[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 8th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
010/09:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
3
016/05:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
2
018/18:04:49
685 2
7 2
9 2
9
N/A 0
7 0
0 220
9
000/00:07:35
370 -0
6 -0
0 217
7
020/01:03:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 217
7
Coasting Arc #1 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2019/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4063778
34 A = 6778543
26 meter
Y = -992253
85 meter E =
0012196
Z = -5344310
40 I = 51
99840
XDOT = 1538
917868 Wp = 91
89651
YDOT = 7499
491326 meter/sec RA = 79
70807 deg
ZDOT = -223
043941 TA = 175
99043
MA = 175
98065
Ha = 220
703 n
mi
Hp = 216
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13332606
11 X = 4100531
26
Y = -3255426
02 feet Y = -946603
82 meter
Z = -17533826
79 Z = -5324481
24
XDOT = 5048
943137 XDOT = 1456
025482
YDOT = 24604
630334 feet/sec YDOT = 7516
237119 meter/sec
ZDOT = -731
771461 ZDOT = -215
769143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6813097
06 X = 2076631
99
Y = 12044651
73 feet Y = 3671209
85 meter
Z = -17444177
80 Z = -5316985
39
XDOT = -21403
886185 XDOT = -6523
904509
YDOT = 11097
536579 feet/sec YDOT = 3382
529149 meter/sec
ZDOT = -699
864534 ZDOT = -213
318710
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 19007
51645976
00016717 00000-0 10270-3 0 9007
2 25544 51
6412 80
4578 0002789 252
3091 107
7757 15
53725750 30288
Satellite: ISS
Catalog Number: 25544
Epoch time: 19007
51645976 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 80
4578 deg
Eccentricity:
0002789
Arg of perigee: 252
3091 deg
Mean anomaly: 107
7757 deg
Mean motion: 15
53725750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 319
Coasting Arc #2 (Orbit 3043)
---------------------------------------
Vector Time (GMT): 2019/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4351910
49 A = 6779195
85 meter
Y = -636280
02 meter E =
0002502
Z = 5158232
81 I = 51
99404
XDOT = -768
345055 Wp = 30
55291
YDOT = -7467
257158 meter/sec RA = 74
73733 deg
ZDOT = -1566
913708 TA = 74
49073
MA = 74
46311
Ha = 220
745 n
mi
Hp = 216
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14277921
56 X = -4369527
38
Y = -2087532
88 feet Y = -685045
05 meter
Z = 16923335
98 Z = 5137050
38
XDOT = -2520
817110 XDOT = -677
175921
YDOT = -24498
875190 feet/sec YDOT = -7475
339436 meter/sec
ZDOT = -5140
793006 ZDOT = -1570
425181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2179276
91 X = -664243
60
Y = -14376813
38 feet Y = -4382052
72 meter
Z = 16827778
45 Z = 5129106
87
XDOT = 21675
258154 XDOT = 6606
618685
YDOT = -9329
626522 feet/sec YDOT = -2843
670164 meter/sec
ZDOT = -5155
703757 ZDOT = -1571
458505
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 19008
54554586
00016717 00000-0 10270-3 0 9018
2 25544 51
6411 75
3312 0002783 256
7006 103
3836 15
53774800 30442
Satellite: ISS
Catalog Number: 25544
Epoch time: 19008
54554586 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 75
3312 deg
Eccentricity:
0002783
Arg of perigee: 256
7006 deg
Mean anomaly: 103
3836 deg
Mean motion: 15
53774800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3044
Checksum: 294
Coasting Arc #3 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2019/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4568879
55 A = 6781839
04 meter
Y = 2166490
16 meter E =
0007449
Z = -4526976
32 I = 51
99186
XDOT = -113
762986 Wp = 120
34621
YDOT = 6953
405935 meter/sec RA = 69
