[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 7th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 ET - UTC (sec) : 68 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
341/18:07:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
1
342/18:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
4
344/22:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
4
348/01:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 215
4
348/05:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
349/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
351/07:21:01
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
353/08:42:47
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
Coasting Arc #1 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2017/340/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2968459
32 A = 6787524
26 meter
Y = 5708699
46 meter E =
0013900
Z = 2136198
31 I = 51
28550
XDOT = -3644
338262 Wp = 122
15769
YDOT = 3950
707808 meter/sec RA = 257
95953 deg
ZDOT = -5474
643521 TA = 34
02528
MA = 33
93623
Ha = 220
855 n
mi
Hp = 215
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9739039
75 X = 2894025
86
Y = 18729328
94 feet Y = 5741478
39 meter
Z = 7008524
64 Z = 2150438
02
XDOT = -11956
490360 XDOT = -3661
652092
YDOT = 12961
639789 feet/sec YDOT = 3909
858106 meter/sec
ZDOT = -17961
428876 ZDOT = -5492
388258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15662941
60 X = -4774064
60
Y = 14122041
30 feet Y = 4304398
19 meter
Z = 7070805
16 Z = 2155181
41
XDOT = -14506
813153 XDOT = -4421
676649
YDOT = -7026
010892 feet/sec YDOT = -2141
528120 meter/sec
ZDOT = -18040
772565 ZDOT = -5498
827478
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 17340
61978750
00016717 00000-0 10270-3 0 9005
2 25544 51
6417 258
7256 0003025 205
9108 154
1894 15
54072761 8240
Satellite: ISS
Catalog Number: 25544
Epoch time: 17340
61978750 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 258
7256 deg
Eccentricity:
0003025
Arg of perigee: 205
9108 deg
Mean anomaly: 154
1894 deg
Mean motion: 15
54072761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 824
Checksum: 309
Coasting Arc #2 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2017/341/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2364285
01 A = 6789240
48 meter
Y = -6340634
54 meter E =
0007978
Z = -502801
72 I = 51
29910
XDOT = 4350
676506 Wp = 44
36086
YDOT = -2089
592316 meter/sec RA = 252
96334 deg
ZDOT = 5956
205797 TA = 310
19100
MA = 310
26082
Ha = 220
674 n
mi
Hp = 215
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7756840
57 X = -2290764
25
Y = -20802606
76 feet Y = -6366662
47 meter
Z = -1649611
95 Z = -514108
65
XDOT = 14273
873052 XDOT = 4344
787240
YDOT = -6855
617834 feet/sec YDOT = -2040
973523 meter/sec
ZDOT = 19541
357602 ZDOT = 5977
325532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17939167
70 X = 5467858
31
Y = -13074347
94 feet Y = -3985061
25 meter
Z = -1698803
02 Z = -517795
16
XDOT = 9464
796884 XDOT = 2884
870090
YDOT = 10461
326084 feet/sec YDOT = 3188
612190 meter/sec
ZDOT = 19635
386606 ZDOT = 5984
865837
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 17341
58433441
00016717 00000-0 10270-3 0 9016
2 25544 51
6413 253
9176 0003047 214
0132 146
0826 15
54118523 8394
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
58433441 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 253
9176 deg
Eccentricity:
0003047
Arg of perigee: 214
0132 deg
Mean anomaly: 146
0826 deg
Mean motion: 15
54118523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 839
Checksum: 284
Coasting Arc #3 (Orbit 841)
---------------------------------------
Vector Time (GMT): 2017/341/18:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2249977
11 A = 6780976
86 meter
Y = 4615146
59 meter E =
0007137
Z = -4435904
96 I = 51
26857
XDOT = -4460
917997 Wp = 85
62720
YDOT = -5306
929997 meter/sec RA = 252
12684 deg
ZDOT = -3262
721110 TA = 151
30861
MA = 151
26932
Ha = 220
722 n
mi
Hp = 215
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7381814
67 X = -2279870
27
Y = 15141557
06 feet Y = 4589819
03 meter
Z = -14553493
96 Z = -4446906
86
XDOT = -14635
