[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 2nd 2014
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) : 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
There are no maneuvers
Coasting Arc #1 (Orbit 2546)
---------------------------------------
Vector Time (GMT): 2014/001/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6379285
87 A = 6800719
18 meter
Y = 2191134
24 meter E =
0009189
Z = 846026
86 I = 51
51038
XDOT = -852
578516 Wp = 107
11118
YDOT = 4786
704829 meter/sec RA = 204
68019 deg
ZDOT = -5917
758636 TA = 63
73992
MA = 63
64551
Ha = 227
622 n
mi
Hp = 221
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20929415
58 X = 6350200
29
Y = 7188760
62 feet Y = 2262308
76 meter
Z = 2775678
68 Z = 876945
97
XDOT = -2797
173608 XDOT = -877
294732
YDOT = 15704
412169 feet/sec YDOT = 4777
033215 meter/sec
ZDOT = -19415
218623 ZDOT = -5921
959822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3356548
52 X = -1023075
99
Y = 21856678
16 feet Y = 6661915
50 meter
Z = 2905565
28 Z = 885616
30
XDOT = -14334
549698 XDOT = -4369
170748
YDOT = 403
203176 feet/sec YDOT = 122
896328 meter/sec
ZDOT = -19433
619793 ZDOT = -5923
367313
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 14001
53397860
00016717 00000-0 10270-3 0 9004
2 25544 51
6459 205
5958 0005549 337
7171 22
3738 15
50104383 25471
Satellite: ISS
Catalog Number: 25544
Epoch time: 14001
53397860 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 205
5958 deg
Eccentricity:
0005549
Arg of perigee: 337
7171 deg
Mean anomaly: 22
3738 deg
Mean motion: 15
50104383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2547
Checksum: 309
Coasting Arc #2 (Orbit 2561)
---------------------------------------
Vector Time (GMT): 2014/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6497996
87 A = 6800977
72 meter
Y = -1916271
20 meter E =
0014425
Z = -488972
89 I = 51
53818
XDOT = 943
276561 Wp = 22
39887
YDOT = -4705
622039 meter/sec RA = 199
71765 deg
ZDOT = 5977
178088 TA = 332
32603
MA = 332
40273
Ha = 227
667 n
mi
Hp = 221
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21318887
38 X = -6473710
51
Y = -6286978
99 feet Y = -1988800
10 meter
Z = -1604241
78 Z = -520480
12
XDOT = 3094
739374 XDOT = 966
790856
YDOT = -15438
392518 feet/sec YDOT = -4694
942796 meter/sec
ZDOT = 19610
164330 ZDOT = 5981
817026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2018216
83 X = 615152
49
Y = -22124769
79 feet Y = -6743629
83 meter
Z = -1736668
68 Z = -529336
61
XDOT = 14106
669494 XDOT = 4299
712862
YDOT = -237
117845 feet/sec YDOT = -72
273519 meter/sec
ZDOT = 19630
394459 ZDOT = 5983
344231
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 14002
50102346
00016717 00000-0 10270-3 0 9016
2 25544 51
6445 200
8028 0005488 340
4800 19
6140 15
50089881 25622
Satellite: ISS
Catalog Number: 25544
Epoch time: 14002
50102346 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 200
8028 deg
Eccentricity:
0005488
Arg of perigee: 340
4800 deg
Mean anomaly: 19
6140 deg
Mean motion: 15
50089881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2562
Checksum: 272
Coasting Arc #3 (Orbit 2577)
---------------------------------------
Vector Time (GMT): 2014/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6592096
38 A = 6800885
23 meter
Y = 1660775
36 meter E =
0008098
Z = 92462
28 I = 51
56826
XDOT = -1078
388568 Wp = 112
22678
YDOT = 4637
693382 meter/sec RA = 194
75888 deg
ZDOT = -5998
040715 TA = 66
77844
MA = 66
69319
Ha = 227
775 n
mi
Hp = 221
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21627612
79 X = 6572586
13
Y = 5448738
06 feet Y = 1734383
