[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 16th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
323/23:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
5
328/13:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 213
6
333/15:51:39
863 0
6 1
3 1
3
N/A -1
1 -0
0 221
5
000/00:03:19
725 0
2 -0
0 214
7
Coasting Arc #1 (Orbit 527)
---------------------------------------
Vector Time (GMT): 2017/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6410889
27 A = 6788179
43 meter
Y = -1602934
80 meter E =
0011997
Z = -1536334
71 I = 51
68471
XDOT = 2475
098446 Wp = 133
69874
YDOT = -4411
637114 meter/sec RA = 3
45220 deg
ZDOT = -5761
521105 TA = 63
07615
MA = 62
95362
Ha = 222
336 n
mi
Hp = 213
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21033101
29 X = -6385025
42
Y = -5258972
44 feet Y = -1674481
16 meter
Z = -5040468
21 Z = -1567414
70
XDOT = 8120
401726 XDOT = 2552
233898
YDOT = -14473
875047 feet/sec YDOT = -4383
527699 meter/sec
ZDOT = -18902
628296 ZDOT = -5749
310118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16623142
98 X = 5066733
98
Y = -13867698
83 feet Y = -4226874
60 meter
Z = -5178079
54 Z = -1578278
64
XDOT = 5826
395436 XDOT = 1775
885329
YDOT = 13978
463448 feet/sec YDOT = 4260
635659 meter/sec
ZDOT = -18847
661775 ZDOT = -5744
767309
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 17319
52912091
00016717 00000-0 10270-3 0 9007
2 25544 51
6416 3
8651 0004186 118
6018 241
5556 15
54159345 5287
Satellite: ISS
Catalog Number: 25544
Epoch time: 17319
52912091 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 3
8651 deg
Eccentricity:
0004186
Arg of perigee: 118
6018 deg
Mean anomaly: 241
5556 deg
Mean motion: 15
54159345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 528
Checksum: 298
Coasting Arc #2 (Orbit 543)
---------------------------------------
Vector Time (GMT): 2017/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5604196
65 A = 6785218
87 meter
Y = 2275029
12 meter E =
0016641
Z = 3061671
03 I = 51
64133
XDOT = -4322
390025 Wp = 92
61505
YDOT = 4004
178773 meter/sec RA = 358
47823 deg
ZDOT = 4912
683171 TA = 302
55164
MA = 302
71226
Ha = 222
354 n
mi
Hp = 213
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18386471
96 X = 5563467
68
Y = 7464006
29 feet Y = 2337471
36 meter
Z = 10044852
45 Z = 3088796
23
XDOT = -14181
069636 XDOT = -4390
708588
YDOT = 13137
069464 feet/sec YDOT = 3955
460892 meter/sec
ZDOT = 16117
726939 ZDOT = 4891
519839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16644782
72 X = -5073329
77
Y = 10691170
36 feet Y = 3258668
72 meter
Z = 10164786
60 Z = 3098226
95
XDOT = -1748
824848 XDOT = -533
041814
YDOT = -18030
285824 feet/sec YDOT = -5495
631119 meter/sec
ZDOT = 16023
117147 ZDOT = 4883
846106
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 17320
55793759
00016717 00000-0 10270-3 0 9011
2 25544 51
6410 358
7368 0004235 119
9366 240
2207 15
54143010 5442
Satellite: ISS
Catalog Number: 25544
Epoch time: 17320
55793759 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 358
7368 deg
Eccentricity:
0004235
Arg of perigee: 119
9366 deg
Mean anomaly: 240
2207 deg
Mean motion: 15
54143010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 544
Checksum: 297
Coasting Arc #3 (Orbit 558)
---------------------------------------
Vector Time (GMT): 2017/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4342816
90 A = 6781275
21 meter
Y = -2941851
52 meter E =
0011541
Z = -4308211
40 I = 51
59608
XDOT = 5844
086206 Wp = 86
57394
YDOT = -3477
964641 meter/sec RA = 353
49188 deg
ZDOT = -3523
596447 TA = 147
51388
MA = 147
