[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 25th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15234 4853 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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
143/16:17:59
113 -4
8 7
1 7
1
N/A 3
2 -0
7 226
0
000/00:19:54
227 4
2 -0
1 220
4
143/19:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 220
4
143/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
0
000/00:00:00
000 0
0 0
0 220
5
144/08:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
0
000/00:00:00
000 0
0 0
0 220
2
147/06:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
4
000/00:00:00
000 0
0 0
0 219
9
154/16:09:25
000 0
0 0
0 0
0
N/A 0
0 0
0 227
3
000/00:00:00
000 0
0 0
0 218
6
155/08:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
3
Coasting Arc #1 (Orbit 1125)
---------------------------------------
Vector Time (GMT): 2019/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4960358
62 A = 6792450
31 meter
Y = -4348557
35 meter E =
0007010
Z = -1611816
08 I = 51
95448
XDOT = 2151
051153 Wp = 129
59202
YDOT = 4579
014087 meter/sec RA = 127
73663 deg
ZDOT = -5754
950023 TA = 67
94960
MA = 67
87516
Ha = 223
579 n
mi
Hp = 216
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16274142
45 X = 5016446
12
Y = -14266920
45 feet Y = -4292773
32 meter
Z = -5288110
51 Z = -1587584
75
XDOT = 7057
254438 XDOT = 2127
641953
YDOT = 15023
012096 feet/sec YDOT = 4602
938546 meter/sec
ZDOT = -18881
069629 ZDOT = -5744
557188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3807416
69 X = -1160500
61
Y = -21331907
21 feet Y = -6501965
32 meter
Z = -5177852
60 Z = -1578209
47
XDOT = 15018
834397 XDOT = 4577
740724
YDOT = 1873
936058 feet/sec YDOT = 571
175710 meter/sec
ZDOT = -18834
336707 ZDOT = -5740
705828
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 19142
52913619
00016717 00000-0 10270-3 0 9000
2 25544 51
6368 128
6541 0001985 14
7360 345
3850 15
52691816 11264
Satellite: ISS
Catalog Number: 25544
Epoch time: 19142
52913619 = yrday
fracday
Element set: 900
Inclination: 51
6368 deg
RA of node: 128
6541 deg
Eccentricity:
0001985
Arg of perigee: 14
7360 deg
Mean anomaly: 345
3850 deg
Mean motion: 15
52691816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1126
Checksum: 308
Coasting Arc #2 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2019/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4952995
05 A = 6790324
45 meter
Y = 3744835
38 meter E =
0014341
Z = 2730103
85 I = 51
96743
XDOT = -1286
659811 Wp = 72
22598
YDOT = -5498
669769 meter/sec RA = 122
79237 deg
ZDOT = 5190
063170 TA = 318
50414
MA = 318
61294
Ha = 223
522 n
mi
Hp = 216
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16249983
76 X = -5007764
11
Y = 12286205
30 feet Y = 3689140
93 meter
Z = 8957033
64 Z = 2705911
45
XDOT = -4221
324840 XDOT = -1250
287001
YDOT = -18040
255149 feet/sec YDOT = -5512
855395 meter/sec
ZDOT = 17027
766307 ZDOT = 5183
900676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2459708
18 X = 749719
05
Y = 20271210
21 feet Y = 6178664
87 meter
Z = 8846984
62 Z = 2696560
91
XDOT = -16305
035394 XDOT = -4969
774788
YDOT = -5467
227694 feet/sec YDOT = -1666
411001 meter/sec
ZDOT = 17000
301746 ZDOT = 5181
691972
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 19143
55891986
00016717 00000-0 10270-3 0 9017
2 25544 51
6370 123
5326 0001750 13
5677 346
5521 15
52729014 11428
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
55891986 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 123
5326 deg
Eccentricity:
0001750
Arg of perigee: 13
5677 deg
Mean anomaly: 346
5521 deg
Mean motion: 15
52729014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 299
Coasting Arc #3 (Orbit 1143)
