[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 11th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 32291 73 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
016/01:57:55
297 -1
3 3
5 3
5
N/A 3
1 -0
3 228
5
000/00:07:50
593 -1
0 -0
1 221
1
Coasting Arc #1 (Orbit 2686)
---------------------------------------
Vector Time (GMT): 2014/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6243885
20 A = 6797524
24 meter
Y = 29955
70 meter E =
0016592
Z = 2662079
16 I = 51
77236
XDOT = 2206
466252 Wp = 60
01470
YDOT = -5169
167814 meter/sec RA = 160
10189 deg
ZDOT = 5217
186330 TA = 329
93554
MA = 330
03069
Ha = 228
240 n
mi
Hp = 220
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20485187
68 X = -6256687
62
Y = 98279
86 feet Y = -39939
14 meter
Z = 8733855
50 Z = 2631716
18
XDOT = 7239
062505 XDOT = 2238
761664
YDOT = -16959
211987 feet/sec YDOT = -5144
313425 meter/sec
ZDOT = 17116
753052 ZDOT = 5227
983168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6818323
06 X = -2078224
87
Y = -19374795
02 feet Y = -5905437
52 meter
Z = 8605846
47 Z = 2623062
01
XDOT = 16945
385424 XDOT = 5164
953477
YDOT = 1684
058035 feet/sec YDOT = 513
300889 meter/sec
ZDOT = 17163
022458 ZDOT = 5231
289245
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 14010
55918386
00016717 00000-0 10270-3 0 9008
2 25544 51
6457 160
8739 0005495 11
5494 348
5782 15
50318644 26878
Satellite: ISS
Catalog Number: 25544
Epoch time: 14010
55918386 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 160
8739 deg
Eccentricity:
0005495
Arg of perigee: 11
5494 deg
Mean anomaly: 348
5782 deg
Mean motion: 15
50318644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2687
Checksum: 330
Coasting Arc #2 (Orbit 2701)
---------------------------------------
Vector Time (GMT): 2014/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6072593
54 A = 6796510
32 meter
Y = -159628
75 meter E =
0006967
Z = -3057909
70 I = 51
79819
XDOT = -2341
119322 Wp = 55
83140
YDOT = 5362
206747 meter/sec RA = 155
15646 deg
ZDOT = -4933
301652 TA = 159
07014
MA = 159
04160
Ha = 228
259 n
mi
Hp = 219
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19923207
15 X = 6088781
51
Y = -523716
36 feet Y = -91630
41 meter
Z = -10032512
13 Z = -3028370
68
XDOT = -7680
837672 XDOT = -2376
942399
YDOT = 17592
541820 feet/sec YDOT = 5335
826893 meter/sec
ZDOT = -16185
372875 ZDOT = -4944
761093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7359907
04 X = 2243299
66
Y = 18588281
84 feet Y = 5665708
31 meter
Z = -9907941
68 Z = -3019940
62
XDOT = -17769
069768 XDOT = -5416
012465
YDOT = -1610
261887 feet/sec YDOT = -490
807823 meter/sec
ZDOT = -16234
474966 ZDOT = -4948
267970
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 14011
52608741
00016717 00000-0 10270-3 0 9018
2 25544 51
6458 156
0816 0005685 15
2145 344
9176 15
50342769 27027
Satellite: ISS
Catalog Number: 25544
Epoch time: 14011
52608741 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 156
0816 deg
Eccentricity:
0005685
Arg of perigee: 15
2145 deg
Mean anomaly: 344
9176 deg
Mean motion: 15
50342769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2702
Checksum: 299
Coasting Arc #3 (Orbit 2717)
---------------------------------------
Vector Time (GMT): 2014/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5861132
39 A = 6795383
21 meter
Y = 265295
43 meter E =
0015254
Z = 3410502