29 meter
Z = 303353
94 Z = 124438
08
XDOT = -3538
020236 XDOT = -1101
031951
YDOT = 15215
529469 feet/sec YDOT = 4625
507950 meter/sec
ZDOT = -19678
611271 ZDOT = -6003
333997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -750941
65 X = -228887
02
Y = 22288535
42 feet Y = 6793545
60 meter
Z = 437813
00 Z = 133445
40
XDOT = -13966
708773 XDOT = -4257
052834
YDOT = -64
860923 feet/sec YDOT = -19
769609 meter/sec
ZDOT = -19701
584768 ZDOT = -6005
043037
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 14003
53252295
00016717 00000-0 10270-3 0 9020
2 25544 51
6449 195
6916 0005623 344
9435 15
1548 15
50157512 25784
Satellite: ISS
Catalog Number: 25544
Epoch time: 14003
53252295 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 195
6916 deg
Eccentricity:
0005623
Arg of perigee: 344
9435 deg
Mean anomaly: 15
1548 deg
Mean motion: 15
50157512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2578
Checksum: 308
Coasting Arc #4 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2014/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6645046
86 A = 6800943
65 meter
Y = -1373736
47 meter E =
0015970
Z = 280804
79 I = 51
59765
XDOT = 1213
733255 Wp = 31
20383
YDOT = -4616
207290 meter/sec RA = 189
80050 deg
ZDOT = 5999
366775 TA = 331
82057
MA = 331
90690
Ha = 227
838 n
mi
Hp = 221
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21801334
83 X = -6630555
60
Y = -4507009
43 feet Y = -1447964
61 meter
Z = 921275
56 Z = 248559
61
XDOT = 3982
064486 XDOT = 1236
119861
YDOT = -15145
037040 feet/sec YDOT = -4602
509642 meter/sec
ZDOT = 19682
961859 ZDOT = 6005
317022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -590924
25 X = -180113
71
Y = -22259687
56 feet Y = -6784752
77 meter
Z = 785621
78 Z = 239457
52
XDOT = 14001
309096 XDOT = 4267
599012
YDOT = 342
858982 feet/sec YDOT = 104
503418 meter/sec
ZDOT = 19708
697640 ZDOT = 6007
211041
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 14004
56400982
00016717 00000-0 10270-3 0 9033
2 25544 51
6442 190
5791 0005439 348
4723 11
6302 15
50135164 25942
Satellite: ISS
Catalog Number: 25544
Epoch time: 14004
56400982 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 190
5791 deg
Eccentricity:
0005439
Arg of perigee: 348
4723 deg
Mean anomaly: 11
6302 deg
Mean motion: 15
50135164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 289
Coasting Arc #5 (Orbit 2608)
---------------------------------------
Vector Time (GMT): 2014/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6671652
92 A = 6800569
95 meter
Y = 1114911
72 meter E =
0006690
Z = -691284
88 I = 51
62828
XDOT = -1382
710954 Wp = 112
30000
YDOT = 4613
248954 meter/sec RA = 184
84574 deg
ZDOT = -5953
068483 TA = 75
15105
MA = 75
07696
Ha = 227
925 n
mi
Hp = 220
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21888625
05 X = 6662047
88
Y = 3657846
84 feet Y = 1189464
71 meter
Z = -2267995
01 Z = -658898
54
XDOT = -4536
453261 XDOT = -1405
276750
YDOT = 15135
331213 feet/sec YDOT = 4597
660590 meter/sec
ZDOT = -19531
064576 ZDOT = -5959
840116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1820566
12 X = 554908
55
Y = 22130905
39 feet Y = 6745499
96 meter
Z = -2131693
54 Z = -649740
19
XDOT = -14140
220132 XDOT = -4309
939096
YDOT = -704
486225 feet/sec YDOT = -214
727401 meter/sec
ZDOT = -19560
259942 ZDOT = -5961
967230
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 14005
53101282
00016717 00000-0 10270-3 0 9043
2 25544 51
6448 185
7873 0005638 352
8208 7
2861 15
50206537 26094
Satellite: ISS
Catalog Number: 25544
Epoch time: 14005
53101282 = yrday
fracday
Element set: 904