44280
Ha = 222
308 n
mi
Hp = 213
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14248086
95 X = -4288669
83
Y = -9651743
85 feet Y = -2990113
06 meter
Z = -14134551
84 Z = -4329176
54
XDOT = 19173
511174 XDOT = 5899
659748
YDOT = -11410
645146 feet/sec YDOT = -3412
301304 meter/sec
ZDOT = -11560
355798 ZDOT = -3495
071990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15932530
32 X = 4856235
24
Y = -6300461
14 feet Y = -1920380
56 meter
Z = -14227029
34 Z = -4336398
54
XDOT = -1814
111986 XDOT = -552
941333
YDOT = 21174
592124 feet/sec YDOT = 6454
015679 meter/sec
ZDOT = -11433
188415 ZDOT = -3484
835829
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 17321
52244829
00016717 00000-0 10270-3 0 9029
2 25544 51
6414 353
9287 0004208 125
2607 234
8940 15
54160771 5593
Satellite: ISS
Catalog Number: 25544
Epoch time: 17321
52244829 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 353
9287 deg
Eccentricity:
0004208
Arg of perigee: 125
2607 deg
Mean anomaly: 234
8940 deg
Mean motion: 15
54160771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 559
Checksum: 306
Coasting Arc #4 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2017/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2782046
10 A = 6778203
87 meter
Y = 3536617
02 meter E =
0009492
Z = 5063962
56 I = 51
55235
XDOT = -6894
950232 Wp = 125
34495
YDOT = 2852
422561 meter/sec RA = 348
49322 deg
ZDOT = 1788
109681 TA = 307
30078
MA = 307
38726
Ha = 222
207 n
mi
Hp = 213
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9127447
84 X = 2717693
04
Y = 11603074
20 feet Y = 3567367
78 meter
Z = 16614050
39 Z = 5077321
03
XDOT = -22621
227795 XDOT = -6935
020322
YDOT = 9358
341734 feet/sec YDOT = 2775
094417 meter/sec
ZDOT = 5866
501577 ZDOT = 1754
518026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14647078
57 X = -4464429
55
Y = 1205584
44 feet Y = 367462
14 meter
Z = 16672671
08 Z = 5081830
14
XDOT = 4641
566018 XDOT = 1414
749322
YDOT = -23021
226962 feet/sec YDOT = -7016
869978 meter/sec
ZDOT = 5716
973852 ZDOT = 1742
533630
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 17322
55125456
00016717 00000-0 10270-3 0 9038
2 25544 51
6403 348
7998 0004214 127
2774 232
8764 15
54180145 5753
Satellite: ISS
Catalog Number: 25544
Epoch time: 17322
55125456 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 348
7998 deg
Eccentricity:
0004214
Arg of perigee: 127
2774 deg
Mean anomaly: 232
8764 deg
Mean motion: 15
54180145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 315
Coasting Arc #5 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2017/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1029401
28 A = 6777263
88 meter
Y = -4099856
09 meter E =
0018155
Z = -5313020
90 I = 51
51865
XDOT = 7372
261721 Wp = 99
32523
YDOT = -2056
360806 meter/sec RA = 343
48607 deg
ZDOT = 156
014210 TA = 172
18077
MA = 172
15243
Ha = 222
216 n
mi
Hp = 213
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3377300
77 X = -957670
39
Y = -13450971
43 feet Y = -4110966
24 meter
Z = -17431170
92 Z = -5317847
50
XDOT = 24187
210370 XDOT = 7393
950713
YDOT = -6746
590570 feet/sec YDOT = -1973
797877 meter/sec
ZDOT = 511
857643 ZDOT = 191
879851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13125020
58 X = 4000506
27
Y = 4398591
28 feet Y = 1340690
62 meter
Z = -17451840
65 Z = -5319321
03
XDOT = -6840
562990 XDOT = -2085
003599
YDOT = 23106
668371 feet/sec YDOT = 7042
912519 meter/sec
ZDOT = 671
323183 ZDOT = 204
619306
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 17323
51575518
00016717 00000-0 10270-3 0 9044
2 25544 51
6419 343
