[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 4th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 ET - UTC (sec) : 67 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 3484)
---------------------------------------
Vector Time (GMT): 2012/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3397462
03 A = 6799960
38 meter
Y = 5863493
37 meter E =
0030590
Z = 355843
53 I = 51
37329
XDOT = -4315
662963 Wp = 128
14006
YDOT = -2117
600776 meter/sec RA = 302
49387 deg
ZDOT = -5979
123463 TA = 48
01123
MA = 47
75108
Ha = 233
070 n
mi
Hp = 214
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11146528
98 X = -3464504
96
Y = 19237182
96 feet Y = 5825126
00 meter
Z = 1167465
65 Z = 339175
15
XDOT = -14158
999224 XDOT = -4262
617002
YDOT = -6947
509109 feet/sec YDOT = -2165
565149 meter/sec
ZDOT = -19616
546793 ZDOT = -5999
960094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6988407
12 X = 2130066
49
Y = -21110044
03 feet Y = -6434341
42 meter
Z = 1097952
44 Z = 334655
91
XDOT = 13622
705099 XDOT = 4152
200514
YDOT = 3424
773406 feet/sec YDOT = 1043
870934 meter/sec
ZDOT = -19702
442798 ZDOT = -6005
304565
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 12277
53296872
00016717 00000-0 10270-3 0 9008
2 25544 51
6478 302
9856 0017938 126
5016 233
7790 15
50465770 34856
Satellite: ISS
Catalog Number: 25544
Epoch time: 12277
53296872 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 302
9856 deg
Eccentricity:
0017938
Arg of perigee: 126
5016 deg
Mean anomaly: 233
7790 deg
Mean motion: 15
50465770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 338
Coasting Arc #2 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2012/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3214064
26 A = 6799860
44 meter
Y = -5993363
41 meter E =
0022881
Z = 101358
37 I = 51
35807
XDOT = 4162
455887 Wp = 97
40455
YDOT = 2353
048421 meter/sec RA = 297
52062 deg
ZDOT = 5977
222802 TA = 263
68869
MA = 263
94935
Ha = 232
973 n
mi
Hp = 214
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10544830
24 X = 3280352
03
Y = -19663265
78 feet Y = -5957051
09 meter
Z = 332540
57 Z = 117133
88
XDOT = 13656
351334 XDOT = 4106
797740
YDOT = 7719
975134 feet/sec YDOT = 2399
284847 meter/sec
ZDOT = 19610
311029 ZDOT = 5997
308800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5934313
87 X = -1808778
87
Y = 21507516
49 feet Y = 6555491
03 meter
Z = 398374
33 Z = 121424
50
XDOT = -13339
774462 XDOT = -4065
963256
YDOT = -4104
723991 feet/sec YDOT = -1251
119872 meter/sec
ZDOT = 19693
080859 ZDOT = 6002
451046
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 12278
56422111
00016717 00000-0 10270-3 0 9010
2 25544 51
6479 297
8737 0017875 130
1458 230
1262 15
50507985 35017
Satellite: ISS
Catalog Number: 25544
Epoch time: 12278
56422111 = yrday
fracday
Element set: 901
Inclination: 51
6479 deg
RA of node: 297
8737 deg
Eccentricity:
0017875
Arg of perigee: 130
1458 deg
Mean anomaly: 230
1262 deg
Mean motion: 15
50507985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 311
Coasting Arc #3 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2012/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3072429
55 A = 6799647
76 meter
Y = 6015877
15 meter E =
0028457
Z = -663912
33 I = 51
34375
XDOT = -4029
421123 Wp = 135
61334
YDOT = -2694
631603 meter/sec RA = 292
54523 deg
ZDOT = -5944
053571 TA = 51
58215
MA = 51
32699
Ha = 232
862 n
mi
Hp = 214
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10080149
46 X = -3136246
81
Y = 19737129
77 feet Y = 5981162
47 meter
Z = -2178190
06 Z = -678993
69
XDOT = -13219
885574 XDOT = -3970
114386
YDOT = -8840
654864 feet/sec YDOT = -2739
359887 meter/sec
ZDOT = -19501
488093 ZDOT = -5963
484391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5083620
94 X = 1549487
66
Y = -21564838
13 feet Y = -6572962
66 meter
Z = -2241153
98 Z = -683103
73
XDOT = 13254
683691 XDOT = 4040
027589
YDOT = 5101
812690 feet/sec YDOT = 1555
032508 meter/sec
ZDOT = -19581
516994 ZDOT = -5968
446380
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 12279
53100019
