[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 21st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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 3298)
---------------------------------------
Vector Time (GMT): 2012/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3625781
57 A = 6792612
37 meter
Y = 3474288
39 meter E =
0026371
Z = 4554269
00 I = 51
65583
XDOT = -6489
021686 Wp = 79
17207
YDOT = -2685
275831 meter/sec RA = 2
06121 deg
ZDOT = -3097
511605 TA = 41
89598
MA = 41
69449
Ha = 234
130 n
mi
Hp = 214
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11895608
81 X = -3686486
09
Y = 11398583
94 feet Y = 3433403
44 meter
Z = 14941827
44 Z = 4536507
36
XDOT = -21289
441228 XDOT = -6443
464961
YDOT = -8809
960077 feet/sec YDOT = -2757
585549 meter/sec
ZDOT = -10162
439650 ZDOT = -3128
924434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11994773
46 X = 3656006
95
Y = -11391204
20 feet Y = -3472039
04 meter
Z = 14867996
12 Z = 4531765
22
XDOT = 20390
044403 XDOT = 6214
885534
YDOT = 7950
678917 feet/sec YDOT = 2423
366934 meter/sec
ZDOT = -10292
024544 ZDOT = -3137
009081
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 12265
54280042
00016717 00000-0 10270-3 0 9008
2 25544 51
6495 2
3980 0017890 85
7616 274
5578 15
50015113 32995
Satellite: ISS
Catalog Number: 25544
Epoch time: 12265
54280042 = yrday
fracday
Element set: 900
Inclination: 51
6495 deg
RA of node: 2
3980 deg
Eccentricity:
0017890
Arg of perigee: 85
7616 deg
Mean anomaly: 274
5578 deg
Mean motion: 15
50015113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3299
Checksum: 307
Coasting Arc #2 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2012/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3678054
89 A = 6793116
58 meter
Y = -3672630
56 meter E =
0026171
Z = -4397940
92 I = 51
62768
XDOT = 6419
159715 Wp = 95
72044
YDOT = 2372
721973 meter/sec RA = 357
10688 deg
ZDOT = 3401
967896 TA = 208
80258
MA = 208
94732
Ha = 233
938 n
mi
Hp = 214
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12067109
22 X = 3740213
93
Y = -12049312
86 feet Y = -3631152
90 meter
Z = -14428940
02 Z = -4379921
88
XDOT = 21060
235286 XDOT = 6375
624299
YDOT = 7784
520909 feet/sec YDOT = 2444
261752 meter/sec
ZDOT = 11161
311996 ZDOT = 3433
046149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11954653
40 X = -3643778
35
Y = 12249232
80 feet Y = 3733566
16 meter
Z = -14354021
49 Z = -4375105
75
XDOT = -20223
929203 XDOT = -6164
253621
YDOT = -6565
923813 feet/sec YDOT = -2001
293578 meter/sec
ZDOT = 11289
547287 ZDOT = 3441
054013
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 12266
50988258
00016717 00000-0 10270-3 0 9010
2 25544 51
6495 357
6079 0017823 89
2178 271
1014 15
50069037 33148
Satellite: ISS
Catalog Number: 25544
Epoch time: 12266
50988258 = yrday
fracday
Element set: 901
Inclination: 51
6495 deg
RA of node: 357
6079 deg
Eccentricity:
0017823
Arg of perigee: 89
2178 deg
Mean anomaly: 271
1014 deg
Mean motion: 15
50069037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3314
Checksum: 322
Coasting Arc #3 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2012/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3762139
53 A = 6793899
84 meter
Y = 3830893
27 meter E =
0028076
Z = 4139726
46 I = 51
60024
XDOT = -6340
384855 Wp = 86
01897
YDOT = -2135
552926 meter/sec RA = 352
14890 deg
ZDOT = -3761
907995 TA = 42