75 I = 51
82352
XDOT = 2449
084190 Wp = 69
35117
YDOT = -5599
215555 meter/sec RA = 150
21187 deg
ZDOT = 4632
946353 TA = 330
38767
MA = 330
47396
Ha = 228
325 n
mi
Hp = 219
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19229436
97 X = -5880230
39
Y = 870391
82 feet Y = 199645
47 meter
Z = 11189313
47 Z = 3381983
99
XDOT = 8035
053117 XDOT = 2489
008618
YDOT = -18370
129773 feet/sec YDOT = -5571
605447 meter/sec
ZDOT = 15199
955225 ZDOT = 4644
940145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7755164
17 X = -2363774
04
Y = -17693613
05 feet Y = -5393013
26 meter
Z = 11069013
06 Z = 3373835
18
XDOT = 18705
186137 XDOT = 5701
340735
YDOT = 1366
446321 feet/sec YDOT = 416
492839 meter/sec
ZDOT = 15251
356768 ZDOT = 4648
613543
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 14012
55742592
00016717 00000-0 10270-3 0 9026
2 25544 51
6467 150
9695 0005613 18
5248 341
6106 15
50398797 27182
Satellite: ISS
Catalog Number: 25544
Epoch time: 14012
55742592 = yrday
fracday
Element set: 902
Inclination: 51
6467 deg
RA of node: 150
9695 deg
Eccentricity:
0005613
Arg of perigee: 18
5248 deg
Mean anomaly: 341
6106 deg
Mean motion: 15
50398797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2718
Checksum: 322
Coasting Arc #4 (Orbit 2732)
---------------------------------------
Vector Time (GMT): 2014/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5648247
58 A = 6794285
14 meter
Y = -305877
80 meter E =
0010188
Z = -3776203
12 I = 51
84663
XDOT = -2532
344231 Wp = 50
49655
YDOT = 5828
979303 meter/sec RA = 145
26848 deg
ZDOT = -4261
270591 TA = 174
41981
MA = 174
40845
Ha = 228
320 n
mi
Hp = 219
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18530996
00 X = 5669591
59
Y = -1003536
10 feet Y = -242595
87 meter
Z = -12389117
84 Z = -3748713
16
XDOT = -8308
215980 XDOT = -2576
637279
YDOT = 19123
947844 feet/sec YDOT = 5800
413679 meter/sec
ZDOT = -13980
546558 ZDOT = -4273
679392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7922259
87 X = 2414704
81
Y = 16867220
26 feet Y = 5141128
73 meter
Z = -12273133
98 Z = -3740851
24
XDOT = -19580
437919 XDOT = -5968
117478
YDOT = -1011
497388 feet/sec YDOT = -308
304404 meter/sec
ZDOT = -14033
743686 ZDOT = -4277
485076
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 14013
52428499
00016717 00000-0 10270-3 0 9032
2 25544 51
6471 146
1772 0005762 21
9063 338
2333 15
50403555 27338
Satellite: ISS
Catalog Number: 25544
Epoch time: 14013
52428499 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 146
1772 deg
Eccentricity:
0005762
Arg of perigee: 21
9063 deg
Mean anomaly: 338
2333 deg
Mean motion: 15
50403555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2733
Checksum: 294
Coasting Arc #5 (Orbit 2748)
---------------------------------------
Vector Time (GMT): 2014/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5404078
83 A = 6793007
27 meter
Y = 310241
26 meter E =
0013238
Z = 4090981
56 I = 51
86909
XDOT = 2586
768114 Wp = 77
37527
YDOT = -6093
984318 meter/sec RA = 140
32561 deg
ZDOT = 3871
470139 TA = 332
66683
MA = 332
73642
Ha = 228
412 n
mi
Hp = 219
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17729917
41 X = -5427018
79
Y = 1017851
92 feet Y = 249680
85 meter
Z = 13421855
50 Z = 4064673
93
XDOT = 8486
772029 XDOT = 2635
914032
YDOT = -19993
386871 feet/sec YDOT = -6064
782910 meter/sec
ZDOT = 12701
673684 ZDOT = 3884