00016717 00000-0 10270-3 0 9029
2 25544 51
6473 293
0795 0017928 133
6563 226
6077 15
50519518 35162
Satellite: ISS
Catalog Number: 25544
Epoch time: 12279
53100019 = yrday
fracday
Element set: 902
Inclination: 51
6473 deg
RA of node: 293
0795 deg
Eccentricity:
0017928
Arg of perigee: 133
6563 deg
Mean anomaly: 226
6077 deg
Mean motion: 15
50519518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 315
Coasting Arc #4 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2012/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2872310
43 A = 6799081
39 meter
Y = -6057141
22 meter E =
0024343
Z = 1136985
42 I = 51
33177
XDOT = 3951
920752 Wp = 103
61500
YDOT = 2990
418450 meter/sec RA = 287
56981 deg
ZDOT = 5836
082420 TA = 268
75180
MA = 269
03069
Ha = 232
711 n
mi
Hp = 214
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9423590
65 X = 2934305
87
Y = -19872510
57 feet Y = -6024674
55 meter
Z = 3730267
12 Z = 1151090
11
XDOT = 12965
619265 XDOT = 3889
836793
YDOT = 9811
084152 feet/sec YDOT = 3034
264510 meter/sec
ZDOT = 19147
252033 ZDOT = 5855
129951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4033374
42 X = -1229372
52
Y = 21610403
18 feet Y = 6586850
89 meter
Z = 3789194
49 Z = 1154946
48
XDOT = -13346
481829 XDOT = -4068
007662
YDOT = -5925
154768 feet/sec YDOT = -1805
987173 meter/sec
ZDOT = 19225
670524 ZDOT = 5859
984376
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 12280
56220730
00016717 00000-0 10270-3 0 9038
2 25544 51
6473 287
9676 0017836 137
4705 222
7831 15
50586521 35321
Satellite: ISS
Catalog Number: 25544
Epoch time: 12280
56220730 = yrday
fracday
Element set: 903
Inclination: 51
6473 deg
RA of node: 287
9676 deg
Eccentricity:
0017836
Arg of perigee: 137
4705 deg
Mean anomaly: 222
7831 deg
Mean motion: 15
50586521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 313
Coasting Arc #5 (Orbit 3546)
---------------------------------------
Vector Time (GMT): 2012/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2730915
87 A = 6798403
71 meter
Y = 5978351
42 meter E =
0025447
Z = -1701210
78 I = 51
32051
XDOT = -3899
289434 Wp = 140
89378
YDOT = -3376
810682 meter/sec RA = 282
59182 deg
ZDOT = -5673
080253 TA = 57
82866
MA = 57
58208
Ha = 232
596 n
mi
Hp = 214
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8959697
73 X = -2789299
88
Y = 19614013
84 feet Y = 5947486
07 meter
Z = -5581400
19 Z = -1714619
76
XDOT = -12792
944338 XDOT = -3833
680571
YDOT = -11078
775203 feet/sec YDOT = -3420
048468 meter/sec
ZDOT = -18612
468021 ZDOT = -5691
863472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3273735
74 X = 997834
65
Y = -21298819
01 feet Y = -6491880
03 meter
Z = -5637438
58 Z = -1718291
28
XDOT = 13654
585023 XDOT = 4161
917515
YDOT = 6989
053376 feet/sec YDOT = 2130
263469 meter/sec
ZDOT = -18689
760465 ZDOT = -5696
638990
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 12281
52894489
00016717 00000-0 10270-3 0 9044
2 25544 51
6465 283
1731 0017841 140
7822 219
4625 15
50583499 35476
Satellite: ISS
Catalog Number: 25544
Epoch time: 12281
52894489 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 283
1731 deg
Eccentricity:
0017841
Arg of perigee: 140
7822 deg
Mean anomaly: 219
4625 deg
Mean motion: 15
50583499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3547
Checksum: 334
Coasting Arc #6 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2012/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2543909
60 A = 6797411
29 meter
Y = -5917860
83 meter E =
0025388
Z = 2169527
89 I = 51
31198
XDOT = 3907
682796 Wp = 112
96454
YDOT = 3699
681954 meter/sec RA = 277
61398 deg
ZDOT = 5448
787267 TA = 271
17258
MA = 271
46343
Ha = 232
413 n
mi
Hp = 214
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8346160
10 X = 2599356
10
Y = -19415553
90 feet Y = -5889103
08 meter
Z = 7117873
65 Z = 2182021
27
XDOT = 12820
481613 XDOT = 3839
552527
YDOT = 12138
064155 feet/sec YDOT = 3742
999520 meter/sec
ZDOT = 17876
598644 ZDOT = 5467
605057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2367377
01 X = -721576
51
Y = 20982641
12 feet Y = 6395509