80134
MA = 42
58308
Ha = 233
977 n
mi
Hp = 214
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12342977
46 X = -3824807
62
Y = 12568547
48 feet Y = 3788472
50 meter
Z = 13581779
74 Z = 4121297
74
XDOT = -20801
787582 XDOT = -6297
758925
YDOT = -7006
407238 feet/sec YDOT = -2206
216923 meter/sec
ZDOT = -12342
217831 ZDOT = -3792
605646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11995210
72 X = 3656140
23
Y = -12981064
79 feet Y = -3956628
55 meter
Z = 13505150
70 Z = 4116369
93
XDOT = 20003
627470 XDOT = 6097
105653
YDOT = 5429
980312 feet/sec YDOT = 1655
057999 meter/sec
ZDOT = -12468
905755 ZDOT = -3800
522474
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 12267
54141309
00016717 00000-0 10270-3 0 9024
2 25544 51
6494 352
4966 0017861 92
4284 267
8912 15
50097092 33300
Satellite: ISS
Catalog Number: 25544
Epoch time: 12267
54141309 = yrday
fracday
Element set: 902
Inclination: 51
6494 deg
RA of node: 352
4966 deg
Eccentricity:
0017861
Arg of perigee: 92
4284 deg
Mean anomaly: 267
8912 deg
Mean motion: 15
50097092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 318
Coasting Arc #4 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2012/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3794893
62 A = 6794529
65 meter
Y = -4061324
35 meter E =
0024204
Z = -3931209
37 I = 51
57261
XDOT = 6200
095880 Wp = 98
08790
YDOT = 1887
845921 meter/sec RA = 347
19071 deg
ZDOT = 4052
927854 TA = 214
42809
MA = 214
58514
Ha = 233
824 n
mi
Hp = 214
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12450438
39 X = 3859123
02
Y = -13324554
96 feet Y = -4018528
62 meter
Z = -12897668
55 Z = -3912617
72
XDOT = 20341
521916 XDOT = 6158
836636
YDOT = 6193
720214 feet/sec YDOT = 1956
948841 meter/sec
ZDOT = 13297
007395 ZDOT = 4082
947203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11834813
68 X = -3607251
21
Y = 13945716
64 feet Y = 4250654
43 meter
Z = -12820343
51 Z = -3907640
70
XDOT = -19531
775233 XDOT = -5953
285091
YDOT = -4292
517831 feet/sec YDOT = -1308
359435 meter/sec
ZDOT = 13420
917879 ZDOT = 4090
695769
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 12268
50844991
00016717 00000-0 10270-3 0 9039
2 25544 51
6491 347
7062 0017827 95
9648 264
3535 15
50139138 33452
Satellite: ISS
Catalog Number: 25544
Epoch time: 12268
50844991 = yrday
fracday
Element set: 903
Inclination: 51
6491 deg
RA of node: 347
7062 deg
Eccentricity:
0017827
Arg of perigee: 95
9648 deg
Mean anomaly: 264
3535 deg
Mean motion: 15
50139138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 335
Coasting Arc #5 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2012/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3855014
94 A = 6795383
55 meter
Y = 4249267
74 meter E =
0029626
Z = 3614021
23 I = 51
54662
XDOT = -6050
738920 Wp = 93
62045
YDOT = -1726
075742 meter/sec RA = 342
22920 deg
ZDOT = -4395
448569 TA = 43
48951
MA = 43
25625
Ha = 233
790 n
mi
Hp = 214
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12647686
83 X = -3919800
66
Y = 13941167
11 feet Y = 4205796
63 meter
Z = 11857025
03 Z = 3595136
08
XDOT = -19851
505644 XDOT = -6009
635862
YDOT = -5662
978156 feet/sec YDOT = -1793
509446 meter/sec
ZDOT = -14420
763023 ZDOT = -4424
742676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11741647
59 X = 3578854
19
Y = -14775333
83 feet Y = -4503521
75 meter
Z = 11778471
35 Z = 3590078
07
XDOT = 19025