9915 0004050 131
3534 228
7967 15
54166221 5909
Satellite: ISS
Catalog Number: 25544
Epoch time: 17323
51575518 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 343
9915 deg
Eccentricity:
0004050
Arg of perigee: 131
3534 deg
Mean anomaly: 228
7967 deg
Mean motion: 15
54166221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 590
Checksum: 307
Coasting Arc #6 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2017/323/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6510606
04 A = 6789078
16 meter
Y = 1839683
74 meter E =
0014760
Z = -478538
01 I = 51
54014
XDOT = -901
409415 Wp = 136
63196
YDOT = -4714
866425 meter/sec RA = 341
00078 deg
ZDOT = -5982
018761 TA = 48
53763
MA = 48
41098
Ha = 222
061 n
mi
Hp = 213
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21360256
03 X = -6528369
43
Y = 6035707
80 feet Y = 1766778
40 meter
Z = -1570006
59 Z = -510208
32
XDOT = -2957
379970 XDOT = -819
561117
YDOT = -15468
721867 feet/sec YDOT = -4724
488636 meter/sec
ZDOT = -19626
045803 ZDOT = -5986
199086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6211353
54 X = -1893220
56
Y = 21299000
12 feet Y = 6491935
24 meter
Z = -1710820
88 Z = -521458
21
XDOT = -13060
856497 XDOT = -3980
949060
YDOT = -5357
706139 feet/sec YDOT = -1633
028831 meter/sec
ZDOT = -19643
737238 ZDOT = -5987
411110
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 17324
03015331
00016717 00000-0 10270-3 0 9055
2 25544 51
6394 341
4266 0003792 132
7619 227
3853 15
54175283 5989
Satellite: ISS
Catalog Number: 25544
Epoch time: 17324
03015331 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 341
4266 deg
Eccentricity:
0003792
Arg of perigee: 132
7619 deg
Mean anomaly: 227
3853 deg
Mean motion: 15
54175283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 598
Checksum: 308
Coasting Arc #7 (Orbit 613)
---------------------------------------
Vector Time (GMT): 2017/324/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6363430
82 A = 6787087
09 meter
Y = -973611
52 meter E =
0015724
Z = 2133149
66 I = 51
50210
XDOT = -1049
438796 Wp = 83
47770
YDOT = 5248
580866 meter/sec RA = 336
01980 deg
ZDOT = 5493
049315 TA = 300
21974
MA = 300
37534
Ha = 221
962 n
mi
Hp = 213
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20877397
69 X = 6363483
04
Y = -3194263
51 feet Y = -902451
13 meter
Z = 6998522
49 Z = 2164061
95
XDOT = -3443
040668 XDOT = -1134
734936
YDOT = 17219
753499 feet/sec YDOT = 5236
368055 meter/sec
ZDOT = 18021
815339 ZDOT = 5487
744518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8011056
92 X = 2441770
15
Y = -19492344
50 feet Y = -5941266
60 meter
Z = 7135814
15 Z = 2174996
15
XDOT = 11493
751350 XDOT = 3503
295412
YDOT = 11351
268660 feet/sec YDOT = 3459
866687 meter/sec
ZDOT = 17997
338623 ZDOT = 5485
588812
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 17325
05894654
00016717 00000-0 10270-3 0 9062
2 25544 51
6382 336
2969 0003862 139
4686 220
6755 15
54211249 6143
Satellite: ISS
Catalog Number: 25544
Epoch time: 17325
05894654 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 336
2969 deg
Eccentricity:
0003862
Arg of perigee: 139
4686 deg
Mean anomaly: 220
6755 deg
Mean motion: 15
54211249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 614
Checksum: 329
Coasting Arc #8 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2017/325/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5749151
86 A = 6783481
66 meter
Y = -98412
02 meter E =
0008154
Z = -3604019
09 I = 51
46050
XDOT = 2849
324561 Wp = 104
27002
YDOT = -5586
527097 meter/sec RA = 331
02866 deg
ZDOT = -4403
056227 TA = 118
49429
MA = 118