557734 XDOT = -4385
394261
YDOT = -17411
187653 feet/sec YDOT = -5356
392480 meter/sec
ZDOT = -10704
465585 ZDOT = -3284
207847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10342448
73 X = -3152378
37
Y = 13241892
67 feet Y = 4036128
89 meter
Z = -14603018
76 Z = -4451000
12
XDOT = -9558
032334 XDOT = -2913
288255
YDOT = -19359
725738 feet/sec YDOT = -5900
844405 meter/sec
ZDOT = -10798
986993 ZDOT = -3291
531235
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 17341
77724329
00016717 00000-0 10270-3 0 9026
2 25544 51
6368 252
9521 0003123 210
4451 149
6529 15
54114866 8424
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
77724329 = yrday
fracday
Element set: 902
Inclination: 51
6368 deg
RA of node: 252
9521 deg
Eccentricity:
0003123
Arg of perigee: 210
4451 deg
Mean anomaly: 149
6529 deg
Mean motion: 15
54114866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 842
Checksum: 304
Coasting Arc #4 (Orbit 857)
---------------------------------------
Vector Time (GMT): 2017/342/18:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3114094
59 A = 6778274
92 meter
Y = -3172798
73 meter E =
0005681
Z = 5116091
11 I = 51
27041
XDOT = 4000
902240 Wp = 158
38061
YDOT = 6366
671731 meter/sec RA = 247
10567 deg
ZDOT = 1507
336584 TA = 276
99408
MA = 277
05870
Ha = 220
618 n
mi
Hp = 215
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10216845
78 X = 3124490
82
Y = -10409444
66 feet Y = -3137916
99 meter
Z = 16785075
81 Z = 5131243
44
XDOT = 13126
319686 XDOT = 3922
089165
YDOT = 20888
030614 feet/sec YDOT = 6410
971790 meter/sec
ZDOT = 4945
330000 ZDOT = 1526
580668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11950805
33 X = 3642605
47
Y = -8224408
68 feet Y = -2506799
77 meter
Z = 16852792
04 Z = 5136731
01
XDOT = 8143
946558 XDOT = 2482
274911
YDOT = 22178
825063 feet/sec YDOT = 6760
105879 meter/sec
ZDOT = 5029
761566 ZDOT = 1533
071325
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 17342
80608852
00016717 00000-0 10270-3 0 9034
2 25544 51
6370 247
8226 0003103 215
7581 144
3364 15
54078843 8582
Satellite: ISS
Catalog Number: 25544
Epoch time: 17342
80608852 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 247
8226 deg
Eccentricity:
0003103
Arg of perigee: 215
7581 deg
Mean anomaly: 144
3364 deg
Mean motion: 15
54078843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 858
Checksum: 310
Coasting Arc #5 (Orbit 857)
---------------------------------------
Vector Time (GMT): 2017/342/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4715106
94 A = 6781165
94 meter
Y = 2123550
42 meter E =
0006907
Z = 4380927
49 I = 51
28049
XDOT = 8
891851 Wp = 85
95231
YDOT = 6901
042485 meter/sec RA = 247
02554 deg
ZDOT = -3349
631055 TA = 38
10475
MA = 38
05593
Ha = 220
547 n
mi
Hp = 215
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15469510
96 X = 4669730
03
Y = 6967028
94 feet Y = 2176023
98 meter
Z = 14373121
67 Z = 4403721
90
XDOT = 29
172738 XDOT = -52
007281
YDOT = 22641
215502 feet/sec YDOT = 6900
801619 meter/sec
ZDOT = -10989
603198 ZDOT = -3349
735348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14227730
00 X = 4336612
10
Y = 9083413
29 feet Y = 2768624
37 meter
Z = 14473948
67 Z = 4411659
56
XDOT = -2456
162812 XDOT = -748
638425
YDOT = 21387
196860 feet/sec YDOT = 6518
817603 meter/sec
ZDOT = -10991
108416 ZDOT = -3350
089845
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 17342
80608749
00016717 00000-0 10270-3 0 9040
2 25544 51
6371 247
8224 0003277 215
3253 144
7683 15
54094135 8585
Satellite: ISS
Catalog Number: 25544
Epoch time: 17342
80608749 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 247
8224 deg
Eccentricity:
0003277
Arg of perigee: 215
3253 deg
Mean anomaly: 144
7683 deg
Mean motion: 15
54094135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 858
Checksum: 319
Coasting Arc #6 (Orbit 872)
---------------------------------------
Vector Time (GMT): 2017/343/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4806153
23 A = 6784856
88 meter
Y = -3549839
77 meter E =
0003389
Z = -3219276
21 I = 51
30732
XDOT = 1174
757493 Wp = 126
09927
YDOT = -5896
592771 meter/sec RA = 242
01509 deg
ZDOT = 4749
793032 TA = 196