---------------------------------------
Vector Time (GMT): 2019/143/16:27:56
227
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3014277
70 A = 6797742
85 meter
Y = 6030639
78 meter E =
0014199
Z = -794045
72 I = 51
98410
XDOT = -4566
409862 Wp = 10
05097
YDOT = -1499
668875 meter/sec RA = 121
83980 deg
ZDOT = 5974
459382 TA = 341
41097
MA = 341
46279
Ha = 226
019 n
mi
Hp = 220
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9889362
52 X = -3077632
96
Y = 19785563
57 feet Y = 5996577
87 meter
Z = -2605136
88 Z = -808841
10
XDOT = -14981
659651 XDOT = -4578
321420
YDOT = -4920
173473 feet/sec YDOT = -1550
801024 meter/sec
ZDOT = 19601
244693 ZDOT = 5952
248300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21735607
40 X = 6625013
14
Y = -4058868
58 feet Y = -1237143
14 meter
Z = -2672772
30 Z = -814661
00
XDOT = 4895
380171 XDOT = 1492
111876
YDOT = 13436
393167 feet/sec YDOT = 4095
412637 meter/sec
ZDOT = 19500
641416 ZDOT = 5943
795504
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 19143
68764416
00016717 00000-0 10270-3 0 9029
2 25544 51
6408 122
8911 0007360 326
1202 33
9478 15
51143083 11447
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
68764416 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 122
8911 deg
Eccentricity:
0007360
Arg of perigee: 326
1202 deg
Mean anomaly: 33
9478 deg
Mean motion: 15
51143083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1144
Checksum: 290
Coasting Arc #4 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4363226
92 A = 6786900
47 meter
Y = -594212
16 meter E =
0003384
Z = 5163706
14 I = 51
95068
XDOT = 2787
511541 Wp = 358
62894
YDOT = -6967
495145 meter/sec RA = 121
15007 deg
ZDOT = 1556
921722 TA = 76
44061
MA = 76
40292
Ha = 226
177 n
mi
Hp = 220
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14315048
94 X = -4381340
45
Y = -1949514
95 feet Y = -643106
74 meter
Z = 16941293
10 Z = 5142467
10
XDOT = 9145
379071 XDOT = 2857
654210
YDOT = -22859
236039 feet/sec YDOT = -6935
931241 meter/sec
ZDOT = 5108
010899 ZDOT = 1570
631931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14392219
29 X = 4386748
44
Y = 2199560
68 feet Y = 670426
09 meter
Z = 16845017
17 Z = 5134361
23
XDOT = -9347
572768 XDOT = -2849
140180
YDOT = 21647
103619 feet/sec YDOT = 6598
037183 meter/sec
ZDOT = 5170
809956 ZDOT = 1576
062875
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 19143
88092002
00016717 00000-0 10270-3 0 9037
2 25544 51
6412 121
9322 0007410 326
7363 33
3321 15
51133737 11477
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88092002 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 121
9322 deg
Eccentricity:
0007410
Arg of perigee: 326
7363 deg
Mean anomaly: 33
3321 deg
Mean motion: 15
51133737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 268
Coasting Arc #5 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/21:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2557613
95 A = 6797338
75 meter
Y = 6165082
78 meter E =
0013272
Z = -1240320
55 I = 51
98478
XDOT = -4853
472866 Wp = 5
76688
YDOT = -834
875506 meter/sec RA = 120
88395 deg
ZDOT = 5876
623347 TA = 340
82425
MA = 340
87416
Ha = 225
992 n
mi
Hp = 220
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8391121
87 X = -2620338
78
Y = 20226649
55 feet Y = 6136131
19 meter
Z = -4069293
13 Z = -1252896
08
XDOT = -15923
467407 XDOT = -4872
321752
YDOT = -2739
092866 feet/sec YDOT = -889
256558 meter/sec
ZDOT = 19280
260325 ZDOT = 5853
001063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2255940
63 X = 687610
70
Y = -21770784
41 feet Y = -6635735
09 meter
Z = -4126875
69 Z = -1257871
71
XDOT = 14579
756782 XDOT = 4443
909867
YDOT = -2112
481705 feet/sec YDOT = -643
884424 meter/sec
ZDOT = 19173