41215
Ha = 221
931 n
mi
Hp = 213
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18862046
78 X = -5730117
23
Y = -322874
09 feet Y = -162596
29 meter
Z = -11824209
62 Z = -3631900
97
XDOT = 9348
177694 XDOT = 2932
971107
YDOT = -18328
500975 feet/sec YDOT = -5554
196006 meter/sec
ZDOT = -14445
722528 ZDOT = -4389
012054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9692876
64 X = -2954388
80
Y = 16093156
47 feet Y = 4905194
09 meter
Z = -11947863
69 Z = -3641708
85
XDOT = -9957
040492 XDOT = -3034
905942
YDOT = -16649
955127 feet/sec YDOT = -5074
906323 meter/sec
ZDOT = -14382
424908 ZDOT = -4383
763112
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 17326
02343840
00016717 00000-0 10270-3 0 9077
2 25544 51
6381 331
4876 0003828 139
9503 220
1933 15
54206091 6299
Satellite: ISS
Catalog Number: 25544
Epoch time: 17326
02343840 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 331
4876 deg
Eccentricity:
0003828
Arg of perigee: 139
9503 deg
Mean anomaly: 220
1933 deg
Mean motion: 15
54206091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 300
Coasting Arc #9 (Orbit 644)
---------------------------------------
Vector Time (GMT): 2017/326/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4762318
00 A = 6779845
88 meter
Y = 1265386
53 meter E =
0011536
Z = 4651623
46 I = 51
41998
XDOT = -4312
876627 Wp = 124
65772
YDOT = 5661
275927 meter/sec RA = 326
02511 deg
ZDOT = 2863
960446 TA = 296
75765
MA = 296
87564
Ha = 221
844 n
mi
Hp = 213
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15624402
88 X = 4725218
52
Y = 4151530
61 feet Y = 1318434
27 meter
Z = 15261231
82 Z = 4674667
65
XDOT = -14149
857700 XDOT = -4389
773911
YDOT = 18573
739918 feet/sec YDOT = 5612
616241 meter/sec
ZDOT = 9396
195690 ZDOT = 2842
823122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11175782
38 X = 3406378
47
Y = -11547111
82 feet Y = -3519559
68 meter
Z = 15363217
94 Z = 4682708
83
XDOT = 8481
290698 XDOT = 2585
097405
YDOT = 20633
822910 feet/sec YDOT = 6289
189223 meter/sec
ZDOT = 9301
429874 ZDOT = 2835
075826
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 17327
05222419
00016717 00000-0 10270-3 0 9080
2 25544 51
6381 326
3578 0003809 144
0037 216
1373 15
54187770 6452
Satellite: ISS
Catalog Number: 25544
Epoch time: 17327
05222419 = yrday
fracday
Element set: 908
Inclination: 51
6381 deg
RA of node: 326
3578 deg
Eccentricity:
0003809
Arg of perigee: 144
0037 deg
Mean anomaly: 216
1373 deg
Mean motion: 15
54187770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 645
Checksum: 306
Coasting Arc #10 (Orbit 659)
---------------------------------------
Vector Time (GMT): 2017/327/23:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3504172
09 A = 6777427
19 meter
Y = -2538408
59 meter E =
0016612
Z = -5230545
37 I = 51
38493
XDOT = 5368
135021 Wp = 94
97881
YDOT = -5368
109549 meter/sec RA = 321
01109 deg
ZDOT = -995
328814 TA = 165
46819
MA = 165
42037
Ha = 221
971 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11496627
58 X = -3450118
74
Y = -8328112
17 feet Y = -2577292
08 meter
Z = -17160581
93 Z = -5247436
64
XDOT = 17611
991540 XDOT = 5432
598567
YDOT = -17611
907969 feet/sec YDOT = -5307
718896 meter/sec
ZDOT = -3265
514481 ZDOT = -969
095512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12709710
59 X = -3873919
79
Y = 6118146
98 feet Y = 1864811
20 meter
Z = -17235051
63 Z = -5253243
74
XDOT = -6784
065566 XDOT = -2067
783185
YDOT = -22923
518611 feet/sec YDOT = -6987
088473 meter/sec
ZDOT = -3148
207126 ZDOT = -959
573532
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 17328
01670687
