[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 24th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
331/13:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
9
337/11:31:53
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
0
337/17:35:42
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
1
337/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
1
338/16:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
0
341/20:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
1
Coasting Arc #1 (Orbit 2327)
---------------------------------------
Vector Time (GMT): 2018/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3587775
10 A = 6789565
65 meter
Y = -5748414
81 meter E =
0016206
Z = -315333
53 I = 51
34291
XDOT = 4210
102269 Wp = 53
19428
YDOT = 2311
940611 meter/sec RA = 304
10297 deg
ZDOT = 5978
530713 TA = 303
39300
MA = 303
54794
Ha = 223
063 n
mi
Hp = 212
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11770915
69 X = 3653320
59
Y = -18859628
64 feet Y = -5707927
30 meter
Z = -1034558
82 Z = -297746
18
XDOT = 13812
671485 XDOT = 4154
895293
YDOT = 7585
106992 feet/sec YDOT = 2358
711717 meter/sec
ZDOT = 19614
602077 ZDOT = 5998
848567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10964702
87 X = 3342041
44
Y = 19343581
73 feet Y = 5895923
71 meter
Z = -954723
83 Z = -290999
82
XDOT = -11780
559279 XDOT = -3590
714468
YDOT = 7611
143422 feet/sec YDOT = 2319
876515 meter/sec
ZDOT = 19705
606211 ZDOT = 6006
268773
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 18327
50056307
00016717 00000-0 10270-3 0 9004
2 25544 51
6371 304
8129 0005302 76
4536 283
7207 15
54034357 23284
Satellite: ISS
Catalog Number: 25544
Epoch time: 18327
50056307 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 304
8129 deg
Eccentricity:
0005302
Arg of perigee: 76
4536 deg
Mean anomaly: 283
7207 deg
Mean motion: 15
54034357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2328
Checksum: 292
Coasting Arc #2 (Orbit 2343)
---------------------------------------
Vector Time (GMT): 2018/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4151563
20 A = 6788821
55 meter
Y = 5189508
46 meter E =
0011827
Z = -1377193
92 I = 51
32385
XDOT = -3077
050471 Wp = 118
23702
YDOT = -3983
922626 meter/sec RA = 299
11119 deg
ZDOT = -5779
809045 TA = 76
82828
MA = 76
69635
Ha = 223
067 n
mi
Hp = 212
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13620614
19 X = -4202595
35
Y = 17025946
39 feet Y = 5142797
60 meter
Z = -4518352
77 Z = -1397484
65
XDOT = -10095
309945 XDOT = -3004
196552
YDOT = -13070
612290 feet/sec YDOT = -4017
924399 meter/sec
ZDOT = -18962
628099 ZDOT = -5794
580078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8832165
60 X = -2692044
07
Y = -19913760
70 feet Y = -6069714
26 meter
Z = -4610257
96 Z = -1405206
63
XDOT = 14745
187370 XDOT = 4494
333110
YDOT = -2166
861627 feet/sec YDOT = -660
459424 meter/sec
ZDOT = -19028
478343 ZDOT = -5799
880199
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 18328
52947589
00016717 00000-0 10270-3 0 9019
2 25544 51
6384 299
6835 0005287 77
5390 282
6354 15
54013327 23448
Satellite: ISS
Catalog Number: 25544
Epoch time: 18328
52947589 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 299
6835 deg
Eccentricity:
0005287
Arg of perigee: 77
5390 deg
Mean anomaly: 282
6354 deg
Mean motion: 15
54013327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2344
Checksum: 341
Coasting Arc #3 (Orbit 2359)
---------------------------------------
