[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 21st 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
201/17:46:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
7
209/14:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 212
4
212/23:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 212
2
214/15:20:49
459 -0
6 0
7 0
7
N/A 0
1 -0
0 223
0
000/00:01:38
918 0
1 -0
0 212
6
Coasting Arc #1 (Orbit 2676)
---------------------------------------
Vector Time (GMT): 2017/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5142636
16 A = 6782381
18 meter
Y = -1985190
45 meter E =
0011290
Z = -3959603
82 I = 51
32268
XDOT = -535
184889 Wp = 80
74190
YDOT = -6525
007143 meter/sec RA = 236
20724 deg
ZDOT = 3977
981523 TA = 230
90197
MA = 231
00242
Ha = 222
809 n
mi
Hp = 212
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16872165
87 X = -5100821
28
Y = -6513092
04 feet Y = -2042464
68 meter
Z = -12990826
18 Z = -3984483
72
XDOT = -1755
855935 XDOT = -481
503776
YDOT = -21407
503749 feet/sec YDOT = -6530
692216 meter/sec
ZDOT = 13051
120483 ZDOT = 3975
511460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1694534
18 X = 516494
02
Y = 17926523
75 feet Y = 5464004
44 meter
Z = -13100389
84 Z = -3992998
82
XDOT = -17007
157026 XDOT = -5183
781462
YDOT = 11110
562728 feet/sec YDOT = 3386
499520 meter/sec
ZDOT = 13041
234857 ZDOT = 3974
968385
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 17200
50869150
00016717 00000-0 10270-3 0 9001
2 25544 51
6400 237
2171 0006024 49
2680 310
8995 15
54194842 26772
Satellite: ISS
Catalog Number: 25544
Epoch time: 17200
50869150 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 237
2171 deg
Eccentricity:
0006024
Arg of perigee: 49
2680 deg
Mean anomaly: 310
8995 deg
Mean motion: 15
54194842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2677
Checksum: 297
Coasting Arc #2 (Orbit 2692)
---------------------------------------
Vector Time (GMT): 2017/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5319149
66 A = 6786181
12 meter
Y = 3315063
37 meter E =
0018074
Z = 2587057
77 I = 51
35396
XDOT = -900
210616 Wp = 87
99133
YDOT = 5545
235817 meter/sec RA = 231
20429 deg
ZDOT = -5222
512489 TA = 62
76552
MA = 62
58148
Ha = 222
846 n
mi
Hp = 212
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17451278
42 X = 5269117
85
Y = 10876192
17 feet Y = 3374265
66 meter
Z = 8487722
33 Z = 2612775
24
XDOT = -2953
446904 XDOT = -936
783777
YDOT = 18193
030896 feet/sec YDOT = 5534
965178 meter/sec
ZDOT = -17134
227326 ZDOT = -5226
973575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1581892
48 X = 482160
83
Y = -20454927
12 feet Y = -6234661
79 meter
Z = 8600795
18 Z = 2621522
37
XDOT = 15946
679988 XDOT = 4860
548060
YDOT = -6023
870533 feet/sec YDOT = -1836
075738 meter/sec
ZDOT = -17154
792179 ZDOT = -5228
780656
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 17201
53748496
00016717 00000-0 10270-3 0 9015
2 25544 51
6395 232
0881 0006088 52
1730 307
9973 15
54210311 26936
Satellite: ISS
Catalog Number: 25544
Epoch time: 17201
53748496 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 232
0881 deg
Eccentricity:
0006088
Arg of perigee: 52
1730 deg
Mean anomaly: 307
9973 deg
Mean motion: 15
54210311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2693
Checksum: 305
Coasting Arc #3 (Orbit 2696)
---------------------------------------
Vector Time (GMT): 2017/201/17:46:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 422043
07 A = 6780538
84 meter
Y = -5068413
79 meter E =
0013045
Z = 4472773
23 I = 51