00016717 00000-0 10270-3 0 9092
2 25544 51
6376 321
5493 0004085 146
4583 213
6829 15
54209353 6605
Satellite: ISS
Catalog Number: 25544
Epoch time: 17328
01670687 = yrday
fracday
Element set: 909
Inclination: 51
6376 deg
RA of node: 321
5493 deg
Eccentricity:
0004085
Arg of perigee: 146
4583 deg
Mean anomaly: 213
6829 deg
Mean motion: 15
54209353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 321
Coasting Arc #11 (Orbit 668)
---------------------------------------
Vector Time (GMT): 2017/328/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5409288
94 A = 6781946
96 meter
Y = 479957
50 meter E =
0009134
Z = -4069889
36 I = 51
38680
XDOT = 2332
782386 Wp = 94
58202
YDOT = -6205
335013 meter/sec RA = 318
16293 deg
ZDOT = -3840
465556 TA = 135
54892
MA = 135
47558
Ha = 221
832 n
mi
Hp = 213
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17747010
96 X = -5394484
17
Y = 1574663
73 feet Y = 419550
15 meter
Z = -13352655
37 Z = -4096130
32
XDOT = 7653
485520 XDOT = 2420
654036
YDOT = -20358
710672 feet/sec YDOT = -6178
756705 meter/sec
ZDOT = -12599
952611 ZDOT = -3828
920421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1215275
04 X = -370415
83
Y = -17687143
80 feet Y = -5391041
43 meter
Z = -13469128
41 Z = -4105390
34
XDOT = 18909
030275 XDOT = 5763
472428
YDOT = 8235
814734 feet/sec YDOT = 2510
276331 meter/sec
ZDOT = -12547
650993 ZDOT = -3824
524023
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 17328
59539495
00016717 00000-0 10270-3 0 9108
2 25544 51
6387 318
6666 0003813 147
1267 213
0123 15
54211752 6697
Satellite: ISS
Catalog Number: 25544
Epoch time: 17328
59539495 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 318
6666 deg
Eccentricity:
0003813
Arg of perigee: 147
1267 deg
Mean anomaly: 213
0123 deg
Mean motion: 15
54211752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 669
Checksum: 319
Coasting Arc #12 (Orbit 684)
---------------------------------------
Vector Time (GMT): 2017/329/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4550012
76 A = 6778495
99 meter
Y = 917808
72 meter E =
0009615
Z = 4936160
78 I = 51
35288
XDOT = -3638
725275 Wp = 133
92051
YDOT = 6400
629834 meter/sec RA = 313
15225 deg
ZDOT = 2154
791473 TA = 294
95130
MA = 295
05116
Ha = 221
571 n
mi
Hp = 213
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14927863
40 X = 4515433
72
Y = 3011183
48 feet Y = 968496
51 meter
Z = 16194753
20 Z = 4958179
61
XDOT = -11938
075048 XDOT = -3720
495421
YDOT = 20999
441711 feet/sec YDOT = 6359
481818 meter/sec
ZDOT = 7069
525830 ZDOT = 2136
917175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3058021
51 X = -932084
96
Y = 14811798
36 feet Y = 4514636
14 meter
Z = 16292252
66 Z = 4965878
61
XDOT = -19883
080030 XDOT = -6060
362793
YDOT = -11825
648560 feet/sec YDOT = -3604
457681 meter/sec
ZDOT = 6989
130504 ZDOT = 2130
286978
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 17329
62416776
00016717 00000-0 10270-3 0 9110
2 25544 51
6397 313
5384 0003716 153
8520 206
2821 15
54252037 6855
Satellite: ISS
Catalog Number: 25544
Epoch time: 17329
62416776 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 313
5384 deg
Eccentricity:
0003716
Arg of perigee: 153
8520 deg
Mean anomaly: 206
2821 deg
Mean motion: 15
54252037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 685
Checksum: 309
Coasting Arc #13 (Orbit 699)
---------------------------------------
Vector Time (GMT): 2017/330/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3484097
90 A = 6777105
51 meter
Y = -2426997
31 meter E =
0016701
Z = -5296237
30 I = 51
32579
XDOT = 4588
992486 Wp = 99