155075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7913308
48 X = -2411976
42
Y = -15991660
74 feet Y = -4874258
19 meter
Z = 13310842
75 Z = 4057144
87
XDOT = 20521
814183 XDOT = 6255
048963
YDOT = 483
930451 feet/sec YDOT = 147
502001 meter/sec
ZDOT = 12756
085805 ZDOT = 3888
054954
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 14014
55557499
00016717 00000-0 10270-3 0 9040
2 25544 51
6482 141
0650 0005784 25
3918 334
7516 15
50475376 27491
Satellite: ISS
Catalog Number: 25544
Epoch time: 14014
55557499 = yrday
fracday
Element set: 904
Inclination: 51
6482 deg
RA of node: 141
0650 deg
Eccentricity:
0005784
Arg of perigee: 25
3918 deg
Mean anomaly: 334
7516 deg
Mean motion: 15
50475376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2749
Checksum: 325
Coasting Arc #6 (Orbit 2763)
---------------------------------------
Vector Time (GMT): 2014/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5174283
23 A = 6791930
07 meter
Y = -249001
77 meter E =
0013774
Z = -4407062
14 I = 51
88905
XDOT = -2603
802013 Wp = 53
50562
YDOT = 6331
580902 meter/sec RA = 135
38373 deg
ZDOT = -3414
283737 TA = 181
93514
MA = 181
94048
Ha = 228
377 n
mi
Hp = 219
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16975994
86 X = 5198090
82
Y = -816934
95 feet Y = -191006
25 meter
Z = -14458865
29 Z = -4381868
78
XDOT = -8542
657523 XDOT = -2657
824407
YDOT = 20772
903222 feet/sec YDOT = 6302
161678 meter/sec
ZDOT = -11201
718296 ZDOT = -3427
063274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7699323
84 X = 2346753
91
Y = 15252387
87 feet Y = 4648927
82 meter
Z = -14352548
43 Z = -4374656
76
XDOT = -21309
510450 XDOT = -6495
138785
YDOT = 162
741586 feet/sec YDOT = 49
603635 meter/sec
ZDOT = -11256
575080 ZDOT = -3431
004084
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 14015
52238895
00016717 00000-0 10270-3 0 9055
2 25544 51
6486 136
2728 0005891 28
4928 331
6544 15
50470637 27640
Satellite: ISS
Catalog Number: 25544
Epoch time: 14015
52238895 = yrday
fracday
Element set: 905
Inclination: 51
6486 deg
RA of node: 136
2728 deg
Eccentricity:
0005891
Arg of perigee: 28
4928 deg
Mean anomaly: 331
6544 deg
Mean motion: 15
50470637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2764
Checksum: 329
Coasting Arc #7 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2014/016/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3796758
95 A = 6790144
00 meter
Y = 1987141
82 meter E =
0016162
Z = -5280793
93 I = 51
89057
XDOT = -4537
715882 Wp = 66
91368
YDOT = 6081
669355 meter/sec RA = 132
48351 deg
ZDOT = -970
195445 TA = 193
78845
MA = 193
83264
Ha = 228
546 n
mi
Hp = 221
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12456558
23 X = 3799908
07
Y = 6519494
15 feet Y = 2029617
49 meter
Z = -17325439
40 Z = -5262342
37
XDOT = -14887
519299 XDOT = -4600
672395
YDOT = 19952
983449 feet/sec YDOT = 6030
573762 meter/sec
ZDOT = -3183
055923 ZDOT = -992
391254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6570409
51 X = -2002660
82
Y = -12537161
46 feet Y = -3821326
81 meter
Z = -17247892
59 Z = -5257157
66
XDOT = 22698
316897 XDOT = 6918
446990
YDOT = -7369
242334 feet/sec YDOT = -2246
145063 meter/sec
ZDOT = -3277
606596 ZDOT = -999
014490
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 14016
10246982
00016717 00000-0 10270-3 0 9067
2 25544 51
6493 133
4005 0004544 8
1691 351