33916
XDOT = 6129
912349 Wp = 88
50142
YDOT = 3336
788375 meter/sec RA = 230
04546 deg
ZDOT = 3194
997440 TA = 329
24808
MA = 329
32445
Ha = 222
777 n
mi
Hp = 212
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1384655
73 X = 456961
68
Y = -16628654
16 feet Y = -5063499
51 meter
Z = 14674452
86 Z = 4474907
57
XDOT = 20111
260989 XDOT = 6076
624314
YDOT = 10947
468423 feet/sec YDOT = 3405
038879 meter/sec
ZDOT = 10482
275066 ZDOT = 3224
645391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5710890
50 X = 1740679
42
Y = 15668927
99 feet Y = 4775889
25 meter
Z = 14684665
56 Z = 4475886
06
XDOT = -21634
031877 XDOT = -6594
052916
YDOT = -2084
849108 feet/sec YDOT = -635
462008 meter/sec
ZDOT = 10612
709878 ZDOT = 3234
753971
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 17201
79468283
00016717 00000-0 10270-3 0 9027
2 25544 51
6387 230
8064 0005941 51
3957 308
7727 15
54222206 26971
Satellite: ISS
Catalog Number: 25544
Epoch time: 17201
79468283 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 230
8064 deg
Eccentricity:
0005941
Arg of perigee: 51
3957 deg
Mean anomaly: 308
7727 deg
Mean motion: 15
54222206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2697
Checksum: 322
Coasting Arc #4 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2017/202/17:46:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1809877
94 A = 6777834
29 meter
Y = 4026946
33 meter E =
0019543
Z = -5160060
95 I = 51
35089
XDOT = -6044
233999 Wp = 72
03436
YDOT = -4487
912212 meter/sec RA = 225
02881 deg
ZDOT = -1380
815582 TA = 184
60059
MA = 184
61857
Ha = 222
948 n
mi
Hp = 212
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5937919
75 X = -1829709
09
Y = 13211766
18 feet Y = 4006596
79 meter
Z = -16929333
83 Z = -5168900
34
XDOT = -19830
164038 XDOT = -5986
892529
YDOT = -14724
121432 feet/sec YDOT = -4555
182156 meter/sec
ZDOT = -4530
234850 ZDOT = -1410
037483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -413322
26 X = -125980
63
Y = -14432401
79 feet Y = -4398996
07 meter
Z = -16968999
49 Z = -5172151
04
XDOT = 23153
115603 XDOT = 7057
069636
YDOT = 4820
441772 feet/sec YDOT = 1469
270652 meter/sec
ZDOT = -4658
635403 ZDOT = -1419
952071
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 17202
75917593
00016717 00000-0 10270-3 0 9038
2 25544 51
6380 225
9978 0006109 54
6610 305
5113 15
54196332 27124
Satellite: ISS
Catalog Number: 25544
Epoch time: 17202
75917593 = yrday
fracday
Element set: 903
Inclination: 51
6380 deg
RA of node: 225
9978 deg
Eccentricity:
0006109
Arg of perigee: 54
6610 deg
Mean anomaly: 305
5113 deg
Mean motion: 15
54196332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 306
Coasting Arc #5 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2017/203/17:46:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3206411
93 A = 6777166
52 meter
Y = -2802282
78 meter E =
0008731
Z = 5265960
45 I = 51
37298
XDOT = 5554
990896 Wp = 60
64406
YDOT = 5263
989305 meter/sec RA = 220
00989 deg
ZDOT = -576
239955 TA = 34
89978
MA = 34
84256
Ha = 222
758 n
mi
Hp = 212
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10519724
19 X = 3211930
51
Y = -9193841
15 feet Y = -2766396
23 meter
Z = 17276773
14 Z = 5281549
02
XDOT = 18225
035747 XDOT = 5498
513763
YDOT = 17270
306119 feet/sec YDOT = 5325
793264 meter/sec
ZDOT = -1890
551035 ZDOT = -549
392615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5227615
25 X = -1593377
13
Y = 12863284
28 feet Y = 3920729
05 meter
Z = 17346070
41 Z = 5287082
26
XDOT = -23079
627065 XDOT = -7034
670329
YDOT = -6967