195922 ZDOT = 5843
990117
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 19143
88091881
00016717 00000-0 10270-3 0 9042
2 25544 51
6394 121
9306 0007440 325
1939 34
8724 15
51148117 11474
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88091881 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 121
9306 deg
Eccentricity:
0007440
Arg of perigee: 325
1939 deg
Mean anomaly: 34
8724 deg
Mean motion: 15
51148117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 310
Coasting Arc #6 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2019/144/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 482404
06 A = 6793781
12 meter
Y = -6010945
72 meter E =
0010537
Z = 3127101
06 I = 51
98242
XDOT = 5501
672545 Wp = 61
57910
YDOT = -2113
568300 meter/sec RA = 118
50493 deg
ZDOT = -4894
051855 TA = 82
66493
MA = 82
54518
Ha = 226
019 n
mi
Hp = 220
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1582690
49 X = 534394
58
Y = -19720950
51 feet Y = -6005260
81 meter
Z = 10259517
90 Z = 3129569
96
XDOT = 18050
106774 XDOT = 5548
670781
YDOT = -6934
279198 feet/sec YDOT = -2051
781384 meter/sec
ZDOT = -16056
600575 ZDOT = -4867
212860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1769080
62 X = -539215
77
Y = -19698990
13 feet Y = -6004252
19 meter
Z = 10271253
47 Z = 3130678
06
XDOT = 15323
576076 XDOT = 4670
625988
YDOT = -9714
360075 feet/sec YDOT = -2960
936951 meter/sec
ZDOT = -15934
677709 ZDOT = -4856
889766
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 19144
39632340
00016717 00000-0 10270-3 0 9051
2 25544 51
6405 119
3734 0007145 329
5529 30
5206 15
51178791 11556
Satellite: ISS
Catalog Number: 25544
Epoch time: 19144
39632340 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 119
3734 deg
Eccentricity:
0007145
Arg of perigee: 329
5529 deg
Mean anomaly: 30
5206 deg
Mean motion: 15
51178791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 301
Coasting Arc #7 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2019/145/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -589465
46 A = 6795185
28 meter
Y = 6276633
36 meter E =
0009760
Z = -2521062
71 I = 52
00362
XDOT = -5258
694051 Wp = 5
35225
YDOT = 1642
323005 meter/sec RA = 113
56875 deg
ZDOT = 5329
523747 TA = 326
53713
MA = 326
59876
Ha = 226
165 n
mi
Hp = 219
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1933941
80 X = -647362
83
Y = 20592629
14 feet Y = 6269718
09 meter
Z = -8271203
12 Z = -2524066
08
XDOT = -17252
933237 XDOT = -5302
556013
YDOT = 5388
198834 feet/sec YDOT = 1583
270801 meter/sec
ZDOT = 17485
314131 ZDOT = 5303
872608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1908182
82 X = 581614
12
Y = 20589325
69 feet Y = 6275626
47 meter
Z = -8285397
58 Z = -2525389
18
XDOT = -14594
413122 XDOT = -4448
377119
YDOT = 8327
375697 feet/sec YDOT = 2538
184113 meter/sec
ZDOT = 17368
807766 ZDOT = 5294
012607
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 19145
36270512
00016717 00000-0 10270-3 0 9069
2 25544 51
6420 114
5778 0007090 333
5661 26
5127 15
51190299 11700
Satellite: ISS
Catalog Number: 25544
Epoch time: 19145
36270512 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 114
5778 deg
Eccentricity:
0007090
Arg of perigee: 333
5661 deg
Mean anomaly: 26
5127 deg
Mean motion: 15
51190299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 293
Coasting Arc #8 (Orbit 1185)
---------------------------------------
Vector Time (GMT): 2019/146/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 676503
53 A = 6796508
28 meter
Y = -6505445
49 meter E =
0010080
Z = 1841415
09 I = 52
01804
XDOT = 5036
983482 Wp = 84
28511
YDOT = -1088
272428 meter/sec RA = 108
63533 deg
ZDOT = -5667
612438 TA = 75
60486
MA = 75
49300
Ha = 226
348 n
mi
Hp = 219