77019 deg
ZDOT = 3213
169875 TA = 181
81520
MA = 181
81791
Ha = 220
671 n
mi
Hp = 216
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14989762
30 X = 4566302
82
Y = 7107907
37 feet Y = 2217568
46 meter
Z = -14852284
51 Z = -4504788
92
XDOT = -373
238143 XDOT = -207
116984
YDOT = 22813
011599 feet/sec YDOT = 6951
611565 meter/sec
ZDOT = 10541
895915 ZDOT = 3212
391004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2138486
53 X = -651810
69
Y = 16540849
95 feet Y = 5041651
07 meter
Z = -14752384
01 Z = -4496526
65
XDOT = -20644
916717 XDOT = -6292
570615
YDOT = 6728
254013 feet/sec YDOT = 2050
771823 meter/sec
ZDOT = 10537
492209 ZDOT = 3211
827625
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 19009
51031552
00016717 00000-0 10270-3 0 9020
2 25544 51
6401 70
5248 0002559 259
9208 100
1656 15
53761331 30592
Satellite: ISS
Catalog Number: 25544
Epoch time: 19009
51031552 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 70
5248 deg
Eccentricity:
0002559
Arg of perigee: 259
9208 deg
Mean anomaly: 100
1656 deg
Mean motion: 15
53761331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 286
Coasting Arc #4 (Orbit 3072)
---------------------------------------
Vector Time (GMT): 2019/010/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4652323
57 A = 6780659
40 meter
Y = 1104698
14 meter E =
0009024
Z = -4816210
70 I = 51
97857
XDOT = 1020
585536 Wp = 116
02267
YDOT = 7125
448360 meter/sec RA = 65
31324 deg
ZDOT = 2620
177588 TA = 179
71165
MA = 179
71113
Ha = 220
606 n
mi
Hp = 216
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15263528
77 X = 4663018
83
Y = 3624337
71 feet Y = 1156783
71 meter
Z = -15801216
22 Z = -4793585
81
XDOT = 3348
377742 XDOT = 928
103771
YDOT = 23377
455249 feet/sec YDOT = 7136
344020 meter/sec
ZDOT = 8596
383163 ZDOT = 2624
910888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8079213
10 X = -2462544
15
Y = 13566532
47 feet Y = 4135079
10 meter
Z = -15699206
37 Z = -4785118
10
XDOT = -22295
734635 XDOT = -6795
739917
YDOT = -3306
072325 feet/sec YDOT = -1007
690845 meter/sec
ZDOT = 8616
837495 ZDOT = 2626
412068
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 19010
41076376
00016717 00000-0 10270-3 0 9035
2 25544 51
6417 66
0374 0002646 261
1351 98
9502 15
53777853 30736
Satellite: ISS
Catalog Number: 25544
Epoch time: 19010
41076376 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 66
0374 deg
Eccentricity:
0002646
Arg of perigee: 261
1351 deg
Mean anomaly: 98
9502 deg
Mean motion: 15
53777853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3073
Checksum: 305
Coasting Arc #5 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2019/011/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4942485
45 A = 6784026
47 meter
Y = -2506569
41 meter E =
0008687
Z = 3907010
07 I = 51
97482
XDOT = 20
374774 Wp = 79
16747
YDOT = -6470
835885 meter/sec RA = 60
34905 deg
ZDOT = -4116
306404 TA = 53
82269
MA = 53
74236
Ha = 220
737 n
mi
Hp = 216
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16215503
44 X = -4933066
75
Y = -8223652
92 feet Y = -2561787
22 meter
Z = 12818274
51 Z = 3883024
48
XDOT = 66
846372 XDOT = 112
726387
YDOT = -21229
776524 feet/sec YDOT = -6470
091508 meter/sec
ZDOT = -13504
942271 ZDOT = -4115
983386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12519322
11 X = 3815889
38
Y = -13288862
46 feet Y = -4050445
28 meter
Z = 12710306
42 Z = 3874101
40
XDOT = 19340
254041 XDOT = 5894
909432
YDOT = 5275
983932 feet/sec YDOT = 1608
119902 meter/sec
ZDOT = -13502
643506 ZDOT = -4115
605741
