Date:
March 29th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19568 79 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 1014)
---------------------------------------
Vector Time (GMT): 2010/083/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5142191
25 A = 6727512
93 meter
Y = -2608544
33 meter E =
0018156
Z = 3451726
33 I = 51
36911
XDOT = 106
612086 Wp = 94
39772
YDOT = 6232
885940 meter/sec RA = 304
52030 deg
ZDOT = 4529
690867 TA = 306
71238
MA = 306
87902
Ha = 192
467 n
mi
Hp = 181
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16870706
18 X = 5154210
60
Y = -8558216
31 feet Y = -2550973
97 meter
Z = 11324561
44 Z = 3476736
08
XDOT = 349
777185 XDOT = 14
902750
YDOT = 20449
100853 feet/sec YDOT = 6233
565515 meter/sec
ZDOT = 14861
190510 ZDOT = 4529
985818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13050390
51 X = 3977759
03
Y = -13612238
54 feet Y = -4149010
31 meter
Z = 11423824
01 Z = 3481981
56
XDOT = 5986
328513 XDOT = 1824
632931
YDOT = 18271
860287 feet/sec YDOT = 5569
263015 meter/sec
ZDOT = 14862
503176 ZDOT = 4530
090968
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 10083
60645148
00016717 00000-0 10270-3 0 9003
2 25544 51
6438 304
8250 0005871 100
7471 259
4354 15
73785969 10151
Satellite: ISS
Catalog Number: 25544
Epoch time: 10083
60645148 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 304
8250 deg
Eccentricity:
0005871
Arg of perigee: 100
7471 deg
Mean anomaly: 259
4354 deg
Mean motion: 15
73785969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1015
Checksum: 308
Coasting Arc #2 (Orbit 1029)
---------------------------------------
Vector Time (GMT): 2010/084/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -630846
88 A = 6725785
35 meter
Y = -5389799
23 meter E =
0013044
Z = -3986960
36 I = 51
34636
XDOT = 5585
234508 Wp = 106
36964
YDOT = -3546
709879 meter/sec RA = 299
31369 deg
ZDOT = 3917
892154 TA = 204
32706
MA = 204
38869
Ha = 192
518 n
mi
Hp = 181
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2069707
61 X = -551162
63
Y = -17683068
34 feet Y = -5396408
41 meter
Z = -13080578
60 Z = -3989831
13
XDOT = 18324
260196 XDOT = 5605
447200
YDOT = -11636
187267 feet/sec YDOT = -3484
139243 meter/sec
ZDOT = 12853
976883 ZDOT = 3945
074122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7977202
42 X = -2431451
30
Y = -15907137
55 feet Y = -4848495
52 meter
Z = -13092110
16 Z = -3990475
18
XDOT = 11946
999779 XDOT = 3641
445533
YDOT = -16640
434673 feet/sec YDOT = -5072
004488 meter/sec
ZDOT = 12961
842406 ZDOT = 3950
769565
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 10084
55891704
00016717 00000-0 10270-3 0 9010
2 25544 51
6428 299
9345 0005976 104
8516 255
3310 15
73817647 10303
Satellite: ISS
Catalog Number: 25544
Epoch time: 10084
55891704 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 299
9345 deg
Eccentricity:
0005976
Arg of perigee: 104
8516 deg
Mean anomaly: 255
3310 deg
Mean motion: 15
73817647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1030
Checksum: 317
Coasting Arc #3 (Orbit 1045)
---------------------------------------
Vector Time (GMT): 2010/085/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4591098
72 A = 6727421
50 meter
Y = 3542679
33 meter E =
0010818
Z = -3417856
43 I = 51
33801
XDOT = -1283
385947 Wp = 98
23027
YDOT = -6056
053053 meter/sec RA = 294
21018 deg
ZDOT = -4567
150040 TA = 122
33122
MA = 122
22643
Ha = 192
409 n
mi
Hp = 181
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15062659
84 X = -4613769
28
Y = 11622963
69 feet Y = 3491211
91 meter
Z = -11213439
72 Z = -3440215
01
XDOT = -4210
583814 XDOT = -1193
384621
YDOT = -19868
940461 feet/sec YDOT = -6069