062601 XDOT = 5798
839081
YDOT = 3449
460806 feet/sec YDOT = 1051
395654 meter/sec
ZDOT = -14541
691121 ZDOT = -4432
307454
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 12269
53993146
00016717 00000-0 10270-3 0 9041
2 25544 51
6493 342
5947 0017795 99
0789 261
2376 15
50179131 33618
Satellite: ISS
Catalog Number: 25544
Epoch time: 12269
53993146 = yrday
fracday
Element set: 904
Inclination: 51
6493 deg
RA of node: 342
5947 deg
Eccentricity:
0017795
Arg of perigee: 99
0789 deg
Mean anomaly: 261
2376 deg
Mean motion: 15
50179131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 343
Coasting Arc #6 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2012/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3853169
08 A = 6796092
70 meter
Y = -4501866
21 meter E =
0022358
Z = -3350474
88 I = 51
52005
XDOT = 5856
819176 Wp = 98
68113
YDOT = 1562
164635 meter/sec RA = 337
26744 deg
ZDOT = 4659
995088 TA = 222
36219
MA = 222
53503
Ha = 233
697 n
mi
Hp = 214
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12641630
83 X = 3919499
31
Y = -14769902
25 feet Y = -4458407
15 meter
Z = -10992371
66 Z = -3331594
82
XDOT = 19215
286009 XDOT = 5816
278289
YDOT = 5125
212056 feet/sec YDOT = 1627
433067 meter/sec
ZDOT = 15288
697796 ZDOT = 4688
348526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11403833
13 X = -3475888
34
Y = 15799817
36 feet Y = 4815784
33 meter
Z = -10913818
71 Z = -3326531
94
XDOT = -18336
433672 XDOT = -5588
944983
YDOT = -2646
576691 feet/sec YDOT = -806
676575 meter/sec
ZDOT = 15405
751492 ZDOT = 4695
673055
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 12270
50692324
00016717 00000-0 10270-3 0 9055
2 25544 51
6486 337
8040 0017827 102
6619 257
6526 15
50206192 33760
Satellite: ISS
Catalog Number: 25544
Epoch time: 12270
50692324 = yrday
fracday
Element set: 905
Inclination: 51
6486 deg
RA of node: 337
8040 deg
Eccentricity:
0017827
Arg of perigee: 102
6619 deg
Mean anomaly: 257
6526 deg
Mean motion: 15
50206192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 309
Coasting Arc #7 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2012/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3875097
52 A = 6796933
28 meter
Y = 4705263
95 meter E =
0030872
Z = 2972761
08 I = 51
49603
XDOT = -5655
615863 Wp = 101
85360
YDOT = -1495
122083 meter/sec RA = 332
30280 deg
ZDOT = -4968
303298 TA = 44
08126
MA = 43
83556
Ha = 233
597 n
mi
Hp = 214
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12713574
53 X = -3941865
75
Y = 15437217
68 feet Y = 4661557
23 meter
Z = 9753153
14 Z = 2953773
27
XDOT = -18555
170154 XDOT = -5614
341855
YDOT = -4905
256178 feet/sec YDOT = -1558
136545 meter/sec
ZDOT = -16300
207669 ZDOT = -4995
677585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11126100
38 X = 3391235
40
Y = -16663959
52 feet Y = -5079174
86 meter
Z = 9674141
13 Z = 2948678
22
XDOT = 17645
060877 XDOT = 5378
214555
YDOT = 2180
534665 feet/sec YDOT = 664
626966 meter/sec
ZDOT = -16413
215950 ZDOT = -5002
748222
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 12271
53835596
00016717 00000-0 10270-3 0 9060
2 25544 51
6489 332
6922 0017753 105
7356 254
5754 15
50258253 33927
Satellite: ISS
Catalog Number: 25544
Epoch time: 12271
53835596 = yrday
fracday
Element set: 906
Inclination: 51
6489 deg
RA of node: 332
6922 deg
Eccentricity:
0017753
Arg of perigee: 105
7356 deg
Mean anomaly: 254