Vector Time (GMT): 2018/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4428559
91 A = 6785968
81 meter
Y = -4246379
16 meter E =
0018416
Z = 2879780
11 I = 51
29999
XDOT = 1959
410952 Wp = 81
54690
YDOT = 5463
971735 meter/sec RA = 294
11487 deg
ZDOT = 5018
789796 TA = 311
43898
MA = 311
59704
Ha = 222
926 n
mi
Hp = 212
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14529396
03 X = 4461726
27
Y = -13931690
16 feet Y = -4196670
81 meter
Z = 9448097
46 Z = 2901372
96
XDOT = 6428
513622 XDOT = 1873
786617
YDOT = 17926
416453 feet/sec YDOT = 5485
403910 meter/sec
ZDOT = 16465
845787 ZDOT = 5028
100742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6013065
82 X = 1832782
46
Y = 19162047
59 feet Y = 5840592
10 meter
Z = 9545724
54 Z = 2909536
84
XDOT = -17466
197008 XDOT = -5323
696848
YDOT = -2782
452042 feet/sec YDOT = -848
091382 meter/sec
ZDOT = 16506
963536 ZDOT = 5031
322486
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 18329
55838319
00016717 00000-0 10270-3 0 9024
2 25544 51
6389 294
5560 0005148 82
2292 277
9445 15
54050395 23604
Satellite: ISS
Catalog Number: 25544
Epoch time: 18329
55838319 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 294
5560 deg
Eccentricity:
0005148
Arg of perigee: 82
2292 deg
Mean anomaly: 277
9445 deg
Mean motion: 15
54050395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2360
Checksum: 332
Coasting Arc #4 (Orbit 2374)
---------------------------------------
Vector Time (GMT): 2018/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4523946
38 A = 6782278
59 meter
Y = 2913963
39 meter E =
0012936
Z = -4141339
15 I = 51
27441
XDOT = -865
787305 Wp = 75
54266
YDOT = -6632
340198 meter/sec RA = 289
10706 deg
ZDOT = -3727
572250 TA = 155
87945
MA = 155
81882
Ha = 223
072 n
mi
Hp = 212
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14842343
75 X = -4536078
23
Y = 9560247
33 feet Y = 2863306
10 meter
Z = -13587070
71 Z = -4163344
31
XDOT = -2840
509530 XDOT = -773
451490
YDOT = -21759
646319 feet/sec YDOT = -6641
505335 meter/sec
ZDOT = -12229
567748 ZDOT = -3731
554463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2273422
59 X = -692939
20
Y = -17430340
87 feet Y = -5312767
90 meter
Z = -13686371
11 Z = -4171605
92
XDOT = 19555
947284 XDOT = 5960
652732
YDOT = 7048
412576 feet/sec YDOT = 2148
356153 meter/sec
ZDOT = -12246
590764 ZDOT = -3732
760865
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 18330
52298436
00016717 00000-0 10270-3 0 9034
2 25544 51
6385 289
7477 0005271 83
5518 276
6235 15
54021552 23757
Satellite: ISS
Catalog Number: 25544
Epoch time: 18330
52298436 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 289
7477 deg
Eccentricity:
0005271
Arg of perigee: 83
5518 deg
Mean anomaly: 276
6235 deg
Mean motion: 15
54021552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2375
Checksum: 325
Coasting Arc #5 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2018/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4428688
64 A = 6778995
85 meter
Y = -1332856
73 meter E =
0010632
Z = 4948493
85 I = 51
25448
XDOT = -122
708913 Wp = 107
13114
YDOT = 7383
002342 meter/sec RA = 284
09052 deg
ZDOT = 2091
589176 TA = 322
37893
MA = 322
45326
Ha = 222
800 n
mi
Hp = 212
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14529818
38 X = 4419226
53
Y = -4372889
52 feet Y = -1283385
45 meter
Z = 16235216
06 Z = 4969983
92
XDOT = -402
588296 XDOT = -215
418494
YDOT = 24222
448628 feet/sec YDOT = 7381
111546 meter/sec
ZDOT = 6862