901773 meter/sec
ZDOT = -14984
088058 ZDOT = -4573
165551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9781509
75 X = -2981404
17
Y = 16257362
17 feet Y = 4955243
99 meter
Z = -11302144
89 Z = -3444893
76
XDOT = -9839
894221 XDOT = -2999
199758
YDOT = -16322
657627 feet/sec YDOT = -4975
146045 meter/sec
ZDOT = -15008
135471 ZDOT = -4574
479691
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 10085
57485754
00016717 00000-0 10270-3 0 9028
2 25544 51
6421 294
7190 0005974 107
7942 252
3873 15
73858407 10467
Satellite: ISS
Catalog Number: 25544
Epoch time: 10085
57485754 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 294
7190 deg
Eccentricity:
0005974
Arg of perigee: 107
7942 deg
Mean anomaly: 252
3873 deg
Mean motion: 15
73858407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1046
Checksum: 329
Coasting Arc #4 (Orbit 1061)
---------------------------------------
Vector Time (GMT): 2010/086/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1611376
63 A = 6725503
19 meter
Y = 5151673
57 meter E =
0015979
Z = 3998282
09 I = 51
32025
XDOT = -4858
580002 Wp = 89
76378
YDOT = 4548
060902 meter/sec RA = 289
00134 deg
ZDOT = -3888
519782 TA = 40
55428
MA = 40
43534
Ha = 192
273 n
mi
Hp = 181
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5286668
75 X = 1534227
23
Y = 16901816
18 feet Y = 5169261
99 meter
Z = 13117723
38 Z = 4005922
14
XDOT = -15940
223103 XDOT = -4890
186623
YDOT = 14921
459653 feet/sec YDOT = 4493
552251 meter/sec
ZDOT = -12757
610833 ZDOT = -3912
199721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11203539
26 X = 3414838
77
Y = 13685768
77 feet Y = 4171422
32 meter
Z = 13148207
65 Z = 4007573
69
XDOT = -8061
703492 XDOT = -2457
207224
YDOT = 18988
518684 feet/sec YDOT = 5787
700495 meter/sec
ZDOT = -12851
530025 ZDOT = -3917
146352
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 10086
59077402
00016717 00000-0 10270-3 0 9039
2 25544 51
6419 289
5022 0005833 112
8303 247
3477 15
73886033 10620
Satellite: ISS
Catalog Number: 25544
Epoch time: 10086
59077402 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 289
5022 deg
Eccentricity:
0005833
Arg of perigee: 112
8303 deg
Mean anomaly: 247
3477 deg
Mean motion: 15
73886033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1062
Checksum: 303
Coasting Arc #5 (Orbit 1077)
---------------------------------------
Vector Time (GMT): 2010/087/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3856795
82 A = 6727335
29 meter
Y = -4351221
80 meter E =
0018000
Z = 3371092
64 I = 51
31735
XDOT = 2386
355341 Wp = 98
70058
YDOT = 5699
376756 meter/sec RA = 283
89434 deg
ZDOT = 4602
656309 TA = 301
28035
MA = 301
45651
Ha = 192
180 n
mi
Hp = 181
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12653529
61 X = 3888789
26
Y = -14275662
06 feet Y = -4307913
53 meter
Z = 11060015
23 Z = 3389907
05
XDOT = 7829
249805 XDOT = 2300
087801
YDOT = 18698
742638 feet/sec YDOT = 5725
580589 meter/sec
ZDOT = 15100
578441 ZDOT = 4614
038940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5959073
14 X = 1816325
49
Y = -18075956
18 feet Y = -5509551
44 meter
Z = 11134609
62 Z = 3393829
01
XDOT = 13152
837763 XDOT = 4008
984950
YDOT = 13713
222152 feet/sec YDOT = 4179
790112 meter/sec
ZDOT = 15145
948265 ZDOT = 4616
485031
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 10087
60666702
00016717 00000-0 10270-3 0 9040
2 25544 51
6409 284
2852 0005913 117
4229 242
7536 15
73941556 10783
Satellite: ISS
Catalog Number: 25544
Epoch time: 10087
60666702 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 284
2852 deg
Eccentricity:
0005913
Arg of perigee: 117
4229 deg
Mean anomaly: 242
7536 deg
