =
0010136
Z = 5079800
64 I = 51
78852
XDOT = -5803
876000 Wp = 117
11877
YDOT = -4788
079669 meter/sec RA = 29
53191 deg
ZDOT = -1657
981109 TA = 348
76517
MA = 348
78778
Ha = 196
912 n
mi
Hp = 185
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11718566
82 X = -3624998
73
Y = 8440689
92 feet Y = 2532483
14 meter
Z = 16666012
61 Z = 5062319
63
XDOT = -19041
587926 XDOT = -5741
849475
YDOT = -15708
922800 feet/sec YDOT = -4852
635304 meter/sec
ZDOT = -5439
570568 ZDOT = -1686
024946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4516011
20 X = 1376480
21
Y = 13800031
09 feet Y = 4206249
48 meter
Z = 16597916
01 Z = 5059044
80
XDOT = -19673
883964 XDOT = -5996
599832
YDOT = 13104
771932 feet/sec YDOT = 3994
334485 meter/sec
ZDOT = -5549
416998 ZDOT = -1691
462301
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 09081
74766860
00010596 00000-0 82463-4 0 9024
2 25544 51
6425 29
8474 0009040 148
1291 212
0420 15
71423723 32357
Satellite: ISS
Catalog Number: 25544
Epoch time: 09081
74766860 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 29
8474 deg
Eccentricity:
0009040
Arg of perigee: 148
1291 deg
Mean anomaly: 212
0420 deg
Mean motion: 15
71423723 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3235
Checksum: 291
Coasting Arc #4 (Orbit 3250)
---------------------------------------
Vector Time (GMT): 2009/082/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5896093
67 A = 6739316
20 meter
Y = 3204445
21 meter E =
0014707
Z = 606306
57 I = 51
79882
XDOT = -2767
331451 Wp = 88
74751
YDOT = 3932
236188 meter/sec RA = 24
44620 deg
ZDOT = 6004
074134 TA = 277
82761
MA = 277
99455
Ha = 196
736 n
mi
Hp = 185
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19344139
33 X = 5856877
52
Y = 10513271
69 feet Y = 3270159
55 meter
Z = 1989194
78 Z = 634853
91
XDOT = -9079
171427 XDOT = -2840
263067
YDOT = 12901
037362 feet/sec YDOT = 3900
883028 meter/sec
ZDOT = 19698
405952 ZDOT = 5990
453098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15553971
19 X = 4740850
42
Y = -15567328
36 feet Y = -4744921
68 meter
Z = 2100897
89 Z = 640353
68
XDOT = 8637
493661 XDOT = 2632
708068
YDOT = 11333
553612 feet/sec YDOT = 3454
467141 meter/sec
ZDOT = 19645
477905 ZDOT = 5987
941666
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 09082
76518462
00010596 00000-0 82463-4 0 9031
2 25544 51
6422 24
6415 0009073 152
2349 207
9299 15
71431663 32515
Satellite: ISS
Catalog Number: 25544
Epoch time: 09082
76518462 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 24
6415 deg
Eccentricity:
0009073
Arg of perigee: 152
2349 deg
Mean anomaly: 207
9299 deg
Mean motion: 15
71431663 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3251
Checksum: 306
Coasting Arc #5 (Orbit 3265)
---------------------------------------
Vector Time (GMT): 2009/083/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1129249
73 A = 6727412
18 meter
Y = -4024159
62 meter E =
0020259
Z = -5287343
84 I = 51
73079
XDOT = 7307
690312 Wp = 112
19871
YDOT = 2360
174123 meter/sec RA = 19
33407 deg
ZDOT = -243
797073 TA = 155
53315
MA = 155
43687
Ha = 196
612 n
mi
Hp = 185
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3704887
56 X = 1199849
38
Y = -13202623
42 feet Y = -4011137
49 meter
Z = -17346928
62 Z = -5281686
09
XDOT = 23975
361915 XDOT = 7281
939640
YDOT = 7743
353421 feet/sec YDOT = 2441
748972 meter/sec
ZDOT = -799
859162 ZDOT = -208
359393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11711797
87 X = -3569755
99
Y = -7185112
99 feet Y = -2190022
44 meter
Z = -17325106
96 Z = -5280692
60
XDOT = 13328
263437 XDOT = 4062
454696
YDOT = -20195
813013 feet/sec YDOT = -6155
683806 meter/sec
ZDOT = -661
310168 ZDOT = -201
567339
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 09083
71909371
00010596 00000-0 82463-4 0 9041
2 25544 51
6416 19
7606 0008985 155
7688 204
3898 15
71444797 32664
Satellite: ISS
Catalog Number: 25544
Epoch time: 09083
71909371 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 19
