[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 15th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
107/20:46:03
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
3
109/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 217
4
114/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
2
116/09:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
6
118/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 217
5
118/11:34:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
5
Coasting Arc #1 (Orbit 550)
---------------------------------------
Vector Time (GMT): 2019/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4504904
34 A = 6783274
33 meter
Y = -970680
27 meter E =
0012014
Z = -4988516
96 I = 51
34118
XDOT = 3630
615139 Wp = 80
36078
YDOT = -6428
139667 meter/sec RA = 312
16540 deg
ZDOT = -2030
057927 TA = 169
80268
MA = 169
77829
Ha = 223
344 n
mi
Hp = 217
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14779869
87 X = -4469483
71
Y = -3184646
57 feet Y = -1020859
49 meter
Z = -16366525
44 Z = -5010313
96
XDOT = 11911
466990 XDOT = 3712
087462
YDOT = -21089
697071 feet/sec YDOT = -6387
084159 meter/sec
ZDOT = -6660
295037 ZDOT = -2012
223565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14773616
65 X = -4502998
36
Y = 2663697
49 feet Y = 811895
00 meter
Z = -16464952
13 Z = -5018517
41
XDOT = 3180
520827 XDOT = 969
422748
YDOT = -22981
313413 feet/sec YDOT = -7004
704328 meter/sec
ZDOT = -6578
959301 ZDOT = -2005
266795
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 19105
51960560
00016717 00000-0 10270-3 0 9005
2 25544 51
6391 312
7326 0001421 200
2218 159
8878 15
52554164 5519
Satellite: ISS
Catalog Number: 25544
Epoch time: 19105
51960560 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 312
7326 deg
Eccentricity:
0001421
Arg of perigee: 200
2218 deg
Mean anomaly: 159
8878 deg
Mean motion: 15
52554164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 551
Checksum: 288
Coasting Arc #2 (Orbit 566)
---------------------------------------
Vector Time (GMT): 2019/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3850028
26 A = 6782174
08 meter
Y = 1884935
14 meter E =
0003470
Z = 5254014
11 I = 51
31601
XDOT = -4134
944038 Wp = 139
74709
YDOT = 6416
430593 meter/sec RA = 307
16139 deg
ZDOT = 725
162582 TA = 303
27760
MA = 303
31084
Ha = 223
255 n
mi
Hp = 217
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12631326
32 X = 3803143
14
Y = 6184170
42 feet Y = 1927727
08 meter
Z = 17237579
11 Z = 5272602
11
XDOT = -13566
089363 XDOT = -4209
909511
YDOT = 21051
281472 feet/sec YDOT = 6369
771648 meter/sec
ZDOT = 2379
142330 ZDOT = 704
894020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13943423
03 X = 4249955
34
Y = 691836
00 feet Y = 210871
61 meter
Z = 17321397
72 Z = 5279562
03
XDOT = -4028
479619 XDOT = -1227
880588
YDOT = 23701
407622 feet/sec YDOT = 7224
189043 meter/sec
ZDOT = 2286
823129 ZDOT = 697
023690
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 19106
54948450
00016717 00000-0 10270-3 0 9014
2 25544 51
6394 307
6103 0001380 201
3746 158
7348 15
52527373 5679
Satellite: ISS
Catalog Number: 25544
Epoch time: 19106
54948450 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 307
6103 deg
Eccentricity:
0001380
Arg of perigee: 201
3746 deg
Mean anomaly: 158
7348 deg
Mean motion: 15
52527373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 567
Checksum: 307
Coasting Arc #3 (Orbit 581)
---------------------------------------
Vector Time (GMT): 2019/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3198335
28 A = 6782069
45 meter
Y = -2848539
19 meter E =
0014311
Z = -5271085
45 I = 51
29458
XDOT = 4474