Mean motion: 15
73941556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1078
Checksum: 317
Coasting Arc #6 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2010/088/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2527380
65 A = 6725233
56 meter
Y = -4775300
46 meter E =
0013277
Z = -4019074
66 I = 51
30457
XDOT = 3950
668738 Wp = 113
83150
YDOT = -5342
784311 meter/sec RA = 278
68341 deg
ZDOT = 3868
517088 TA = 196
28622
MA = 196
32893
Ha = 192
232 n
mi
Hp = 181
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8291931
28 X = -2454270
61
Y = -15666996
26 feet Y = -4803154
83 meter
Z = -13185940
48 Z = -4031174
53
XDOT = 12961
511607 XDOT = 3991
326530
YDOT = -17528
819917 feet/sec YDOT = -5298
377801 meter/sec
ZDOT = 12691
985197 ZDOT = 3887
808810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13904449
25 X = -4238076
13
Y = -10936355
43 feet Y = -3333401
14 meter
Z = -13234135
55 Z = -4033764
51
XDOT = 3791
300096 XDOT = 1155
588269
YDOT = -20252
399814 feet/sec YDOT = -6172
931463 meter/sec
ZDOT = 12768
440458 ZDOT = 3891
820652
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 10088
55904627
00016717 00000-0 10270-3 0 9057
2 25544 51
6411 279
3939 0006061 120
2359 239
9405 15
73958858 10931
Satellite: ISS
Catalog Number: 25544
Epoch time: 10088
55904627 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 279
3939 deg
Eccentricity:
0006061
Arg of perigee: 120
2359 deg
Mean anomaly: 239
9405 deg
Mean motion: 15
73958858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1093
Checksum: 332
Coasting Arc #7 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2010/089/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3045908
06 A = 6727027
48 meter
Y = 4937345
35 meter E =
0010494
Z = -3411159
36 I = 51
30812
XDOT = -3342
362863 Wp = 106
83312
YDOT = -5209
710837 meter/sec RA = 273
57559 deg
ZDOT = -4570
705251 TA = 113
66332
MA = 113
55315
Ha = 192
079 n
mi
Hp = 181
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9993136
69 X = -3084321
08
Y = 16198639
60 feet Y = 4903069
06 meter
Z = -11191467
71 Z = -3426050
27
XDOT = -10965
757423 XDOT = -3261
654750
YDOT = -17092
227157 feet/sec YDOT = -5246
636340 meter/sec
ZDOT = -14995
752135 ZDOT = -4586
745950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2107887
64 X = -642484
15
Y = 18880988
35 feet Y = 5754925
25 meter
Z = -11250455
28 Z = -3429138
77
XDOT = -15730
026627 XDOT = -4794
512116
YDOT = -10701
169800 feet/sec YDOT = -3261
716555 meter/sec
ZDOT = -15059
612288 ZDOT = -4590
169825
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 10089
57489261
00016717 00000-0 10270-3 0 9063
2 25544 51
6414 274
1772 0006004 122
5309 237
6435 15
74012466 11092
Satellite: ISS
Catalog Number: 25544
Epoch time: 10089
57489261 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 274
1772 deg
Eccentricity:
0006004
Arg of perigee: 122
5309 deg
Mean anomaly: 237
6435 deg
Mean motion: 15
74012466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1109
Checksum: 299
Coasting Arc #8 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2010/090/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3304816
89 A = 6725205
99 meter
Y = 4292732
62 meter E =
0015490
Z = 3970497
47 I = 51
30078
XDOT = -2975
269992 Wp = 95
33461
YDOT = 5930
566878 meter/sec RA = 268
36356 deg
ZDOT = -3923
736498 TA = 35
42620
MA = 35
32340
Ha = 191
973 n
mi
Hp = 181
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10842575
11 X = 3237281
04
Y = 14083768
44 feet Y = 4329311
76 meter
Z = 13026566
51 Z = 3986388
01
XDOT = -9761
384488 XDOT = -3022
304551
YDOT = 19457
240413 feet/sec YDOT = 5897
032334 meter/sec
ZDOT = -12873