9533 15
49860770 27733
Satellite: ISS
Catalog Number: 25544
Epoch time: 14016
10246982 = yrday
fracday
Element set: 906
Inclination: 51
6493 deg
RA of node: 133
4005 deg
Eccentricity:
0004544
Arg of perigee: 8
1691 deg
Mean anomaly: 351
9533 deg
Mean motion: 15
49860770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 304
Coasting Arc #8 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2014/017/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3738220
16 A = 6789817
01 meter
Y = -1968594
58 meter E =
0004731
Z = 5311922
64 I = 51
91020
XDOT = 4247
520380 Wp = 48
26382
YDOT = -6348
292665 meter/sec RA = 127
54653 deg
ZDOT = 639
184411 TA = 35
66981
MA = 35
63820
Ha = 228
633 n
mi
Hp = 220
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12264501
83 X = -3741732
21
Y = -6458643
65 feet Y = -2010417
58 meter
Z = 17427567
71 Z = 5293754
62
XDOT = 13935
434319 XDOT = 4315
087825
YDOT = -20827
731841 feet/sec YDOT = -6300
416413 meter/sec
ZDOT = 2097
061715 ZDOT = 659
981773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6660266
58 X = 2030049
25
Y = 12264935
75 feet Y = 3738352
42 meter
Z = 17351207
43 Z = 5288648
03
XDOT = -22283
833273 XDOT = -6792
112382
YDOT = 9021
248792 feet/sec YDOT = 2749
676632 meter/sec
ZDOT = 2185
764687 ZDOT = 666
221077
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 14017
13413753
00016717 00000-0 10270-3 0 9074
2 25544 51
6493 128
2909 0004551 10
5511 349
5734 15
49903728 27898
Satellite: ISS
Catalog Number: 25544
Epoch time: 14017
13413753 = yrday
fracday
Element set: 907
Inclination: 51
6493 deg
RA of node: 128
2909 deg
Eccentricity:
0004551
Arg of perigee: 10
5511 deg
Mean anomaly: 349
5734 deg
Mean motion: 15
49903728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 316
Coasting Arc #9 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2014/018/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3711306
42 A = 6789634
78 meter
Y = 1970760
07 meter E =
0016766
Z = -5347043
15 I = 51
92850
XDOT = -3920
578652 Wp = 72
13892
YDOT = 6561
810847 meter/sec RA = 122
61054 deg
ZDOT = -298
503299 TA = 194
99500
MA = 195
04477
Ha = 228
604 n
mi
Hp = 220
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12176202
16 X = 3714966
85
Y = 6465748
27 feet Y = 2012282
84 meter
Z = -17542792
48 Z = -5329005
55
XDOT = -12862
790853 XDOT = -3992
212893
YDOT = 21528
250809 feet/sec YDOT = 6517
567909 meter/sec
ZDOT = -979
341531 ZDOT = -317
722436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6792907
80 X = -2070478
30
Y = -12106877
37 feet Y = -3690176
22 meter
Z = -17466977
17 Z = -5323934
64
XDOT = 21615
276774 XDOT = 6588
336361
YDOT = -10576
412834 feet/sec YDOT = -3223
690632 meter/sec
ZDOT = -1061
428245 ZDOT = -323
523329
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 14018
10130521
00016717 00000-0 10270-3 0 9082
2 25544 51
6499 123
5007 0004705 14
3431 345
7852 15
49933249 28043
Satellite: ISS
Catalog Number: 25544
Epoch time: 14018
10130521 = yrday
fracday
Element set: 908
Inclination: 51
6499 deg
RA of node: 123
5007 deg
Eccentricity:
0004705
Arg of perigee: 14
3431 deg
Mean anomaly: 345
7852 deg
Mean motion: 15
49933249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 289
Coasting Arc #10 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2014/019/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3669391
11 A = 6789461
43 meter