7606 deg
Eccentricity:
0008985
Arg of perigee: 155
7688 deg
Mean anomaly: 204
3898 deg
Mean motion: 15
71444797 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3266
Checksum: 355
Coasting Arc #6 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2009/084/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6594678
20 A = 6739060
29 meter
Y = -830623
66 meter E =
0021751
Z = 1032395
17 I = 51
74210
XDOT = -319
466645 Wp = 137
77355
YDOT = -4906
624241 meter/sec RA = 14
21413 deg
ZDOT = -5932
284645 TA = 30
95479
MA = 30
82677
Ha = 196
574 n
mi
Hp = 185
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21636083
33 X = -6589915
07
Y = -2725143
24 feet Y = -904342
45 meter
Z = 3387123
27 Z = 1000369
98
XDOT = -1048
118915 XDOT = -235
758322
YDOT = -16097
848561 feet/sec YDOT = -4909
729321 meter/sec
ZDOT = -19462
876133 ZDOT = -5933
632741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8048322
51 X = -2453128
70
Y = 20287998
94 feet Y = 6183782
08 meter
Z = 3262010
95 Z = 994260
94
XDOT = -14341
936573 XDOT = -4371
422267
YDOT = -2528
548629 feet/sec YDOT = -770
701622 meter/sec
ZDOT = -19468
471811 ZDOT = -5933
990208
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 09084
73658349
00010596 00000-0 82463-4 0 9051
2 25544 51
6421 14
5560 0009066 159
5734 200
5792 15
71436994 32826
Satellite: ISS
Catalog Number: 25544
Epoch time: 09084
73658349 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 14
5560 deg
Eccentricity:
0009066
Arg of perigee: 159
5734 deg
Mean anomaly: 200
5792 deg
Mean motion: 15
71436994 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3282
Checksum: 327
Coasting Arc #7 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2009/085/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1703619
43 A = 6728826
39 meter
Y = 4231387
78 meter E =
0014200
Z = 4943882
48 I = 51
67814
XDOT = -7388
786225 Wp = 146
94477
YDOT = 498
040721 meter/sec RA = 9
12881 deg
ZDOT = 2105
333899 TA = 282
57688
MA = 282
73566
Ha = 196
394 n
mi
Hp = 186
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5589302
59 X = 1632160
17
Y = 13882505
83 feet Y = 4250039
62 meter
Z = 16220086
87 Z = 4951984
66
XDOT = -24241
424624 XDOT = -7404
033608
YDOT = 1633
991866 feet/sec YDOT = 415
329977 meter/sec
ZDOT = 6907
263448 ZDOT = 2069
401994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14781231
67 X = 4505319
41
Y = -2107827
06 feet Y = -642465
69 meter
Z = 16252007
41 Z = 4953611
86
XDOT = -4224
856413 XDOT = -1287
736235
YDOT = 22915
059888 feet/sec YDOT = 6984
510254 meter/sec
ZDOT = 6766
993106 ZDOT = 2062
579499
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 09085
75405885
00010596 00000-0 82463-4 0 9060
2 25544 51
6414 9
3498 0008967 163
4159 196
7298 15
71438101 32980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09085
75405885 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 9
3498 deg
Eccentricity:
0008967
Arg of perigee: 163
4159 deg
Mean anomaly: 196
7298 deg
Mean motion: 15
71438101 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3298
Checksum: 350
Coasting Arc #8 (Orbit 3312)
---------------------------------------
Vector Time (GMT): 2009/086/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6009813
53 A = 6736501
29 meter
Y = -1629756
06 meter E =
0008073
Z = -2583845
09 I = 51
67399
XDOT = 3456
061991 Wp = 132
91811
YDOT = 4409
792502 meter/sec RA = 3
97559 deg
ZDOT = 5262
012561 TA = 197
83661
MA = 197
86497
Ha = 196
242 n
mi
Hp = 186
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19717235
98 X = 6040143
02
Y = -5346968
70 feet Y = -1562381
48 meter
Z = -8477182
04 Z = -2554575
37
XDOT = 11338
786060 XDOT = 3380
931985
YDOT = 14467
823169 feet/sec YDOT = 4448
020618 meter/sec
ZDOT = 17263
820738 ZDOT = 5278
619335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -944043
52 X = -287744
47
Y = -20454608
14 feet Y = -6234564
56 meter
Z = -8363006
15 Z = -2549044
27
XDOT = 15065
256053 XDOT = 4591
890045
YDOT = -7773
621497 feet/sec YDOT = -2369