85739
YDOT = -6125
246033 meter/sec RA = 308
13071 deg
ZDOT = -215
336778 TA = 168
09792
MA = 168
05840
Ha = 221
721 n
mi
Hp = 213
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11430767
38 X = -3430972
82
Y = -7962589
61 feet Y = -2465661
66 meter
Z = -17376106
64 Z = -5313033
19
XDOT = 15055
749625 XDOT = 4658
191575
YDOT = -20095
951551 feet/sec YDOT = -6073
541860 meter/sec
ZDOT = -706
485493 ZDOT = -192
876762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7803331
54 X = 2378455
45
Y = -11427755
04 feet Y = -3483179
73 meter
Z = -17450180
22 Z = -5318814
93
XDOT = 19473
529921 XDOT = 5935
531920
YDOT = 14205
498074 feet/sec YDOT = 4329
835813 meter/sec
ZDOT = -605
813367 ZDOT = -184
651914
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 17330
58863928
00016717 00000-0 10270-3 0 9123
2 25544 51
6393 308
7291 0003675 154
5107 205
6228 15
54219373 7005
Satellite: ISS
Catalog Number: 25544
Epoch time: 17330
58863928 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 308
7291 deg
Eccentricity:
0003675
Arg of perigee: 154
5107 deg
Mean anomaly: 205
6228 deg
Mean motion: 15
54219373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 700
Checksum: 312
Coasting Arc #14 (Orbit 715)
---------------------------------------
Vector Time (GMT): 2017/331/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2318397
64 A = 6778095
54 meter
Y = 3862606
74 meter E =
0005786
Z = 5059272
01 I = 51
30960
XDOT = -5177
669233 Wp = 93
24289
YDOT = 5388
639209 meter/sec RA = 303
10896 deg
ZDOT = -1740
013651 TA = 13
65502
MA = 13
63937
Ha = 221
567 n
mi
Hp = 213
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7606291
46 X = 2250456
87
Y = 12672594
29 feet Y = 3888152
66 meter
Z = 16598661
44 Z = 5070369
26
XDOT = -16987
103782 XDOT = -5229
089389
YDOT = 17679
262496 feet/sec YDOT = 5330
451501 meter/sec
ZDOT = -5708
706204 ZDOT = -1765
290251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12432891
48 X = -3789545
32
Y = 7890449
51 feet Y = 2405009
01 meter
Z = 16647218
79 Z = 5074072
29
XDOT = -17625
753341 XDOT = -5372
329618
YDOT = -15480
371863 feet/sec YDOT = -4718
417344 meter/sec
ZDOT = -5821
729762 ZDOT = -1774
463232
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 17331
61740381
00016717 00000-0 10270-3 0 9136
2 25544 51
6392 303
6009 0003670 158
0931 202
0379 15
54228336 7168
Satellite: ISS
Catalog Number: 25544
Epoch time: 17331
61740381 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 303
6009 deg
Eccentricity:
0003670
Arg of perigee: 158
0931 deg
Mean anomaly: 202
0379 deg
Mean motion: 15
54228336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 716
Checksum: 288
Coasting Arc #15 (Orbit 730)
---------------------------------------
Vector Time (GMT): 2017/332/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1159980
60 A = 6781203
25 meter
Y = -5129632
89 meter E =
0011003
Z = -4292699
65 I = 51
30317
XDOT = 5397
581225 Wp = 125
31054
YDOT = -4152
382963 meter/sec RA = 298
09054 deg
ZDOT = 3503
549157 TA = 180
57389
MA = 180
57515
Ha = 221
562 n
mi
Hp = 213
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3805710
64 X = -1081681
32
Y = -16829504
22 feet Y = -5142166
72 meter
Z = -14083660
28 Z = -4298144
46
XDOT = 17708
599820 XDOT = 5426
594347
YDOT = -13623
303686 feet/sec YDOT = -4091
861351 meter/sec
ZDOT = 11494
583850 ZDOT = 3529
839732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16630721
56 X = 5069043
93
Y = -4525311
60 feet Y = -1379314
98 meter
Z = -14106941
14 Z = -4299795
66
XDOT = 14131
816707 XDOT = 4307
377732
YDOT = 15738
217623 feet/sec YDOT = 4797
008732 meter/sec