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2219499
78 X = 740254
42
Y = -21343325
09 feet Y = -6497524
07 meter
Z = 6041388
09 Z = 1844855
54
XDOT = 16525
536358 XDOT = 5076
308637
YDOT = -3570
447599 feet/sec YDOT = -1031
724951 meter/sec
ZDOT = -18594
528996 ZDOT = -5643
049217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2117181
16 X = -645316
82
Y = -21349124
80 feet Y = -6507213
24 meter
Z = 6057597
66 Z = 1846355
77
XDOT = 14047
649275 XDOT = 4281
723499
YDOT = -6663
077150 feet/sec YDOT = -2030
905915 meter/sec
ZDOT = -18482
997912 ZDOT = -5633
617763
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 19146
39351157
00016717 00000-0 10270-3 0 9079
2 25544 51
6400 109
4624 0007183 337
8936 22
1904 15
51168275 11867
Satellite: ISS
Catalog Number: 25544
Epoch time: 19146
39351157 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 109
4624 deg
Eccentricity:
0007183
Arg of perigee: 337
8936 deg
Mean anomaly: 22
1904 deg
Mean motion: 15
51168275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1186
Checksum: 310
Coasting Arc #9 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2019/147/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4381456
10 A = 6788066
30 meter
Y = -1769867
21 meter E =
0013382
Z = -4884620
60 I = 51
99970
XDOT = 165
298931 Wp = 40
20629
YDOT = 7242
398032 meter/sec RA = 104
14033 deg
ZDOT = -2469
738188 TA = 205
58745
MA = 205
65373
Ha = 226
446 n
mi
Hp = 219
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14374855
97 X = 4424648
46
Y = -5806650
95 feet Y = -1720628
79 meter
Z = -16025658
15 Z = -4863232
31
XDOT = 542
319327 XDOT = 96
296733
YDOT = 23761
148399 feet/sec YDOT = 7243
860907 meter/sec
ZDOT = -8102
815578 ZDOT = -2469
102226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15555111
74 X = 4741198
06
Y = -1223963
25 feet Y = -373064
00 meter
Z = -15928459
16 Z = -4854994
35
XDOT = -6606
597445 XDOT = -2013
690901
YDOT = 21722
785456 feet/sec YDOT = 6621
105007 meter/sec
ZDOT = -8100
612313 ZDOT = -2469
066633
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 19147
29546722
00016717 00000-0 10270-3 0 9084
2 25544 51
6411 104
9856 0007149 339
5502 20
5362 15
51151160 12008
Satellite: ISS
Catalog Number: 25544
Epoch time: 19147
29546722 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 104
9856 deg
Eccentricity:
0007149
Arg of perigee: 339
5502 deg
Mean anomaly: 20
5362 deg
Mean motion: 15
51151160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 286
Coasting Arc #10 (Orbit 1215)
---------------------------------------
Vector Time (GMT): 2019/148/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4261793
81 A = 6786916
46 meter
Y = 1235265
77 meter E =
0004638
Z = 5132535
69 I = 52
00290
XDOT = -130
331820 Wp = 29
35933
YDOT = -7475
451672 meter/sec RA = 99
19753 deg
ZDOT = 1694
208493 TA = 44
37275
MA = 44
33560
Ha = 226
736 n
mi
Hp = 219
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13982263
16 X = -4300221
30
Y = 4052709
23 feet Y = 1187392
16 meter
Z = 16839027
86 Z = 5111740
14
XDOT = -427
597836 XDOT = -54
959068
YDOT = -24525
760078 feet/sec YDOT = -7476
487825 meter/sec
ZDOT = 5558
426815 ZDOT = 1693
757892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14666078
39 X = -4470220
69
Y = -82366
76 feet Y = -25105
39 meter
Z = 16744561
94 Z = 5103742
48
XDOT = 6459
164844 XDOT = 1968
753444
YDOT = -22592
993391 feet/sec YDOT = -6886
344385 meter/sec
ZDOT = 5557
100978 ZDOT = 1693
804378
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 19148
32627018
00016717 00000-0 10270-3 0 9098
2 25544 51
6409 99
8697 0007260 344
5645 15
5284 15
51171142 12164
Satellite: ISS
Catalog Number: 25544
Epoch time: 19148
32627018 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 99