151241 ZDOT = -3938
305216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15866461
90 X = 4836097
59
Y = 7906821
36 feet Y = 2409999
15 meter
Z = 13089803
90 Z = 3989772
23
XDOT = 445
200709 XDOT = 135
697176
YDOT = 20576
918744 feet/sec YDOT = 6271
844833 meter/sec
ZDOT = -12930
829140 ZDOT = -3941
316722
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 10090
59071549
00016717 00000-0 10270-3 0 9074
2 25544 51
6408 268
9595 0005998 127
7237 232
4475 15
74011493 11251
Satellite: ISS
Catalog Number: 25544
Epoch time: 10090
59071549 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 268
9595 deg
Eccentricity:
0005998
Arg of perigee: 127
7237 deg
Mean anomaly: 232
4475 deg
Mean motion: 15
74011493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1125
Checksum: 329
Coasting Arc #9 (Orbit 1140)
---------------------------------------
Vector Time (GMT): 2010/091/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2139910
54 A = 6726744
79 meter
Y = -5363327
81 meter E =
0017386
Z = 3440002
52 I = 51
30967
XDOT = 4200
314836 Wp = 104
23522
YDOT = 4598
899637 meter/sec RA = 263
25520 deg
ZDOT = 4533
942011 TA = 296
73714
MA = 296
91496
Ha = 191
861 n
mi
Hp = 181
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7020703
87 X = 2183014
12
Y = -17596219
86 feet Y = -5339156
86 meter
Z = 11286097
50 Z = 3450503
30
XDOT = 13780
560487 XDOT = 4126
551659
YDOT = 15088
253403 feet/sec YDOT = 4645
457877 meter/sec
ZDOT = 14875
137832 ZDOT = 4554
167901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1826021
33 X = -556571
30
Y = -18831980
19 feet Y = -5739987
56 meter
Z = 11327638
83 Z = 3452664
31
XDOT = 17690
161820 XDOT = 5391
961323
YDOT = 7326
569259 feet/sec YDOT = 2233
138310 meter/sec
ZDOT = 14955
604475 ZDOT = 4558
468244
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 10091
60651215
00016717 00000-0 10270-3 0 9082
2 25544 51
6418 263
7424 0005976 131
9794 228
1880 15
74087501 11410
Satellite: ISS
Catalog Number: 25544
Epoch time: 10091
60651215 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 263
7424 deg
Eccentricity:
0005976
Arg of perigee: 131
9794 deg
Mean anomaly: 228
1880 deg
Mean motion: 15
74087501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1141
Checksum: 306
Coasting Arc #10 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2010/092/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4003447
52 A = 6725109
02 meter
Y = -3727501
50 meter E =
0012492
Z = -3926317
49 I = 51
31033
XDOT = 1937
026545 Wp = 120
02848
YDOT = -6280
650204 meter/sec RA = 258
04403 deg
ZDOT = 3990
866436 TA = 191
63477
MA = 191
66367
Ha = 191
825 n
mi
Hp = 181
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13134670
33 X = -3942394
89
Y = -12229335
62 feet Y = -3771929
19 meter
Z = -12881619
05 Z = -3945617
97
XDOT = 6355
073965 XDOT = 1987
726875
YDOT = -20605
807757 feet/sec YDOT = -6258
705613 meter/sec
ZDOT = 13093
393819 ZDOT = 4000
399937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17278763
23 X = -5266567
03
Y = -4640778
67 feet Y = -1414509
34 meter
Z = -12958388
73 Z = -3949716
88
XDOT = -4501
704370 XDOT = -1372
119492
YDOT = -19874
470269 feet/sec YDOT = -6057
738538 meter/sec
ZDOT = 13131
067383 ZDOT = 4002
349338
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 10092
55880050
00016717 00000-0 10270-3 0 9099
2 25544 51
6429 258
8519 0005964 134
4228 225
7424 15
74104320 11561
Satellite: ISS
Catalog Number: 25544
Epoch time: 10092
55880050 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 258
8519 deg
Eccentricity:
0005964
Arg of perigee: 134
4228 deg
Mean anomaly: 225
7424 deg
Mean motion: 15
74104320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 304