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 19011
43984628
00016717 00000-0 10270-3 0 9047
2 25544 51
6417 60
9103 0002597 268
2116 91
8739 15
53763414 30890
Satellite: ISS
Catalog Number: 25544
Epoch time: 19011
43984628 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 60
9103 deg
Eccentricity:
0002597
Arg of perigee: 268
2116 deg
Mean anomaly: 91
8739 deg
Mean motion: 15
53763414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 321
Coasting Arc #6 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2019/012/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5057122
55 A = 6787525
82 meter
Y = 3655718
67 meter E =
0003332
Z = -2667039
86 I = 51
96807
XDOT = -1197
842187 Wp = 22
70410
YDOT = 5470
938901 meter/sec RA = 55
39308 deg
ZDOT = 5232
899327 TA = 307
36489
MA = 307
39524
Ha = 220
649 n
mi
Hp = 216
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16591609
43 X = 5028822
26
Y = 11993827
66 feet Y = 3712112
78 meter
Z = -8750130
78 Z = -2642543
19
XDOT = -3929
928436 XDOT = -1284
348932
YDOT = 17949
274610 feet/sec YDOT = 5457
059949 meter/sec
ZDOT = 17168
304879 ZDOT = 5226
870791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16015025
22 X = -4881379
69
Y = 12828380
28 feet Y = 3910090
31 meter
Z = -8640012
76 Z = -2633475
89
XDOT = -15275
550381 XDOT = -4655
987756
YDOT = -7537
472005 feet/sec YDOT = -2297
421467 meter/sec
ZDOT = 17140
369567 ZDOT = 5224
384644
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 19012
40461053
00016717 00000-0 10270-3 0 9058
2 25544 51
6409 56
1042 0002736 271
8670 88
2169 15
53736965 31046
Satellite: ISS
Catalog Number: 25544
Epoch time: 19012
40461053 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 56
1042 deg
Eccentricity:
0002736
Arg of perigee: 271
8670 deg
Mean anomaly: 88
2169 deg
Mean motion: 15
53736965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 298
Coasting Arc #7 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2019/013/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4919827
30 A = 6789853
48 meter
Y = -4522724
69 meter E =
0011382
Z = 1166650
56 I = 51
95657
XDOT = 2485
265098 Wp = 128
15233
YDOT = -4231
797933 meter/sec RA = 50
44339 deg
ZDOT = -5892
736247 TA = 39
23448
MA = 39
15204
Ha = 220
645 n
mi
Hp = 216
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16141165
68 X = -4874554
16
Y = -14838335
61 feet Y = -4577488
52 meter
Z = 3827593
72 Z = 1142861
96
XDOT = 8153
756882 XDOT = 2561
024903
YDOT = -13883
851485 feet/sec YDOT = -4203
582207 meter/sec
ZDOT = -19333
124171 ZDOT = -5880
479989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18424144
95 X = 5615679
38
Y = -11919331
32 feet Y = -3633012
19 meter
Z = 3720797
06 Z = 1134098
94
XDOT = 10489
407808 XDOT = 3197
171500
YDOT = 10162
394236 feet/sec YDOT = 3097
497763 meter/sec
ZDOT = -19277
230702 ZDOT = -5875
699918
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 19013
43369127
00016717 00000-0 10270-3 0 9062
2 25544 51
6411 50
9773 0002610 276
4387 83
6468 15
53761259 31202
Satellite: ISS
Catalog Number: 25544
Epoch time: 19013
43369127 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 50
9773 deg
Eccentricity:
0002610
Arg of perigee: 276
4387 deg
Mean anomaly: 83
6468 deg
Mean motion: 15
53761259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 308
Coasting Arc #8 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/014/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4509238
10 A = 6790421
98 meter
Y = 5051344
66 meter E =
0011609
Z = 414851
99 I = 51
93644
XDOT = -3782
800362 Wp = 38
77662