854726 Wp = 100
12094
YDOT = -6179
976831 meter/sec RA = 302
15352 deg
ZDOT = 623
488533 TA = 175
87561
MA = 175
86380
Ha = 223
341 n
mi
Hp = 217
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10493225
99 X = -3140640
26
Y = -9345601
01 feet Y = -2883983
05 meter
Z = -17293587
42 Z = -5286481
48
XDOT = 14681
281909 XDOT = 4540
599826
YDOT = -20275
514538 feet/sec YDOT = -6129
568218 meter/sec
ZDOT = 2045
566054 ZDOT = 645
385997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13314726
10 X = -4058328
52
Y = -4214839
65 feet Y = -1284683
13 meter
Z = -17362874
51 Z = -5292204
15
XDOT = 4655
153255 XDOT = 1418
890712
YDOT = -23556
457868 feet/sec YDOT = -7180
008358 meter/sec
ZDOT = 2145
204543 ZDOT = 653
858345
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 19107
51499308
00016717 00000-0 10270-3 0 9026
2 25544 51
6373 302
8072 0001383 201
4279 158
6815 15
52560650 5823
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
51499308 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 302
8072 deg
Eccentricity:
0001383
Arg of perigee: 201
4279 deg
Mean anomaly: 158
6815 deg
Mean motion: 15
52560650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 582
Checksum: 303
Coasting Arc #4 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:46:03
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1905911
08 A = 6792368
24 meter
Y = 6235475
06 meter E =
0014059
Z = 1877051
06 I = 51
32536
XDOT = -5242
081495 Wp = 119
17907
YDOT = 90
018805 meter/sec RA = 300
31828 deg
ZDOT = -5596
658854 TA = 40
06720
MA = 39
96359
Ha = 223
298 n
mi
Hp = 217
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6252989
10 X = -1984614
02
Y = 20457595
34 feet Y = 6213721
93 meter
Z = 6158304
00 Z = 1867601
13
XDOT = -17198
430102 XDOT = -5215
512852
YDOT = 295
337288 feet/sec YDOT = 31
546277 meter/sec
ZDOT = -18361
741646 ZDOT = -5622
058576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13981611
98 X = 4261595
33
Y = -16206787
59 feet Y = -4939828
86 meter
Z = 6114928
49 Z = 1863830
20
XDOT = 14573
295977 XDOT = 4441
940614
YDOT = 5569
829319 feet/sec YDOT = 1697
683976 meter/sec
ZDOT = -18476
557721 ZDOT = -5631
654793
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 19107
90119682
00016717 00000-0 10270-3 0 9034
2 25544 51
6400 300
8877 0001446 201
9114 158
1977 15
52579617 5881
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90119682 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 300
8877 deg
Eccentricity:
0001446
Arg of perigee: 201
9114 deg
Mean anomaly: 158
1977 deg
Mean motion: 15
52579617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 319
Coasting Arc #5 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2019/108/20:46:03
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2343879
87 A = 6793791
93 meter
Y = -6329711
40 meter E =
0009114
Z = -736382
78 I = 51
31287
XDOT = 4741
803120 Wp = 41
81453
YDOT = 1072
297697 meter/sec RA = 295
33145 deg
ZDOT = 5925
023999 TA = 310
19882
MA = 310
27856
Ha = 223
357 n
mi
Hp = 217
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7689894
57 X = 2418063
28
Y = -20766769
68 feet Y = -6303085
76 meter
Z = -2415953
99 Z = -724816
30
XDOT = 15557
096850 XDOT = 4700
679136
YDOT = 3518
037063 feet/sec YDOT = 1125
094359 meter/sec
ZDOT = 19439
055116 ZDOT = 5947
958214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15122435
15 X = -4609318
23
Y = 16185121
36 feet Y = 4933224
99 meter
Z = -2363014
39 Z = -720246
78
XDOT = -11693
555928 XDOT = -3564
195847
YDOT = -8096
651558 feet/sec YDOT = -2467
859395 meter/sec
ZDOT = 19542
600771 ZDOT = 5956
584715
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 19108
86670624