47648
MA = 196
48750
Ha = 220
647 n
mi
Hp = 215
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15768219
25 X = -4750463
10
Y = -11646455
92 feet Y = -3603273
92 meter
Z = -10561929
82 Z = -3242487
91
XDOT = 3854
191250 XDOT = 1217
535304
YDOT = -19345
776808 feet/sec YDOT = -5883
216865 meter/sec
ZDOT = 15583
310472 ZDOT = 4755
603266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14117592
49 X = -4303042
19
Y = -13520169
65 feet Y = -4120947
71 meter
Z = -10664409
52 Z = -3250512
02
XDOT = 5156
806983 XDOT = 1571
794769
YDOT = -17693
490882 feet/sec YDOT = -5392
976021 meter/sec
ZDOT = 15609
971281 ZDOT = 4757
919246
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 17343
77062386
00016717 00000-0 10270-3 0 9059
2 25544 51
6375 243
0136 0003184 214
8996 145
1949 15
54126468 8736
Satellite: ISS
Catalog Number: 25544
Epoch time: 17343
77062386 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 243
0136 deg
Eccentricity:
0003184
Arg of perigee: 214
8996 deg
Mean anomaly: 145
1949 deg
Mean motion: 15
54126468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 873
Checksum: 329
Coasting Arc #7 (Orbit 888)
---------------------------------------
Vector Time (GMT): 2017/344/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4636343
42 A = 6788033
35 meter
Y = 4646620
96 meter E =
0013386
Z = 1698946
26 I = 51
33317
XDOT = -2463
957358 Wp = 128
93810
YDOT = 4540
283563 meter/sec RA = 237
01664 deg
ZDOT = -5671
759081 TA = 32
34355
MA = 32
26155
Ha = 220
421 n
mi
Hp = 215
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15211100
47 X = 4575786
41
Y = 15244819
43 feet Y = 4698129
06 meter
Z = 5573970
67 Z = 1721321
33
XDOT = -8083
849599 XDOT = -2486
994208
YDOT = 14895
943449 feet/sec YDOT = 4512
601320 meter/sec
ZDOT = -18608
133468 ZDOT = -5683
784030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13438092
33 X = 4095930
54
Y = 16795553
71 feet Y = 5119284
77 meter
Z = 5672591
65 Z = 1729005
94
XDOT = -8299
206455 XDOT = -2529
598127
YDOT = 12967
055744 feet/sec YDOT = 3952
358591 meter/sec
ZDOT = -18662
166380 ZDOT = -5688
228313
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 17344
79945727
00016717 00000-0 10270-3 0 9062
2 25544 51
6364 237
8849 0003234 221
9918 138
0987 15
54139244 8891
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
79945727 = yrday
fracday
Element set: 906
Inclination: 51
6364 deg
RA of node: 237
8849 deg
Eccentricity:
0003234
Arg of perigee: 221
9918 deg
Mean anomaly: 138
0987 deg
Mean motion: 15
54139244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 889
Checksum: 357
Coasting Arc #8 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2017/344/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3260816
10 A = 6777303
08 meter
Y = -2727924
73 meter E =
0003372
Z = 5278015
13 I = 51
30519
XDOT = 4525
850002 Wp = 176
41411
YDOT = 6178
624125 meter/sec RA = 236
13856 deg
ZDOT = 393
960917 TA = 269
79272
MA = 269
83136
Ha = 220
321 n
mi
Hp = 215
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10698215
56 X = 3265440
05
Y = -8949884
29 feet Y = -2691434
40 meter
Z = 17316322
61 Z = 5293866
34
XDOT = 14848
589245 XDOT = 4454
508923
YDOT = 20271
076527 feet/sec YDOT = 6228
836367 meter/sec
ZDOT = 1292
522695 ZDOT = 415
773121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2123322
51 X = -647188
70
Y = -13696296
18 feet Y = -4174631
08 meter
Z = 17387071
23 Z = 5299579
31
XDOT = 24035
433852 XDOT = 7326
000238
YDOT = -1949
848507 feet/sec YDOT = -594
313825 meter/sec
ZDOT = 1388
424419 ZDOT = 423
191763
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 17344
99236219
00016717 00000-0 10270-3 0 9074
2 25544 51
6410 236
9248 0003407 222
6026 137
4863 15
54164183 8926
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
99236219 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 236
9248 deg
Eccentricity:
0003407
Arg of perigee: 222
6026 deg
Mean anomaly: 137
4863 deg
Mean motion: 15
54164183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 314
Coasting Arc #9 (Orbit 906)
---------------------------------------
Vector Time (GMT): 2017/345/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4284633