YDOT = 2875
738620 meter/sec RA = 45
49541 deg
ZDOT = 6019
442985 TA = 325
67808
MA = 325
75303
Ha = 220
759 n
mi
Hp = 216
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14794088
26 X = 4450402
30
Y = 16572653
09 feet Y = 5101441
12 meter
Z = 1361062
97 Z = 436613
29
XDOT = -12410
762341 XDOT = -3843
915441
YDOT = 9434
837993 feet/sec YDOT = 2833
094801 meter/sec
ZDOT = 19748
828690 ZDOT = 6000
919343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19578556
08 X = -5967543
89
Y = 10484413
48 feet Y = 3195649
23 meter
Z = 1458624
68 Z = 444588
80
XDOT = -5466
184572 XDOT = -1666
093057
YDOT = -12978
294828 feet/sec YDOT = -3955
784264 meter/sec
ZDOT = 19664
819561 ZDOT = 5993
837002
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 19014
46277080
00016717 00000-0 10270-3 0 9073
2 25544 51
6414 45
8500 0002607 285
9319 74
1546 15
53724749 31364
Satellite: ISS
Catalog Number: 25544
Epoch time: 19014
46277080 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 45
8500 deg
Eccentricity:
0002607
Arg of perigee: 285
9319 deg
Mean anomaly: 74
1546 deg
Mean motion: 15
53724749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 311
Coasting Arc #9 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2019/015/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3777907
98 A = 6788679
91 meter
Y = -5277424
20 meter E =
0004799
Z = -1982862
86 I = 51
90623
XDOT = 5015
380254 Wp = 155
62207
YDOT = -1488
872079 meter/sec RA = 40
54560 deg
ZDOT = -5602
120700 TA = 46
17116
MA = 46
13150
Ha = 220
715 n
mi
Hp = 216
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12394711
23 X = -3708981
96
Y = -17314383
84 feet Y = -5319285
92 meter
Z = -6505455
58 Z = -2001047
26
XDOT = 16454
659626 XDOT = 5058
868340
YDOT = -4884
750915 feet/sec YDOT = -1432
543195 meter/sec
ZDOT = -18379
661090 ZDOT = -5577
652429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19589474
41 X = 5970871
80
Y = -8282747
65 feet Y = -2524581
48 meter
Z = -6586827
03 Z = -2007664
88
XDOT = 553
824581 XDOT = 168
805732
YDOT = 15814
816611 feet/sec YDOT = 4820
356103 meter/sec
ZDOT = -18269
004007 ZDOT = -5568
392421
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 19015
42753056
00016717 00000-0 10270-3 0 9083
2 25544 51
6406 41
0441 0002495 287
5756 72
5124 15
53763345 31511
Satellite: ISS
Catalog Number: 25544
Epoch time: 19015
42753056 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 41
0441 deg
Eccentricity:
0002495
Arg of perigee: 287
5756 deg
Mean anomaly: 72
5124 deg
Mean motion: 15
53763345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 298
Coasting Arc #10 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2019/016/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5935885
86 A = 6787014
32 meter
Y = -1565394
65 meter E =
0010896
Z = 2883134
39 I = 51
87923
XDOT = -977
222899 Wp = 98
29596
YDOT = -5666
918362 meter/sec RA = 36
39863 deg
ZDOT = -5073
960553 TA = 48
99603
MA = 48
90185
Ha = 220
807 n
mi
Hp = 216
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19474691
13 X = -5931944
61
Y = -5135809
23 feet Y = -1631752
00 meter
Z = 9459102
34 Z = 2854309
69
XDOT = -3206
111872 XDOT = -889
134827
YDOT = -18592
251844 feet/sec YDOT = -5677
353515 meter/sec
ZDOT = -16646
852209 ZDOT = -5078
493905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20197890
67 X = 6156317
08
Y = -354929
70 feet Y = -108182
57 meter
Z = 9329200
69 Z = 2843540
37
XDOT = 7994
746794 XDOT = 2436
798823
YDOT = 15584
833332 feet/sec YDOT = 4750
257200 meter/sec
ZDOT = -16666
538570 ZDOT = -5079
960956