00016717 00000-0 10270-3 0 9049
2 25544 51
6391 296
0859 0001405 207
5952 152
5126 15
52517857 6033
Satellite: ISS
Catalog Number: 25544
Epoch time: 19108
86670624 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 296
0859 deg
Eccentricity:
0001405
Arg of perigee: 207
5952 deg
Mean anomaly: 152
5126 deg
Mean motion: 15
52517857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 316
Coasting Arc #6 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2019/109/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4333691
84 A = 6782366
27 meter
Y = 440841
87 meter E =
0003964
Z = 5196956
16 I = 51
26900
XDOT = -2082
465100 Wp = 141
63407
YDOT = 7294
762645 meter/sec RA = 292
69792 deg
ZDOT = 1114
241409 TA = 297
60981
MA = 297
65006
Ha = 223
105 n
mi
Hp = 217
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14218149
07 X = 4303195
84
Y = 1446331
59 feet Y = 489134
07 meter
Z = 17050381
11 Z = 5217933
81
XDOT = -6832
234580 XDOT = -2169
294880
YDOT = 23932
948312 feet/sec YDOT = 7270
989639 meter/sec
ZDOT = 3655
647666 ZDOT = 1103
914059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13554781
06 X = 4131497
27
Y = 4156312
53 feet Y = 1266844
06 meter
Z = 17145148
31 Z = 5225841
21
XDOT = -11066
662078 XDOT = -3373
118601
YDOT = 21159
682331 feet/sec YDOT = 6449
471174 meter/sec
ZDOT = 3608
213993 ZDOT = 1099
783625
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 19109
44601107
00016717 00000-0 10270-3 0 9055
2 25544 51
6404 293
2062 0001266 216
1146 143
9920 15
52543857 6124
Satellite: ISS
Catalog Number: 25544
Epoch time: 19109
44601107 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 293
2062 deg
Eccentricity:
0001266
Arg of perigee: 216
1146 deg
Mean anomaly: 143
9920 deg
Mean motion: 15
52543857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 283
Coasting Arc #7 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2019/110/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3965631
15 A = 6781905
18 meter
Y = -1543649
90 meter E =
0014021
Z = -5292824
81 I = 51
25513
XDOT = 2502
426032 Wp = 95
63126
YDOT = -7231
409485 meter/sec RA = 287
68636 deg
ZDOT = 233
287989 TA = 176
61262
MA = 176
60312
Ha = 223
154 n
mi
Hp = 217
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13010600
89 X = -3922364
85
Y = -5064468
17 feet Y = -1587754
67 meter
Z = -17364910
80 Z = -5311983
53
XDOT = 8210
059160 XDOT = 2581
970520
YDOT = -23725
096734 feet/sec YDOT = -7202
980834 meter/sec
ZDOT = 765
380540 ZDOT = 245
637543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11792934
20 X = -3594486
34
Y = -7269252
45 feet Y = -2215668
15 meter
Z = -17451342
99 Z = -5319169
34
XDOT = 11747
001508 XDOT = 3580
486060
YDOT = -21036
820011 feet/sec YDOT = -6412
022739 meter/sec
ZDOT = 821
937330 ZDOT = 250
526498
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 19110
41151650
00016717 00000-0 10270-3 0 9068
2 25544 51
6397 288
4025 0001259 223
8226 136
2826 15
52575113 6272
Satellite: ISS
Catalog Number: 25544
Epoch time: 19110
41151650 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 288
4025 deg
Eccentricity:
0001259
Arg of perigee: 223
8226 deg
Mean anomaly: 136
2826 deg
Mean motion: 15
52575113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 294
Coasting Arc #8 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2019/111/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3605210
14 A = 6782734
46 meter
Y = 2635514
73 meter E =
0003639
Z = 5102878
71 I = 51
24860
XDOT = -2851
859060 Wp = 57
74342
YDOT = 6942
867316 meter/sec RA = 282
67690 deg
ZDOT = -1568
239274 TA = 47
47561
MA = 47
44488
Ha = 223
008 n
mi
Hp = 217
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11828117