30 A = 6778039
11 meter
Y = 1215260
46 meter E =
0012084
Z = -5120194
03 I = 51
32668
XDOT = -3690
396396 Wp = 114
55961
YDOT = -6533
876167 meter/sec RA = 231
11678 deg
ZDOT = 1535
307048 TA = 170
32895
MA = 170
30567
Ha = 220
340 n
mi
Hp = 215
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14057195
88 X = -4273032
69
Y = 3987075
01 feet Y = 1167411
83 meter
Z = -16798536
83 Z = -5140979
35
XDOT = -12107
599724 XDOT = -3624
516374
YDOT = -21436
601599 feet/sec YDOT = -6574
776406 meter/sec
ZDOT = 5037
096613 ZDOT = 1517
539892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3623396
41 X = -1104411
23
Y = 14044877
12 feet Y = 4280878
54 meter
Z = -16890967
65 Z = -5148366
94
XDOT = -23608
214905 XDOT = -7195
783903
YDOT = -118
393652 feet/sec YDOT = -36
086385 meter/sec
ZDOT = 4959
182275 ZDOT = 1511
558758
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 17345
95688967
00016717 00000-0 10270-3 0 9083
2 25544 51
6410 232
1172 0003282 226
9496 133
1382 15
54154111 9075
Satellite: ISS
Catalog Number: 25544
Epoch time: 17345
95688967 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 232
1172 deg
Eccentricity:
0003282
Arg of perigee: 226
9496 deg
Mean anomaly: 133
1382 deg
Mean motion: 15
54154111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 907
Checksum: 312
Coasting Arc #10 (Orbit 922)
---------------------------------------
Vector Time (GMT): 2017/346/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5139474
20 A = 6780825
03 meter
Y = 254451
77 meter E =
0006208
Z = 4411413
26 I = 51
35800
XDOT = 2526
493576 Wp = 78
14134
YDOT = 6441
791799 meter/sec RA = 226
10100 deg
ZDOT = -3309
822574 TA = 45
41999
MA = 45
36934
Ha = 220
068 n
mi
Hp = 215
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16861791
99 X = 5114818
21
Y = 834815
50 feet Y = 311786
81 meter
Z = 14473140
60 Z = 4436319
57
XDOT = 8289
020920 XDOT = 2470
349588
YDOT = 21134
487530 feet/sec YDOT = 6469
731013 meter/sec
ZDOT = -10858
997946 ZDOT = -3297
685609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8966306
04 X = 2732930
08
Y = -14191933
26 feet Y = -4325701
26 meter
Z = 14583659
74 Z = 4445099
49
XDOT = 21479
451946 XDOT = 6546
936953
YDOT = 2448
735528 feet/sec YDOT = 746
374589 meter/sec
ZDOT = -10806
046695 ZDOT = -3293
683032
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 17346
98571320
00016717 00000-0 10270-3 0 9092
2 25544 51
6414 226
9884 0003189 232
6453 127
4409 15
54168542 9230
Satellite: ISS
Catalog Number: 25544
Epoch time: 17346
98571320 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 226
9884 deg
Eccentricity:
0003189
Arg of perigee: 232
6453 deg
Mean anomaly: 127
4409 deg
Mean motion: 15
54168542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 923
Checksum: 326
Coasting Arc #11 (Orbit 937)
---------------------------------------
Vector Time (GMT): 2017/347/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5746470
47 A = 6784663
52 meter
Y = -1566485
91 meter E =
0002403
Z = -3252239
60 I = 51
39287
XDOT = -1058
490487 Wp = 125
59801
YDOT = -5935
318136 meter/sec RA = 221
09733 deg
ZDOT = 4730
199483 TA = 196
57513
MA = 196
58299
Ha = 220
171 n
mi
Hp = 215
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18853249
57 X = -5712728
57
Y = -5139389
48 feet Y = -1630558
02 meter
Z = -10670077
44 Z = -3280072
60
XDOT = -3472
737817 XDOT = -1015
018713
YDOT = -19472
828529 feet/sec YDOT = -5946
912117 meter/sec
ZDOT = 15519
027176 ZDOT = 4725
162845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13465938
40 X = -4104418
03
Y = 14066969
27 feet Y = 4287612
23 meter
Z = -10793413
50 Z = -3289832
43
XDOT = -17797
841520 XDOT = -5424
782095
YDOT = -5149
080324 feet/sec YDOT = -1569
439683 meter/sec
ZDOT = 15497
512617 ZDOT = 4723
641846
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 17347
95023301
00016717 00000-0 10270-3 0 9103
2 25544 51
6401 222
1812 0003255 235
2004 124
8843 15
54155278 9381
Satellite: ISS
Catalog Number: 25544
Epoch time: 17347
95023301 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 222
1812 deg
Eccentricity:
0003255
Arg of perigee: 235
2004 deg
Mean anomaly: 124
8843 deg
Mean motion: 15