288218 feet/sec YDOT = -2123
629449 meter/sec
ZDOT = -1772
731437 ZDOT = -540
328542
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 17203
78796354
00016717 00000-0 10270-3 0 9043
2 25544 51
6382 220
8694 0005953 57
0600 303
1125 15
54222454 27286
Satellite: ISS
Catalog Number: 25544
Epoch time: 17203
78796354 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 220
8694 deg
Eccentricity:
0005953
Arg of perigee: 57
0600 deg
Mean anomaly: 303
1125 deg
Mean motion: 15
54222454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 303
Coasting Arc #6 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2017/204/17:46:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4500620
53 A = 6779087
79 meter
Y = 1562420
12 meter E =
0016617
Z = -4837465
16 I = 51
40532
XDOT = -4588
652066 Wp = 92
37240
YDOT = -5611
984757 meter/sec RA = 214
99288 deg
ZDOT = 2463
226219 TA = 201
89994
MA = 201
97105
Ha = 222
972 n
mi
Hp = 212
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14765815
39 X = -4494259
91
Y = 5126050
26 feet Y = 1512127
12 meter
Z = -15870948
70 Z = -4859311
72
XDOT = -15054
632764 XDOT = -4537
521219
YDOT = -18412
023480 feet/sec YDOT = -5663
012511 meter/sec
ZDOT = 8081
450850 ZDOT = 2441
060137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10655737
75 X = 3247868
87
Y = -11299555
62 feet Y = -3444104
55 meter
Z = -15967717
55 Z = -4866960
31
XDOT = 21063
568626 XDOT = 6420
175717
YDOT = 8611
266824 feet/sec YDOT = 2624
714128 meter/sec
ZDOT = 7984
340650 ZDOT = 2433
627030
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 17204
75244976
00016717 00000-0 10270-3 0 9050
2 25544 51
6386 216
0599 0006117 61
0315 299
1450 15
54206332 27431
Satellite: ISS
Catalog Number: 25544
Epoch time: 17204
75244976 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 216
0599 deg
Eccentricity:
0006117
Arg of perigee: 61
0315 deg
Mean anomaly: 299
1450 deg
Mean motion: 15
54206332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 305
Coasting Arc #7 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2017/205/17:46:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5565680
44 A = 6782698
92 meter
Y = -332339
42 meter E =
0017188
Z = 3851360
98 I = 51
44446
XDOT = 3197
451211 Wp = 75
73271
YDOT = 5631
842850 meter/sec RA = 209
98715 deg
ZDOT = -4115
137365 TA = 57
65016
MA = 57
48389
Ha = 222
933 n
mi
Hp = 212
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18260106
44 X = 5550275
51
Y = -1090352
44 feet Y = -270186
59 meter
Z = 12635698
74 Z = 3878359
27
XDOT = 10490
325497 XDOT = 3154
225677
YDOT = 18477
174705 feet/sec YDOT = 5667
357498 meter/sec
ZDOT = -13501
106839 ZDOT = -4099
710116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15471418
67 X = -4715688
41
Y = 9603374
46 feet Y = 2927108
54 meter
Z = 12755063
37 Z = 3887743
32
XDOT = -17392
555664 XDOT = -5301
250967
YDOT = -10093
034601 feet/sec YDOT = -3076
356946 meter/sec
ZDOT = -13433
756127 ZDOT = -4094
608868
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 17205
78123189
00016717 00000-0 10270-3 0 9067
2 25544 51
6384 210
9312 0006132 64
8829 295
2959 15
54202485 27596
Satellite: ISS
Catalog Number: 25544
Epoch time: 17205
78123189 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 210
9312 deg
Eccentricity:
0006132
Arg of perigee: 64
8829 deg
Mean anomaly: 295
2959 deg
Mean motion: 15
54202485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 327
Coasting Arc #8 (Orbit 2773)
---------------------------------------
Vector Time (GMT): 2017/206/17:46:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6268416