Coasting Arc #11 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2010/093/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1265101
52 A = 6726240
74 meter
Y = 5572070
91 meter E =
0009919
Z = -3553251
78 I = 51
32200
XDOT = -4914
823297 Wp = 111
80602
YDOT = -3931
128815 meter/sec RA = 252
93627 deg
ZDOT = -4428
286682 TA = 110
76057
MA = 110
65427
Ha = 191
650 n
mi
Hp = 181
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4150595
54 X = -1310054
26
Y = 18281072
55 feet Y = 5557672
40 meter
Z = -11657650
21 Z = -3559506
95
XDOT = -16124
748349 XDOT = -4848
987514
YDOT = -12897
404249 feet/sec YDOT = -3985
721251 meter/sec
ZDOT = -14528
499614 ZDOT = -4452
003026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5315829
85 X = 1620264
94
Y = 17960821
37 feet Y = 5474458
35 meter
Z = -11682324
87 Z = -3560772
62
XDOT = -18975
756905 XDOT = -5783
810705
YDOT = -3866
169105 feet/sec YDOT = -1178
408343 meter/sec
ZDOT = -14622
822257 ZDOT = -4457
036224
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 10093
57454944
00016717 00000-0 10270-3 0 9103
2 25544 51
6429 253
6347 0005852 138
1020 222
0592 15
74147930 11728
Satellite: ISS
Catalog Number: 25544
Epoch time: 10093
57454944 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 253
6347 deg
Eccentricity:
0005852
Arg of perigee: 138
1020 deg
Mean anomaly: 222
0592 deg
Mean motion: 15
74147930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 295
Coasting Arc #12 (Orbit 1187)
---------------------------------------
Vector Time (GMT): 2010/094/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4571511
23 A = 6725286
07 meter
Y = 3111698
45 meter E =
0015166
Z = 3812080
38 I = 51
32906
XDOT = -932
479446 Wp = 101
21703
YDOT = 6442
098701 meter/sec RA = 247
72516 deg
ZDOT = -4129
318566 TA = 32
15244
MA = 32
06004
Ha = 191
497 n
mi
Hp = 182
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14998396
43 X = 4517857
49
Y = 10208984
40 feet Y = 3162519
84 meter
Z = 12506825
40 Z = 3834158
45
XDOT = -3059
315767 XDOT = -984
387344
YDOT = 21135
494425 feet/sec YDOT = 6431
380896 meter/sec
ZDOT = -13547
633089 ZDOT = -4133
974689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18031100
71 X = 5495879
49
Y = 1360429
72 feet Y = 414658
98 meter
Z = 12594624
97 Z = 3838841
69
XDOT = 8107
083507 XDOT = 2471
039053
YDOT = 18470
155373 feet/sec YDOT = 5629
703358 meter/sec
ZDOT = -13565
927321 ZDOT = -4134
894647
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 10094
59027394
00016717 00000-0 10270-3 0 9112
2 25544 51
6429 248
4175 0005885 141
9771 218
1809 15
74164253 11881
Satellite: ISS
Catalog Number: 25544
Epoch time: 10094
59027394 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 248
4175 deg
Eccentricity:
0005885
Arg of perigee: 141
9771 deg
Mean anomaly: 218
1809 deg
Mean motion: 15
74164253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1188
Checksum: 327
Coasting Arc #13 (Orbit 1203)
---------------------------------------
Vector Time (GMT): 2010/095/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 378946
25 A = 6725621
50 meter
Y = -5627262
65 meter E =
0016142
Z = 3656187
61 I = 51
34451
XDOT = 5532
724953 Wp = 111
42962
YDOT = 3186
528867 meter/sec RA = 242
61903 deg
ZDOT = 4309
895382 TA = 292
72269
MA = 292
89323
Ha = 191
348 n
mi
Hp = 182
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1243261
98 X = 424082
10
Y = -18462147
81 feet Y = -5622772
64 meter
Z = 11995366
19 Z = 3658138
22
XDOT = 18151
984754 XDOT = 5475
744780
YDOT = 10454
491034 feet/sec YDOT = 3248
080541 meter/sec
ZDOT = 14140
076711 ZDOT = 4336
634840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8516422