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 19016
26365639
00016717 00000-0 10270-3 0 9093
2 25544 51
6409 36
8756 0002461 282
8169 77
2708 15
53746403 31644
Satellite: ISS
Catalog Number: 25544
Epoch time: 19016
26365639 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 36
8756 deg
Eccentricity:
0002461
Arg of perigee: 282
8169 deg
Mean anomaly: 77
2708 deg
Mean motion: 15
53746403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 331
Coasting Arc #11 (Orbit 3178)
---------------------------------------
Vector Time (GMT): 2019/017/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6163460
49 A = 6789600
38 meter
Y = 2446517
45 meter E =
0008308
Z = -1436278
19 I = 51
86186
XDOT = -621
587000 Wp = 20
23508
YDOT = 4965
757434 meter/sec RA = 31
44152 deg
ZDOT = 5808
748195 TA = 324
15194
MA = 324
20767
Ha = 220
844 n
mi
Hp = 216
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20221327
05 X = 6142621
36
Y = 8026632
05 feet Y = 2515325
15 meter
Z = -4712198
79 Z = -1406388
99
XDOT = -2039
327427 XDOT = -705
284813
YDOT = 16291
855099 feet/sec YDOT = 4958
337968 meter/sec
ZDOT = 19057
572819 ZDOT = 5805
525886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21705202
72 X = -6615745
79
Y = -1860986
59 feet Y = -567228
71 meter
Z = -4577620
65 Z = -1395258
78
XDOT = -2747
829280 XDOT = -837
538364
YDOT = -14645
005144 feet/sec YDOT = -4463
797568 meter/sec
ZDOT = 19042
338499 ZDOT = 5804
104775
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 19017
22841387
00016717 00000-0 10270-3 0 9101
2 25544 51
6422 32
0692 0002514 292
5250 67
5636 15
53750443 31791
Satellite: ISS
Catalog Number: 25544
Epoch time: 19017
22841387 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 32
0692 deg
Eccentricity:
0002514
Arg of perigee: 292
5250 deg
Mean anomaly: 67
5636 deg
Mean motion: 15
53750443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3179
Checksum: 296
Coasting Arc #12 (Orbit 3194)
---------------------------------------
Vector Time (GMT): 2019/018/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6012500
70 A = 6790372
73 meter
Y = -3140924
78 meter E =
0009463
Z = -164950
09 I = 51
83478
XDOT = 2320
053665 Wp = 141
28530
YDOT = -4134
888587 meter/sec RA = 26
48746 deg
ZDOT = -6025
404106 TA = 40
48649
MA = 40
41613
Ha = 220
796 n
mi
Hp = 216
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19726052
16 X = -5976129
91
Y = -10304871
33 feet Y = -3207957
37 meter
Z = -541174
85 Z = -194068
29
XDOT = 7611
724622 XDOT = 2395
386534
YDOT = -13565
907437 feet/sec YDOT = -4108
522333 meter/sec
ZDOT = -19768
386175 ZDOT = -6013
951685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21921706
45 X = 6681736
13
Y = 3819339
07 feet Y = 1164134
55 meter
Z = -672169
90 Z = -204877
39
XDOT = -2972
463113 XDOT = -906
006757
YDOT = 13681
082635 feet/sec YDOT = 4169
993987 meter/sec
ZDOT = -19716
112675 ZDOT = -6009
471143
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 19018
25748783
00016717 00000-0 10270-3 0 9112
2 25544 51
6412 26
9424 0002449 294
4719 65
6178 15
53763080 31952
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
25748783 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 26
9424 deg
Eccentricity:
0002449
Arg of perigee: 294
4719 deg
Mean anomaly: 65
6178 deg
Mean motion: 15
53763080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3195
Checksum: 328
Coasting Arc #13 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/018/18:08:37
370
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1683386
47 A = 6779967
15 meter
Y = -3846985
