Date:
January 11th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
014/18:07:10
671 6
6 9
7 9
7
N/A 5
3 0
0 193
5
000/00:02:17
342 4
8 -0
0 192
8
Coasting Arc #1 (Orbit 2068)
---------------------------------------
Vector Time (GMT): 2009/007/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3251511
52 A = 6736551
95 meter
Y = 5663570
69 meter E =
0013855
Z = 1641560
75 I = 51
90608
XDOT = -4971
069374 Wp = 90
50386
YDOT = 1173
525565 meter/sec RA = 48
77478 deg
ZDOT = 5755
934399 TA = 287
54095
MA = 287
69229
Ha = 194
548 n
mi
Hp = 185
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10667688
71 X = 3179964
46
Y = 18581268
67 feet Y = 5699530
71 meter
Z = 5385698
01 Z = 1657183
63
XDOT = -16309
282724 XDOT = -5011
783808
YDOT = 3850
149492 feet/sec YDOT = 1117
707739 meter/sec
ZDOT = 18884
299210 ZDOT = 5731
686161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12664516
74 X = -3860144
70
Y = 17262989
49 feet Y = 5261759
20 meter
Z = 5446841
34 Z = 1660197
24
XDOT = -8924
010614 XDOT = -2720
038435
YDOT = -12518
166473 feet/sec YDOT = -3815
537141 meter/sec
ZDOT = 18789
998048 ZDOT = 5727
191405
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 09007
58116526
00010596 00000-0 82463-4 0 9000
2 25544 51
6413 49
0351 0006508 169
5856 190
5442 15
72045418 20692
Satellite: ISS
Catalog Number: 25544
Epoch time: 09007
58116526 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 49
0351 deg
Eccentricity:
0006508
Arg of perigee: 169
5856 deg
Mean anomaly: 190
5442 deg
Mean motion: 15
72045418 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2069
Checksum: 302
Coasting Arc #2 (Orbit 2083)
---------------------------------------
Vector Time (GMT): 2009/008/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3789018
76 A = 6726088
40 meter
Y = -2020670
83 meter E =
0017130
Z = -5191032
40 I = 51
85173
XDOT = 4796
509089 Wp = 120
88643
YDOT = 5883
148210 meter/sec RA = 43
64513 deg
ZDOT = 1205
293775 TA = 160
64882
MA = 160
58370
Ha = 194
397 n
mi
Hp = 186
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12431163
90 X = 3836549
64
Y = -6629497
47 feet Y = -1978033
22 meter
Z = -17030946
20 Z = -5172510
28
XDOT = 15736
578375 XDOT = 4724
511190
YDOT = 19301
667357 feet/sec YDOT = 5936
382795 meter/sec
ZDOT = 3954
375903 ZDOT = 1228
421229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11293539
06 X = 3442270
70
Y = 8566585
11 feet Y = 2611095
14 meter
Z = -16958973
92 Z = -5169095
25
XDOT = -10253
990068 XDOT = -3125
416173
YDOT = 21562
302997 feet/sec YDOT = 6572
189954 meter/sec
ZDOT = 4044
737616 ZDOT = 1232
836025
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 09008
53466622
00010596 00000-0 82463-4 0 9012
2 25544 51
6424 44
1524 0006559 174
7184 185
4048 15
72080415 20848
Satellite: ISS
Catalog Number: 25544
Epoch time: 09008
53466622 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 44
1524 deg
Eccentricity:
0006559
Arg of perigee: 174
7184 deg
Mean anomaly: 185
4048 deg
Mean motion: 15
72080415 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2084
Checksum: 300
Coasting Arc #3 (Orbit 2099)
---------------------------------------
Vector Time (GMT): 2009/009/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5016957
20 A = 6737447
11 meter
Y = -4459129
82 meter E =
0016837
Z = -458954
23 I = 51
86709
XDOT = 3470
400010 Wp = 152
44502
YDOT = -3293
755517 meter/sec RA = 38
55411 deg
ZDOT = -6036
370388 TA = 32
53025
MA = 32
42662
Ha = 194
260 n
mi
Hp = 186
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16459833
34 X = -4964492
11
Y = -14629691
02 feet Y = -4514938
92 meter
Z = -1505755
36 Z = -483199
70
XDOT = 11385
826804 XDOT = 3536
296688
YDOT = -10806
284504 feet/sec YDOT = -3254
577999 meter/sec
ZDOT = -19804
364790 ZDOT = -6019
351865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5967632
61 X = 1818934
42
Y = -21190738
29 feet Y = -6458937