Inclination: 51
6448 deg
RA of node: 185
7873 deg
Eccentricity:
0005638
Arg of perigee: 352
8208 deg
Mean anomaly: 7
2861 deg
Mean motion: 15
50206537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2609
Checksum: 301
Coasting Arc #6 (Orbit 2624)
---------------------------------------
Vector Time (GMT): 2014/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6652696
73 A = 6800373
32 meter
Y = -836025
69 meter E =
0016915
Z = 1072883
90 I = 51
65798
XDOT = 1541
953345 Wp = 40
70150
YDOT = -4661
089111 meter/sec RA = 179
89177 deg
ZDOT = 5889
378655 TA = 330
92030
MA = 331
01440
Ha = 227
999 n
mi
Hp = 220
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21826432
84 X = -6648065
35
Y = -2742866
44 feet Y = -910394
52 meter
Z = 3519960
31 Z = 1040577
48
XDOT = 5058
902052 XDOT = 1565
351558
YDOT = -15292
287110 feet/sec YDOT = -4643
715304 meter/sec
ZDOT = 19322
108449 ZDOT = 5896
925931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3069949
64 X = -935720
65
Y = -21804379
27 feet Y = -6645974
80 meter
Z = 3383941
64 Z = 1031425
41
XDOT = 14460
086664 XDOT = 4407
434415
YDOT = 988
932655 feet/sec YDOT = 301
426673 meter/sec
ZDOT = 19354
580443 ZDOT = 5899
276119
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 14006
56247093
00016717 00000-0 10270-3 0 9059
2 25544 51
6445 180
6752 0005387 356
7260 3
3854 15
50185300 26254
Satellite: ISS
Catalog Number: 25544
Epoch time: 14006
56247093 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 180
6752 deg
Eccentricity:
0005387
Arg of perigee: 356
7260 deg
Mean anomaly: 3
3854 deg
Mean motion: 15
50185300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2625
Checksum: 297
Coasting Arc #7 (Orbit 2639)
---------------------------------------
Vector Time (GMT): 2014/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6608442
21 A = 6799747
63 meter
Y = 595267
17 meter E =
0005356
Z = -1488073
25 I = 51
68776
XDOT = -1720
991233 Wp = 101
94293
YDOT = 4728
921891 meter/sec RA = 174
94069 deg
ZDOT = -5769
816460 TA = 94
25138
MA = 94
19017
Ha = 228
067 n
mi
Hp = 220
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21681240
84 X = 6608523
20
Y = 1952976
27 feet Y = 669167
47 meter
Z = -4882130
08 Z = -1455970
27
XDOT = -5646
296696 XDOT = -1745
715368
YDOT = 15514
835599 feet/sec YDOT = 4709
538566 meter/sec
ZDOT = -18929
844029 ZDOT = -5778
236704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4165338
18 X = 1269595
08
Y = 21397247
83 feet Y = 6521881
14 meter
Z = -4746920
86 Z = -1446861
48
XDOT = -14878
462627 XDOT = -4534
955409
YDOT = -1297
221224 feet/sec YDOT = -395
393029 meter/sec
ZDOT = -18966
008356 ZDOT = -5780
839347
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 14007
52944703
00016717 00000-0 10270-3 0 9069
2 25544 51
6449 175
8833 0005609 1
0360 359
0801 15
50246668 26407
Satellite: ISS
Catalog Number: 25544
Epoch time: 14007
52944703 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 175
8833 deg
Eccentricity:
0005609
Arg of perigee: 1
0360 deg
Mean anomaly: 359
0801 deg
Mean motion: 15
50246668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2640
Checksum: 300
Coasting Arc #8 (Orbit 2655)
---------------------------------------
Vector Time (GMT): 2014/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6517669
59 A = 6799248
76 meter
Y = -347341
16 meter E =
0017151
Z = 1868642
14 I = 51
71666
XDOT = 1880
827920 Wp = 50
52593
YDOT = -4848
378501 meter/sec RA = 169
99066 deg
ZDOT = 5635
106598 TA = 330
00073
MA = 330
09888
Ha = 228
139 n
mi
Hp = 220
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21383430
42 X = -6522378