31 meter E =
0010587
Z = -5332141
26 I = 51
77901
XDOT = 7009
536306 Wp = 83
95277
YDOT = 3087
631521 meter/sec RA = 23
85327 deg
ZDOT = -13
623148 TA = 185
91126
MA = 185
92377
Ha = 220
933 n
mi
Hp = 217
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5522921
49 X = 1752179
72
Y = -12621342
88 feet Y = -3827775
31 meter
Z = -17493901
76 Z = -5323797
40
XDOT = 22997
166358 XDOT = 6974
554755
YDOT = 10130
024675 feet/sec YDOT = 3165
821443 meter/sec
ZDOT = -44
695369 ZDOT = 20
341535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1218892
23 X = -371518
35
Y = -13771363
24 feet Y = -4197511
51 meter
Z = -17455698
59 Z = -5320496
93
XDOT = 24015
135401 XDOT = 7319
813270
YDOT = -2258
248618 feet/sec YDOT = -688
314179 meter/sec
ZDOT = 108
180945 ZDOT = 32
973552
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 19018
77202723
00016717 00000-0 10270-3 0 9129
2 25544 51
6413 24
3826 0004471 284
2858 75
7797 15
53231605 32031
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
77202723 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 24
3826 deg
Eccentricity:
0004471
Arg of perigee: 284
2858 deg
Mean anomaly: 75
7797 deg
Mean motion: 15
53231605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 304
Coasting Arc #14 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2019/019/18:08:37
370
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2992413
52 A = 6780761
74 meter
Y = 3259003
90 meter E =
0004294
Z = 5139763
83 I = 51
75086
XDOT = -6599
276752 Wp = 354
27146
YDOT = -3568
408796 meter/sec RA = 18
87252 deg
ZDOT = -1575
451830 TA = 110
92206
MA = 110
87609
Ha = 221
021 n
mi
Hp = 217
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9817629
65 X = -3053599
91
Y = 10692270
02 feet Y = 3225197
99 meter
Z = 16862742
24 Z = 5125079
79
XDOT = -21651
170446 XDOT = -6551
230794
YDOT = -11707
377940 feet/sec YDOT = -3641
937695 meter/sec
ZDOT = -5168
805218 ZDOT = -1607
391790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3223574
46 X = -982545
50
Y = 14232548
87 feet Y = 4338080
89 meter
Z = 16796002
10 Z = 5119421
44
XDOT = -23534
738636 XDOT = -7173
388336
YDOT = 954
628802 feet/sec YDOT = 290
970859 meter/sec
ZDOT = -5312
471758 ZDOT = -1619
241392
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 19019
80146179
00016717 00000-0 10270-3 0 9137
2 25544 51
6411 19
2583 0004694 287
7083 72
3556 15
53255828 32193
Satellite: ISS
Catalog Number: 25544
Epoch time: 19019
80146179 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 19
2583 deg
Eccentricity:
0004694
Arg of perigee: 287
7083 deg
Mean anomaly: 72
3556 deg
Mean motion: 15
53255828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 324
Coasting Arc #15 (Orbit 3222)
---------------------------------------
Vector Time (GMT): 2019/020/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1848405
23 A = 6780091
42 meter
Y = -3806305
07 meter E =
0010435
Z = -5306667
12 I = 51
73709
XDOT = 7145
822171 Wp = 90
34668
YDOT = 2701
923569 meter/sec RA = 17
44596 deg
ZDOT = 551
887056 TA = 184
91342
MA = 184
92367
Ha = 220
970 n
mi
Hp = 217
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6064321
62 X = 1916607
38
Y = -12487877
53 feet Y = -3785253
02 meter
Z = -17410325
18 Z = -5297523
17
XDOT = 23444
298462 XDOT = 7112
396704
YDOT = 8864
578640 feet/sec YDOT = 2781
646177 meter/sec
ZDOT = 1810
653072 ZDOT = 586
517234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13277554
92 X = -4046998
74
Y = 4228917
23 feet Y = 1288973
97 meter
Z = -17368514
60 Z = -5293923
25
XDOT = -9590
336391 XDOT = -2923