54155278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 938
Checksum: 278
Coasting Arc #12 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 905672
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2663173
64 A = 6777344
25 meter
Y = 3295561
59 meter E =
0012453
Z = -5300245
91 I = 51
37116
XDOT = -5875
261749 Wp = 96
71174
YDOT = -4913
157238 meter/sec RA = 220
52814 deg
ZDOT = -104
420653 TA = 172
29792
MA = 172
27878
Ha = 220
220 n
mi
Hp = 215
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8737446
34 X = -2674081
31
Y = 10812209
94 feet Y = 3265719
50 meter
Z = -17389258
23 Z = -5313209
20
XDOT = -19275
793141 XDOT = -5819
377614
YDOT = -16119
282277 feet/sec YDOT = -4978
545958 meter/sec
ZDOT = -342
587445 ZDOT = -132
825710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12630138
52 X = 3849666
22
Y = 5630748
54 feet Y = 1716252
16 meter
Z = -17447275
61 Z = -5317929
61
XDOT = -10350
471830 XDOT = -3154
823814
YDOT = 21783
293447 feet/sec YDOT = 6639
547843 meter/sec
ZDOT = -467
988866 ZDOT = -142
643006
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 17348
07883599
00016717 00000-0 10270-3 0 9111
2 25544 51
6403 221
5408 0002993 236
2792 123
8076 15
54134703 9400
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
07883599 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 221
5408 deg
Eccentricity:
0002993
Arg of perigee: 236
2792 deg
Mean anomaly: 123
8076 deg
Mean motion: 15
54134703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 315
Coasting Arc #13 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2017/348/05:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 890441
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -78955
55 A = 6779966
81 meter
Y = -4915969
08 meter E =
0006868
Z = 4666842
94 I = 51
38099
XDOT = 6641
709653 Wp = 137
56809
YDOT = 2586
708550 meter/sec RA = 219
76945 deg
ZDOT = 2829
744796 TA = 284
21181
MA = 284
28809
Ha = 220
094 n
mi
Hp = 215
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -259040
53 X = -46647
46
Y = -16128507
48 feet Y = -4916671
67 meter
Z = 15311164
50 Z = 4666537
55
XDOT = 21790
386000 XDOT = 6598
545106
YDOT = 8486
576609 feet/sec YDOT = 2660
739160 meter/sec
ZDOT = 9283
939618 ZDOT = 2861
903817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4956693
74 X = -1510800
25
Y = 15350803
48 feet Y = 4678924
90 meter
Z = 15310507
30 Z = 4666642
62
XDOT = -16616
776344 XDOT = -5064
793430
YDOT = -14791
329749 feet/sec YDOT = -4508
397307 meter/sec
ZDOT = 9426
339783 ZDOT = 2873
148366
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 17348
27173863
00016717 00000-0 10270-3 0 9120
2 25544 51
6373 220
5798 0003035 240
6394 119
4456 15
54170632 9439
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
27173863 = yrday
fracday
Element set: 912
Inclination: 51
6373 deg
RA of node: 220
5798 deg
Eccentricity:
0003035
Arg of perigee: 240
6394 deg
Mean anomaly: 119
4456 deg
Mean motion: 15
54170632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 313
Coasting Arc #14 (Orbit 957)
---------------------------------------
Vector Time (GMT): 2017/349/05:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 890441
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1465981
03 A = 6777642
03 meter
Y = 4065613
35 meter E =
0011619
Z = -5231086
99 I = 51
39938
XDOT = -6655
342244 Wp = 86
90724
YDOT = -3662
763083 meter/sec RA = 214
75458 deg
ZDOT = -982
866429 TA = 173
65032
MA = 173
63558
Ha = 220
096 n
mi
Hp = 215
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4809649
05 X = -1485924
55
Y = 13338626
47 feet Y = 4049108
65 meter
Z = -17162358
89 Z = -5238256
46
XDOT = -21835
112349 XDOT = -6609
115274
YDOT = -12016
939248 feet/sec YDOT = -3736
929120 meter/sec
ZDOT = -3224
627392 ZDOT = -1015
084358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8624856
57 X = 2628856
28
Y = -11204914
90 feet Y = -3415258
06 meter
Z = -17194765
89 Z = -5240964
64
XDOT = 16155
729441 XDOT = 4924
266334
YDOT = 17596
414468 feet/sec YDOT = 5363
387130 meter/sec
ZDOT = -3367
155676 ZDOT = -1026
309050
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 17349
23625378
00016717 00000-0 10270-3 0 9131