39
Y = -1139570
74 feet Y = -420252
29 meter
Z = 6130715
69 Z = 1836968
82
XDOT = 6170
695276 XDOT = 1907
530283
YDOT = -15906
753612 feet/sec YDOT = -4827
196766 meter/sec
ZDOT = 18487
882540 ZDOT = 5644
308083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5224691
03 X = -1592485
83
Y = -20805546
71 feet Y = -6341530
64 meter
Z = 5997267
93 Z = 1827967
27
XDOT = 15466
168762 XDOT = 4714
088239
YDOT = 1479
769605 feet/sec YDOT = 451
033776 meter/sec
ZDOT = 18527
362733 ZDOT = 5647
140161
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 14008
56087497
00016717 00000-0 10270-3 0 9073
2 25544 51
6449 170
7714 0005362 4
8875 355
2327 15
50240863 26566
Satellite: ISS
Catalog Number: 25544
Epoch time: 14008
56087497 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 170
7714 deg
Eccentricity:
0005362
Arg of perigee: 4
8875 deg
Mean anomaly: 355
2327 deg
Mean motion: 15
50240863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2656
Checksum: 323
Coasting Arc #9 (Orbit 2670)
---------------------------------------
Vector Time (GMT): 2014/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6406169
89 A = 6798427
07 meter
Y = 147280
25 meter E =
0005120
Z = -2277426
00 I = 51
74475
XDOT = -2044
510233 Wp = 77
79845
YDOT = 4984
314117 meter/sec RA = 165
04270 deg
ZDOT = -5437
961367 TA = 127
44521
MA = 127
39862
Ha = 228
191 n
mi
Hp = 220
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21017617
74 X = 6415109
84
Y = 483202
91 feet Y = 218968
21 meter
Z = -7471870
07 Z = -2246284
02
XDOT = -6707
710737 XDOT = -2073
678137
YDOT = 16352
736603 feet/sec YDOT = 4961
288254 meter/sec
ZDOT = -17841
080600 ZDOT = -5447
963929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6094503
16 X = 1857604
56
Y = 20168662
19 feet Y = 6147408
24 meter
Z = -7340618
46 Z = -2237420
51
XDOT = -16121
220209 XDOT = -4913
747920
YDOT = -1626
320619 feet/sec YDOT = -495
702525 meter/sec
ZDOT = -17883
965114 ZDOT = -5451
032567
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 14009
52782367
00016717 00000-0 10270-3 0 9089
2 25544 51
6450 165
9793 0005572 8
9140 351
2109 15
50278865 26718
Satellite: ISS
Catalog Number: 25544
Epoch time: 14009
52782367 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 165
9793 deg
Eccentricity:
0005572
Arg of perigee: 8
9140 deg
Mean anomaly: 351
2109 deg
Mean motion: 15
50278865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2671
Checksum: 321
Coasting Arc #10 (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 = -6250798
61 A = 6797620
21 meter
Y = 46661
37 meter E =
0016616
Z = 2645897
77 I = 51
77220
XDOT = 2181
227637 Wp = 60
30373
YDOT = -5169
213856 meter/sec RA = 160
09585 deg
ZDOT = 5227
606334 TA = 329
44548
MA = 329
54217
Ha = 228
259 n
mi
Hp = 220
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20507869
46 X = -6263708
72
Y = 153088
49 feet Y = -23311
38 meter
Z = 8680766
96 Z = 2615500
95
XDOT = 7156
258652 XDOT = 2213
474823
YDOT = -16959
363044 feet/sec YDOT = -5144
641971 meter/sec
ZDOT = 17150
939415 ZDOT = 5238
280449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6877424
16 X = -2096238
88
Y = -19377969
76 feet Y = -5906405
18 meter
Z = 8552612
81 Z = 2606836
38
XDOT = 16918
113815 XDOT = 5156
641091
YDOT = 1609
879287 feet/sec YDOT = 490
691207 meter/sec
ZDOT = 17196
691459 ZDOT = 5241
551557
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
55922043
00016717 00000-0 10270-3 0 9092
2 25544 51
6454 160
8674 0005390 12
4386 347
6897 15
50298100 26878
Satellite: ISS
Catalog Number: 25544
Epoch time: 14010
55922043 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 160