26 X = 3550683
75
Y = 8646701
86 feet Y = 2675525
91 meter
Z = 16741728
06 Z = 5120259
29
XDOT = -9356
492980 XDOT = -2921
666456
YDOT = 22778
436076 feet/sec YDOT = 6910
585491 meter/sec
ZDOT = -5145
141976 ZDOT = -1582
262424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10179433
41 X = 3102691
30
Y = 10412563
74 feet Y = 3173749
43 meter
Z = 16820015
49 Z = 5126740
72
XDOT = -12090
301410 XDOT = -3685
123870
YDOT = 20248
783364 feet/sec YDOT = 6171
829169 meter/sec
ZDOT = -5209
225149 ZDOT = -1587
771825
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 19111
44138945
00016717 00000-0 10270-3 0 9075
2 25544 51
6395 283
2810 0001285 226
8339 133
2705 15
52566417 6430
Satellite: ISS
Catalog Number: 25544
Epoch time: 19111
44138945 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 283
2810 deg
Eccentricity:
0001285
Arg of perigee: 226
8339 deg
Mean anomaly: 133
2705 deg
Mean motion: 15
52566417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 309
Coasting Arc #9 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2019/112/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3287668
57 A = 6784566
60 meter
Y = -3674618
42 meter E =
0010056
Z = -4670258
46 I = 51
24762
XDOT = 3141
492981 Wp = 116
02579
YDOT = -6389
909708 meter/sec RA = 277
66825 deg
ZDOT = 2816
594378 TA = 182
11475
MA = 182
11901
Ha = 223
095 n
mi
Hp = 217
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10786314
20 X = -3223647
73
Y = -12055834
70 feet Y = -3711025
42 meter
Z = -15322370
28 Z = -4686073
50
XDOT = 10306
735501 XDOT = 3199
031629
YDOT = -20964
270696 feet/sec YDOT = -6354
457644 meter/sec
ZDOT = 9240
795205 ZDOT = 2831
994494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8847369
11 X = -2696678
10
Y = -13462075
40 feet Y = -4103240
58 meter
Z = -15393483
72 Z = -4691933
84
XDOT = 12158
479948 XDOT = 3705
904688
YDOT = -18635
989692 feet/sec YDOT = -5680
249658 meter/sec
ZDOT = 9311
039156 ZDOT = 2838
004735
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 19112
40689544
00016717 00000-0 10270-3 0 9089
2 25544 51
6386 278
4784 0001362 230
1476 129
9556 15
52569423 6584
Satellite: ISS
Catalog Number: 25544
Epoch time: 19112
40689544 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 278
4784 deg
Eccentricity:
0001362
Arg of perigee: 230
1476 deg
Mean anomaly: 129
9556 deg
Mean motion: 15
52569423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 337
Coasting Arc #10 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2019/113/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2983070
84 A = 6787032
34 meter
Y = 4611376
53 meter E =
0009550
Z = 3980384
66 I = 51
25369
XDOT = -3423
551401 Wp = 81
41670
YDOT = 5620
391236 meter/sec RA = 272
66396 deg
ZDOT = -3936
086209 TA = 49
78282
MA = 49
69930
Ha = 222
905 n
mi
Hp = 217
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9786977
81 X = 2911948
68
Y = 15129188
10 feet Y = 4644337
55 meter
Z = 13059004
78 Z = 3994702
84
XDOT = -11232
124019 XDOT = -3467
026222
YDOT = 18439
603794 feet/sec YDOT = 5581
863707 meter/sec
ZDOT = -12913
668664 ZDOT = -3952
822184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7713764
06 X = 2351155
29
Y = 16232452
54 feet Y = 4947651
54 meter
Z = 13123269
46 Z = 3999972
53
XDOT = -12198
001723 XDOT = -3717
950925
YDOT = 16323
477329 feet/sec YDOT = 4975
395890 meter/sec
ZDOT = -12989
868060 ZDOT = -3959
311785
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 19113
43676570
00016717 00000-0 10270-3 0 9099
2 25544 51
6396 273
3560 0001397 241
5443 118
5568 15
52588670 6749
Satellite: ISS
Catalog Number: 25544
Epoch time: 19113
43676570 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 273