37 A = 6786342
44 meter
Y = -731730
75 meter E =
0011141
Z = -2494593
86 I = 51
48626
XDOT = -1475
549447 Wp = 60
38290
YDOT = -5338
897664 meter/sec RA = 204
99323 deg
ZDOT = 5297
020409 TA = 271
59553
MA = 271
72315
Ha = 222
949 n
mi
Hp = 212
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20565670
52 X = -6247650
84
Y = -2400691
44 feet Y = -801712
23 meter
Z = -8184363
06 Z = -2524992
81
XDOT = -4841
041493 XDOT = -1441
468583
YDOT = -17516
068451 feet/sec YDOT = -5355
207914 meter/sec
ZDOT = 17378
675881 ZDOT = 5289
935365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19050996
84 X = 5806743
84
Y = -7972079
31 feet Y = -2429889
77 meter
Z = -8318617
24 Z = -2535514
53
XDOT = 12329
862368 XDOT = 3758
142050
YDOT = 11440
820172 feet/sec YDOT = 3487
161989 meter/sec
ZDOT = 17348
135177 ZDOT = 5287
711602
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 17206
74571276
00016717 00000-0 10270-3 0 9079
2 25544 51
6391 206
1225 0006041 68
2641 291
9155 15
54216302 27744
Satellite: ISS
Catalog Number: 25544
Epoch time: 17206
74571276 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 206
1225 deg
Eccentricity:
0006041
Arg of perigee: 68
2641 deg
Mean anomaly: 291
9155 deg
Mean motion: 15
54216302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2774
Checksum: 297
Coasting Arc #9 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2017/207/17:46:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6519372
22 A = 6788814
50 meter
Y = 1687092
02 meter E =
0017682
Z = 812431
98 I = 51
52532
XDOT = -499
690824 Wp = 110
30416
YDOT = 4835
100015 meter/sec RA = 200
01062 deg
ZDOT = -5931
930766 TA = 60
89544
MA = 60
71852
Ha = 223
049 n
mi
Hp = 212
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21389016
48 X = 6496075
86
Y = 5535078
81 feet Y = 1759865
80 meter
Z = 2665459
24 Z = 844043
92
XDOT = -1639
405592 XDOT = -524
907193
YDOT = 15863
189027 feet/sec YDOT = 4829
371266 meter/sec
ZDOT = -19461
715110 ZDOT = -5934
419205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21237037
89 X = -6473049
15
Y = 6029282
85 feet Y = 1837725
41 meter
Z = 2804953
88 Z = 854949
94
XDOT = -6275
273889 XDOT = -1912
703481
YDOT = -12900
688040 feet/sec YDOT = -3932
129715 meter/sec
ZDOT = -19473
408386 ZDOT = -5935
494876
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 17207
77448901
00016717 00000-0 10270-3 0 9082
2 25544 51
6402 200
9931 0006043 72
4293 287
7520 15
54199764 27904
Satellite: ISS
Catalog Number: 25544
Epoch time: 17207
77448901 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 200
9931 deg
Eccentricity:
0006043
Arg of perigee: 72
4293 deg
Mean anomaly: 287
7520 deg
Mean motion: 15
54199764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 320
Coasting Arc #10 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2017/208/17:46:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6267453
56 A = 6788784
85 meter
Y = -2424993
51 meter E =
0019291
Z = 902396
62 I = 51
55646
XDOT = 2488
857905 Wp = 60
92015
YDOT = -4197
423127 meter/sec RA = 195
03327 deg
ZDOT = 5919
829576 TA = 308
86310
MA = 309
03507
Ha = 223
075 n
mi
Hp = 212
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20562511
68 X = -6244254
17
Y = -7956015
44 feet Y = -2494950
73 meter
Z = 2960618
84 Z = 872008
07
XDOT = 8165
544308 XDOT = 2506
854447
YDOT = -13771
073251 feet/sec YDOT = -4169
490471 meter/sec
ZDOT = 19422
013045 ZDOT = 5931
963147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21715354
59 X = 6618840
08
Y = -3915854
96 feet Y = -1193552