169212 ZDOT = 2090
768652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2009477
33 X = -612488
69
Y = 14934792
06 feet Y = 4552124
62 meter
Z = 16331993
52 Z = 4977991
62
XDOT = -20762
015351 XDOT = -6328
262279
YDOT = -10316
891569 feet/sec YDOT = -3144
588550 meter/sec
ZDOT = 6857
521960 ZDOT = 2090
172693
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 18331
55188679
00016717 00000-0 10270-3 0 9046
2 25544 51
6390 284
6206 0005025 87
9790 272
1938 15
54059009 23911
Satellite: ISS
Catalog Number: 25544
Epoch time: 18331
55188679 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 284
6206 deg
Eccentricity:
0005025
Arg of perigee: 87
9790 deg
Mean anomaly: 272
1938 deg
Mean motion: 15
54059009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 331
Coasting Arc #6 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2018/331/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1690353
45 A = 6789623
18 meter
Y = -6568915
31 meter E =
0016542
Z = 91120
88 I = 51
28935
XDOT = 4622
481513 Wp = 58
19615
YDOT = 1283
483813 meter/sec RA = 283
81372 deg
ZDOT = 5983
157233 TA = 302
79022
MA = 302
94946
Ha = 223
036 n
mi
Hp = 212
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5545779
03 X = 1763240
65
Y = -21551559
43 feet Y = -6549605
08 meter
Z = 298953
00 Z = 99508
46
XDOT = 15165
621761 XDOT = 4578
722473
YDOT = 4210
904897 feet/sec YDOT = 1334
930349 meter/sec
ZDOT = 19629
780947 ZDOT = 6005
505640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20890914
84 X = 6367550
84
Y = 7666193
05 feet Y = 2336655
64 meter
Z = 337509
95 Z = 102873
03
XDOT = -5132
322076 XDOT = -1564
331769
YDOT = 13015
822491 feet/sec YDOT = 3967
222695 meter/sec
ZDOT = 19730
077416 ZDOT = 6013
727597
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 18331
61619459
00016717 00000-0 10270-3 0 9059
2 25544 51
6392 284
3000 0005153 87
7950 272
3793 15
54026528 23922
Satellite: ISS
Catalog Number: 25544
Epoch time: 18331
61619459 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 284
3000 deg
Eccentricity:
0005153
Arg of perigee: 87
7950 deg
Mean anomaly: 272
3793 deg
Mean motion: 15
54026528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 315
Coasting Arc #7 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2018/332/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2383798
57 A = 6788254
09 meter
Y = 6102515
07 meter E =
0011362
Z = -1771225
70 I = 51
27893
XDOT = -4074
739798 Wp = 120
47271
YDOT = -3218
476688 meter/sec RA = 278
81836 deg
ZDOT = -5637
599200 TA = 79
06978
MA = 78
94197
Ha = 223
026 n
mi
Hp = 212
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7820861
43 X = -2443257
71
Y = 20021374
89 feet Y = 6075525
46 meter
Z = -5811107
93 Z = -1782949
35
XDOT = -13368
568890 XDOT = -4011
062454
YDOT = -10559
306720 feet/sec YDOT = -3263
686776 meter/sec
ZDOT = -18496
060369 ZDOT = -5657
238547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19309358
98 X = -5885492
62
Y = -9409866
09 feet Y = -2868127
18 meter
Z = -5864586
73 Z = -1787526
04
XDOT = 10932
954074 XDOT = 3332
364402
YDOT = -10918
932648 feet/sec YDOT = -3328
090671 meter/sec
ZDOT = -18583
940393 ZDOT = -5664
385032
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 18332
58078780
00016717 00000-0 10270-3 0 9063
2 25544 51
6401 279
4919 0005180 89
9026 270
2720 15
54030541 24079
Satellite: ISS
Catalog Number: 25544
Epoch time: 18332
58078780 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 279
4919 deg
Eccentricity:
0005180