ZDOT = 11611
882576 ZDOT = 3539
301809
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 17332
58186491
00016717 00000-0 10270-3 0 9140
2 25544 51
6394 298
7921 0003623 163
1787 196
9486 15
54232758 7311
Satellite: ISS
Catalog Number: 25544
Epoch time: 17332
58186491 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 298
7921 deg
Eccentricity:
0003623
Arg of perigee: 163
1787 deg
Mean anomaly: 196
9486 deg
Mean motion: 15
54232758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 731
Checksum: 345
Coasting Arc #16 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2017/333/13:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 934927
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 56756
27 A = 6785060
14 meter
Y = 6060953
79 meter E =
0014747
Z = 3031293
86 I = 51
30223
XDOT = -5341
023196 Wp = 109
07597
YDOT = 2510
542901 meter/sec RA = 293
08130 deg
ZDOT = -4904
892379 TA = 35
95594
MA = 35
85680
Ha = 221
437 n
mi
Hp = 214
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 186208
23 X = -25747
97
Y = 19885019
01 feet Y = 6061127
12 meter
Z = 9945189
85 Z = 3031369
29
XDOT = -17523
041983 XDOT = -5344
873807
YDOT = 8236
689308 feet/sec YDOT = 2450
794487 meter/sec
ZDOT = -16092
166599 ZDOT = -4930
847196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19834968
49 X = -6045698
40
Y = 1426951
92 feet Y = 434934
95 meter
Z = 9944510
48 Z = 3031086
79
XDOT = -9257
648525 XDOT = -2821
731270
YDOT = -15391
874131 feet/sec YDOT = -4691
443235 meter/sec
ZDOT = -16207
692245 ZDOT = -4940
104596
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 17333
61061781
00016717 00000-0 10270-3 0 9150
2 25544 51
6399 293
6625 0003527 165
2374 194
8882 15
54256131 7474
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
61061781 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 293
6625 deg
Eccentricity:
0003527
Arg of perigee: 165
2374 deg
Mean anomaly: 194
8882 deg
Mean motion: 15
54256131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 328
Coasting Arc #17 (Orbit 747)
---------------------------------------
Vector Time (GMT): 2017/333/15:53:19
725
Vector Time (MET): N/A
Weight (LBS) : 934788
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2930841
07 A = 6778831
69 meter
Y = -3474046
27 meter E =
0014079
Z = -5041986
66 I = 51
27964
XDOT = 4158
892709 Wp = 116
79113
YDOT = -6164
466474 meter/sec RA = 292
64116 deg
ZDOT = 1827
685843 TA = 171
03480
MA = 171
00963
Ha = 221
479 n
mi
Hp = 214
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9615620
32 X = -2867283
58
Y = -11397789
60 feet Y = -3506465
47 meter
Z = -16541950
98 Z = -5056069
73
XDOT = 13644
661118 XDOT = 4218
638160
YDOT = -20224
627541 feet/sec YDOT = -6117
624871 meter/sec
ZDOT = 5996
344630 ZDOT = 1848
033829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3587168
42 X = 1093368
94
Y = -14403161
78 feet Y = -4390083
71 meter
Z = -16603826
60 Z = -5060846
35
XDOT = 23305
134455 XDOT = 7103
404982
YDOT = -1222
036780 feet/sec YDOT = -372
476810 meter/sec
ZDOT = 6087
615126 ZDOT = 1855
505090
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 17333
67491471
00016717 00000-0 10270-3 0 9160
2 25544 51
6416 293
3427 0003253 182
7310 177
3826 15
54014398 7483
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
67491471 = yrday
fracday
Element set: 916
Inclination: 51
6416 deg
RA of node: 293
3427 deg
Eccentricity:
0003253
Arg of perigee: 182
7310 deg
Mean anomaly: 177
3826 deg
Mean motion: 15
54014398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 748
Checksum: 317
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