01 meter
Z = 7170114
69 Z = 2185450
96
XDOT = -14135
064293 XDOT = -4308
367597
YDOT = -7797
750754 feet/sec YDOT = -2376
754430 meter/sec
ZDOT = 17954
008918 ZDOT = 5472
381918
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 12282
56010603
00016717 00000-0 10270-3 0 9058
2 25544 51
6462 278
0610 0017758 144
8965 215
3359 15
50663301 35630
Satellite: ISS
Catalog Number: 25544
Epoch time: 12282
56010603 = yrday
fracday
Element set: 905
Inclination: 51
6462 deg
RA of node: 278
0610 deg
Eccentricity:
0017758
Arg of perigee: 144
8965 deg
Mean anomaly: 215
3359 deg
Mean motion: 15
50663301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 302
Coasting Arc #7 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2012/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2436032
48 A = 6796298
88 meter
Y = 5730497
11 meter E =
0022212
Z = -2709305
74 I = 51
30456
XDOT = -3939
704578 Wp = 142
52086
YDOT = -4089
822482 meter/sec RA = 272
63302 deg
ZDOT = -5147
716665 TA = 68
22237
MA = 67
98615
Ha = 232
289 n
mi
Hp = 215
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7992232
54 X = -2486769
74
Y = 18800843
55 feet Y = 5702971
98 meter
Z = -8888798
36 Z = -2721263
65
XDOT = -12925
539954 XDOT = -3868
671876
YDOT = -13418
052761 feet/sec YDOT = -4133
481947 meter/sec
ZDOT = -16888
834202 ZDOT = -5166
682868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1845536
48 X = 562519
52
Y = -20323633
85 feet Y = -6194643
60 meter
Z = -8938799
56 Z = -2724546
11
XDOT = 14812
911229 XDOT = 4514
975343
YDOT = 8750
708192 feet/sec YDOT = 2667
215857 meter/sec
ZDOT = -16966
827844 ZDOT = -5171
489127
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 12283
52680075
00016717 00000-0 10270-3 0 9062
2 25544 51
6455 273
2660 0017720 147
8939 212
3295 15
50655983 35786
Satellite: ISS
Catalog Number: 25544
Epoch time: 12283
52680075 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 273
2660 deg
Eccentricity:
0017720
Arg of perigee: 147
8939 deg
Mean anomaly: 212
3295 deg
Mean motion: 15
50655983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3578
Checksum: 332
Coasting Arc #8 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2012/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2295901
61 A = 6794996
82 meter
Y = -5566295
34 meter E =
0025683
Z = 3147946
97 I = 51
30017
XDOT = 4030
249648 Wp = 124
72704
YDOT = 4401
675551 meter/sec RA = 267
65256 deg
ZDOT = 4801
343897 TA = 271
69021
MA = 271
98437
Ha = 232
090 n
mi
Hp = 215
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7532485
60 X = 2342682
31
Y = -18262123
82 feet Y = -5540359
28 meter
Z = 10327910
02 Z = 3159214
59
XDOT = 13222
603831 XDOT = 3957
405626
YDOT = 14441
192752 feet/sec YDOT = 4446
337472 meter/sec
ZDOT = 15752
440606 ZDOT = 4820
745470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1224447
56 X = -373211
62
Y = 19691842
03 feet Y = 6002073
45 meter
Z = 10375033
33 Z = 3162310
16
XDOT = -15625
185455 XDOT = -4762
556527
YDOT = -9386
117614 feet/sec YDOT = -2860
888649 meter/sec
ZDOT = 15832
212954 ZDOT = 4825
658508
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 12284
55791496
00016717 00000-0 10270-3 0 9077
2 25544 51
6451 268
1534 0017659 152
2909 207
9186 15
50736300 35943
Satellite: ISS
Catalog Number: 25544
Epoch time: 12284
55791496 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 268
1534 deg
Eccentricity:
0017659
Arg of perigee: 152
2909 deg
Mean anomaly: 207
9186 deg
Mean motion: 15
50736300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3594
Checksum: 334
Coasting Arc #9 (Orbit 3608)
---------------------------------------
Vector Time (GMT): 2012/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2256181
71 A = 6793594
98 meter
Y = 5276471
18 meter E =
0019823
Z = -3633293
91 I = 51
29755
XDOT = -4134
748622 Wp = 139
62456
YDOT = -4751
848004 meter/sec RA = 262
66843 deg
ZDOT = -4361
536746 TA = 83
64678
MA = 83
42106
Ha = 231
955 n
mi
Hp = 215
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7402170
96 X = -2297366
74
Y = 17311257
14 feet Y = 5251010
46 meter
Z = -11920255