03 meter
Z = -1600388
63 Z = -487798
45
XDOT = 13200
759257 XDOT = 4023
591421
YDOT = 5184
431469 feet/sec YDOT = 1580
214712 meter/sec
ZDOT = -19738
311479 ZDOT = -6016
237339
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 09009
55171987
00010596 00000-0 82463-4 0 9023
2 25544 51
6413 38
9438 0006584 177
3254 182
7945 15
72114852 21004
Satellite: ISS
Catalog Number: 25544
Epoch time: 09009
55171987 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 38
9438 deg
Eccentricity:
0006584
Arg of perigee: 177
3254 deg
Mean anomaly: 182
7945 deg
Mean motion: 15
72114852 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2100
Checksum: 317
Coasting Arc #4 (Orbit 2115)
---------------------------------------
Vector Time (GMT): 2009/010/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2120977
64 A = 6725376
40 meter
Y = 3579861
76 meter E =
0007147
Z = 5281791
19 I = 51
80210
XDOT = -6500
000254 Wp = 160
83357
YDOT = -4124
522069 meter/sec RA = 33
44312 deg
ZDOT = 178
644986 TA = 287
43569
MA = 287
51382
Ha = 194
138 n
mi
Hp = 186
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6958588
07 X = -2186508
13
Y = 11744953
30 feet Y = 3555776
49 meter
Z = 17328711
25 Z = 5271329
08
XDOT = -21325
460152 XDOT = -6454
263887
YDOT = -13531
896552 feet/sec YDOT = -4196
953141 meter/sec
ZDOT = 586
105598 ZDOT = 147
178962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13667800
60 X = -4165945
62
Y = -979683
44 feet Y = -298607
51 meter
Z = 17288191
24 Z = 5269440
69
XDOT = 2344
694396 XDOT = 714
662852
YDOT = -24146
489790 feet/sec YDOT = -7359
850088 meter/sec
ZDOT = 463
377185 ZDOT = 141
237366
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 09010
56875692
00010596 00000-0 82463-4 0 9031
2 25544 51
6404 33
7349 0006472 180
9289 179
1862 15
72150365 21166
Satellite: ISS
Catalog Number: 25544
Epoch time: 09010
56875692 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 33
7349 deg
Eccentricity:
0006472
Arg of perigee: 180
9289 deg
Mean anomaly: 179
1862 deg
Mean motion: 15
72150365 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2116
Checksum: 317
Coasting Arc #5 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2009/011/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6150407
87 A = 6737014
89 meter
Y = 2643497
22 meter E =
0006476
Z = -751834
72 I = 51
81713
XDOT = -1276
518353 Wp = 75
50677
YDOT = 4659
798780 meter/sec RA = 28
32556 deg
ZDOT = 5985
903524 TA = 276
33054
MA = 276
40430
Ha = 193
919 n
mi
Hp = 186
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20178503
51 X = 6124042
93
Y = 8672891
13 feet Y = 2712127
33 meter
Z = -2466649
34 Z = -722020
43
XDOT = -4188
052338 XDOT = -1357
607848
YDOT = 15288
053741 feet/sec YDOT = 4645
069782 meter/sec
ZDOT = 19638
791090 ZDOT = 5979
506036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1779929
81 X = 542522
61
Y = 21903943
52 feet Y = 6676321
98 meter
Z = -2350428
03 Z = -716410
46
XDOT = -13927
229798 XDOT = -4245
019642
YDOT = 3220
065792 feet/sec YDOT = 981
476053 meter/sec
ZDOT = 19614
155936 ZDOT = 5978
394729
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 09011
52221458
00010596 00000-0 82463-4 0 9044
2 25544 51
6409 28
8523 0006587 184
4305 175
6800 15
72220337 21312
Satellite: ISS
Catalog Number: 25544
Epoch time: 09011
52221458 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 28
8523 deg
Eccentricity:
0006587
Arg of perigee: 184
4305 deg
Mean anomaly: 175
6800 deg
Mean motion: 15
72220337 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2131
Checksum: 286
Coasting Arc #6 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2009/012/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 61205
54 A = 6725974
80 meter
Y = -4368910
29 meter E =
0013203
Z = -5123592
03 I = 51
75226
XDOT = 7310
869488 Wp = 105
56196
YDOT = 1852
495860 meter/sec RA = 23
23247 deg
ZDOT = -1498
955394 TA = 150
10362