2 25544 51
6377 215
7709 0002886 244
1368 115
9487 15
54149881 9587
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
23625378 = yrday
fracday
Element set: 913
Inclination: 51
6377 deg
RA of node: 215
7709 deg
Eccentricity:
0002886
Arg of perigee: 244
1368 deg
Mean anomaly: 115
9487 deg
Mean motion: 15
54149881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 958
Checksum: 352
Coasting Arc #15 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2017/349/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911610
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6078439
12 A = 6788347
94 meter
Y = 2622666
03 meter E =
0012337
Z = 1470390
42 I = 51
44511
XDOT = -760
016372 Wp = 129
50656
YDOT = 5005
801551 meter/sec RA = 213
53510 deg
ZDOT = -5762
153630 TA = 34
39629
MA = 34
31649
Ha = 220
057 n
mi
Hp = 215
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19942385
56 X = 6041517
50
Y = 8604547
35 feet Y = 2690432
73 meter
Z = 4824115
55 Z = 1499828
43
XDOT = -2493
492035 XDOT = -787
946117
YDOT = 16423
233434 feet/sec YDOT = 4997
146848 meter/sec
ZDOT = -18904
703511 ZDOT = -5765
913007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15323651
37 X = -4670648
94
Y = 15350836
34 feet Y = 4678934
92 meter
Z = 4954452
56 Z = 1510117
14
XDOT = -13280
397412 XDOT = -4047
865131
YDOT = -7124
412170 feet/sec YDOT = -2171
520829 meter/sec
ZDOT = -18922
102412 ZDOT = -5767
456815
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 17349
49345760
00016717 00000-0 10270-3 0 9144
2 25544 51
6413 214
4911 0002956 245
1892 114
8953 15
54134322 9625
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
49345760 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 214
4911 deg
Eccentricity:
0002956
Arg of perigee: 245
1892 deg
Mean anomaly: 114
8953 deg
Mean motion: 15
54134322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 962
Checksum: 313
Coasting Arc #16 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2017/350/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911610
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5865244
17 A = 6789153
05 meter
Y = -3400927
46 meter E =
0009833
Z = 231200
34 I = 51
47545
XDOT = 2578
009682 Wp = 40
17648
YDOT = -4029
413094 meter/sec RA = 208
55135 deg
ZDOT = 5993
378718 TA = 322
32027
MA = 322
38910
Ha = 219
894 n
mi
Hp = 215
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19242927
08 X = -5827901
24
Y = -11157898
51 feet Y = -3466307
86 meter
Z = 758531
31 Z = 202798
93
XDOT = 8458
037015 XDOT = 2593
762930
YDOT = -13219
859233 feet/sec YDOT = -4000
496540 meter/sec
ZDOT = 19663
316004 ZDOT = 6005
939856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17214058
06 X = 5246844
90
Y = -14093969
26 feet Y = -4295841
83 meter
Z = 632887
75 Z = 192904
19
XDOT = 8417
067027 XDOT = 2565
522030
YDOT = 11189
787039 feet/sec YDOT = 3410
647090 meter/sec
ZDOT = 19719
662944 ZDOT = 6010
553265
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 17350
52226472
00016717 00000-0 10270-3 0 9159
2 25544 51
6406 209
3615 0003012 253
1280 106
9542 15
54184051 9782
Satellite: ISS
Catalog Number: 25544
Epoch time: 17350
52226472 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 209
3615 deg
Eccentricity:
0003012
Arg of perigee: 253
1280 deg
Mean anomaly: 106
9542 deg
Mean motion: 15
54184051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 978
Checksum: 285
Coasting Arc #17 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2017/351/07:21:01
000
Vector Time (MET): N/A
Weight (LBS) : 911610
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -494411
05 A = 6778620
36 meter
Y = -4574357
13 meter E =
0004748
Z = 4977392
68 I = 51
46289
XDOT = 7238
393707 Wp = 151
87815
YDOT = 1468
615632 meter/sec RA = 204
32858 deg
ZDOT = 2063
786480 TA = 277
97131
MA = 278
02519
Ha = 219
867 n
mi
Hp = 215
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1622083
48 X = -467400
48
Y = -15007733
35 feet Y = -4579735
49 meter
Z = 16330028
48 Z = 4975056
08
XDOT = 23748
010849 XDOT = 7211
408358
YDOT = 4818
292757 feet/sec YDOT = 1549
409189 meter/sec
ZDOT = 6770
953019 ZDOT = 2098
883184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5676779