8697 deg
Eccentricity:
0007260
Arg of perigee: 344
5645 deg
Mean anomaly: 15
5284 deg
Mean motion: 15
51171142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 316
Coasting Arc #11 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2019/149/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4200382
30 A = 6786293
30 meter
Y = -699873
51 meter E =
0015521
Z = -5296130
64 I = 52
00611
XDOT = 133
204210 Wp = 55
20100
YDOT = 7599
975316 meter/sec RA = 94
25480 deg
ZDOT = -891
925210 TA = 206
25547
MA = 206
33423
Ha = 226
762 n
mi
Hp = 219
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13780781
83 X = 4233622
18
Y = -2296172
94 feet Y = -652715
64 meter
Z = -17375756
70 Z = -5275645
90
XDOT = 437
021685 XDOT = 52
541731
YDOT = 24934
302217 feet/sec YDOT = 7601
013953 meter/sec
ZDOT = -2926
263813 ZDOT = -891
473495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14008624
12 X = 4269828
63
Y = 1471172
26 feet Y = 448413
31 meter
Z = -17282748
09 Z = -5267781
62
XDOT = -6066
264390 XDOT = -1848
997386
YDOT = 23140
540083 feet/sec YDOT = 7053
236617 meter/sec
ZDOT = -2924
961653 ZDOT = -891
528312
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 19149
29264711
00016717 00000-0 10270-3 0 9104
2 25544 51
6421 95
0742 0007308 347
4990 12
5979 15
51155723 12317
Satellite: ISS
Catalog Number: 25544
Epoch time: 19149
29264711 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 95
0742 deg
Eccentricity:
0007308
Arg of perigee: 347
4990 deg
Mean anomaly: 12
5979 deg
Mean motion: 15
51155723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 305
Coasting Arc #12 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2019/150/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4175515
85 A = 6785978
63 meter
Y = 114238
03 meter E =
0007295
Z = 5346725
34 I = 52
00487
XDOT = -140
059661 Wp = 11
49197
YDOT = -7663
772644 meter/sec RA = 89
31096 deg
ZDOT = 61
303329 TA = 77
96743
MA = 77
88569
Ha = 227
002 n
mi
Hp = 219
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13699198
98 X = -4202454
68
Y = 374796
67 feet Y = 67393
42 meter
Z = 17541749
80 Z = 5326376
59
XDOT = -459
513323 XDOT = -54
648540
YDOT = -25143
611038 feet/sec YDOT = -7664
861331 meter/sec
ZDOT = 201
126407 ZDOT = 60
829778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13476214
51 X = -4107550
18
Y = -3071012
94 feet Y = -936044
74 meter
Z = 17449413
55 Z = 5318581
25
XDOT = 5581
080290 XDOT = 1701
113272
YDOT = -23485
944135 feet/sec YDOT = -7158
515772 meter/sec
ZDOT = 199
750472 ZDOT = 60
883944
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 19150
32344862
00016717 00000-0 10270-3 0 9117
2 25544 51
6404 89
9584 0007329 352
6548 7
4495 15
51168880 12475
Satellite: ISS
Catalog Number: 25544
Epoch time: 19150
32344862 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 89
9584 deg
Eccentricity:
0007329
Arg of perigee: 352
6548 deg
Mean anomaly: 7
4495 deg
Mean motion: 15
51168880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 326
Coasting Arc #13 (Orbit 1261)
---------------------------------------
Vector Time (GMT): 2019/151/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213342
72 A = 6786224
13 meter
Y = 433180
29 meter E =
0014961
Z = -5313375
55 I = 52
00515
XDOT = 158
916968 Wp = 66
86157
YDOT = 7615
187263 meter/sec RA = 84
36816 deg
ZDOT = 754
248104 TA = 210
27837
MA = 210
36489
Ha = 227
021 n
mi
Hp = 219
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13823302
89 X = 4233995
42
Y = 1421195
18 feet Y = 480412
84 meter
Z = -17432334
50 Z = -5292858
21
XDOT = 521
381129 XDOT = 70
086190
YDOT = 24984
210182 feet/sec YDOT = 7616
467626 meter/sec
ZDOT = 2474
567271 ZDOT = 754
805070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13230506