Arg of perigee: 89
9026 deg
Mean anomaly: 270
2720 deg
Mean motion: 15
54030541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 306
Coasting Arc #8 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2018/333/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2935838
17 A = 6785160
17 meter
Y = -5190546
46 meter E =
0017944
Z = 3220905
23 I = 51
26366
XDOT = 3483
115441 Wp = 88
91369
YDOT = 4926
173269 meter/sec RA = 273
81705 deg
ZDOT = 4741
164272 TA = 308
62125
MA = 308
78177
Ha = 223
004 n
mi
Hp = 212
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9632014
98 X = 2978016
59
Y = -17029351
90 feet Y = -5157480
22 meter
Z = 10567274
38 Z = 3235268
73
XDOT = 11427
544098 XDOT = 3404
740555
YDOT = 16161
985792 feet/sec YDOT = 4964
685400 meter/sec
ZDOT = 15555
000894 ZDOT = 4757
894025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16365885
43 X = 4988321
88
Y = 10655971
19 feet Y = 3247940
02 meter
Z = 10632492
58 Z = 3240783
74
XDOT = -16092
935979 XDOT = -4905
126886
YDOT = 9047
474791 feet/sec YDOT = 2757
670316 meter/sec
ZDOT = 15629
600450 ZDOT = 4763
902217
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 18333
60968431
00016717 00000-0 10270-3 0 9079
2 25544 51
6392 274
3642 0005220 93
7146 266
4603 15
54030794 24231
Satellite: ISS
Catalog Number: 25544
Epoch time: 18333
60968431 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 274
3642 deg
Eccentricity:
0005220
Arg of perigee: 93
7146 deg
Mean anomaly: 266
4603 deg
Mean motion: 15
54030794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 304
Coasting Arc #9 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/334/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3445245
89 A = 6781297
02 meter
Y = 3865415
38 meter E =
0013879
Z = -4392282
67 I = 51
25060
XDOT = -2811
067760 Wp = 79
31342
YDOT = -6291
504172 meter/sec RA = 268
80510 deg
ZDOT = -3338
355887 TA = 156
72888
MA = 156
66599
Ha = 222
990 n
mi
Hp = 212
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11303300
16 X = -3466878
47
Y = 12681809
00 feet Y = 3826767
46 meter
Z = -14410376
22 Z = -4409070
97
XDOT = -9222
663253 XDOT = -2724
289406
YDOT = -20641
417888 feet/sec YDOT = -6322
454148 meter/sec
ZDOT = -10952
611177 ZDOT = -3351
800636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12124507
96 X = -3695550
03
Y = -11806547
92 feet Y = -3598635
80 meter
Z = -14486322
85 Z = -4415431
21
XDOT = 20199
203187 XDOT = 6156
717131
YDOT = -7257
417644 feet/sec YDOT = -2212
060898 meter/sec
ZDOT = -11012
291518 ZDOT = -3356
546455
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 18334
57427220
00016717 00000-0 10270-3 0 9083
2 25544 51
6400 269
5564 0005190 96
8204 263
3539 15
54055035 24380
Satellite: ISS
Catalog Number: 25544
Epoch time: 18334
57427220 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 269
5564 deg
Eccentricity:
0005190
Arg of perigee: 96
8204 deg
Mean anomaly: 263
3539 deg
Mean motion: 15
54055035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 307
Coasting Arc #10 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2018/335/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3856501
46 A = 6778400
43 meter
Y = -2274389
18 meter E =
0009867
Z = 5082410
53 I = 51
24297
XDOT = 2096
733324 Wp = 113
31180
YDOT = 7201
189280 meter/sec RA = 263
78404 deg
ZDOT = 1625
198914 TA = 320
89489
MA = 320
96617
Ha = 222
786 n
mi
Hp = 212
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12652563
83 X = 3856959
79
Y = -7461906
77 feet Y = -2231260
