[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 18th 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) : 132 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 3435)
---------------------------------------
Vector Time (GMT): 2014/316/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 291767
34 A = 6798577
13 meter
Y = 6749077
89 meter E =
0018555
Z = 667352
58 I = 52
02499
XDOT = -4763
139094 Wp = 42
39106
YDOT = -395
318447 meter/sec RA = 83
10199 deg
ZDOT = 5997
030235 TA = 324
77320
MA = 324
89570
Ha = 227
635 n
mi
Hp = 218
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 957241
95 X = 213034
07
Y = 22142644
01 feet Y = 6751900
40 meter
Z = 2189476
98 Z = 668578
76
XDOT = -15627
096764 XDOT = -4787
496578
YDOT = -1296
976532 feet/sec YDOT = -448
719173 meter/sec
ZDOT = 19675
296047 ZDOT = 5973
832100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22092467
86 X = -6733784
20
Y = -1765858
79 feet Y = -538233
76 meter
Z = 2193493
01 Z = 668576
67
XDOT = 3078
951171 XDOT = 938
464317
YDOT = -13864
120325 feet/sec YDOT = -4225
783875 meter/sec
ZDOT = 19576
427356 ZDOT = 5966
895058
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 14316
65257513
00016717 00000-0 10270-3 0 9006
2 25544 51
6461 83
5832 0006015 20
9198 339
2198 15
50890190 34364
Satellite: ISS
Catalog Number: 25544
Epoch time: 14316
65257513 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 83
5832 deg
Eccentricity:
0006015
Arg of perigee: 20
9198 deg
Mean anomaly: 339
2198 deg
Mean motion: 15
50890190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 304
Coasting Arc #2 (Orbit 3450)
---------------------------------------
Vector Time (GMT): 2014/317/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -335336
61 A = 6797876
89 meter
Y = -6658850
97 meter E =
0007966
Z = -1327780
03 I = 52
01773
XDOT = 4856
993185 Wp = 100
70655
YDOT = 915
333865 meter/sec RA = 78
17168 deg
ZDOT = -5848
245244 TA = 93
64057
MA = 93
54947
Ha = 227
595 n
mi
Hp = 218
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1100185
74 X = -254400
86
Y = -21846623
93 feet Y = -6662148
40 meter
Z = -4356233
69 Z = -1329212
43
XDOT = 15935
017012 XDOT = 4874
805980
YDOT = 3003
063862 feet/sec YDOT = 969
747467 meter/sec
ZDOT = -19187
156313 ZDOT = -5824
607096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21838947
65 X = 6656511
24
Y = 1225976
59 feet Y = 373677
67 meter
Z = -4361135
70 Z = -1329274
16
XDOT = -4580
354351 XDOT = -1396
092006
YDOT = 14059
601392 feet/sec YDOT = 4285
366504 meter/sec
ZDOT = -19086
502639 ZDOT = -5817
566004
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 14317
61910313
00016717 00000-0 10270-3 0 9018
2 25544 51
6453 78
7888 0005978 24
2216 335
9215 15
50934471 34518
Satellite: ISS
Catalog Number: 25544
Epoch time: 14317
61910313 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 78
7888 deg
Eccentricity:
0005978
Arg of perigee: 24
2216 deg
Mean anomaly: 335
9215 deg
Mean motion: 15
50934471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3451
Checksum: 310
Coasting Arc #3 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2014/318/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 374567
62 A = 6796916
67 meter
Y = 6492776
59 meter E =
0019049
Z = 1938039
52 I = 52
00813
XDOT = -5015
432040 Wp = 55
40439
YDOT = -1400
196092 meter/sec RA = 73
23912 deg
ZDOT = 5631
565285 TA = 325
84162
MA = 325
96403
Ha = 227
669 n
mi
Hp = 218
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1228896
39 X = 292521
55
Y = 21301760
46 feet Y = 6496506
53 meter
Z = 6358397
37 Z = 1939659
74
XDOT = -16454
829529 XDOT = -5026
758655
YDOT = -4593
819199 feet/sec YDOT = -1456
345137 meter/sec