8674 deg
Eccentricity:
0005390
Arg of perigee: 12
4386 deg
Mean anomaly: 347
6897 deg
Mean motion: 15
50298100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2687
Checksum: 314
Coasting Arc #11 (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 = 6083231
13 A = 6796664
85 meter
Y = -184750
88 meter E =
0006869
Z = -3035339
11 I = 51
79809
XDOT = -2305
278365 Wp = 57
52375
YDOT = 5361
482199 meter/sec RA = 155
15058 deg
ZDOT = -4951
015279 TA = 157
08315
MA = 157
05249
Ha = 228
295 n
mi
Hp = 219
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19958107
40 X = 6099589
60
Y = -606138
07 feet Y = -116632
64 meter
Z = -9958461
64 Z = -3005748
00
XDOT = -7563
249229 XDOT = -2341
009956
YDOT = 17590
164695 feet/sec YDOT = 5335
503655 meter/sec
ZDOT = -16243
488448 ZDOT = -4962
300388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7449137
48 X = 2270497
10
Y = 18592303
23 feet Y = 5666934
02 meter
Z = -9833667
88 Z = -2997301
97
XDOT = -17726
010598 XDOT = -5402
888030
YDOT = -1506
820166 feet/sec YDOT = -459
278787 meter/sec
ZDOT = -16291
855395 ZDOT = -4965
757524
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
52614117
00016717 00000-0 10270-3 0 9102
2 25544 51
6456 156
0751 0005567 16
1237 344
0090 15
50309448 27027
Satellite: ISS
Catalog Number: 25544
Epoch time: 14011
52614117 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 156
0751 deg
Eccentricity:
0005567
Arg of perigee: 16
1237 deg
Mean anomaly: 344
0090 deg
Mean motion: 15
50309448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2702
Checksum: 273
Coasting Arc #12 (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 = -5877836
14 A = 6795608
30 meter
Y = 304133
78 meter E =
0015340
Z = 3378839
26 I = 51
82352
XDOT = 2397
422088 Wp = 69
61158
YDOT = -5596
902936 meter/sec RA = 150
20628 deg
ZDOT = 4662
434287 TA = 329
68478
MA = 329
77342
Ha = 228
373 n
mi
Hp = 219
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19284239
30 X = -5897213
39
Y = 997814
23 feet Y = 238295
47 meter
Z = 11085430
63 Z = 3350238
68
XDOT = 7865
558031 XDOT = 2437
181253
YDOT = -18362
542442 feet/sec YDOT = -5569
871474 meter/sec
ZDOT = 15296
700416 ZDOT = 4674
176712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7893528
63 X = -2405947
53
Y = -17698308
05 feet Y = -5394444
30 meter
Z = 10964779
46 Z = 3342064
78
XDOT = 18636
570320 XDOT = 5680
426634
YDOT = 1220
558690 feet/sec YDOT = 372
026289 meter/sec
ZDOT = 15347
041632 ZDOT = 4677
778289
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
55750646
00016717 00000-0 10270-3 0 9115
2 25544 51
6465 150
9632 0005479 19
4758 340
6601 15
50352765 27181
Satellite: ISS
Catalog Number: 25544
Epoch time: 14012
55750646 = yrday
fracday
Element set: 911
Inclination: 51
6465 deg
RA of node: 150
9632 deg
Eccentricity:
0005479
Arg of perigee: 19
4758 deg
Mean anomaly: 340
6601 deg
Mean motion: 15
50352765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2718
Checksum: 310
Coasting Arc #13 (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 = 5672580
26 A = 6794588
18 meter
Y = -363059
32 meter E =
0009915
Z = -3734607
53 I = 51
84675
XDOT = -2462
004281 Wp = 51
59757
YDOT = 5825
111914 meter/sec RA = 145
26330 deg
ZDOT = -4307
640800 TA = 172
69202
MA = 172
67756
Ha = 228
385 n
mi
Hp = 219
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18610827
61 X = 5694359
82
Y = -1191139
49 feet Y = -299502
85 meter
Z = -12252649
38 Z = -3706998
32
XDOT = -8077
441867 XDOT = -2506
034062
YDOT = 19111
259562 feet/sec YDOT = 5797
334352 meter/sec
ZDOT = -14132
679790 ZDOT = -4319