5754 deg
Mean motion: 15
50258253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 331
Coasting Arc #8 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2012/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3827104
16 A = 6797638
91 meter
Y = -4963490
31 meter E =
0021073
Z = -2653859
39 I = 51
47132
XDOT = 5430
691770 Wp = 97
48018
YDOT = 1429
031880 meter/sec RA = 327
33758 deg
ZDOT = 5191
729249 TA = 232
62437
MA = 232
81646
Ha = 233
560 n
mi
Hp = 214
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12556116
01 X = 3895214
41
Y = -16284417
04 feet Y = -4920312
77 meter
Z = -8706887
76 Z = -2635101
32
XDOT = 17817
230216 XDOT = 5389
088059
YDOT = 4688
424802 feet/sec YDOT = 1489
529331 meter/sec
ZDOT = 17033
232445 ZDOT = 5218
010164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10573945
17 X = -3222938
49
Y = 17674376
05 feet Y = 5387149
82 meter
Z = -8628806
23 Z = -2630060
14
XDOT = -16857
060863 XDOT = -5138
032151
YDOT = -1769
371337 feet/sec YDOT = -539
304384 meter/sec
ZDOT = 17141
722392 ZDOT = 5224
796985
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 12272
50530263
00016717 00000-0 10270-3 0 9072
2 25544 51
6480 327
9010 0017838 109
3011 251
0071 15
50272082 34072
Satellite: ISS
Catalog Number: 25544
Epoch time: 12272
50530263 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 327
9010 deg
Eccentricity:
0017838
Arg of perigee: 109
3011 deg
Mean anomaly: 251
0071 deg
Mean motion: 15
50272082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 268
Coasting Arc #9 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2012/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3801544
35 A = 6798370
31 meter
Y = 5161643
32 meter E =
0031630
Z = 2217150
78 I = 51
44953
XDOT = -5202
674564 Wp = 110
52054
YDOT = -1469
674185 meter/sec RA = 322
36997 deg
ZDOT = -5446
880691 TA = 44
77395
MA = 44
51909
Ha = 233
425 n
mi
Hp = 214
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12472258
36 X = -3869750
89
Y = 16934525
33 feet Y = 5118751
01 meter
Z = 7274116
74 Z = 2198516
54
XDOT = -17069
142269 XDOT = -5159
393742
YDOT = -4821
765700 feet/sec YDOT = -1527
612474 meter/sec
ZDOT = -17870
343473 ZDOT = -5472
049930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10087870
42 X = 3074782
90
Y = -18484937
75 feet Y = -5634209
03 meter
Z = 7196533
75 Z = 2193503
49
XDOT = 16111
025036 XDOT = 4910
640431
YDOT = 1727
261409 feet/sec YDOT = 526
469278 meter/sec
ZDOT = -17974
228067 ZDOT = -5478
544715
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 12273
53668665
00016717 00000-0 10270-3 0 9085
2 25544 51
6483 322
7888 0017787 112
4541 247
8496 15
50330181 34234
Satellite: ISS
Catalog Number: 25544
Epoch time: 12273
53668665 = yrday
fracday
Element set: 908
Inclination: 51
6483 deg
RA of node: 322
7888 deg
Eccentricity:
0017787
Arg of perigee: 112
4541 deg
Mean anomaly: 247
8496 deg
Mean motion: 15
50330181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 333
Coasting Arc #10 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2012/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3701954
23 A = 6798949
49 meter
Y = -5403522
48 meter E =
0020742
Z = -1845674
43 I = 51
42763
XDOT = 4973
677003 Wp = 95
54948
YDOT = 1508
133124 meter/sec RA = 317
40155 deg
ZDOT = 5613
318067 TA = 244
15218
MA = 244
36623
Ha = 233
407 n
mi
Hp = 214
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12145519