70 meter
Z = 16674575
23 Z = 5101145
30
XDOT = 6879
046339 XDOT = 2008
157344
YDOT = 23625
949081 feet/sec YDOT = 7224
141100 meter/sec
ZDOT = 5332
017434 ZDOT = 1635
169300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7066739
49 X = 2153942
20
Y = 12767279
88 feet Y = 3891466
91 meter
Z = 16759076
36 Z = 5108166
48
XDOT = -22896
879115 XDOT = -6978
968754
YDOT = 5589
428156 feet/sec YDOT = 1703
657702 meter/sec
ZDOT = 5375
985735 ZDOT = 1638
600452
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 18335
60316124
00016717 00000-0 10270-3 0 9099
2 25544 51
6401 264
4281 0005050 101
7244 258
4476 15
54071669 24540
Satellite: ISS
Catalog Number: 25544
Epoch time: 18335
60316124 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 264
4281 deg
Eccentricity:
0005050
Arg of perigee: 101
7244 deg
Mean anomaly: 258
4476 deg
Mean motion: 15
54071669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 293
Coasting Arc #11 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2018/336/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4225300
14 A = 6777581
91 meter
Y = 525777
33 meter E =
0019924
Z = -5290470
37 I = 51
24556
XDOT = -1277
867132 Wp = 95
04198
YDOT = -7541
349907 meter/sec RA = 258
75733 deg
ZDOT = 270
274768 TA = 177
55830
MA = 177
54856
Ha = 222
969 n
mi
Hp = 212
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13862533
28 X = -4205166
85
Y = 1724991
23 feet Y = 478639
83 meter
Z = -17357186
25 Z = -5310946
77
XDOT = -4192
477466 XDOT = -1194
755543
YDOT = -24741
961638 feet/sec YDOT = -7555
175209 meter/sec
ZDOT = 886
728241 ZDOT = 264
268864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1532112
51 X = -466987
89
Y = -13769223
01 feet Y = -4196859
17 meter
Z = -17449311
38 Z = -5318550
11
XDOT = 23793
890752 XDOT = 7252
377901
YDOT = -3741
643342 feet/sec YDOT = -1140
452891 meter/sec
ZDOT = 860
608147 ZDOT = 262
313363
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 18336
56774335
00016717 00000-0 10270-3 0 9109
2 25544 51
6409 259
6200 0005161 103
4109 256
7619 15
54060677 24690
Satellite: ISS
Catalog Number: 25544
Epoch time: 18336
56774335 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 259
6200 deg
Eccentricity:
0005161
Arg of perigee: 103
4109 deg
Mean anomaly: 256
7619 deg
Mean motion: 15
54060677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 313
Coasting Arc #12 (Orbit 2483)
---------------------------------------
Vector Time (GMT): 2018/337/11:31:53
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3195784
16 A = 6778897
18 meter
Y = -3322209
44 meter E =
0010987
Z = 4963271
76 I = 51
25553
XDOT = 3552
207773 Wp = 116
67055
YDOT = 6487
080822 meter/sec RA = 254
12489 deg
ZDOT = 2046
595948 TA = 313
28848
MA = 313
38007
Ha = 222
749 n
mi
Hp = 212
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10484856
18 X = 3208587
18
Y = -10899637
26 feet Y = -3286400
59 meter
Z = 16283700
01 Z = 4978826
97
XDOT = 11654
224976 XDOT = 3469
461971
YDOT = 21283
073563 feet/sec YDOT = 6526
341328 meter/sec
ZDOT = 6714
553636 ZDOT = 2063
650922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5329964
45 X = 1624573
16
Y = 14072333
08 feet Y = 4289247
12 meter
Z = 16354024
23 Z = 4984706
58
XDOT = -23185
593914 XDOT = -7066
969025
YDOT = 858
383037 feet/sec YDOT = 261
635150 meter/sec
ZDOT = 6790
488143 ZDOT = 2069
740786
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 18337
53232159
00016717 00000-0 10270-3 0 9111
2 25544 51
6393 254
8123 0005000 108
5830 251