MA = 150
02814
Ha = 193
794 n
mi
Hp = 186
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 200805
58 X = 134943
68
Y = -14333695
18 feet Y = -4367813
02 meter
Z = -16809685
14 Z = -5123116
06
XDOT = 23985
792284 XDOT = 7296
892678
YDOT = 6077
742324 feet/sec YDOT = 1934
172250 meter/sec
ZDOT = -4917
832659 ZDOT = -1463
473887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12695530
64 X = 3869597
74
Y = -6661254
68 feet Y = -2030350
43 meter
Z = -16808088
61 Z = -5123105
41
XDOT = 5788
574789 XDOT = 1764
357596
YDOT = 23037
338344 feet/sec YDOT = 7021
780727 meter/sec
ZDOT = -4779
588256 ZDOT = -1456
818501
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 09012
53922041
00010596 00000-0 82463-4 0 9053
2 25544 51
6400 23
6425 0006381 188
9109 171
1941 15
72186037 21472
Satellite: ISS
Catalog Number: 25544
Epoch time: 09012
53922041 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 23
6425 deg
Eccentricity:
0006381
Arg of perigee: 188
9109 deg
Mean anomaly: 171
1941 deg
Mean motion: 15
72186037 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2147
Checksum: 285
Coasting Arc #7 (Orbit 2162)
---------------------------------------
Vector Time (GMT): 2009/013/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6439163
77 A = 6735755
99 meter
Y = -562162
95 meter E =
0016477
Z = 1858816
57 I = 51
75765
XDOT = -1196
040952 Wp = 135
23714
YDOT = -5085
402601 meter/sec RA = 18
08925 deg
ZDOT = -5662
440855 TA = 24
15959
MA = 24
08240
Ha = 193
594 n
mi
Hp = 186
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21125865
38 X = -6441428
56
Y = -1844366
63 feet Y = -634182
21 meter
Z = 6098479
58 Z = 1827530
37
XDOT = -3924
018872 XDOT = -1111
579842
YDOT = -16684
391734 feet/sec YDOT = -5098
304764 meter/sec
ZDOT = -18577
561861 ZDOT = -5668
046294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8936397
37 X = -2723813
92
Y = -19269558
26 feet Y = -5873361
36 meter
Z = 5976642
52 Z = 1821680
64
XDOT = 11163
902547 XDOT = 3402
757496
YDOT = -10965
705382 feet/sec YDOT = -3342
347000 meter/sec
ZDOT = -18599
687157 ZDOT = -5669
184645
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 09013
55620955
00010596 00000-0 82463-4 0 9066
2 25544 51
6397 18
4331 0006194 192
8879 167
2126 15
72239161 21631
Satellite: ISS
Catalog Number: 25544
Epoch time: 09013
55620955 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 18
4331 deg
Eccentricity:
0006194
Arg of perigee: 192
8879 deg
Mean anomaly: 167
2126 deg
Mean motion: 15
72239161 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2163
Checksum: 317
Coasting Arc #8 (Orbit 2178)
---------------------------------------
Vector Time (GMT): 2009/014/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2130901
44 A = 6727503
65 meter
Y = 4307872
82 meter E =
0010756
Z = 4707424
56 I = 51
70139
XDOT = -7175
923528 Wp = 152
57996
YDOT = 554
083594 meter/sec RA = 13
01126 deg
ZDOT = 2729
426581 TA = 270
49755
MA = 270
62080
Ha = 193
351 n
mi
Hp = 186
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6991146
47 X = 2059704
41
Y = 14133441
00 feet Y = 4331303
47 meter
Z = 15444306
30 Z = 4717603
53
XDOT = -23543
056195 XDOT = -7194
844823
YDOT = 1817
859562 feet/sec YDOT = 473
732324 meter/sec
ZDOT = 8954
811619 ZDOT = 2694
520780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8595359
46 X = -2619865
56
Y = 13172564
15 feet Y = 4014997
55 meter
Z = 15484192
90 Z = 4719582
00
XDOT = -12697
997713 XDOT = -3870
349703
YDOT = -18697
778552 feet/sec YDOT = -5699
082903 meter/sec
ZDOT = 8818
951275 ZDOT = 2688
016349
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 09014
57318267
00010596 00000-0 82463-4 0 9070
2 25544 51
6394 13
2240 0006242 197
7919 162
3026 15
72246459 21793
Satellite: ISS
Catalog Number: 25544
Epoch time: 09014
57318267 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 13
2240 deg
Eccentricity:
0006242
Arg of perigee: 197