Y = -2010483
32 meter E =
0005961
Z = 5343752
38 I = 51
94423
XDOT = 3604
918082 Wp = 39
67312
YDOT = -6764
110572 meter/sec RA = 117
67507 deg
ZDOT = -64
972222 TA = 50
97020
MA = 50
91715
Ha = 228
696 n
mi
Hp = 220
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12038684
75 X = -3672594
50
Y = -6596073
89 feet Y = -2051534
72 meter
Z = 17531995
98 Z = 5325919
51
XDOT = 11827
159062 XDOT = 3680
603560
YDOT = -22191
963820 feet/sec YDOT = -6723
374894 meter/sec
ZDOT = -213
163458 ZDOT = -47
276523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6814441
97 X = 2077041
91
Y = 12025968
32 feet Y = 3665515
14 meter
Z = 17457046
46 Z = 5320907
76
XDOT = -20906
582701 XDOT = -6372
326407
YDOT = 12067
688315 feet/sec YDOT = 3678
231398 meter/sec
ZDOT = -137
464832 ZDOT = -41
899281
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 14019
13292588
00016717 00000-0 10270-3 0 9099
2 25544 51
6498 118
3908 0004721 17
1626 342
9683 15
49975584 28206
Satellite: ISS
Catalog Number: 25544
Epoch time: 14019
13292588 = yrday
fracday
Element set: 909
Inclination: 51
6498 deg
RA of node: 118
3908 deg
Eccentricity:
0004721
Arg of perigee: 17
1626 deg
Mean anomaly: 342
9683 deg
Mean motion: 15
49975584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 339
Coasting Arc #11 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2014/020/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3668710
61 A = 6789448
82 meter
Y = 2060776
44 meter E =
0016830
Z = -5342199
51 I = 51
95776
XDOT = -3260
040584 Wp = 77
37306
YDOT = 6907
014252 meter/sec RA = 112
74009 deg
ZDOT = 430
320726 TA = 196
69511
MA = 196
75059
Ha = 228
650 n
mi
Hp = 220
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12036452
13 X = 3671344
17
Y = 6761077
55 feet Y = 2101816
97 meter
Z = -17526901
28 Z = -5324371
33
XDOT = -10695
671207 XDOT = -3339
124393
YDOT = 22660
807913 feet/sec YDOT = 6870
116218 meter/sec
ZDOT = 1411
813404 ZDOT = 414
291987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6933420
18 X = -2113306
47
Y = -12047274
33 feet Y = -3672009
22 meter
Z = -17451976
50 Z = -5319362
44
XDOT = 19963
433376 XDOT = 6084
854493
YDOT = -13412
474979 feet/sec YDOT = -4088
122374 meter/sec
ZDOT = 1343
117926 ZDOT = 409
382344
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 14020
10004929
00016717 00000-0 10270-3 0 9100
2 25544 51
6496 113
5999 0004844 20
2800 339
8543 15
50003334 28359
Satellite: ISS
Catalog Number: 25544
Epoch time: 14020
10004929 = yrday
fracday
Element set: 910
Inclination: 51
6496 deg
RA of node: 113
5999 deg
Eccentricity:
0004844
Arg of perigee: 20
2800 deg
Mean anomaly: 339
8543 deg
Mean motion: 15
50003334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2835
Checksum: 283
Coasting Arc #12 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2014/021/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3659884
54 A = 6789470
74 meter
Y = -2149901
06 meter E =
0007684
Z = 5295665
92 I = 51
96936
XDOT = 2933
809516 Wp = 38
37447
YDOT = -7033
675301 meter/sec RA = 107
80563 deg
ZDOT = -821
403754 TA = 59
48254
MA = 59
40671
Ha = 228
741 n
mi
Hp = 220
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12007495
22 X = -3661296
18
Y = -7053481
17 feet Y = -2190836
02 meter
Z = 17374232
01 Z = 5277883
55
XDOT = 9625
359303 XDOT = 3016
233661
YDOT = -23076
362537 feet/sec YDOT = -7000
406725 meter/sec
ZDOT = -2694