399832 meter/sec
ZDOT = 17328
954430 ZDOT = 5281
865310
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 09086
70792737
00010596 00000-0 82463-4 0 9072
2 25544 51
6404 4
4687 0009008 168
1877 191
9498 15
71493026 33135
Satellite: ISS
Catalog Number: 25544
Epoch time: 09086
70792737 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 4
4687 deg
Eccentricity:
0009008
Arg of perigee: 168
1877 deg
Mean anomaly: 191
9498 deg
Mean motion: 15
71493026 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3313
Checksum: 337
Coasting Arc #9 (Orbit 3328)
---------------------------------------
Vector Time (GMT): 2009/087/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4193417
18 A = 6731635
80 meter
Y = -3221699
46 meter E =
0010816
Z = -4169088
44 I = 51
62759
XDOT = 6012
786275 Wp = 123
98949
YDOT = -3048
696634 meter/sec RA = 358
90691 deg
ZDOT = -3704
739417 TA = 108
16808
MA = 108
05029
Ha = 196
060 n
mi
Hp = 186
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13757930
38 X = -4136827
03
Y = -10569880
12 feet Y = -3268276
58 meter
Z = -13678111
67 Z = -4189322
59
XDOT = 19726
989090 XDOT = 6064
427577
YDOT = -10002
285544 feet/sec YDOT = -2981
169670 meter/sec
ZDOT = -12154
656881 ZDOT = -3675
403332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13086690
70 X = -3988823
33
Y = 11294614
85 feet Y = 3442598
61 meter
Z = -13757323
67 Z = -4193232
26
XDOT = -5027
692970 XDOT = -1532
440817
YDOT = -20440
292530 feet/sec YDOT = -6230
201163 meter/sec
ZDOT = -12040
317107 ZDOT = -3669
888654
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 09087
72537512
00010596 00000-0 82463-4 0 9084
2 25544 51
6395 359
2629 0008999 171
6810 188
4503 15
71514467 33293
Satellite: ISS
Catalog Number: 25544
Epoch time: 09087
72537512 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 359
2629 deg
Eccentricity:
0008999
Arg of perigee: 171
6810 deg
Mean anomaly: 188
4503 deg
Mean motion: 15
71514467 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3329
Checksum: 347
Coasting Arc #10 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2009/088/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4254577
28 A = 6732855
19 meter
Y = 3523057
94 meter E =
0013986
Z = 3833275
10 I = 51
60263
XDOT = -5931
045924 Wp = 121
37801
YDOT = -2651
502463 meter/sec RA = 353
73751 deg
ZDOT = -4142
075822 TA = 11
94891
MA = 11
91576
Ha = 195
987 n
mi
Hp = 186
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13958586
87 X = -4312278
07
Y = 11558589
05 feet Y = 3475158
32 meter
Z = 12576361
88 Z = 3812465
82
XDOT = -19458
812085 XDOT = -5880
833876
YDOT = -8699
155063 feet/sec YDOT = -2717
546302 meter/sec
ZDOT = -13589
487606 ZDOT = -4170
767099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8801666
65 X = 2682747
99
Y = 15906133
55 feet Y = 4848189
51 meter
Z = 12495342
57 Z = 3808580
42
XDOT = -10932
603118 XDOT = -3332
257430
YDOT = 16823
291876 feet/sec YDOT = 5127
739364 meter/sec
ZDOT = -13701
677382 ZDOT = -4176
271266
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 09088
74280770
00010596 00000-0 82463-4 0 9099
2 25544 51
6399 354
0566 0008981 176
7325 183
3897 15
71549202 33451
Satellite: ISS
Catalog Number: 25544
Epoch time: 09088
74280770 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 354
0566 deg
Eccentricity:
0008981
Arg of perigee: 176
7325 deg
Mean anomaly: 183
3897 deg
Mean motion: 15
71549202 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3345
Checksum: 350
Coasting Arc #11 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2009/089/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5905464
71 A = 6735121
66 meter
Y = 1236167
50 meter E =
0015232
Z = 2991365
87 I = 51
58033
XDOT = -3513
313386 Wp = 120
07161
YDOT = 4716
751366 meter/sec RA = 348
66651 deg
ZDOT = 4960
402955 TA = 274
46655
MA = 274
64055
Ha = 195
800 n
mi
Hp = 186
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19374884
22 X = 5876671
11
Y = 4055667
64 feet Y = 1302044
90 meter