7919 deg
Mean anomaly: 162
3026 deg
Mean motion: 15
72246459 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2179
Checksum: 313
Coasting Arc #9 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2009/014/18:08:19
342
Vector Time (MET): N/A
Weight (LBS) : 639553
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5185869
89 A = 6736196
04 meter
Y = -1992404
45 meter E =
0003079
Z = -3809820
60 I = 51
70970
XDOT = 4754
529509 Wp = 221
17743
YDOT = 4364
853428 meter/sec RA = 11
76293 deg
ZDOT = 4184
942339 TA = 92
72055
MA = 92
68530
Ha = 193
480 n
mi
Hp = 192
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17014008
82 X = 5226270
89
Y = -6536760
00 feet Y = -1934186
97 meter
Z = -12499411
42 Z = -3784530
13
XDOT = 15598
850095 XDOT = 4685
038367
YDOT = 14320
385262 feet/sec YDOT = 4417
632595 meter/sec
ZDOT = 13730
125784 ZDOT = 4207
870772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12570377
62 X = 3831451
10
Y = -13290599
40 feet Y = -4050974
70 meter
Z = -12401072
02 Z = -3779846
75
XDOT = 19220
840252 XDOT = 5858
512109
YDOT = 5271
633591 feet/sec YDOT = 1606
793919 meter/sec
ZDOT = 13819
651159 ZDOT = 4212
229673
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 09014
76386230
00010596 00000-0 82463-4 0 9087
2 25544 51
6430 12
2481 0008028 264
0696 95
9550 15
70420874 21824
Satellite: ISS
Catalog Number: 25544
Epoch time: 09014
76386230 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 12
2481 deg
Eccentricity:
0008028
Arg of perigee: 264
0696 deg
Mean anomaly: 95
9550 deg
Mean motion: 15
70420874 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2182
Checksum: 301
Coasting Arc #10 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2009/015/18:08:19
342
Vector Time (MET): N/A
Weight (LBS) : 639553
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5469008
72 A = 6739056
51 meter
Y = -2821834
00 meter E =
0004915
Z = -2738857
44 I = 51
69110
XDOT = 4437
368167 Wp = 235
32191
YDOT = -3585
112023 meter/sec RA = 6
70775 deg
ZDOT = -5163
106620 TA = 335
88770
MA = 335
91070
Ha = 192
819 n
mi
Hp = 192
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17942942
00 X = -5423743
39
Y = -9257985
55 feet Y = -2882738
43 meter
Z = -8985752
75 Z = -2765315
61
XDOT = 14558
294511 XDOT = 4502
208710
YDOT = -11762
178553 feet/sec YDOT = -3535
128054 meter/sec
ZDOT = -16939
326181 ZDOT = -5141
392886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20142772
47 X = -6139517
05
Y = -251758
40 feet Y = -76735
96 meter
Z = -9088924
66 Z = -2770304
24
XDOT = 7806
151690 XDOT = 2379
315035
YDOT = -15616
809891 feet/sec YDOT = -4760
003655 meter/sec
ZDOT = -16855
010004 ZDOT = -5137
407049
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 09015
78200955
00010596 00000-0 82463-4 0 9090
2 25544 51
6435 7
0474 0008149 267
6899 92
3330 15
70421279 21985
Satellite: ISS
Catalog Number: 25544
Epoch time: 09015
78200955 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 7
0474 deg
Eccentricity:
0008149
Arg of perigee: 267
6899 deg
Mean anomaly: 92
3330 deg
Mean motion: 15
70421279 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2198
Checksum: 325
Coasting Arc #11 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2009/016/18:08:19
342
Vector Time (MET): N/A
Weight (LBS) : 639553
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2259544
69 A = 6731374
81 meter
Y = 3900248
79 meter E =
0004910
Z = 5003310
14 I = 51
63637
XDOT = -7244
663845 Wp = 316
92415
YDOT = -1722
926705 meter/sec RA = 1
56240 deg
ZDOT = -1926
273080 TA = 151
71535
MA = 151
68868
Ha = 192
865 n
mi
Hp = 192
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7413204
37 X = -2327294
85
Y = 12796091
81 feet Y = 3874602
22 meter
Z = 16415059
50 Z = 4992169
01
XDOT = -23768
582167 XDOT = -7215
501987
YDOT = -5652
646670 feet/sec YDOT = -1803
777604 meter/sec
ZDOT = -6319
793569 ZDOT = -1961