894207 ZDOT = -806
951568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6967534
07 X = 2123704
38
Y = 12164530
19 feet Y = 3707748
80 meter
Z = 17299513
01 Z = 5272891
56
XDOT = -19000
184978 XDOT = -5791
256381
YDOT = 14657
491396 feet/sec YDOT = 4467
603378 meter/sec
ZDOT = -2632
822364 ZDOT = -802
484256
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 14021
13162312
00016717 00000-0 10270-3 0 9116
2 25544 51
6496 108
4896 0004864 23
4817 336
6555 15
50045967 28517
Satellite: ISS
Catalog Number: 25544
Epoch time: 14021
13162312 = yrday
fracday
Element set: 911
Inclination: 51
6496 deg
RA of node: 108
4896 deg
Eccentricity:
0004864
Arg of perigee: 23
4817 deg
Mean anomaly: 336
6555 deg
Mean motion: 15
50045967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 307
Coasting Arc #13 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2014/022/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3699256
83 A = 6789662
28 meter
Y = 2236385
65 meter E =
0016290
Z = -5249338
79 I = 51
97800
XDOT = -2588
311826 Wp = 82
35298
YDOT = 7097
538455 meter/sec RA = 102
87100 deg
ZDOT = 1205
075072 TA = 199
15077
MA = 199
21208
Ha = 228
689 n
mi
Hp = 220
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12136669
37 X = 3699473
48
Y = 7337223
27 feet Y = 2277754
21 meter
Z = -17222240
11 Z = -5231368
01
XDOT = -8491
836701 XDOT = -2673
339528
YDOT = 23285
887321 feet/sec YDOT = 7068
118907 meter/sec
ZDOT = 3953
658372 ZDOT = 1192
294870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7150277
98 X = -2179404
73
Y = -12353218
12 feet Y = -3765260
88 meter
Z = -17146739
34 Z = -5226326
15
XDOT = 17839
860248 XDOT = 5437
589404
YDOT = -15713
224674 feet/sec YDOT = -4789
390881 meter/sec
ZDOT = 3898
621452 ZDOT = 1188
299819
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 14022
09870273
00016717 00000-0 10270-3 0 9125
2 25544 51
6488 103
6979 0004947 26
5049 333
6354 15
50070472 28669
Satellite: ISS
Catalog Number: 25544
Epoch time: 14022
09870273 = yrday
fracday
Element set: 912
Inclination: 51
6488 deg
RA of node: 103
6979 deg
Eccentricity:
0004947
Arg of perigee: 26
5049 deg
Mean anomaly: 333
6354 deg
Mean motion: 15
50070472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2866
Checksum: 318
Coasting Arc #14 (Orbit 2881)
---------------------------------------
Vector Time (GMT): 2014/023/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3736271
09 A = 6789912
65 meter
Y = -2360389
14 meter E =
0009658
Z = 5150882
17 I = 51
98544
XDOT = 2271
052509 Wp = 42
33868
YDOT = -7140
491506 meter/sec RA = 97
93722 deg
ZDOT = -1616
078181 TA = 63
23237
MA = 63
13358
Ha = 228
766 n
mi
Hp = 219
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12258107
26 X = -3734620
16
Y = -7744058
86 feet Y = -2402161
20 meter
Z = 16899219
71 Z = 5132736
07
XDOT = 7450
959674 XDOT = 2358
580622
YDOT = -23426
809403 feet/sec YDOT = -7114
605774 meter/sec
ZDOT = -5302
093771 ZDOT = -1604
833096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7275970
51 X = 2217715
81
Y = 12643663
11 feet Y = 3853788
52 meter
Z = 16822999
28 Z = 5127650
18
XDOT = -16691
530019 XDOT = -5087
578350
YDOT = 16633
601677 feet/sec YDOT = 5069
921791 meter/sec
ZDOT = -5253
515969 ZDOT = -1601
271667
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 14023
13023018
00016717 00000-0 10270-3 0 9139
2 25544 51
6490 98
5872 0004960 29
7667 330
3765 15