ZDOT = 18476
264057 ZDOT = 5607
173216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21324418
90 X = -6499682
88
Y = -686674
66 feet Y = -209298
44 meter
Z = 6364121
21 Z = 1939784
14
XDOT = 5979
682583 XDOT = 1822
607251
YDOT = -14548
750939 feet/sec YDOT = -4434
459286 meter/sec
ZDOT = 18372
483152 ZDOT = 5599
932865
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 14318
65004041
00016717 00000-0 10270-3 0 9026
2 25544 51
6458 73
6738 0006146 27
7623 332
3855 15
50978835 34679
Satellite: ISS
Catalog Number: 25544
Epoch time: 14318
65004041 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 73
6738 deg
Eccentricity:
0006146
Arg of perigee: 27
7623 deg
Mean anomaly: 332
3855 deg
Mean motion: 15
50978835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3467
Checksum: 319
Coasting Arc #4 (Orbit 3481)
---------------------------------------
Vector Time (GMT): 2014/319/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -338160
08 A = 6795615
20 meter
Y = -6285287
97 meter E =
0007513
Z = -2571054
10 I = 51
99328
XDOT = 5199
967796 Wp = 73
59102
YDOT = 1880
973158 meter/sec RA = 68
30534 deg
ZDOT = -5292
965695 TA = 135
08846
MA = 135
02766
Ha = 227
671 n
mi
Hp = 218
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1109449
08 X = -255361
86
Y = -20621023
54 feet Y = -6288606
61 meter
Z = -8435216
87 Z = -2572495
58
XDOT = 17060
261798 XDOT = 5204
259740
YDOT = 6171
171777 feet/sec YDOT = 1939
146431 meter/sec
ZDOT = -17365
373016 ZDOT = -5267
694242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20644857
84 X = 6292552
67
Y = 403885
49 feet Y = 123104
30 meter
Z = -8440206
97 Z = -2572575
08
XDOT = -7338
206584 XDOT = -2236
685367
YDOT = 15185
073450 feet/sec YDOT = 4628
410387 meter/sec
ZDOT = -17257
932011 ZDOT = -5260
217677
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 14319
61652042
00016717 00000-0 10270-3 0 9034
2 25544 51
6449 68
8788 0006194 31
0171 329
1345 15
51009068 34828
Satellite: ISS
Catalog Number: 25544
Epoch time: 14319
61652042 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 68
8788 deg
Eccentricity:
0006194
Arg of perigee: 31
0171 deg
Mean anomaly: 329
1345 deg
Mean motion: 15
51009068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3482
Checksum: 306
Coasting Arc #5 (Orbit 3497)
---------------------------------------
Vector Time (GMT): 2014/320/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 272657
97 A = 6794091
38 meter
Y = 6010638
83 meter E =
0017552
Z = 3133945
07 I = 51
97693
XDOT = -5437
967488 Wp = 68
85968
YDOT = -2311
927159 meter/sec RA = 63
36852 deg
ZDOT = 4891
358611 TA = 327
04333
MA = 327
15263
Ha = 227
694 n
mi
Hp = 217
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 894547
13 X = 190201
39
Y = 19719943
66 feet Y = 6013226
92 meter
Z = 10281972
03 Z = 3135069
16
XDOT = -17841
100684 XDOT = -5435
471860
YDOT = -7585
062858 feet/sec YDOT = -2372
723932 meter/sec
ZDOT = 16047
764473 ZDOT = 4864
947426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19737004
55 X = -6015838
99
Y = -226729
23 feet Y = -69107
07 meter
Z = 10285649
53 Z = 3135065
98
XDOT = 8516
253375 XDOT = 2595
754029
YDOT = -16071
285913 feet/sec YDOT = -4898
527946 meter/sec
ZDOT = 15935
546775 ZDOT = 4857
154657
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 14320
64740539
00016717 00000-0 10270-3 0 9049
2 25544 51
6455 63
7634 0006288 34
2911 325
8645 15
51066021 34985
Satellite: ISS
Catalog Number: 25544
Epoch time: 14320
64740539 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 63
7634 deg
Eccentricity:
0006288
Arg of perigee: 34
2911 deg
Mean anomaly: 325
8645 deg
Mean motion: 15
51066021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3498