42 X = 4032658
36
Y = 4614387
64 feet Y = 1406465
35 meter
Z = -17339288
07 Z = -5285015
00
XDOT = -4967
140156 XDOT = -1513
984319
YDOT = 23455
403262 feet/sec YDOT = 7149
206914 meter/sec
ZDOT = 2476
305770 ZDOT = 754
777999
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 19151
28982357
00016717 00000-0 10270-3 0 9121
2 25544 51
6416 85
1632 0007378 354
4386 5
6682 15
51151485 12622
Satellite: ISS
Catalog Number: 25544
Epoch time: 19151
28982357 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 85
1632 deg
Eccentricity:
0007378
Arg of perigee: 354
4386 deg
Mean anomaly: 5
6682 deg
Mean motion: 15
51151485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1262
Checksum: 317
Coasting Arc #14 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2019/152/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4289638
41 A = 6786784
76 meter
Y = -1010800
47 meter E =
0010989
Z = 5160230
27 I = 52
00253
XDOT = -145
436348 Wp = 20
68266
YDOT = -7498
715757 meter/sec RA = 79
42406 deg
ZDOT = -1578
744280 TA = 84
53231
MA = 84
40697
Ha = 227
206 n
mi
Hp = 218
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14073616
82 X = -4303082
46
Y = -3316274
52 feet Y = -1058846
00 meter
Z = 16929889
35 Z = 5139359
71
XDOT = -477
153374 XDOT = -53
903977
YDOT = -24602
085816 feet/sec YDOT = -7499
830149 meter/sec
ZDOT = -5179
607219 ZDOT = -1579
229346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13141321
08 X = -4005474
67
Y = -6289978
73 feet Y = -1917185
52 meter
Z = 16835301
25 Z = 5131399
82
XDOT = 4402
847499 XDOT = 1341
987918
YDOT = -23163
108464 feet/sec YDOT = -7060
115460 meter/sec
ZDOT = -5181
009741 ZDOT = -1579
171769
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 19152
32062115
00016717 00000-0 10270-3 0 9139
2 25544 51
6411 80
0469 0007468 359
2965
8174 15
51178250 12784
Satellite: ISS
Catalog Number: 25544
Epoch time: 19152
32062115 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 80
0469 deg
Eccentricity:
0007468
Arg of perigee: 359
2965 deg
Mean anomaly:
8174 deg
Mean motion: 15
51178250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1278
Checksum: 297
Coasting Arc #15 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2019/153/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4420138
95 A = 6787863
97 meter
Y = 1512428
97 meter E =
0012474
Z = -4933103
87 I = 51
99829
XDOT = 118
422290 Wp = 70
92914
YDOT = 7285
844607 meter/sec RA = 74
48259 deg
ZDOT = 2348
656616 TA = 221
93475
MA = 222
03034
Ha = 227
332 n
mi
Hp = 218
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14501768
20 X = 4426860
67
Y = 4962037
31 feet Y = 1561896
35 meter
Z = -16184723
98 Z = -4911615
61
XDOT = 388
524573 XDOT = 25
532449
YDOT = 23903
689655 feet/sec YDOT = 7286
649175 meter/sec
ZDOT = 7705
566327 ZDOT = 2349
007296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13335894
74 X = 4064780
72
Y = 7760039
94 feet Y = 2365260
17 meter
Z = -16087388
76 Z = -4903436
09
XDOT = -3845
010134 XDOT = -1171
959089
YDOT = 22523
684562 feet/sec YDOT = 6865
219054 meter/sec
ZDOT = 7706
360183 ZDOT = 2348
898584
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 19153
28699340
00016717 00000-0 10270-3 0 9142
2 25544 51
6408 75
2522 0007557 2
4964 357
6224 15
51148135 12936
Satellite: ISS
Catalog Number: 25544
Epoch time: 19153
28699340 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 75
2522 deg
Eccentricity:
0007557
Arg of perigee: 2
4964 deg
Mean anomaly: 357
6224 deg
Mean motion: 15
51148135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 312
Coasting Arc #16 (Orbit 1308)
---------------------------------------
Vector Time (GMT): 2019/154/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965074