59 meter
Z = 2826621
14 Z = 861554
12
XDOT = 15
204795 XDOT = 4
634421
YDOT = 14357
582260 feet/sec YDOT = 4376
191073 meter/sec
ZDOT = 19476
250426 ZDOT = 5936
361130
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 17208
80326179
00016717 00000-0 10270-3 0 9090
2 25544 51
6405 195
8639 0006126 74
3371 285
8457 15
54209528 28060
Satellite: ISS
Catalog Number: 25544
Epoch time: 17208
80326179 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 195
8639 deg
Eccentricity:
0006126
Arg of perigee: 74
3371 deg
Mean anomaly: 285
8457 deg
Mean motion: 15
54209528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 334
Coasting Arc #11 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2017/209/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3195694
77 A = 6781086
97 meter
Y = 4118017
10 meter E =
0014682
Z = -4352096
73 I = 51
55684
XDOT = -6661
769235 Wp = 73
38316
YDOT = 1530
420564 meter/sec RA = 190
67522 deg
ZDOT = -3449
118435 TA = 161
53101
MA = 161
47766
Ha = 223
057 n
mi
Hp = 212
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10484562
88 X = 3170548
58
Y = 13510554
78 feet Y = 4153612
98 meter
Z = -14278532
59 Z = -4336634
27
XDOT = -21856
198279 XDOT = -6661
633778
YDOT = 5021
064842 feet/sec YDOT = 1455
924928 meter/sec
ZDOT = -11316
005365 ZDOT = -3481
478485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7428669
00 X = -2264258
31
Y = -15466319
38 feet Y = -4714134
15 meter
Z = -14210752
41 Z = -4331437
33
XDOT = 21223
712670 XDOT = 6468
987622
YDOT = 318
149672 feet/sec YDOT = 96
972020 meter/sec
ZDOT = -11459
293211 ZDOT = -3492
792571
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 17209
63913744
00016717 00000-0 10270-3 0 9104
2 25544 51
6386 191
6958 0006125 77
7184 282
4654 15
54234442 28193
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
63913744 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 191
6958 deg
Eccentricity:
0006125
Arg of perigee: 77
7184 deg
Mean anomaly: 282
4654 deg
Mean motion: 15
54234442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 331
Coasting Arc #12 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2017/210/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1487961
05 A = 6777930
44 meter
Y = -4207527
21 meter E =
0010313
Z = 5093127
71 I = 51
57954
XDOT = 7465
206169 Wp = 102
45664
YDOT = -598
362514 meter/sec RA = 185
67626 deg
ZDOT = 1681
593946 TA = 331
27683
MA = 331
33359
Ha = 222
954 n
mi
Hp = 212
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4881761
96 X = -1465540
44
Y = -13804223
11 feet Y = -4224041
32 meter
Z = 16709736
59 Z = 5085954
12
XDOT = 24492
146224 XDOT = 7463
174114
YDOT = -1963
131608 feet/sec YDOT = -514
892895 meter/sec
ZDOT = 5517
040506 ZDOT = 1717
852293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2159349
38 X = 658169
69
Y = 14517734
58 feet Y = 4425005
50 meter
Z = 16678611
02 Z = 5083640
64
XDOT = -23301
293567 XDOT = -7102
234279
YDOT = -3075
779716 feet/sec YDOT = -937
497658 meter/sec
ZDOT = 5677
448781 ZDOT = 1730
486389
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 17210
66790353
00016717 00000-0 10270-3 0 9119
2 25544 51
6392 186
5674 0005847 81
7627 278
4189 15
54267672 28352
Satellite: ISS
Catalog Number: 25544
Epoch time: 17210
66790353 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 186
5674 deg
Eccentricity:
0005847
Arg of perigee: 81
7627 deg
Mean anomaly: 278
4189 deg
Mean motion: 15
54267672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2835
Checksum: 345