Checksum: 308
Coasting Arc #6 (Orbit 3512)
---------------------------------------
Vector Time (GMT): 2014/321/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -118494
56 A = 6792455
69 meter
Y = -5709669
29 meter E =
0011249
Z = -3691084
94 I = 51
95612
XDOT = 5672
247030 Wp = 56
99239
YDOT = 2703
173798 meter/sec RA = 58
42925 deg
ZDOT = -4367
268792 TA = 166
57880
MA = 166
54886
Ha = 227
743 n
mi
Hp = 217
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -388761
68 X = -36708
45
Y = -18732510
80 feet Y = -5710537
20 meter
Z = -12109858
72 Z = -3691461
74
XDOT = 18609
734349 XDOT = 5662
813131
YDOT = 8868
680440 feet/sec YDOT = 2766
551652 meter/sec
ZDOT = -14328
309685 ZDOT = -4339
736287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18732577
37 X = 5709689
58
Y = 368302
89 feet Y = 112258
72 meter
Z = -12110395
24 Z = -3691248
47
XDOT = -9513
909820 XDOT = -2899
839713
YDOT = 16999
356044 feet/sec YDOT = 5181
403722 meter/sec
ZDOT = -14211
389356 ZDOT = -4331
631476
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 14321
61383781
00016717 00000-0 10270-3 0 9050
2 25544 51
6448 58
9679 0006420 37
7808 322
3793 15
51082157 35135
Satellite: ISS
Catalog Number: 25544
Epoch time: 14321
61383781 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 58
9679 deg
Eccentricity:
0006420
Arg of perigee: 37
7808 deg
Mean anomaly: 322
3793 deg
Mean motion: 15
51082157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3513
Checksum: 319
Coasting Arc #7 (Orbit 3528)
---------------------------------------
Vector Time (GMT): 2014/322/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -84433
35 A = 6790699
43 meter
Y = 5357809
11 meter E =
0014449
Z = 4157404
22 I = 51
93436
XDOT = -5939
215333 Wp = 80
29057
YDOT = -3038
670464 meter/sec RA = 53
48683 deg
ZDOT = 3786
634294 TA = 330
84182
MA = 330
92242
Ha = 227
753 n
mi
Hp = 217
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -277012
30 X = -164535
12
Y = 17578113
86 feet Y = 5356417
16 meter
Z = 13639777
62 Z = 4156799
33
XDOT = -19485
614608 XDOT = -5923
189451
YDOT = -9969
391287 feet/sec YDOT = -3104
996912 meter/sec
ZDOT = 12423
340861 ZDOT = 3757
820796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17569175
31 X = -5355084
63
Y = -699238
99 feet Y = -213128
05 meter
Z = 13636183
50 Z = 4156308
73
XDOT = 10289
658326 XDOT = 3136
287858
YDOT = -18088
219296 feet/sec YDOT = -5513
289241 meter/sec
ZDOT = 12301
029041 ZDOT = 3749
353652
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 14322
64467142
00016717 00000-0 10270-3 0 9069
2 25544 51
6454 53
8524 0006498 40
9083 319
2555 15
51145491 35290
Satellite: ISS
Catalog Number: 25544
Epoch time: 14322
64467142 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 53
8524 deg
Eccentricity:
0006498
Arg of perigee: 40
9083 deg
Mean anomaly: 319
2555 deg
Mean motion: 15
51145491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3529
Checksum: 313
Coasting Arc #8 (Orbit 3543)
---------------------------------------
Vector Time (GMT): 2014/323/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 377791
19 A = 6789135
92 meter
Y = -5004541
57 meter E =
0016254
Z = -4588480
78 I = 51
90981
XDOT = 6162
869044 Wp = 59
45453
YDOT = 3306
728717 meter/sec RA = 48
54092 deg
ZDOT = -3099
288896 TA = 179
56443
MA = 179
56301
Ha = 227
806 n
mi
Hp = 217
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1239472
41 X = 456014
97
Y = -16419099
64 feet Y = -4999879
55 meter
Z = -15054070
79 Z = -4586455
40
XDOT = 20219
386628 XDOT = 6140
490110
YDOT = 10848
847498 feet/sec YDOT = 3375
520743 meter/sec
ZDOT = -10168
270655 ZDOT = -3069