Z = 9814192
49 Z = 3019984
94
XDOT = -11526
618719 XDOT = -3589
892745
YDOT = 15474
906056 feet/sec YDOT = 4677
035349 meter/sec
ZDOT = 16274
287909 ZDOT = 4943
149025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7200664
77 X = 2194762
62
Y = -18378730
28 feet Y = -5601836
99 meter
Z = 9926008
93 Z = 3025447
52
XDOT = 11995
418081 XDOT = 3656
203431
YDOT = 13499
019958 feet/sec YDOT = 4114
501283 meter/sec
ZDOT = 16207
221892 ZDOT = 4939
961233
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 09089
76022726
00010596 00000-0 82463-4 0 9109
2 25544 51
6387 348
8497 0009153 180
2538 179
8621 15
71576155 33610
Satellite: ISS
Catalog Number: 25544
Epoch time: 09089
76022726 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 348
8497 deg
Eccentricity:
0009153
Arg of perigee: 180
2538 deg
Mean anomaly: 179
8621 deg
Mean motion: 15
71576155 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3361
Checksum: 339
Coasting Arc #12 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2009/090/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1785246
47 A = 6729434
32 meter
Y = -4451946
81 meter E =
0016356
Z = -4734224
08 I = 51
53198
XDOT = 7211
927717 Wp = 141
01454
YDOT = 62
266142 meter/sec RA = 343
49773 deg
ZDOT = 2653
501069 TA = 155
19309
MA = 155
11436
Ha = 195
758 n
mi
Hp = 186
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5857107
86 X = 1857894
33
Y = -14606124
69 feet Y = -4431576
93 meter
Z = -15532231
23 Z = -4725374
86
XDOT = 23661
180174 XDOT = 7197
805139
YDOT = 204
285244 feet/sec YDOT = 142
835148 meter/sec
ZDOT = 8705
712170 ZDOT = 2688
502501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13559500
11 X = -4132935
63
Y = -8052824
94 feet Y = -2454501
04 meter
Z = -15497960
03 Z = -4723778
22
XDOT = 3126
040168 XDOT = 952
817043
YDOT = -22328
744305 feet/sec YDOT = -6805
801264 meter/sec
ZDOT = 8842
376198 ZDOT = 2695
156265
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 09090
71404655
00010596 00000-0 82463-4 0 9112
2 25544 51
6385 343
9678 0009166 182
6380 177
4735 15
71577685 33765
Satellite: ISS
Catalog Number: 25544
Epoch time: 09090
71404655 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 343
9678 deg
Eccentricity:
0009166
Arg of perigee: 182
6380 deg
Mean anomaly: 177
4735 deg
Mean motion: 15
71577685 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3376
Checksum: 347
Coasting Arc #13 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2009/091/16:52:03
644
Vector Time (MET): N/A
Weight (LBS) : 638776
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6428132
56 A = 6737769
38 meter
Y = 1168349
13 meter E =
0015603
Z = -1609872
07 I = 51
53301
XDOT = 503
515248 Wp = 165
63719
YDOT = -5106
581875 meter/sec RA = 338
40906 deg
ZDOT = -5743
258326 TA = 32
15509
MA = 32
06003
Ha = 195
408 n
mi
Hp = 186
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21089673
76 X = -6432899
02
Y = 3833166
43 feet Y = 1096439
37 meter
Z = -5281732
52 Z = -1641111
51
XDOT = 1651
952913 XDOT = 588
480189
YDOT = -16753
877543 feet/sec YDOT = -5100
476154 meter/sec
ZDOT = -18842
711044 ZDOT = -5740
605920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1026712
16 X = 312941
87
Y = 21380149
52 feet Y = 6516669
57 meter
Z = -5403635
02 Z = -1647027
95
XDOT = -14817
237948 XDOT = -4516
294126
YDOT = -4026
597418 feet/sec YDOT = -1227
306893 meter/sec
ZDOT = -18832
675360 ZDOT = -5740
199450
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 09091
73143833
00010596 00000-0 82463-4 0 9124
2 25544 51
6387 338
7617 0008961 186
7122 173
3921 15
71624246 33929
Satellite: ISS
Catalog Number: 25544
Epoch time: 09091
73143833 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 338
7617 deg
Eccentricity:
0008961
Arg of perigee: 186
7122 deg
Mean anomaly: 173
3921 deg
Mean motion: 15
71624246 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3392
Checksum: 323
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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