3560 deg
Eccentricity:
0001397
Arg of perigee: 241
5443 deg
Mean anomaly: 118
5568 deg
Mean motion: 15
52588670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 332
Coasting Arc #11 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2019/114/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2716035
60 A = 6789742
32 meter
Y = -5392155
85 meter E =
0003343
Z = -3108631
50 I = 51
26020
XDOT = 3695
983423 Wp = 83
59248
YDOT = -4648
646558 meter/sec RA = 267
66436 deg
ZDOT = 4839
086720 TA = 240
47134
MA = 240
50467
Ha = 223
077 n
mi
Hp = 217
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8910877
96 X = -2640436
99
Y = -17690800
03 feet Y = -5422105
67 meter
Z = -10198922
24 Z = -3121641
64
XDOT = 12125
929866 XDOT = 3724
185429
YDOT = -15251
465085 feet/sec YDOT = -4607
157949 meter/sec
ZDOT = 15876
268766 ZDOT = 4857
108922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6860762
45 X = -2091160
39
Y = -18550086
79 feet Y = -5654066
45 meter
Z = -10257211
39 Z = -3126398
03
XDOT = 12257
658721 XDOT = 3736
134378
YDOT = -13348
748426 feet/sec YDOT = -4068
698520 meter/sec
ZDOT = 15958
182357 ZDOT = 4864
053982
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 19114
40227001
00016717 00000-0 10270-3 0 9100
2 25544 51
6377 268
5536 0001291 235
2444 124
8587 15
52564658 6898
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
40227001 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 268
5536 deg
Eccentricity:
0001291
Arg of perigee: 235
2444 deg
Mean anomaly: 124
8587 deg
Mean motion: 15
52564658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 312
Coasting Arc #12 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2019/114/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4035163
10 A = 6782654
00 meter
Y = 1889192
49 meter E =
0012730
Z = -5125356
84 I = 51
23650
XDOT = -1535
397810 Wp = 81
80365
YDOT = -7348
972015 meter/sec RA = 267
43993 deg
ZDOT = -1501
434162 TA = 173
63813
MA = 173
62195
Ha = 223
176 n
mi
Hp = 217
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13238724
07 X = -4031092
35
Y = 6198138
10 feet Y = 1844091
40 meter
Z = -16815475
20 Z = -5144948
36
XDOT = -5037
394390 XDOT = -1445
812210
YDOT = -24110
800574 feet/sec YDOT = -7365
640956 meter/sec
ZDOT = -4925
965100 ZDOT = -1508
675252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11466821
20 X = -3495087
10
Y = 8899461
33 feet Y = 2712555
81 meter
Z = -16904216
54 Z = -5152405
20
XDOT = -9471
776512 XDOT = -2886
997481
YDOT = -21612
884994 feet/sec YDOT = -6587
607346 meter/sec
ZDOT = -4957
988615 ZDOT = -1511
194930
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 19114
46663809
00016717 00000-0 10270-3 0 9117
2 25544 51
6376 268
2326 0001205 221
7639 138
3421 15
52570205 6906
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
46663809 = yrday
fracday
Element set: 911
Inclination: 51
6376 deg
RA of node: 268
2326 deg
Eccentricity:
0001205
Arg of perigee: 221
7639 deg
Mean anomaly: 138
3421 deg
Mean motion: 15
52570205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 297
Coasting Arc #13 (Orbit 705)
---------------------------------------
Vector Time (GMT): 2019/115/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4181854
77 A = 6782039
32 meter
Y = -748657
74 meter E =
0001968
Z = 5285227
13 I = 51
23553
XDOT = 1143
414951 Wp = 127
58040
YDOT = 7579
931928 meter/sec RA = 262
42874 deg
ZDOT = 167
771890 TA = 320
80442
MA = 320
81867
Ha = 223
078 n
mi
Hp = 217
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13719995
96 X = 4164242
84
Y = -2456226
19 feet Y = -701991
94 meter
Z = 17339984
01 Z = 5305498
31
XDOT = 3751
361389 XDOT = 1057