404217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16417850
36 X = 5004160
79
Y = 1366056
79 feet Y = 416374
11 meter
Z = -15044475
75 Z = -4585556
21
XDOT = -10787
364542 XDOT = -3287
988712
YDOT = 19065
016367 feet/sec YDOT = 5811
016989 meter/sec
ZDOT = -10041
451382 ZDOT = -3060
634381
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 14323
61105649
00016717 00000-0 10270-3 0 9079
2 25544 51
6454 49
0564 0006648 44
5550 315
6135 15
51154796 35446
Satellite: ISS
Catalog Number: 25544
Epoch time: 14323
61105649 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 49
0564 deg
Eccentricity:
0006648
Arg of perigee: 44
5550 deg
Mean anomaly: 315
6135 deg
Mean motion: 15
51154796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3544
Checksum: 309
Coasting Arc #9 (Orbit 3559)
---------------------------------------
Vector Time (GMT): 2014/324/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -730453
25 A = 6787612
36 meter
Y = 4621102
43 meter E =
0010781
Z = 4908013
17 I = 51
88413
XDOT = -6390
742071 Wp = 83
97579
YDOT = -3523
958180 meter/sec RA = 43
59218 deg
ZDOT = 2363
483671 TA = 342
95162
MA = 342
98782
Ha = 227
846 n
mi
Hp = 217
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2396500
15 X = -805915
37
Y = 15161097
20 feet Y = 4612512
06 meter
Z = 16102405
41 Z = 4904281
37
XDOT = -20967
001545 XDOT = -6362
342713
YDOT = -11561
542584 feet/sec YDOT = -3595
264824 meter/sec
ZDOT = 7754
211519 ZDOT = 2332
506501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15198936
55 X = -4632635
86
Y = -2266149
20 feet Y = -690722
27 meter
Z = 16085597
19 Z = 4902890
02
XDOT = 11073
220181 XDOT = 3375
117511
YDOT = -20081
346785 feet/sec YDOT = -6120
794500 meter/sec
ZDOT = 7622
785202 ZDOT = 2323
424930
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 14324
64183992
00016717 00000-0 10270-3 0 9081
2 25544 51
6455 43
9409 0006771 47
8866 312
2860 15
51219062 35605
Satellite: ISS
Catalog Number: 25544
Epoch time: 14324
64183992 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 43
9409 deg
Eccentricity:
0006771
Arg of perigee: 47
8866 deg
Mean anomaly: 312
2860 deg
Mean motion: 15
51219062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3560
Checksum: 320
Coasting Arc #10 (Orbit 3574)
---------------------------------------
Vector Time (GMT): 2014/325/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1160150
60 A = 6786579
35 meter
Y = -4266635
10 meter E =
0020007
Z = -5166335
62 I = 51
85801
XDOT = 6533
395955 Wp = 69
09421
YDOT = 3660
651735 meter/sec RA = 38
63960 deg
ZDOT = -1553
941281 TA = 185
92325
MA = 185
94694
Ha = 227
852 n
mi
Hp = 217
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3806268
38 X = 1232871
93
Y = -13998146
67 feet Y = -4253254
80 meter
Z = -16949920
01 Z = -5160523
10
XDOT = 21435
026098 XDOT = 6499
524856
YDOT = 12010
012255 feet/sec YDOT = 3733
523063 meter/sec
ZDOT = -5098
232550 ZDOT = -1522
284309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14119363
86 X = 4303582
11
Y = 3456480
73 feet Y = 1053535
33 meter
Z = -16924298
58 Z = -5158526
21
XDOT = -11054
083794 XDOT = -3369
284740
YDOT = 20815
841016 feet/sec YDOT = 6344
668342 meter/sec
ZDOT = -4963
943435 ZDOT = -1513
009959
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 14325
60817793
00016717 00000-0 10270-3 0 9092
2 25544 51
6462 39
1446 0006864 51
2791 308
8973 15
51228053 35752
Satellite: ISS
Catalog Number: 25544
Epoch time: 14325
60817793 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 39
1446 deg
Eccentricity:
0006864
Arg of perigee: 51
2791 deg
Mean anomaly: 308
8973 deg
Mean motion: 15
51228053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3575
Checksum: 328