5866 15
54083994 24843
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
53232159 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 254
8123 deg
Eccentricity:
0005000
Arg of perigee: 108
5830 deg
Mean anomaly: 251
5866 deg
Mean motion: 15
54083994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2484
Checksum: 308
Coasting Arc #13 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/17:35:42
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1403505
67 A = 6783700
87 meter
Y = -5505495
59 meter E =
0016453
Z = 3694905
21 I = 51
27196
XDOT = 4858
536971 Wp = 99
80453
YDOT = 4120
897385 meter/sec RA = 252
86634 deg
ZDOT = 4275
666064 TA = 304
52962
MA = 304
68483
Ha = 222
786 n
mi
Hp = 213
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4604677
39 X = 1447017
15
Y = -18062649
56 feet Y = -5489557
50 meter
Z = 12122392
41 Z = 3701828
49
XDOT = 15940
081926 XDOT = 4791
325575
YDOT = 13520
004543 feet/sec YDOT = 4174
852916 meter/sec
ZDOT = 14027
775800 ZDOT = 4299
104489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11596080
51 X = 3534485
34
Y = -14567847
45 feet Y = -4440279
90 meter
Z = 12154155
60 Z = 3704586
63
XDOT = 7763
642687 XDOT = 2366
358291
YDOT = 18023
025457 feet/sec YDOT = 5493
418159 meter/sec
ZDOT = 14132
688368 ZDOT = 4307
643414
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 18337
78954147
00016717 00000-0 10270-3 0 9127
2 25544 51
6376 253
5283 0004838 110
3160 249
8513 15
54061826 24885
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78954147 = yrday
fracday
Element set: 912
Inclination: 51
6376 deg
RA of node: 253
5283 deg
Eccentricity:
0004838
Arg of perigee: 110
3160 deg
Mean anomaly: 249
8513 deg
Mean motion: 15
54061826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 326
Coasting Arc #14 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4172310
40 A = 6784322
49 meter
Y = 4062736
03 meter E =
0016821
Z = 3464421
61 I = 51
27459
XDOT = -1964
170856 Wp = 94
72020
YDOT = 5884
526835 meter/sec RA = 252
72961 deg
ZDOT = -4517
663871 TA = 44
33423
MA = 44
19964
Ha = 222
712 n
mi
Hp = 213
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13688682
40 X = 4109741
04
Y = 13329186
44 feet Y = 4109043
69 meter
Z = 11366212
64 Z = 3484537
81
XDOT = -6444
130105 XDOT = -2007
882511
YDOT = 19306
190402 feet/sec YDOT = 5862
317920 meter/sec
ZDOT = -14821
731861 ZDOT = -4527
311177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8718793
73 X = 2657488
33
Y = 16940374
08 feet Y = 5163426
02 meter
Z = 11456194
34 Z = 3491848
03
XDOT = -10869
783568 XDOT = -3313
110032
YDOT = 15686
427269 feet/sec YDOT = 4781
223031 meter/sec
ZDOT = -14865
786594 ZDOT = -4531
091754
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 18337
78954098
00016717 00000-0 10270-3 0 9133
2 25544 51
6378 253
5272 0004828 110
2475 249
9197 15
54070673 24881
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78954098 = yrday
fracday
Element set: 913
Inclination: 51
6378 deg
RA of node: 253
5272 deg
Eccentricity:
0004828
Arg of perigee: 110
2475 deg
Mean anomaly: 249
9197 deg
Mean motion: 15
54070673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 348
Coasting Arc #15 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2018/338/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2859119
50 A = 6778934
71 meter
Y = 3615591
67 meter E =
0016805
Z = -4985619
28 I = 51
26796
XDOT = -4183
034398 Wp = 84
95144
YDOT = -6085
654328 meter/sec RA = 248
16384 deg
ZDOT = -2018
932445 TA = 165