754070
YDOT = 24868
543070 feet/sec YDOT = 7592
239429 meter/sec
ZDOT = 550
432710 ZDOT = 173
118355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12651825
14 X = 3856276
30
Y = -5569004
49 feet Y = -1697432
57 meter
Z = 17431692
15 Z = 5313179
77
XDOT = 9054
648865 XDOT = 2759
856974
YDOT = 22379
453744 feet/sec YDOT = 6821
257501 meter/sec
ZDOT = 573
887781 ZDOT = 174
920996
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 19115
49650913
00016717 00000-0 10270-3 0 9124
2 25544 51
6365 263
1104 0001213 225
9745 134
1307 15
52522020 7062
Satellite: ISS
Catalog Number: 25544
Epoch time: 19115
49650913 = yrday
fracday
Element set: 912
Inclination: 51
6365 deg
RA of node: 263
1104 deg
Eccentricity:
0001213
Arg of perigee: 225
9745 deg
Mean anomaly: 134
1307 deg
Mean motion: 15
52522020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 706
Checksum: 270
Coasting Arc #14 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2019/116/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4069506
71 A = 6782048
57 meter
Y = -1236663
50 meter E =
0001920
Z = 5281407
10 I = 51
24124
XDOT = 1874
387528 Wp = 131
20572
YDOT = 7428
957292 meter/sec RA = 257
60428 deg
ZDOT = 293
927278 TA = 315
96882
MA = 315
98412
Ha = 223
007 n
mi
Hp = 217
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13351399
97 X = 4057378
77
Y = -4057294
94 feet Y = -1191223
34 meter
Z = 17327451
12 Z = 5301145
82
XDOT = 6149
565380 XDOT = 1789
747767
YDOT = 24373
219461 feet/sec YDOT = 7449
444749 meter/sec
ZDOT = 964
328340 ZDOT = 302
826946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13087021
15 X = 3988924
05
Y = -4510764
73 feet Y = -1374881
09 meter
Z = 17416801
22 Z = 5308641
01
XDOT = 6652
078639 XDOT = 2027
553569
YDOT = 23192
286810 feet/sec YDOT = 7069
009020 meter/sec
ZDOT = 1003
879799 ZDOT = 305
982563
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 19116
46201012
00016717 00000-0 10270-3 0 9135
2 25544 51
6369 258
3091 0001212 237
9016 122
2018 15
52526036 7215
Satellite: ISS
Catalog Number: 25544
Epoch time: 19116
46201012 = yrday
fracday
Element set: 913
Inclination: 51
6369 deg
RA of node: 258
3091 deg
Eccentricity:
0001212
Arg of perigee: 237
9016 deg
Mean anomaly: 122
2018 deg
Mean motion: 15
52526036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 264
Coasting Arc #15 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2019/117/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4351348
95 A = 6782245
94 meter
Y = 106084
95 meter E =
0013480
Z = -5213198
17 I = 51
25144
XDOT = -1446
104527 Wp = 101
45798
YDOT = -7443
668304 meter/sec RA = 252
59344 deg
ZDOT = 1055
260209 TA = 178
72341
MA = 178
71996
Ha = 223
114 n
mi
Hp = 217
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14276079
24 X = -4326888
95
Y = 348047
75 feet Y = 57561
93 meter
Z = -17103668
53 Z = -5234276
02
XDOT = -4744
437426 XDOT = -1367
885712
YDOT = -24421
483938 feet/sec YDOT = -7459
402317 meter/sec
ZDOT = 3462
139794 ZDOT = 1048
425478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14124248
80 X = -4305071
04
Y = 1078845
37 feet Y = 328832
07 meter
Z = -17198975
01 Z = -5242247
58
XDOT = -5945
546865 XDOT = -1812
202684
YDOT = -23112
036207 feet/sec YDOT = -7044
548636 meter/sec
ZDOT = 3431
904480 ZDOT = 1046
044485
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 19117
42750897
00016717 00000-0 10270-3 0 9143
2 25544 51
6377 253
5071 0001134 235
3751 124
7294 15
52575559 7363
Satellite: ISS
Catalog Number: 25544
Epoch time: 19117
42750897 = yrday
fracday
Element set: 914
Inclination: 51
6377 deg
RA of node: 253
5071 deg
Eccentricity:
0001134
Arg of perigee: 235
3751 deg
Mean anomaly: 124