396455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -717130
87 X = -218581
49
Y = 14818759
25 feet Y = 4516757
82 meter
Z = 16371922
33 Z = 4990161
93
XDOT = -22566
314058 XDOT = -6878
212525
YDOT = 6050
048295 feet/sec YDOT = 1844
054720 meter/sec
ZDOT = -6456
628819 ZDOT = -1967
980464
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 09016
80014009
00010596 00000-0 82463-4 0 9109
2 25544 51
6435 1
8465 0008163 272
4549 87
5677 15
70500627 22143
Satellite: ISS
Catalog Number: 25544
Epoch time: 09016
80014009 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 1
8465 deg
Eccentricity:
0008163
Arg of perigee: 272
4549 deg
Mean anomaly: 87
5677 deg
Mean motion: 15
70500627 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2214
Checksum: 292
Coasting Arc #12 (Orbit 2229)
---------------------------------------
Vector Time (GMT): 2009/017/18:08:19
342
Vector Time (MET): N/A
Weight (LBS) : 639553
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6712048
89 A = 6742029
09 meter
Y = 33253
85 meter E =
0009404
Z = 563468
77 I = 51
64299
XDOT = -528
400879 Wp = 13
47171
YDOT = 4790
216957 meter/sec RA = 356
47468 deg
ZDOT = 6000
563809 TA = 352
65221
MA = 352
66599
Ha = 193
383 n
mi
Hp = 192
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22021157
77 X = 6708440
98
Y = 109100
55 feet Y = 108291
67 meter
Z = 1848650
83 Z = 596066
83
XDOT = -1733
598685 XDOT = -611
075969
YDOT = 15715
934898 feet/sec YDOT = 4783
845485 meter/sec
ZDOT = 19686
889137 ZDOT = 5997
796307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19373915
96 X = 5905169
59
Y = -10445543
58 feet Y = -3183801
68 meter
Z = 1975551
07 Z = 602147
96
XDOT = 5143
812945 XDOT = 1567
834186
YDOT = 13268
297982 feet/sec YDOT = 4044
177225 meter/sec
ZDOT = 19676
401507 ZDOT = 5997
367179
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 09017
81825698
00010596 00000-0 82463-4 0 9116
2 25544 51
6436 356
6449 0008123 276
3025 83
7211 15
70490133 22305
Satellite: ISS
Catalog Number: 25544
Epoch time: 09017
81825698 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 356
6449 deg
Eccentricity:
0008123
Arg of perigee: 276
3025 deg
Mean anomaly: 83
7211 deg
Mean motion: 15
70490133 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2230
Checksum: 301
Coasting Arc #13 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2009/018/18:08:19
342
Vector Time (MET): N/A
Weight (LBS) : 639553
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1354232
89 A = 6730124
19 meter
Y = -4002563
29 meter E =
0007263
Z = -5244376
78 I = 51
57387
XDOT = 7479
185828 Wp = 68
07721
YDOT = -1664
703197 meter/sec RA = 351
36339 deg
ZDOT = -658
864904 TA = 195
63322
MA = 195
65566
Ha = 193
677 n
mi
Hp = 192
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4443021
29 X = -1283898
91
Y = -13131769
32 feet Y = -4017313
48 meter
Z = -17205960
56 Z = -5250785
03
XDOT = 24538
011246 XDOT = 7500
445563
YDOT = -5461
624661 feet/sec YDOT = -1580
947687 meter/sec
ZDOT = -2161
630261 ZDOT = -622
479810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10263502
98 X = -3128315
71
Y = -9272382
70 feet Y = -2826222
25 meter
Z = -17231143
54 Z = -5252052
55
XDOT = 17971
908416 XDOT = 5477
837685
YDOT = -16127
148645 feet/sec YDOT = -4915
554907 meter/sec
ZDOT = -2020
089671 ZDOT = -615
723332
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 09018
77272607
00010596 00000-0 82463-4 0 9129
2 25544 51
6434 351
7689 0008148 280
1514 79
8728 15
70532885 22454
Satellite: ISS
Catalog Number: 25544
Epoch time: 09018
77272607 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 351
7689 deg
Eccentricity:
0008148
Arg of perigee: 280
1514 deg
Mean anomaly: 79
8728 deg
Mean motion: 15
70532885 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2245
Checksum: 333
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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