Coasting Arc #11 (Orbit 3590)
---------------------------------------
Vector Time (GMT): 2014/326/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1647559
56 A = 6785756
62 meter
Y = 3902579
36 meter E =
0008880
Z = 5293568
00 I = 51
83013
XDOT = -6647
193887 Wp = 71
59475
YDOT = -3762
729688 meter/sec RA = 33
68449 deg
ZDOT = 706
904676 TA = 11
68404
MA = 11
66345
Ha = 227
935 n
mi
Hp = 216
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5405379
15 X = -1716791
74
Y = 12803738
07 feet Y = 3883767
94 meter
Z = 17367349
09 Z = 5285396
22
XDOT = -21808
378893 XDOT = -6608
058127
YDOT = -12344
913673 feet/sec YDOT = -3836
844131 meter/sec
ZDOT = 2319
241063 ZDOT = 674
707639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13063379
63 X = -3981718
11
Y = -4872153
47 feet Y = -1485032
38 meter
Z = 17331730
44 Z = 5282711
44
XDOT = 10890
476502 XDOT = 3319
417238
YDOT = -21456
106445 feet/sec YDOT = -6539
821245 meter/sec
ZDOT = 2182
677026 ZDOT = 665
279957
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 14326
63891215
00016717 00000-0 10270-3 0 9109
2 25544 51
6454 34
0288 0007038 54
9845 305
1966 15
51291929 35917
Satellite: ISS
Catalog Number: 25544
Epoch time: 14326
63891215 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 34
0288 deg
Eccentricity:
0007038
Arg of perigee: 54
9845 deg
Mean anomaly: 305
1966 deg
Mean motion: 15
51291929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3591
Checksum: 320
Coasting Arc #12 (Orbit 3605)
---------------------------------------
Vector Time (GMT): 2014/327/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2182467
00 A = 6785620
98 meter
Y = -3596731
91 meter E =
0021055
Z = -5341860
01 I = 51
80405
XDOT = 6641
783038 Wp = 80
47789
YDOT = 3789
306623 meter/sec RA = 28
72640 deg
ZDOT = 166
130237 TA = 191
08261
MA = 191
12906
Ha = 227
875 n
mi
Hp = 216
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7160324
79 X = 2248473
87
Y = -11800301
55 feet Y = -3571956
76 meter
Z = -17525787
45 Z = -5331097
56
XDOT = 21790
626766 XDOT = 6598
109468
YDOT = 12432
108342 feet/sec YDOT = 3863
335142 meter/sec
ZDOT = 545
046710 ZDOT = 198
289917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12261432
43 X = 3737284
60
Y = 6465778
93 feet Y = 1970769
42 meter
Z = -17479175
35 Z = -5327652
65
XDOT = -10476
797174 XDOT = -3193
327779
YDOT = 21674
808015 feet/sec YDOT = 6606
481483 meter/sec
ZDOT = 681
440121 ZDOT = 207
702949
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 14327
60520370
00016717 00000-0 10270-3 0 9119
2 25544 51
6464 29
2322 0007046 57
8832 302
3003 15
51300666 36067
Satellite: ISS
Catalog Number: 25544
Epoch time: 14327
60520370 = yrday
fracday
Element set: 911
Inclination: 51
6464 deg
RA of node: 29
2322 deg
Eccentricity:
0007046
Arg of perigee: 57
8832 deg
Mean anomaly: 302
3003 deg
Mean motion: 15
51300666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3606
Checksum: 270
Coasting Arc #13 (Orbit 3621)
---------------------------------------
Vector Time (GMT): 2014/328/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2760193
72 A = 6785796
52 meter
Y = 3296306
98 meter E =
0011035
Z = 5242672
26 I = 51
77596
XDOT = -6574
138846 Wp = 59
51787
YDOT = -3807
296647 meter/sec RA = 23
76592 deg
ZDOT = -1060
244996 TA = 40
65688
MA = 40
57454
Ha = 227
972 n
mi
Hp = 216
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9055753
68 X = -2822316
29
Y = 10814655
46 feet Y = 3265093
01 meter
Z = 17200368
30 Z = 5229112
73
XDOT = -21568
697002 XDOT = -6525
925744
YDOT = -12491
130730 feet/sec YDOT = -3880
543281 meter/sec
ZDOT = -3478
494081 ZDOT = -1092
064927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11547661