7294 deg
Mean motion: 15
52575559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 320
Coasting Arc #16 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2019/118/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4624512
75 A = 6783820
67 meter
Y = 985301
74 meter E =
0005629
Z = 4861338
95 I = 51
26603
XDOT = 940
270106 Wp = 59
50534
YDOT = 7236
076410 meter/sec RA = 247
58490 deg
ZDOT = -2356
228109 TA = 53
71957
MA = 53
66759
Ha = 223
011 n
mi
Hp = 217
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15172285
92 X = 4589537
38
Y = 3232617
27 feet Y = 1036820
74 meter
Z = 15949274
77 Z = 4883718
20
XDOT = 3084
875675 XDOT = 870
729634
YDOT = 23740
408168 feet/sec YDOT = 7246
202335 meter/sec
ZDOT = -7730
407182 ZDOT = -2351
829543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15252041
76 X = 4648822
33
Y = 2188166
56 feet Y = 666953
17 meter
Z = 16050376
62 Z = 4892154
79
XDOT = 4924
179339 XDOT = 1500
889863
YDOT = 22355
212040 feet/sec YDOT = 6813
868630 meter/sec
ZDOT = -7711
148365 ZDOT = -2350
358022
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 19118
45737554
00016717 00000-0 10270-3 0 9153
2 25544 51
6364 248
3847 0001151 237
0016 123
1025 15
52536058 7528
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
45737554 = yrday
fracday
Element set: 915
Inclination: 51
6364 deg
RA of node: 248
3847 deg
Eccentricity:
0001151
Arg of perigee: 237
0016 deg
Mean anomaly: 123
1025 deg
Mean motion: 15
52536058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 295
Coasting Arc #17 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2019/118/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2218750
89 A = 6793720
90 meter
Y = -6394658
66 meter E =
0011675
Z = 513188
50 I = 51
30217
XDOT = 4691
191283 Wp = 50
16097
YDOT = -1143
173016 meter/sec RA = 247
38265 deg
ZDOT = 5954
452614 TA = 315
39791
MA = 315
49180
Ha = 223
064 n
mi
Hp = 217
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7279366
43 X = -2149571
88
Y = -20979851
25 feet Y = -6419083
48 meter
Z = 1683689
31 Z = 502578
66
XDOT = 15391
047517 XDOT = 4674
702414
YDOT = -3750
567639 feet/sec YDOT = -1090
805004 meter/sec
ZDOT = 19535
605689 ZDOT = 5977
200676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14099748
36 X = -4297603
30
Y = -17160939
74 feet Y = -5230654
43 meter
Z = 1636272
34 Z = 498735
81
XDOT = 11768
326240 XDOT = 3586
985838
YDOT = -7769
829326 feet/sec YDOT = -2368
243979 meter/sec
ZDOT = 19638
560206 ZDOT = 5985
833151
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 19118
52174085
00016717 00000-0 10270-3 0 9166
2 25544 51
6385 248
0645 0001268 234
4474 125
6559 15
52583363 7533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
52174085 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 248
0645 deg
Eccentricity:
0001268
Arg of perigee: 234
4474 deg
Mean anomaly: 125
6559 deg
Mean motion: 15
52583363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 323
Coasting Arc #18 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2019/118/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4532029
11 A = 6788870
17 meter
Y = 3710351
91 meter E =
0011266
Z = 3422152
53 I = 51
28590
XDOT = -1450
964139 Wp = 93
30560
YDOT = 5990
983181 meter/sec RA = 247
23269 deg
ZDOT = -4561
581259 TA = 46
41365
MA = 46
32019
Ha = 223
013 n
mi
Hp = 217
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14868861
90 X = 4473579
11
Y = 12173070
57 feet Y = 3760705
43 meter
Z = 11227534
55 Z = 3444025
51
XDOT = -4760
381032 XDOT = -1495
691494
YDOT = 19655
456629 feet/sec YDOT = 5974
507379 meter/sec
ZDOT = -14965
817778 ZDOT = -4568
738175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18833988