Coasting Arc #13 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2017/211/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -372048
26 A = 6777080
57 meter
Y = 4208666
17 meter E =
0020883
Z = -5316893
17 I = 51
60912
XDOT = -7641
318195 Wp = 90
06754
YDOT = -315
910712 meter/sec RA = 180
67194 deg
ZDOT = 285
583340 TA = 182
65574
MA = 182
66685
Ha = 223
055 n
mi
Hp = 212
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1220630
77 X = -393256
38
Y = 13807959
89 feet Y = 4204387
23 meter
Z = -17443875
22 Z = -5318751
85
XDOT = -25069
941586 XDOT = -7638
604894
YDOT = -1036
452467 feet/sec YDOT = -401
345961 meter/sec
ZDOT = 936
953215 ZDOT = 248
471075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3588532
39 X = 1093784
67
Y = -13377764
15 feet Y = -4077542
51 meter
Z = -17452688
62 Z = -5319579
49
XDOT = 23497
659446 XDOT = 7162
086599
YDOT = 5298
907774 feet/sec YDOT = 1615
107090 meter/sec
ZDOT = 772
879221 ZDOT = 235
573587
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 17211
63237084
00016717 00000-0 10270-3 0 9125
2 25544 51
6394 181
7581 0006077 84
1735 276
0110 15
54231688 28504
Satellite: ISS
Catalog Number: 25544
Epoch time: 17211
63237084 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 181
7581 deg
Eccentricity:
0006077
Arg of perigee: 84
1735 deg
Mean anomaly: 276
0110 deg
Mean motion: 15
54231688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 303
Coasting Arc #14 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2017/212/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2210601
48 A = 6778592
56 meter
Y = -4080869
41 meter E =
0011986
Z = 4931894
55 I = 51
64663
XDOT = 7242
682964 Wp = 72
66281
YDOT = 1220
400549 meter/sec RA = 175
67278 deg
ZDOT = -2228
580495 TA = 39
11171
MA = 39
02512
Ha = 222
978 n
mi
Hp = 212
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7252629
54 X = 2232114
01
Y = -13388679
17 feet Y = -4056028
86 meter
Z = 16180756
38 Z = 4942684
98
XDOT = 23762
083214 XDOT = 7239
323100
YDOT = 4003
938808 feet/sec YDOT = 1301
374447 meter/sec
ZDOT = -7311
615797 ZDOT = -2193
406173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9247264
51 X = -2818566
22
Y = 12032458
69 feet Y = 3667493
41 meter
Z = 16229056
64 Z = 4946616
47
XDOT = -21951
814952 XDOT = -6690
913197
YDOT = -7183
309433 feet/sec YDOT = -2189
472715 meter/sec
ZDOT = -7156
220306 ZDOT = -2181
215949
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 17212
66113177
00016717 00000-0 10270-3 0 9136
2 25544 51
6390 176
6301 0006057 87
7541 272
4305 15
54241848 28667
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
66113177 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 176
6301 deg
Eccentricity:
0006057
Arg of perigee: 87
7541 deg
Mean anomaly: 272
4305 deg
Mean motion: 15
54241848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2866
Checksum: 307
Coasting Arc #15 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2618570
27 A = 6779347
06 meter
Y = 4069412
33 meter E =
0017263
Z = -4764186
67 I = 51
65925
XDOT = -7032
950925 Wp = 103
92224
YDOT = -1385
135260 meter/sec RA = 173
89853 deg
ZDOT = 2686
556130 TA = 192
63668
MA = 192
68001
Ha = 223
064 n
mi
Hp = 212
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8591109
80 X = -2640738
99
Y = 13351090
32 feet Y = 4040005
94 meter
Z = -15630533
68 Z = -4776960
45
XDOT = -23073
985975 XDOT = -7029
989145
YDOT = -4544
407021 feet/sec YDOT = -1463
766045 meter/sec
ZDOT = 8814
160531 ZDOT = 2652
399637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15782862
83 X = -4810616
59
Y = -1082858
15 feet Y = -330055
17 meter