31400
MA = 165
26512
Ha = 222
792 n
mi
Hp = 212
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9380313
32 X = -2875119
63
Y = 11862177
41 feet Y = 3583529
87 meter
Z = -16357018
65 Z = -4999546
77
XDOT = -13723
866136 XDOT = -4104
864935
YDOT = -19966
057505 feet/sec YDOT = -6131
994722 meter/sec
ZDOT = -6623
794110 ZDOT = -2039
063064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14977957
94 X = -4565281
58
Y = 1515288
87 feet Y = 461860
05 meter
Z = -16420056
81 Z = -5004833
32
XDOT = 5057
693529 XDOT = 1541
584988
YDOT = -22599
880234 feet/sec YDOT = -6888
443495 meter/sec
ZDOT = -6713
621099 ZDOT = -2046
311711
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 18338
68981263
00016717 00000-0 10270-3 0 9148
2 25544 51
6395 249
0418 0004821 111
8162 248
3504 15
54062626 25026
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
68981263 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 249
0418 deg
Eccentricity:
0004821
Arg of perigee: 111
8162 deg
Mean anomaly: 248
3504 deg
Mean motion: 15
54062626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 308
Coasting Arc #16 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2018/339/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3700656
79 A = 6777601
41 meter
Y = -2067494
42 meter E =
0007341
Z = 5282386
77 I = 51
27667
XDOT = 3574
045495 Wp = 109
71308
YDOT = 6789
365619 meter/sec RA = 243
14018 deg
ZDOT = 150
857582 TA = 338
82791
MA = 338
85828
Ha = 222
735 n
mi
Hp = 213
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12141262
44 X = 3697841
56
Y = -6783118
17 feet Y = -2026127
29 meter
Z = 17330665
25 Z = 5300356
57
XDOT = 11725
871048 XDOT = 3497
126479
YDOT = 22274
821586 feet/sec YDOT = 6828
902986 meter/sec
ZDOT = 494
939574 ZDOT = 168
033109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13284129
52 X = 4049002
68
Y = 3759948
94 feet Y = 1146032
44 meter
Z = 17411708
43 Z = 5307088
73
XDOT = -7281
800683 XDOT = -2219
492848
YDOT = 23041
498376 feet/sec YDOT = 7023
048705 meter/sec
ZDOT = 571
413698 ZDOT = 174
166895
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 18339
71869176
00016717 00000-0 10270-3 0 9152
2 25544 51
6394 243
9134 0004961 115
1917 244
9751 15
54042935 25187
Satellite: ISS
Catalog Number: 25544
Epoch time: 18339
71869176 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 243
9134 deg
Eccentricity:
0004961
Arg of perigee: 115
1917 deg
Mean anomaly: 244
9751 deg
Mean motion: 15
54042935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 333
Coasting Arc #17 (Orbit 2532)
---------------------------------------
Vector Time (GMT): 2018/340/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4494057
15 A = 6778519
68 meter
Y = 466452
46 meter E =
0018122
Z = -5069602
42 I = 51
29407
XDOT = -2684
291876 Wp = 107
70577
YDOT = -6954
111315 meter/sec RA = 238
11622 deg
ZDOT = 1739
450729 TA = 179
22576
MA = 179
22295
Ha = 222
786 n
mi
Hp = 212
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14744282
00 X = -4474313
32
Y = 1530355
84 feet Y = 416307
72 meter
Z = -16632553
86 Z = -5091385
32
XDOT = -8806
731875 XDOT = -2614
779017
YDOT = -22815
325838 feet/sec YDOT = -6983
740444 meter/sec
ZDOT = 5706
859348 ZDOT = 1726
579277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11550449
07 X = -3520576
88
Y = -9113325
46 feet Y = -2777741
60 meter
Z = -16730574
22 Z = -5099479
02
XDOT = 8915
773467 XDOT = 2717
527753
YDOT = -21673
579507 feet/sec YDOT = -6606
107034 meter/sec
ZDOT = 5649