61 Z = -3644355
06
XDOT = -13565
448234 XDOT = -4060
117601
YDOT = -15590
052505 feet/sec YDOT = -4797
668543 meter/sec
ZDOT = -14309
503761 ZDOT = -4381
441546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1073784
54 X = 327289
53
Y = -18767375
27 feet Y = -5720295
98 meter
Z = -11966489
24 Z = -3647385
92
XDOT = 16570
936360 XDOT = 5050
821403
YDOT = 10065
554376 feet/sec YDOT = 3067
980974 meter/sec
ZDOT = -14391
332260 ZDOT = -4386
478073
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 12285
52456516
00016717 00000-0 10270-3 0 9087
2 25544 51
6449 263
3578 0017600 155
1303 205
0700 15
50731732 36093
Satellite: ISS
Catalog Number: 25544
Epoch time: 12285
52456516 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 263
3578 deg
Eccentricity:
0017600
Arg of perigee: 155
1303 deg
Mean anomaly: 205
0700 deg
Mean motion: 15
50731732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3609
Checksum: 294
Coasting Arc #10 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2012/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2195664
22 A = 6792158
28 meter
Y = -5019746
27 meter E =
0025024
Z = 4013663
44 I = 51
29828
XDOT = 4287
748868 Wp = 138
09265
YDOT = 5014
661582 meter/sec RA = 257
68545 deg
ZDOT = 3893
625159 TA = 271
12884
MA = 271
41552
Ha = 231
744 n
mi
Hp = 215
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7203622
77 X = 2232135
17
Y = -16468983
81 feet Y = -4994988
56 meter
Z = 13168187
13 Z = 4024419
22
XDOT = 14067
417545 XDOT = 4212
440610
YDOT = 16452
301778 feet/sec YDOT = 5062
189282 meter/sec
ZDOT = 12774
360757 ZDOT = 3914
271553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -855043
36 X = -260617
22
Y = 17922135
48 feet Y = 5462666
90 meter
Z = 13213126
87 Z = 4027361
07
XDOT = -17587
047704 XDOT = -5360
532140
YDOT = -10397
733853 feet/sec YDOT = -3169
229278 meter/sec
ZDOT = 12859
239057 ZDOT = 3919
496065
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 12286
55563128
00016717 00000-0 10270-3 0 9090
2 25544 51
6449 258
2449 0017560 159
6541 200
5313 15
50808636 36257
Satellite: ISS
Catalog Number: 25544
Epoch time: 12286
55563128 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 258
2449 deg
Eccentricity:
0017560
Arg of perigee: 159
6541 deg
Mean anomaly: 200
5313 deg
Mean motion: 15
50808636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3625
Checksum: 321
Coasting Arc #11 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2012/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2254124
30 A = 6790726
61 meter
Y = 4648004
91 meter E =
0019284
Z = -4411917
87 I = 51
30135
XDOT = -4435
310947 Wp = 134
51014
YDOT = -5284
984141 meter/sec RA = 252
69859 deg
ZDOT = -3323
981532 TA = 101
80957
MA = 101
59320
Ha = 231
596 n
mi
Hp = 215
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7395420
95 X = -2284499
27
Y = 15249359
96 feet Y = 4622627
48 meter
Z = -14474796
15 Z = -4422942
87
XDOT = -14551
545101 XDOT = -4359
736081
YDOT = -17339
186815 feet/sec YDOT = -5334
160426 meter/sec
ZDOT = -10905
451222 ZDOT = -3345
344176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1167333
56 X = 355803
27
Y = -16868266
02 feet Y = -5141447
48 meter
Z = -14520808
78 Z = -4425942
52
XDOT = 18628
725013 XDOT = 5678
035384
YDOT = 10689
875633 feet/sec YDOT = 3258
274093 meter/sec
ZDOT = -10993
272903 ZDOT = -3350
749581
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 12287
52223553
00016717 00000-0 10270-3 0 9105
2 25544 51
6452 253
4489 0017493 162
5783 197
5972 15
50807699 36409
Satellite: ISS
Catalog Number: 25544
Epoch time: 12287
52223553 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 253
4489 deg
Eccentricity:
0017493
Arg of perigee: 162
5783 deg
Mean anomaly: 197
5972 deg
Mean motion: 15
50807699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 338
Coasting Arc #12 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2012/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2298951
64 A = 6789388
24 meter
Y = -4323188
60 meter E =
0023323
Z = 4702992
07 I = 51
30806
XDOT = 4615
226748 Wp = 152
02387
YDOT = 5466