14 X = -2595805
47
Y = -16422104
91 feet Y = -5005457
58 meter
Z = 12002934
48 Z = 3658494
43
XDOT = 19674
527277 XDOT = 5996
795914
YDOT = 260
100924 feet/sec YDOT = 79
278762 meter/sec
ZDOT = 14246
407527 ZDOT = 4342
305014
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 10095
60597010
00016717 00000-0 10270-3 0 9123
2 25544 51
6439 243
2005 0005752 146
4731 213
6798 15
74257987 12049
Satellite: ISS
Catalog Number: 25544
Epoch time: 10095
60597010 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 243
2005 deg
Eccentricity:
0005752
Arg of perigee: 146
4731 deg
Mean anomaly: 213
6798 deg
Mean motion: 15
74257987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1204
Checksum: 306
Coasting Arc #14 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2010/096/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5069056
51 A = 6725456
31 meter
Y = -2448786
88 meter E =
0010523
Z = -3692369
71 I = 51
35898
XDOT = -26
669862 Wp = 125
16823
YDOT = -6391
000260 meter/sec RA = 237
40963 deg
ZDOT = 4277
760957 TA = 190
23044
MA = 190
25188
Ha = 191
255 n
mi
Hp = 182
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16630762
83 X = -5023360
23
Y = -8034077
68 feet Y = -2505216
66 meter
Z = -12114073
86 Z = -3716884
00
XDOT = -87
499546 XDOT = 24
016956
YDOT = -20967
848623 feet/sec YDOT = -6391
015000 meter/sec
ZDOT = 14034
648809 ZDOT = 4277
754653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18299483
12 X = -5577682
46
Y = 1971388
60 feet Y = 600879
25 meter
Z = -12211552
17 Z = -3722081
10
XDOT = -11121
158214 XDOT = -3389
729024
YDOT = -16350
792224 feet/sec YDOT = -4983
721470 meter/sec
ZDOT = 14034
411250 ZDOT = 4277
688549
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 10096
55816468
00016717 00000-0 10270-3 0 9130
2 25544 51
6439 238
3097 0005547 148
9609 211
1883 15
74247307 12197
Satellite: ISS
Catalog Number: 25544
Epoch time: 10096
55816468 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 238
3097 deg
Eccentricity:
0005547
Arg of perigee: 148
9609 deg
Mean anomaly: 211
1883 deg
Mean motion: 15
74247307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 331
Coasting Arc #15 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2010/097/13:12:20
814
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 389762
92 A = 6724957
44 meter
Y = 5514434
48 meter E =
0009277
Z = -3834137
73 I = 51
37510
XDOT = -6032
290305 Wp = 111
04584
YDOT = -2427
657220 meter/sec RA = 232
30443 deg
ZDOT = -4116
071086 TA = 115
79700
MA = 115
70125
Ha = 191
119 n
mi
Hp = 182
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1278749
73 X = 346695
98
Y = 18091976
65 feet Y = 5518552
10 meter
Z = -12579192
04 Z = -3832349
09
XDOT = -19790
978692 XDOT = -5984
700478
YDOT = -7964
754660 feet/sec YDOT = -2494
847943 meter/sec
ZDOT = -13504
170230 ZDOT = -4145
260067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10992145
36 X = 3350405
91
Y = 14432986
08 feet Y = 4399174
16 meter
Z = -12571895
06 Z = -3831913
61
XDOT = -19815
611534 XDOT = -6039
798396
YDOT = 3259
868008 feet/sec YDOT = 993
607769 meter/sec
ZDOT = -13620
232962 ZDOT = -4151
447007
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 10097
57381271
00016717 00000-0 10270-3 0 9143
2 25544 51
6441 233
0918 0005579 153
0786 207
0668 15
74292617 12359
Satellite: ISS
Catalog Number: 25544
Epoch time: 10097
57381271 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 233
0918 deg
Eccentricity:
0005579
Arg of perigee: 153
0786 deg
Mean anomaly: 207
0668 deg
Mean motion: 15
74292617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1235
Checksum: 316
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list