70 X = 1730282
45
Y = 13998402
40 feet Y = 4266713
05 meter
Z = 16320292
52 Z = 4974425
16
XDOT = -23107
908003 XDOT = -7043
290359
YDOT = 1276
644245 feet/sec YDOT = 389
121166 meter/sec
ZDOT = 6926
620320 ZDOT = 2111
233874
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 17351
35817035
00016717 00000-0 10270-3 0 9163
2 25544 51
6385 205
1940 0003027 254
7729 105
3089 15
54199862 9914
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
35817035 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 205
1940 deg
Eccentricity:
0003027
Arg of perigee: 254
7729 deg
Mean anomaly: 105
3089 deg
Mean motion: 15
54199862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 321
Coasting Arc #18 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2017/352/07:21:01
000
Vector Time (MET): N/A
Weight (LBS) : 911610
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1246517
14 A = 6777200
92 meter
Y = 4038852
58 meter E =
0011980
Z = -5307950
39 I = 51
48888
XDOT = -7263
872591 Wp = 91
07543
YDOT = -2427
028768 meter/sec RA = 199
31744 deg
ZDOT = -141
392945 TA = 177
57575
MA = 177
56994
Ha = 219
868 n
mi
Hp = 215
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4089623
16 X = -1265804
54
Y = 13250828
68 feet Y = 4024805
95 meter
Z = -17414535
39 Z = -5314051
98
XDOT = -23831
602989 XDOT = -7235
506218
YDOT = -7962
692809 feet/sec YDOT = -2508
099733 meter/sec
ZDOT = -463
887614 ZDOT = -176
610073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 51798
54 X = 15788
20
Y = -13832657
47 feet Y = -4216194
00 meter
Z = -17442202
42 Z = -5316383
30
XDOT = 24099
416688 XDOT = 7345
502206
YDOT = 869
953401 feet/sec YDOT = 265
161797 meter/sec
ZDOT = -619
981177 ZDOT = -188
970263
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 17352
32267407
00016717 00000-0 10270-3 0 9174
2 25544 51
6390 200
3851 0002919 259
9728 100
1096 15
54185753 10066
Satellite: ISS
Catalog Number: 25544
Epoch time: 17352
32267407 = yrday
fracday
Element set: 917
Inclination: 51
6390 deg
RA of node: 200
3851 deg
Eccentricity:
0002919
Arg of perigee: 259
9728 deg
Mean anomaly: 100
1096 deg
Mean motion: 15
54185753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 304
Coasting Arc #19 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2017/353/07:21:01
000
Vector Time (MET): N/A
Weight (LBS) : 911610
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2963389
54 A = 6778142
05 meter
Y = -3396045
28 meter E =
0003147
Z = 5061978
73 I = 51
52347
XDOT = 6736
642654 Wp = 26
94499
YDOT = 3193
239099 meter/sec RA = 194
30902 deg
ZDOT = -1798
265388 TA = 80
50181
MA = 80
46625
Ha = 219
700 n
mi
Hp = 215
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9722406
64 X = 2976556
20
Y = -11141880
82 feet Y = -3362833
60 meter
Z = 16607541
77 Z = 5076405
53
XDOT = 22101
845978 XDOT = 6709
169400
YDOT = 10476
506230 feet/sec YDOT = 3268
419440 meter/sec
ZDOT = -5899
820828 ZDOT = -1765
607239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5824864
05 X = -1775418
56
Y = 13512547
39 feet Y = 4118624
44 meter
Z = 16672107
38 Z = 5081658
33
XDOT = -23278
624200 XDOT = -7095
324656
YDOT = -2921
009927 feet/sec YDOT = -890
323826 meter/sec
ZDOT = -5755
175669 ZDOT = -1754
177544
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 17353
35147120
00016717 00000-0 10270-3 0 9188
2 25544 51
6389 195
2567 0002962 266
1338 93
9476 15
54206334 10223
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
35147120 = yrday
fracday
Element set: 918
Inclination: 51
6389 deg
RA of node: 195
2567 deg
Eccentricity:
0002962
Arg of perigee: 266
1338 deg
Mean anomaly: 93
9476 deg
Mean motion: 15
54206334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 315
Coasting Arc #20 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2017/353/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 926842
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1817028
87 A = 6779360
78 meter
Y = -4404316
92 meter E =
0005198
Z = 4821423
04 I = 51
53023
XDOT = 7243
966401 Wp = 138
27370
YDOT = -238
923714 meter/sec RA = 194
05930 deg
ZDOT = 2506
390385 TA = 287
02553
MA = 287
08247
Ha = 219
911 n
mi
Hp = 215