707264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8125781
17 X = 2476738
10
Y = 16869931
22 feet Y = 5141955
03 meter
Z = -12136154
08 Z = -3699099
76
XDOT = -19481
409438 XDOT = -5937
933597
YDOT = -816
368053 feet/sec YDOT = -248
828982 meter/sec
ZDOT = -14184
432550 ZDOT = -4323
415041
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
52439872
00016717 00000-0 10270-3 0 9129
2 25544 51
6468 146
1710 0005614 22
8842 337
2558 15
50344485 27331
Satellite: ISS
Catalog Number: 25544
Epoch time: 14013
52439872 = yrday
fracday
Element set: 912
Inclination: 51
6468 deg
RA of node: 146
1710 deg
Eccentricity:
0005614
Arg of perigee: 22
8842 deg
Mean anomaly: 337
2558 deg
Mean motion: 15
50344485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2733
Checksum: 304
Coasting Arc #14 (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 = -5438399
03 A = 6793397
47 meter
Y = 392555
72 meter E =
0013454
Z = 4038675
20 I = 51
86938
XDOT = 2493
406359 Wp = 77
70579
YDOT = -6088
072701 meter/sec RA = 140
32104 deg
ZDOT = 3941
055809 TA = 331
46609
MA = 331
53967
Ha = 228
490 n
mi
Hp = 219
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17842516
51 X = -5462002
82
Y = 1287912
45 feet Y = 331607
81 meter
Z = 13250246
71 Z = 4012199
25
XDOT = 8180
467056 XDOT = 2542
155090
YDOT = -19973
991802 feet/sec YDOT = -6059
917550 meter/sec
ZDOT = 12929
973127 ZDOT = 3953
286249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8205460
89 X = -2501024
48
Y = -15988529
44 feet Y = -4873303
77 meter
Z = 13138511
70 Z = 4004618
36
XDOT = 20383
674028 XDOT = 6212
943844
YDOT = 229
689401 feet/sec YDOT = 70
009329 meter/sec
ZDOT = 12982
467291 ZDOT = 3957
056030
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
55573269
00016717 00000-0 10270-3 0 9133
2 25544 51
6480 141
0591 0005621 26
3954 333
7482 15
50403437 27494
Satellite: ISS
Catalog Number: 25544
Epoch time: 14014
55573269 = yrday
fracday
Element set: 913
Inclination: 51
6480 deg
RA of node: 141
0591 deg
Eccentricity:
0005621
Arg of perigee: 26
3954 deg
Mean anomaly: 333
7482 deg
Mean motion: 15
50403437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2749
Checksum: 301
Coasting Arc #15 (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 = 5219594
40 A = 6792404
14 meter
Y = -361827
91 meter E =
0013323
Z = -4345650
97 I = 51
88947
XDOT = -2486
364845 Wp = 53
92407
YDOT = 6324
916247 meter/sec RA = 135
37991 deg
ZDOT = -3512
913767 TA = 180
37154
MA = 180
37253
Ha = 228
470 n
mi
Hp = 219
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17124653
53 X = 5244361
95
Y = -1187099
45 feet Y = -303320
33 meter
Z = -14257385
08 Z = -4320235
17
XDOT = -8157
364977 XDOT = -2539
842336
YDOT = 20751
037556 feet/sec YDOT = 6296
813333 meter/sec
ZDOT = -11525
307634 ZDOT = -3525
121497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8097411
44 X = 2468091
01
Y = 15236214
19 feet Y = 4643998
09 meter
Z = -14150113
00 Z = -4312954
44
XDOT = -21132
919630 XDOT = -6441
313903
YDOT = 478
505480 feet/sec YDOT = 145
848470 meter/sec
ZDOT = -11577
751226 ZDOT = -3528
898574
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
52259602
00016717 00000-0 10270-3 0 9144
2 25544 51
6484 136
2672 0005712 29
5302 330
6171 15
50385449 27647
Satellite: ISS
Catalog Number: 25544
Epoch time: 14015
52259602 = yrday
fracday
Element set: 914
Inclination: 51
6484 deg
RA of node: 136
2672 deg
Eccentricity:
0005712
Arg of perigee: 29
5302 deg
Mean anomaly: 330
6171 deg
Mean motion: 15
50385449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2764
Checksum: 295
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