134532
YDOT = -22045
745477 feet/sec YDOT = -6719
543221 meter/sec
ZDOT = 1966
584426 ZDOT = 599
414933
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 19020
05882118
00016717 00000-0 10270-3 0 9147
2 25544 51
6389 17
9725 0004327 283
9553 76
1118 15
53229810 32236
Satellite: ISS
Catalog Number: 25544
Epoch time: 19020
05882118 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 17
9725 deg
Eccentricity:
0004327
Arg of perigee: 283
9553 deg
Mean anomaly: 76
1118 deg
Mean motion: 15
53229810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3223
Checksum: 307
Coasting Arc #16 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2019/021/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3180748
28 A = 6781633
66 meter
Y = 3325252
64 meter E =
0004873
Z = 4982035
08 I = 51
70931
XDOT = -6646
862409 Wp = 14
72305
YDOT = -3179
879471 meter/sec RA = 12
46135 deg
ZDOT = -2116
181038 TA = 95
89598
MA = 95
84043
Ha = 221
234 n
mi
Hp = 217
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10435525
86 X = -3241895
16
Y = 10909621
52 feet Y = 3289340
97 meter
Z = 16345259
46 Z = 4966436
36
XDOT = -21807
291367 XDOT = -6600
531120
YDOT = -10432
675430 feet/sec YDOT = -3253
950076 meter/sec
ZDOT = -6942
851173 ZDOT = -2148
355965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15171268
47 X = 4624202
63
Y = -254187
40 feet Y = -77476
32 meter
Z = 16274383
25 Z = 4960432
02
XDOT = 7983
774295 XDOT = 2433
454405
YDOT = 21660
563652 feet/sec YDOT = 6602
139801 meter/sec
ZDOT = -7087
631559 ZDOT = -2160
310099
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 19021
08825525
00016717 00000-0 10270-3 0 9151
2 25544 51
6384 12
8462 0004241 288
1040 71
9650 15
53189664 32399
Satellite: ISS
Catalog Number: 25544
Epoch time: 19021
08825525 = yrday
fracday
Element set: 915
Inclination: 51
6384 deg
RA of node: 12
8462 deg
Eccentricity:
0004241
Arg of perigee: 288
1040 deg
Mean anomaly: 71
9650 deg
Mean motion: 15
53189664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 304
Coasting Arc #17 (Orbit 3253)
---------------------------------------
Vector Time (GMT): 2019/022/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4385325
22 A = 6784191
39 meter
Y = -2863737
04 meter E =
0004046
Z = -4316098
68 I = 51
68619
XDOT = 5794
598897 Wp = 108
32378
YDOT = 3567
632313 meter/sec RA = 7
48129 deg
ZDOT = 3521
879633 TA = 197
52967
MA = 197
54364
Ha = 221
213 n
mi
Hp = 217
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14387549
95 X = 4437987
03
Y = -9395462
72 feet Y = -2814402
57 meter
Z = -14160428
73 Z = -4294669
28
XDOT = 19011
151238 XDOT = 5737
167116
YDOT = 11704
830422 feet/sec YDOT = 3632
110224 meter/sec
ZDOT = 11554
723205 ZDOT = 3549
887554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16942824
19 X = -5164172
81
Y = -3310321
08 feet Y = -1008985
86 meter
Z = -14063304
66 Z = -4286495
26
XDOT = -5717
296546 XDOT = -1742
631987
YDOT = -20340
322346 feet/sec YDOT = -6199
730251 meter/sec
ZDOT = 11680
639531 ZDOT = 3560
258929
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 19022
05334690
00016717 00000-0 10270-3 0 9168
2 25544 51
6392 8
0424 0004316 291
6801 68
3891 15
53220753 32549
Satellite: ISS
Catalog Number: 25544
Epoch time: 19022
05334690 = yrday
fracday
Element set: 916
Inclination: 51
6392 deg
RA of node: 8
0424 deg
Eccentricity:
0004316
Arg of perigee: 291
6801 deg
Mean anomaly: 68
3891 deg
Mean motion: 15
53220753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3254
Checksum: 291
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