744587 ZDOT = 1722
042150
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 18340
68326350
00016717 00000-0 10270-3 0 9163
2 25544 51
6375 239
1049 0004947 119
6672 240
4974 15
54068288 25333
Satellite: ISS
Catalog Number: 25544
Epoch time: 18340
68326350 = yrday
fracday
Element set: 916
Inclination: 51
6375 deg
RA of node: 239
1049 deg
Eccentricity:
0004947
Arg of perigee: 119
6672 deg
Mean anomaly: 240
4974 deg
Mean motion: 15
54068288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2533
Checksum: 330
Coasting Arc #18 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2018/341/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5115528
25 A = 6781444
92 meter
Y = 1065068
53 meter E =
0013039
Z = 4311494
71 I = 51
32312
XDOT = 1540
040874 Wp = 88
56488
YDOT = 6672
034440 meter/sec RA = 233
09974 deg
ZDOT = -3466
015204 TA = 36
82413
MA = 36
73465
Ha = 222
517 n
mi
Hp = 213
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16783229
16 X = 5082294
93
Y = 3494319
34 feet Y = 1122087
59 meter
Z = 14145323
86 Z = 4336263
89
XDOT = 5052
627540 XDOT = 1482
154137
YDOT = 21889
876771 feet/sec YDOT = 6688
932997 meter/sec
ZDOT = -11371
440957 ZDOT = -3458
673926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9759649
76 X = 2974741
25
Y = 13981247
19 feet Y = 4261484
14 meter
Z = 14256619
49 Z = 4345417
62
XDOT = -10244
306728 XDOT = -3122
464691
YDOT = 18744
805526 feet/sec YDOT = 5713
416724 meter/sec
ZDOT = -11339
153965 ZDOT = -3456
174129
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 18341
71213802
00016717 00000-0 10270-3 0 9176
2 25544 51
6382 233
9764 0004741 124
2794 235
8808 15
54080396 25491
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
71213802 = yrday
fracday
Element set: 917
Inclination: 51
6382 deg
RA of node: 233
9764 deg
Eccentricity:
0004741
Arg of perigee: 124
2794 deg
Mean anomaly: 235
8808 deg
Mean motion: 15
54080396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 321
Coasting Arc #19 (Orbit 2551)
---------------------------------------
Vector Time (GMT): 2018/341/20:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2982740
63 A = 6788453
98 meter
Y = -5889668
64 meter E =
0016808
Z = 1557446
60 I = 51
35131
XDOT = 5005
217499 Wp = 79
25283
YDOT = -1008
617427 meter/sec RA = 232
26656 deg
ZDOT = 5721
927299 TA = 297
84441
MA = 298
01461
Ha = 222
817 n
mi
Hp = 213
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9785894
47 X = -2924224
37
Y = -19323059
86 feet Y = -5922696
73 meter
Z = 5109732
93 Z = 1543098
72
XDOT = 16421
317253 XDOT = 4988
329719
YDOT = -3309
112292 feet/sec YDOT = -952
740729 meter/sec
ZDOT = 18772
727359 ZDOT = 5746
200054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15685061
15 X = -4780806
64
Y = -14959013
62 feet Y = -4559507
35 meter
Z = 5045841
02 Z = 1537972
34
XDOT = 13178
433450 XDOT = 4016
786516
YDOT = -7393
360582 feet/sec YDOT = -2253
496305 meter/sec
ZDOT = 18882
020428 ZDOT = 5755
239826
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 18341
90505330
00016717 00000-0 10270-3 0 9188
2 25544 51
6396 233
0122 0005302 127
9948 232
1684 15
54086059 25528
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
90505330 = yrday
fracday
Element set: 918
Inclination: 51
6396 deg
RA of node: 233
0122 deg
Eccentricity:
0005302
Arg of perigee: 127
9948 deg
Mean anomaly: 232
1684 deg
Mean motion: 15
54086059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2552
Checksum: 300
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