13 X = 3771068
38
Y = -17728092
12 feet Y = -5361738
71 meter
Z = -6055362
29 Z = -1827521
70
XDOT = 16317
837936 XDOT = 4929
174514
YDOT = 4947
943321 feet/sec YDOT = 1563
503785 meter/sec
ZDOT = 18416
397859 ZDOT = 5637
371968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9316364
28 X = -2839627
83
Y = 19388507
87 feet Y = 5909617
20 meter
Z = -5979750
56 Z = -1822627
97
XDOT = -15358
604284 XDOT = -4681
302586
YDOT = -1723
404871 feet/sec YDOT = -525
293805 meter/sec
ZDOT = 18515
663084 ZDOT = 5643
574108
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 12274
50358770
00016717 00000-0 10270-3 0 9097
2 25544 51
6476 317
9970 0017865 115
9440 244
3554 15
50340351 34380
Satellite: ISS
Catalog Number: 25544
Epoch time: 12274
50358770 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 317
9970 deg
Eccentricity:
0017865
Arg of perigee: 115
9440 deg
Mean anomaly: 244
3554 deg
Mean motion: 15
50340351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 321
Coasting Arc #11 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2012/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3626935
40 A = 6799471
54 meter
Y = 5571043
75 meter E =
0031654
Z = 1355547
54 I = 51
40821
XDOT = -4748
206574 Wp = 119
33722
YDOT = -1660
048972 meter/sec RA = 312
43112 deg
ZDOT = -5794
889378 TA = 45
85191
MA = 45
59207
Ha = 233
271 n
mi
Hp = 214
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11899394
36 X = -3695547
45
Y = 18277702
60 feet Y = 5530101
63 meter
Z = 4447334
45 Z = 1337760
46
XDOT = -15578
105557 XDOT = -4701
139956
YDOT = -5446
354894 feet/sec YDOT = -1712
883908 meter/sec
ZDOT = -19012
104258 ZDOT = -5817
841781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8635572
22 X = 2632122
41
Y = -20043717
44 feet Y = -6109325
07 meter
Z = 4373221
47 Z = 1332957
90
XDOT = 14702
172449 XDOT = 4481
222162
YDOT = 2102
077064 feet/sec YDOT = 640
713089 meter/sec
ZDOT = -19106
796595 ZDOT = -5823
751602
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 12275
53492305
00016717 00000-0 10270-3 0 9106
2 25544 51
6477 312
8841 0017880 119
3235 240
9705 15
50393025 34543
Satellite: ISS
Catalog Number: 25544
Epoch time: 12275
53492305 = yrday
fracday
Element set: 910
Inclination: 51
6477 deg
RA of node: 312
8841 deg
Eccentricity:
0017880
Arg of perigee: 119
3235 deg
Mean anomaly: 240
9705 deg
Mean motion: 15
50393025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 303
Coasting Arc #12 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2012/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3478487
40 A = 6799777
21 meter
Y = -5771357
04 meter E =
0021426
Z = -937964
90 I = 51
38970
XDOT = 4543
895615 Wp = 94
94128
YDOT = 1800
459794 meter/sec RA = 307
46007 deg
ZDOT = 5887
792821 TA = 254
89681
MA = 255
13396
Ha = 233
224 n
mi
Hp = 214
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11412360
25 X = 3547321
89
Y = -18934898
42 feet Y = -5732073
64 meter
Z = -3077312
65 Z = -920898
46
XDOT = 14907
794011 XDOT = 4494
822713
YDOT = 5907
020322 feet/sec YDOT = 1850
998706 meter/sec
ZDOT = 19316
905581 ZDOT = 5909
747854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7679727
96 X = -2340781
08
Y = 20741913
43 feet Y = 6322135
21 meter
Z = -3006160
94 Z = -916277
85
XDOT = -14121
940917 XDOT = -4304
367592
YDOT = -2471
835270 feet/sec YDOT = -753
415390 meter/sec
ZDOT = 19407
458336 ZDOT = 5915
393301