98 X = 5740599
84
Y = 3510597
43 feet Y = 1070030
10 meter
Z = 11326111
34 Z = 3452198
74
XDOT = 5672
749474 XDOT = 1729
054040
YDOT = 18086
094113 feet/sec YDOT = 5512
641486 meter/sec
ZDOT = -14998
697722 ZDOT = -4571
603066
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 19118
52174180
00016717 00000-0 10270-3 0 9173
2 25544 51
6383 248
0645 0001317 234
6294 125
4735 15
52552037 7536
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
52174180 = yrday
fracday
Element set: 917
Inclination: 51
6383 deg
RA of node: 248
0645 deg
Eccentricity:
0001317
Arg of perigee: 234
6294 deg
Mean anomaly: 125
4735 deg
Mean motion: 15
52552037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 303
Coasting Arc #19 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2019/119/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4536904
52 A = 6791288
57 meter
Y = -4424082
27 meter E =
0004149
Z = -2439903
85 I = 51
30919
XDOT = 2121
726841 Wp = 43
60699
YDOT = -5099
845512 meter/sec RA = 242
23956 deg
ZDOT = 5310
239785 TA = 288
98324
MA = 289
02819
Ha = 223
005 n
mi
Hp = 217
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14884857
36 X = -4475244
23
Y = -14514705
61 feet Y = -4474472
38 meter
Z = -8004933
90 Z = -2461792
70
XDOT = 6961
046065 XDOT = 2152
802768
YDOT = -16731
776615 feet/sec YDOT = -5075
945045 meter/sec
ZDOT = 17422
046539 ZDOT = 5320
621933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20090606
91 X = -6123616
99
Y = -5197578
39 feet Y = -1584221
89 meter
Z = -8103537
32 Z = -2469958
18
XDOT = -2779
289310 XDOT = -847
127382
YDOT = -16451
279529 feet/sec YDOT = -5014
350000 meter/sec
ZDOT = 17469
422951 ZDOT = 5324
680116
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 19119
48723930
00016717 00000-0 10270-3 0 9183
2 25544 51
6395 243
2629 0001316 244
7669 115
3347 15
52566552 7685
Satellite: ISS
Catalog Number: 25544
Epoch time: 19119
48723930 = yrday
fracday
Element set: 918
Inclination: 51
6395 deg
RA of node: 243
2629 deg
Eccentricity:
0001316
Arg of perigee: 244
7669 deg
Mean anomaly: 115
3347 deg
Mean motion: 15
52566552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 332
Coasting Arc #20 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2019/120/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4435726
67 A = 6793104
21 meter
Y = 4967834
82 meter E =
0013038
Z = 1303792
31 I = 51
33235
XDOT = -2880
560823 Wp = 125
12174
YDOT = 4103
489317 meter/sec RA = 237
25156 deg
ZDOT = -5801
491302 TA = 40
63382
MA = 40
53660
Ha = 222
982 n
mi
Hp = 217
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14552909
01 X = 4373512
11
Y = 16298670
68 feet Y = 5017090
39 meter
Z = 4277533
81 Z = 1325188
34
XDOT = -9450
658867 XDOT = -2898
052500
YDOT = 13462
891459 feet/sec YDOT = 4071
178943 meter/sec
ZDOT = -19033
764113 ZDOT = -5815
526655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20828615
00 X = 6348561
85
Y = 6539808
51 feet Y = 1993333
63 meter
Z = 4373879
74 Z = 1333158
55
XDOT = -619
751377 XDOT = -188
900220
YDOT = 14819
107646 feet/sec YDOT = 4516
864010 meter/sec
ZDOT = -19097
570632 ZDOT = -5820
939529
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 19120
51710197
00016717 00000-0 10270-3 0 9191
2 25544 51
6401 238
1407 0001314 247
5168 112
5845 15
52573309 7830
Satellite: ISS
Catalog Number: 25544
Epoch time: 19120
51710197 = yrday
fracday
Element set: 919
Inclination: 51
6401 deg
RA of node: 238
1407 deg
Eccentricity:
0001314
Arg of perigee: 247
5168 deg
Mean anomaly: 112
5845 deg
Mean motion: 15
52573309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 295
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