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4578816
89 A = 6789130
60 meter
Y = -2022309
97 meter E =
0013987
Z = 4584807
24 I = 51
99189
XDOT = -26
867584 Wp = 38
28150
YDOT = -7007
756791 meter/sec RA = 69
54041 deg
ZDOT = -3102
141031 TA = 82
71080
MA = 82
55183
Ha = 227
369 n
mi
Hp = 218
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15022365
12 X = -4578133
28
Y = -6634875
24 feet Y = -2073510
43 meter
Z = 15042018
49 Z = 4562566
09
XDOT = -88
148243 XDOT = 66
565829
YDOT = -22991
328053 feet/sec YDOT = -7007
534320 meter/sec
ZDOT = -10177
628056 ZDOT = -3102
045748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13668273
63 X = -4166089
80
Y = -9267709
00 feet Y = -2824797
70 meter
Z = 14941325
56 Z = 4554116
03
XDOT = 3476
440602 XDOT = 1059
619095
YDOT = -21617
283916 feet/sec YDOT = -6588
948138 meter/sec
ZDOT = -10176
408773 ZDOT = -3101
769394
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 19154
31778900
00016717 00000-0 10270-3 0 9158
2 25544 51
6398 70
1364 0007578 5
3299 354
7931 15
51186845 13099
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
31778900 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 70
1364 deg
Eccentricity:
0007578
Arg of perigee: 5
3299 deg
Mean anomaly: 354
7931 deg
Mean motion: 15
51186845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1309
Checksum: 331
Coasting Arc #17 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2019/154/16:09:25
000
Vector Time (MET): N/A
Weight (LBS) : 945398
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2166260
88 A = 6797838
51 meter
Y = -6418614
52 meter E =
0007784
Z = -567153
20 I = 52
01852
XDOT = 4639
286666 Wp = 94
15715
YDOT = -1041
702912 meter/sec RA = 67
60273 deg
ZDOT = -6002
105339 TA = 91
91879
MA = 91
82964
Ha = 227
334 n
mi
Hp = 218
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7107155
11 X = -2091570
15
Y = -21058446
59 feet Y = -6442421
45 meter
Z = -1860738
84 Z = -577495
89
XDOT = 15220
756779 XDOT = 4679
745730
YDOT = -3417
660472 feet/sec YDOT = -989
595924 meter/sec
ZDOT = -19691
946651 ZDOT = -5979
471050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10462795
95 X = -3189060
21
Y = 19604225
25 feet Y = 5975367
86 meter
Z = -1906942
26 Z = -581236
00
XDOT = -11586
652601 XDOT = -3531
611713
YDOT = -8067
046532 feet/sec YDOT = -2458
835783 meter/sec
ZDOT = -19589
123073 ZDOT = -5970
764713
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 19154
70433761
00016717 00000-0 10270-3 0 9165
2 25544 51
6423 68
2191 0007601 5
1015 355
0213 15
51154314 13155
Satellite: ISS
Catalog Number: 25544
Epoch time: 19154
70433761 = yrday
fracday
Element set: 916
Inclination: 51
6423 deg
RA of node: 68
2191 deg
Eccentricity:
0007601
Arg of perigee: 5
1015 deg
Mean anomaly: 355
0213 deg
Mean motion: 15
51154314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 264
Coasting Arc #18 (Orbit 1325)
---------------------------------------
Vector Time (GMT): 2019/155/08:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 931350
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3049244
48 A = 6786414
60 meter
Y = 3074161
78 meter E =
0006941
Z = 5220747
57 I = 51
97075
XDOT = -4165
833085 Wp = 40
42659
YDOT = -6308
181926 meter/sec RA = 64
20297 deg
ZDOT = 1285
562544 TA = 37
30888
MA = 37
26069
Ha = 227
510 n
mi
Hp = 218
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10004082
93 X = -3108753
73
Y = 10085832
60 feet Y = 3039729
32 meter
Z = 17128436
92 Z = 5205791
36
XDOT = -13667
431381 XDOT = -4101
228187
YDOT = -20696
134928 feet/sec YDOT = -6354
406189 meter/sec
ZDOT = 4217
724882 ZDOT = 1265
482081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5576266
83 X = -1699646
13
Y = 13154593
08 feet Y = 4009519