80 X = -3519727
32
Y = -8223348
30 feet Y = -2506476
56 meter
Z = 17141883
41 Z = 5224846
06
XDOT = 10038
070985 XDOT = 3059
604036
YDOT = -21677
230442 feet/sec YDOT = -6607
219839 meter/sec
ZDOT = -3613
431093 ZDOT = -1101
373797
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 14328
63588940
00016717 00000-0 10270-3 0 9121
2 25544 51
6449 24
1155 0007226 61
7792 298
4087 15
51367292 36220
Satellite: ISS
Catalog Number: 25544
Epoch time: 14328
63588940 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 24
1155 deg
Eccentricity:
0007226
Arg of perigee: 61
7792 deg
Mean anomaly: 298
4087 deg
Mean motion: 15
51367292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3622
Checksum: 325
Coasting Arc #14 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2014/329/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3342713
25 A = 6786672
56 meter
Y = -3074881
71 meter E =
0018918
Z = -5059196
69 I = 51
75074
XDOT = 6371
561634 Wp = 89
93052
YDOT = 3771
630425 meter/sec RA = 18
80440 deg
ZDOT = 1923
745480 TA = 198
71031
MA = 198
77994
Ha = 227
881 n
mi
Hp = 216
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10966906
97 X = 3401425
10
Y = -10088194
58 feet Y = -3037172
71 meter
Z = -16598414
32 Z = -5042815
65
XDOT = 20904
073603 XDOT = 6319
567780
YDOT = 12374
115566 feet/sec YDOT = 3842
590515 meter/sec
ZDOT = 6311
500919 ZDOT = 1954
571973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11157471
78 X = 3400797
40
Y = 9994505
74 feet Y = 3046325
35 meter
Z = -16527938
62 Z = -5037715
69
XDOT = -9472
831091 XDOT = -2887
318916
YDOT = 21194
531791 feet/sec YDOT = 6460
093290 meter/sec
ZDOT = 6442
206061 ZDOT = 1963
584407
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 14329
60213552
00016717 00000-0 10270-3 0 9134
2 25544 51
6458 19
3187 0007189 64
3518 295
8375 15
51370743 36376
Satellite: ISS
Catalog Number: 25544
Epoch time: 14329
60213552 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 19
3187 deg
Eccentricity:
0007189
Arg of perigee: 64
3518 deg
Mean anomaly: 295
8375 deg
Mean motion: 15
51370743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 324
Coasting Arc #15 (Orbit 3652)
---------------------------------------
Vector Time (GMT): 2014/330/14:08:46
376
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3941238
38 A = 6787815
45 meter
Y = 2863028
53 meter E =
0015280
Z = 4717847
71 I = 51
72387
XDOT = -6078
774107 Wp = 65
22870
YDOT = -3759
594514 meter/sec RA = 13
84081 deg
ZDOT = -2783
299556 TA = 52
37189
MA = 52
23332
Ha = 227
936 n
mi
Hp = 216
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12930572
12 X = -3995878
49
Y = 9393138
23 feet Y = 2818649
27 meter
Z = 15478503
00 Z = 4698569
01
XDOT = -19943
484602 XDOT = -6022
761165
YDOT = -12334
627670 feet/sec YDOT = -3827
257960 meter/sec
ZDOT = -9131
560223 ZDOT = -2812
693801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10868745
19 X = -3312793
53
Y = -11826124
83 feet Y = -3604602
85 meter
Z = 15395711
93 Z = 4692613
00
XDOT = 9035
887720 XDOT = 2754
138577
YDOT = -20411
658721 feet/sec YDOT = -6221
473578 meter/sec
ZDOT = -9256
157984 ZDOT = -2821
276954
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 14330
63277346
00016717 00000-0 10270-3 0 9141
2 25544 51
6444 14
2010 0007313 68
1020 292
0908 15
51444414 36535
Satellite: ISS
Catalog Number: 25544
Epoch time: 14330
63277346 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 14
2010 deg
Eccentricity:
0007313
Arg of perigee: 68
1020 deg
Mean anomaly: 292
0908 deg
Mean motion: 15
51444414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3653
Checksum: 270
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