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5961380
82 X = -1791063
66
Y = -14449858
65 feet Y = -4424491
56 meter
Z = 15818317
08 Z = 4812659
04
XDOT = 23766
293968 XDOT = 7233
924922
YDOT = -783
870452 feet/sec YDOT = -157
973169 meter/sec
ZDOT = 8223
065569 ZDOT = 2541
554885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13670734
03 X = 4166839
73
Y = 7658881
75 feet Y = 2334427
16 meter
Z = 15779993
43 Z = 4809742
00
XDOT = -17652
743245 XDOT = -5380
556141
YDOT = 14208
630989 feet/sec YDOT = 4330
790725 meter/sec
ZDOT = 8379
324143 ZDOT = 2554
017999
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 17353
41577135
00016717 00000-0 10270-3 0 9199
2 25544 51
6402 194
9358 0002891 264
6116 95
4707 15
54180471 10239
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
41577135 = yrday
fracday
Element set: 919
Inclination: 51
6402 deg
RA of node: 194
9358 deg
Eccentricity:
0002891
Arg of perigee: 264
6116 deg
Mean anomaly: 95
4707 deg
Mean motion: 15
54180471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1023
Checksum: 312
Coasting Arc #21 (Orbit 1037)
---------------------------------------
Vector Time (GMT): 2017/354/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 926842
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 23604
82 A = 6777263
85 meter
Y = 4253454
89 meter E =
0011684
Z = -5286422
25 I = 51
55496
XDOT = -7601
642279 Wp = 84
06923
YDOT = -719
047312 meter/sec RA = 189
05459 deg
ZDOT = -612
473793 TA = 180
07123
MA = 180
07139
Ha = 219
777 n
mi
Hp = 215
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 77443
62 X = 1718
52
Y = 13954904
51 feet Y = 4253597
08 meter
Z = -17343905
03 Z = -5286360
27
XDOT = -24939
771258 XDOT = -7590
061646
YDOT = -2359
079109 feet/sec YDOT = -803
989252 meter/sec
ZDOT = -2009
428456 ZDOT = -649
372020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8921467
88 X = -2719263
41
Y = -10730419
98 feet Y = -3270632
01 meter
Z = -17344217
97 Z = -5286517
64
XDOT = 20084
472412 XDOT = 6121
747191
YDOT = -13185
715038 feet/sec YDOT = -4019
005943 meter/sec
ZDOT = -2173
283447 ZDOT = -662
416795
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 17354
38026498
00016717 00000-0 10270-3 0 9209
2 25544 51
6396 190
1278 0002980 269
9399 90
1402 15
54209893 10380
Satellite: ISS
Catalog Number: 25544
Epoch time: 17354
38026498 = yrday
fracday
Element set: 920
Inclination: 51
6396 deg
RA of node: 190
1278 deg
Eccentricity:
0002980
Arg of perigee: 269
9399 deg
Mean anomaly: 90
1402 deg
Mean motion: 15
54209893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1038
Checksum: 333
Coasting Arc #22 (Orbit 1053)
---------------------------------------
Vector Time (GMT): 2017/355/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 926842
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1806755
61 A = 6777601
08 meter
Y = -3985952
18 meter E =
0002596
Z = 5175501
85 I = 51
58950
XDOT = 7379
531844 Wp = 7
84370
YDOT = 1592
958225 meter/sec RA = 184
04971 deg
ZDOT = -1346
751198 TA = 95
12234
MA = 95
09270
Ha = 219
615 n
mi
Hp = 215
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5927675
89 X = 1826053
44
Y = -13077270
93 feet Y = -3965640
44 meter
Z = 16979992
95 Z = 5184324
91
XDOT = 24211
062479 XDOT = 7367
712307
YDOT = 5226
240896 feet/sec YDOT = 1675
415248 meter/sec
ZDOT = -4418
475060 ZDOT = -1310
932504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3935347
88 X = 1199494
04
Y = 13759127
37 feet Y = 4193782
02 meter
Z = 17019752
30 Z = 5187620
50
XDOT = -20936
566440 XDOT = -6381
465451
YDOT = 11267
661346 feet/sec YDOT = 3434
383178 meter/sec
ZDOT = -4259
511307 ZDOT = -1298
299046
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 17355
40905481
00016717 00000-0 10270-3 0 9212
2 25544 51
6401 184
9989 0003165 273
1467 86
9324 15
54233615 10549
Satellite: ISS
Catalog Number: 25544
Epoch time: 17355
40905481 = yrday
fracday
Element set: 921
Inclination: 51
6401 deg
RA of node: 184
9989 deg
Eccentricity:
0003165
Arg of perigee: 273
1467 deg
Mean anomaly: 86
9324 deg
Mean motion: 15
54233615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1054
Checksum: 315
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