97 meter
Z = 17060216
15 Z = 5199953
88
XDOT = -19520
635583 XDOT = -5949
889726
YDOT = -13609
697907 feet/sec YDOT = -4148
235922 meter/sec
ZDOT = 4127
331319 ZDOT = 1258
010586
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 19155
41300835
00016717 00000-0 10270-3 0 9170
2 25544 51
6414 64
7016 0007686 8
4007 351
7271 15
51196475 13265
Satellite: ISS
Catalog Number: 25544
Epoch time: 19155
41300835 = yrday
fracday
Element set: 917
Inclination: 51
6414 deg
RA of node: 64
7016 deg
Eccentricity:
0007686
Arg of perigee: 8
4007 deg
Mean anomaly: 351
7271 deg
Mean motion: 15
51196475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1326
Checksum: 299
Coasting Arc #19 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2019/156/08:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 931350
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3317352
32 A = 6786047
12 meter
Y = -2592576
47 meter E =
0018459
Z = -5336726
55 I = 51
95366
XDOT = 4213
921838 Wp = 62
43662
YDOT = 6368
941517 meter/sec RA = 59
25622 deg
ZDOT = -467
556210 TA = 203
07133
MA = 203
15432
Ha = 227
571 n
mi
Hp = 218
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10883701
82 X = 3372019
65
Y = -8505828
30 feet Y = -2555172
85 meter
Z = -17508945
38 Z = -5320479
73
XDOT = 13825
202882 XDOT = 4144
660467
YDOT = 20895
477419 feet/sec YDOT = 6415
677364 meter/sec
ZDOT = -1533
977066 ZDOT = -447
253505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6780549
87 X = 2066711
60
Y = -12141462
57 feet Y = -3700717
79 meter
Z = -17434915
50 Z = -5314162
25
XDOT = 20039
425603 XDOT = 6108
016924
YDOT = 13296
209931 feet/sec YDOT = 4052
684787 meter/sec
ZDOT = -1442
592240 ZDOT = -439
702115
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 19156
37937576
00016717 00000-0 10270-3 0 9185
2 25544 51
6413 59
9052 0007771 12
5494 347
5850 15
51172150 13418
Satellite: ISS
Catalog Number: 25544
Epoch time: 19156
37937576 = yrday
fracday
Element set: 918
Inclination: 51
6413 deg
RA of node: 59
9052 deg
Eccentricity:
0007771
Arg of perigee: 12
5494 deg
Mean anomaly: 347
5850 deg
Mean motion: 15
51172150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 317
Coasting Arc #20 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2019/157/08:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 931350
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3638313
22 A = 6785983
24 meter
Y = 2089393
30 meter E =
0009564
Z = 5329990
58 I = 51
93541
XDOT = -4226
964594 Wp = 29
02515
YDOT = -6385
949567 meter/sec RA = 54
30927 deg
ZDOT = -373
613443 TA = 64
57272
MA = 64
47377
Ha = 227
775 n
mi
Hp = 217
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11936723
17 X = -3687297
11
Y = 6854964
89 feet Y = 2048432
27 meter
Z = 17486845
74 Z = 5312198
44
XDOT = -13867
994074 XDOT = -4153
426123
YDOT = -20951
278108 feet/sec YDOT = -6432
807197 meter/sec
ZDOT = -1225
765890 ZDOT = -393
968992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8205678
32 X = -2501090
75
Y = 11178938
73 feet Y = 3407340
53 meter
Z = 17405856
77 Z = 5305305
14
XDOT = -20388
742279 XDOT = -6214
488647
YDOT = -12871
523290 feet/sec YDOT = -3923
240299 meter/sec
ZDOT = -1317
380654 ZDOT = -401
537623
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 19157
41016609
00016717 00000-0 10270-3 0 9197
2 25544 51
6410 54
7905 0007837 16
2042 343
9359 15
51185061 13574
Satellite: ISS
Catalog Number: 25544
Epoch time: 19157
41016609 = yrday
fracday
Element set: 919
Inclination: 51
6410 deg
RA of node: 54
7905 deg
Eccentricity:
0007837
Arg of perigee: 16
2042 deg
Mean anomaly: 343
9359 deg
Mean motion: 15
51185061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 305
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