50113572 28829
Satellite: ISS
Catalog Number: 25544
Epoch time: 14023
13023018 = yrday
fracday
Element set: 913
Inclination: 51
6490 deg
RA of node: 98
5872 deg
Eccentricity:
0004960
Arg of perigee: 29
7667 deg
Mean anomaly: 330
3765 deg
Mean motion: 15
50113572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2882
Checksum: 302
Coasting Arc #15 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2014/024/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3824775
42 A = 6790323
13 meter
Y = 2466480
27 meter E =
0015134
Z = -5052194
32 I = 51
98929
XDOT = -1946
178296 Wp = 86
52388
YDOT = 7121
295881 meter/sec RA = 93
00273 deg
ZDOT = 2009
332576 TA = 202
91287
MA = 202
98046
Ha = 228
722 n
mi
Hp = 219
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12548475
78 X = 3821452
22
Y = 8092126
88 feet Y = 2509232
75 meter
Z = -16575440
70 Z = -5033622
29
XDOT = -6385
099396 XDOT = -2035
426211
YDOT = 23363
831632 feet/sec YDOT = 7099
033470 meter/sec
ZDOT = 6592
298478 ZDOT = 1999
661553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7590971
94 X = -2313728
25
Y = -12957761
75 feet Y = -3949525
78 meter
Z = -16497440
76 Z = -5028419
94
XDOT = 15400
024106 XDOT = 4693
927348
YDOT = -17335
924436 feet/sec YDOT = -5283
989768 meter/sec
ZDOT = 6550
352685 ZDOT = 1996
547498
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 14024
09726668
00016717 00000-0 10270-3 0 9147
2 25544 51
6479 93
7948 0005011 33
3243 326
8222 15
50135033 28976
Satellite: ISS
Catalog Number: 25544
Epoch time: 14024
09726668 = yrday
fracday
Element set: 914
Inclination: 51
6479 deg
RA of node: 93
7948 deg
Eccentricity:
0005011
Arg of perigee: 33
3243 deg
Mean anomaly: 326
8222 deg
Mean motion: 15
50135033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2897
Checksum: 307
Coasting Arc #16 (Orbit 2912)
---------------------------------------
Vector Time (GMT): 2014/025/02:01:50
593
Vector Time (MET): N/A
Weight (LBS) : 900829
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3914591
30 A = 6790816
12 meter
Y = -2606431
60 meter E =
0011714
Z = 4893896
29 I = 51
99251
XDOT = 1661
201754 Wp = 49
77996
YDOT = -7077
784744 meter/sec RA = 88
06939 deg
ZDOT = -2429
574578 TA = 64
00011
MA = 63
87950
Ha = 228
774 n
mi
Hp = 219
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12843147
30 X = -3908927
51
Y = -8551284
77 feet Y = -2650175
43 meter
Z = 16056090
21 Z = 4874893
60
XDOT = 5450
136989 XDOT = 1752
025689
YDOT = -23221
078555 feet/sec YDOT = -7058
700277 meter/sec
ZDOT = -7971
045204 ZDOT = -2421
284196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7872875
03 X = 2399652
31
Y = 13365804
57 feet Y = 4073897
23 meter
Z = 15976296
30 Z = 4869575
11
XDOT = -14165
273786 XDOT = -4317
575450
YDOT = 17872
576111 feet/sec YDOT = 5447
561199 meter/sec
ZDOT = -7934
918353 ZDOT = -2418
563114
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 14025
12874830
00016717 00000-0 10270-3 0 9158
2 25544 51
6483 88
6840 0005004 36
3453 323
8037 15
50178203 29139
Satellite: ISS
Catalog Number: 25544
Epoch time: 14025
12874830 = yrday
fracday
Element set: 915
Inclination: 51
6483 deg
RA of node: 88
6840 deg
Eccentricity:
0005004
Arg of perigee: 36
3453 deg
Mean anomaly: 323
8037 deg
Mean motion: 15
50178203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2913
Checksum: 291
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