Z = -15687607
29 Z = -4781582
70
XDOT = -7133
311804 XDOT = -2174
233438
YDOT = -21342
062868 feet/sec YDOT = -6505
060762 meter/sec
ZDOT = 8663
283100 ZDOT = 2640
568689
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 17212
98261875
00016717 00000-0 10270-3 0 9141
2 25544 51
6376 175
0227 0006139 94
1013 266
0841 15
54238346 28717
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
98261875 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 175
0227 deg
Eccentricity:
0006139
Arg of perigee: 94
1013 deg
Mean anomaly: 266
0841 deg
Mean motion: 15
54238346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 312
Coasting Arc #16 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197087
27 A = 6783101
02 meter
Y = -3809067
43 meter E =
0017624
Z = 3711361
62 I = 51
70424
XDOT = 5918
456106 Wp = 89
23115
YDOT = 2306
395534 meter/sec RA = 168
90983 deg
ZDOT = -4308
031978 TA = 46
50129
MA = 46
35493
Ha = 222
998 n
mi
Hp = 212
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13769971
34 X = 4221341
51
Y = -12496940
37 feet Y = -3761997
32 meter
Z = 12176383
27 Z = 3731808
31
XDOT = 19417
506911 XDOT = 5913
151635
YDOT = 7566
914481 feet/sec YDOT = 2372
550289 meter/sec
ZDOT = -14133
963184 ZDOT = -4279
294969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17618258
42 X = 5370045
17
Y = 5758343
55 feet Y = 1755143
11 meter
Z = 12267370
90 Z = 3739094
65
XDOT = 3446
190215 XDOT = 1050
398778
YDOT = 19420
508635 feet/sec YDOT = 5919
371032 meter/sec
ZDOT = -14007
169909 ZDOT = -4269
385388
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 17214
01137519
00016717 00000-0 10270-3 0 9155
2 25544 51
6377 169
8922 0006112 98
1018 262
0829 15
54228695 28876
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
01137519 = yrday
fracday
Element set: 915
Inclination: 51
6377 deg
RA of node: 169
8922 deg
Eccentricity:
0006112
Arg of perigee: 98
1018 deg
Mean anomaly: 262
0829 deg
Mean motion: 15
54228695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 325
Coasting Arc #17 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2017/214/15:21:38
918
Vector Time (MET): N/A
Weight (LBS) : 887492
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -169867
01 A = 6777689
08 meter
Y = 4315386
90 meter E =
0019771
Z = -5240919
11 I = 51
70976
XDOT = -7504
018362 Wp = 97
56570
YDOT = 1033
762626 meter/sec RA = 165
60057 deg
ZDOT = 1095
426832 TA = 182
93522
MA = 182
94684
Ha = 222
979 n
mi
Hp = 212
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -557306
47 X = -192652
62
Y = 14158093
51 feet Y = 4313360
22 meter
Z = -17194616
50 Z = -5241799
37
XDOT = -24619
482815 XDOT = -7520
341451
YDOT = 3391
609666 feet/sec YDOT = 949
756265 meter/sec
ZDOT = 3593
920053 ZDOT = 1058
935403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 207992
91 X = 63396
24
Y = -14162058
83 feet Y = -4316595
53 meter
Z = -17199124
04 Z = -5242293
01
XDOT = 23549
631906 XDOT = 7177
927805
YDOT = -3818
530436 feet/sec YDOT = -1163
888077 meter/sec
ZDOT = 3432
335412 ZDOT = 1046
175833
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 17214
65434493
00016717 00000-0 10270-3 0 9167
2 25544 51
6410 166
6918 0005473 94
6757 265
5021 15
54140343 28970
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
65434493 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 166
6918 deg
Eccentricity:
0005473
Arg of perigee: 94
6757 deg
Mean anomaly: 265
5021 deg
Mean motion: 15
54140343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2897
Checksum: 321
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