783560 meter/sec RA = 247
71378 deg
ZDOT = 2743
452102 TA = 270
53790
MA = 270
80514
Ha = 231
371 n
mi
Hp = 215
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7542492
25 X = 2324277
00
Y = -14183689
65 feet Y = -4297338
12 meter
Z = 15429764
01 Z = 4714222
55
XDOT = 15141
820038 XDOT = 4540
425653
YDOT = 17935
641602 feet/sec YDOT = 5517
976004 meter/sec
ZDOT = 9000
827106 ZDOT = 2765
690794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1417410
21 X = -432026
63
Y = 15956499
18 feet Y = 4863540
95 meter
Z = 15476593
32 Z = 4717265
64
XDOT = -19662
658744 XDOT = -5993
178385
YDOT = -10647
268872 feet/sec YDOT = -3245
287552 meter/sec
ZDOT = 9092
259864 ZDOT = 2771
320806
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 12288
55325251
00016717 00000-0 10270-3 0 9118
2 25544 51
6458 248
3357 0017470 167
0463 193
1140 15
50882287 36564
Satellite: ISS
Catalog Number: 25544
Epoch time: 12288
55325251 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 248
3357 deg
Eccentricity:
0017470
Arg of perigee: 167
0463 deg
Mean anomaly: 193
1140 deg
Mean motion: 15
50882287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3656
Checksum: 316
Coasting Arc #13 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2474486
00 A = 6788249
00 meter
Y = 3903104
59 meter E =
0020489
Z = -4980909
85 I = 51
31728
XDOT = -4761
270107 Wp = 132
56314
YDOT = -5628
396670 meter/sec RA = 242
72536 deg
ZDOT = -2064
139262 TA = 117
33529
MA = 117
12658
Ha = 231
215 n
mi
Hp = 216
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8118392
40 X = -2493750
66
Y = 12805461
25 feet Y = 3875325
13 meter
Z = -16341567
74 Z = -4992978
28
XDOT = -15620
964917 XDOT = -4687
950946
YDOT = -18465
868340 feet/sec YDOT = -5681
230423 meter/sec
ZDOT = -6772
110441 ZDOT = -2087
091230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2217398
46 X = 675863
05
Y = -14944104
66 feet Y = -4554963
10 meter
Z = -16391822
64 Z = -4996227
54
XDOT = 20582
194493 XDOT = 6273
452882
YDOT = 10517
393381 feet/sec YDOT = 3205
701503 meter/sec
ZDOT = -6866
482540 ZDOT = -2092
903878
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 12289
51980981
00016717 00000-0 10270-3 0 9123
2 25544 51
6463 243
5397 0017409 170
1813 189
9681 15
50883671 36715
Satellite: ISS
Catalog Number: 25544
Epoch time: 12289
51980981 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 243
5397 deg
Eccentricity:
0017409
Arg of perigee: 170
1813 deg
Mean anomaly: 189
9681 deg
Mean motion: 15
50883671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 342
Coasting Arc #14 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2012/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2637216
35 A = 6787283
76 meter
Y = -3545461
37 meter E =
0020639
Z = 5151362
42 I = 51
33026
XDOT = 4919
586803 Wp = 164
91349
YDOT = 5709
585108 meter/sec RA = 237
73999 deg
ZDOT = 1390
271033 TA = 271
53308
MA = 271
76950
Ha = 230
972 n
mi
Hp = 216
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8652284
61 X = 2651641
58
Y = -11632091
10 feet Y = -3515889
34 meter
Z = 16900795
35 Z = 5164209
55
XDOT = 16140
376651 XDOT = 4848
621583
YDOT = 18732
234607 feet/sec YDOT = 5764
202312 meter/sec
ZDOT = 4561
256669 ZDOT = 1413
998026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2930796
25 X = -893306
70
Y = 14133954
08 feet Y = 4308029
20 meter
Z = 16954239
33 Z = 5167652
15
XDOT = -21417
157000 XDOT = -6527
949454
YDOT = -10111
206529 feet/sec YDOT = -3081
895750 meter/sec
ZDOT = 4658
831469 ZDOT = 1420
011832
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 12290
55077683
00016717 00000-0 10270-3 0 9136
2 25544 51
6470 238
4266 0017396 174
4711 185
6635 15
50955045 36874
Satellite: ISS
Catalog Number: 25544
Epoch time: 12290
55077683 = yrday
fracday
Element set: 913
Inclination: 51
6470 deg
RA of node: 238
4266 deg
Eccentricity:
0017396
Arg of perigee: 174
4711 deg
Mean anomaly: 185
6635 deg
Mean motion: 15
50955045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 334
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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