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 12276
50177779
00016717 00000-0 10270-3 0 9110
2 25544 51
6476 308
0919 0017892 122
7343 237
5535 15
50415118 34693
Satellite: ISS
Catalog Number: 25544
Epoch time: 12276
50177779 = yrday
fracday
Element set: 911
Inclination: 51
6476 deg
RA of node: 308
0919 deg
Eccentricity:
0017892
Arg of perigee: 122
7343 deg
Mean anomaly: 237
5535 deg
Mean motion: 15
50415118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 327
Coasting Arc #13 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2012/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3361237
75 A = 6799988
11 meter
Y = 5881061
34 meter E =
0030689
Z = 404882
08 I = 51
37279
XDOT = -4351
358339 Wp = 127
87115
YDOT = -2055
536433 meter/sec RA = 302
48709 deg
ZDOT = -5975
057546 TA = 47
74869
MA = 47
48879
Ha = 233
102 n
mi
Hp = 214
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11027682
91 X = -3428718
05
Y = 19294820
66 feet Y = 5843096
61 meter
Z = 1328353
26 Z = 388388
61
XDOT = -14276
110036 XDOT = -4299
023492
YDOT = -6743
885934 feet/sec YDOT = -2103
903949 meter/sec
ZDOT = -19603
207173 ZDOT = -5996
069320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6861257
42 X = 2091311
26
Y = -21142399
80 feet Y = -6444203
46 meter
Z = 1259561
15 Z = 383914
24
XDOT = 13693
467609 XDOT = 4173
768927
YDOT = 3210
775342 feet/sec YDOT = 978
644324 meter/sec
ZDOT = -19689
833634 ZDOT = -6001
461292
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
53306418
00016717 00000-0 10270-3 0 9129
2 25544 51
6473 302
9785 0017955 126
3782 233
9028 15
50451231 34852
Satellite: ISS
Catalog Number: 25544
Epoch time: 12277
53306418 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 302
9785 deg
Eccentricity:
0017955
Arg of perigee: 126
3782 deg
Mean anomaly: 233
9028 deg
Mean motion: 15
50451231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 315
Coasting Arc #14 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2012/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3176096
94 A = 6799891
32 meter
Y = -6014427
19 meter E =
0022774
Z = 48075
01 I = 51
35767
XDOT = 4198
882741 Wp = 97
38643
YDOT = 2284
706529 meter/sec RA = 297
51384 deg
ZDOT = 5978
031242 TA = 263
13207
MA = 263
39122
Ha = 232
997 n
mi
Hp = 214
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10420265
55 X = 3242881
92
Y = -19732372
67 feet Y = -5978536
67 meter
Z = 157726
41 Z = 63667
28
XDOT = 13775
862012 XDOT = 4143
982173
YDOT = 7495
756330 feet/sec YDOT = 2331
354539 meter/sec
ZDOT = 19612
963393 ZDOT = 5998
296049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5798596
68 X = -1767412
27
Y = 21547621
15 feet Y = 6567714
93 meter
Z = 222805
04 Z = 67910
98
XDOT = -13403
812176 XDOT = -4085
481951
YDOT = -3869
532041 feet/sec YDOT = -1179
433366 meter/sec
ZDOT = 19696
479464 ZDOT = 6003
486941
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
56432469
00016717 00000-0 10270-3 0 9130
2 25544 51
6474 297
8666 0017896 130
0361 230
2363 15
50498744 35013
Satellite: ISS
Catalog Number: 25544
Epoch time: 12278
56432469 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 297
8666 deg
Eccentricity:
0017896
Arg of perigee: 130
0361 deg
Mean anomaly: 230
2363 deg
Mean motion: 15
50498744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 327
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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