[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 20th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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
082/14:09:43
720 0
7 2
2 2
2
N/A 2
0 -0
2 224
1
000/00:05:27
441 0
4 -0
1 217
1
082/22:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
1
000/00:00:00
000 0
0 0
0 217
0
087/06:36:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 217
1
090/20:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 217
3
Coasting Arc #1 (Orbit 115)
---------------------------------------
Vector Time (GMT): 2019/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3978944
64 A = 6782579
81 meter
Y = -2231244
20 meter E =
0015666
Z = -5033148
86 I = 52
00683
XDOT = 1455
870152 Wp = 84
55806
YDOT = 7227
633195 meter/sec RA = 91
19959 deg
ZDOT = -2057
197053 TA = 165
52487
MA = 165
47995
Ha = 224
382 n
mi
Hp = 215
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13054280
31 X = 4028047
13
Y = -7320355
00 feet Y = -2186474
76 meter
Z = -16512955
56 Z = -5013701
53
XDOT = 4776
476877 XDOT = 1384
933051
YDOT = 23712
707333 feet/sec YDOT = 7243
516938 meter/sec
ZDOT = -6749
334162 ZDOT = -2050
298036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13765828
96 X = 4195824
67
Y = -6116376
98 feet Y = -1864271
70 meter
Z = -16424719
75 Z = -5006254
58
XDOT = 2238
372304 XDOT = 682
255878
YDOT = 23044
313819 feet/sec YDOT = 7023
906852 meter/sec
ZDOT = -6718
784215 ZDOT = -2047
885429
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 19077
51969042
00016717 00000-0 10270-3 0 9007
2 25544 51
6388 91
9813 0003815 118
6385 241
5151 15
52812362 1165
Satellite: ISS
Catalog Number: 25544
Epoch time: 19077
51969042 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 91
9813 deg
Eccentricity:
0003815
Arg of perigee: 118
6385 deg
Mean anomaly: 241
5151 deg
Mean motion: 15
52812362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 116
Checksum: 306
Coasting Arc #2 (Orbit 131)
---------------------------------------
Vector Time (GMT): 2019/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4091377
04 A = 6781270
03 meter
Y = 1000697
89 meter E =
0006756
Z = 5309756
89 I = 52
00151
XDOT = -1006
218684 Wp = 118
09125
YDOT = -7577
052085 meter/sec RA = 86
23861 deg
ZDOT = 648
946877 TA = 325
72424
MA = 325
76782
Ha = 224
481 n
mi
Hp = 215
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13423153
01 X = -4128054
48
Y = 3283129
58 feet Y = 954740
79 meter
Z = 17420462
23 Z = 5289793
64
XDOT = -3301
242401 XDOT = -924
567328
YDOT = -24859
094767 feet/sec YDOT = -7587
847711 meter/sec
ZDOT = 2129
090805 ZDOT = 644
258306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13741181
49 X = -4188312
12
Y = 2298560
69 feet Y = 700601
30 meter
Z = 17330003
77 Z = 5282185
15
XDOT = -1345
077442 XDOT = -409
979604
YDOT = -24031
383774 feet/sec YDOT = -7324
765774 meter/sec
ZDOT = 2108
588082 ZDOT = 642
697647
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 19078
54938805
00016717 00000-0 10270-3 0 9015
2 25544 51
6381 86
8572 0003797 120
4298 239
7230 15
52828319 1320
Satellite: ISS
Catalog Number: 25544
Epoch time: 19078
54938805 = yrday
fracday
Element set: 901
Inclination: 51
6381 deg
RA of node: 86
8572 deg
Eccentricity:
0003797
Arg of perigee: 120
4298 deg
Mean anomaly: 239
7230 deg
Mean motion: 15
52828319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 132
Checksum: 329
Coasting Arc #3 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2019/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4235153
18 A = 6781427
62 meter
Y = 271884
31 meter E =
0017968
Z = -5304936
20 I = 51
99823
XDOT = 526
155831 Wp = 101
57102
YDOT = 7591
987310 meter/sec RA = 81
27718 deg
ZDOT = 807
961754 TA = 176
13556
MA = 176
12167
Ha = 224
329 n
mi
Hp = 215
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13894859
51 X = 4257566
25
Y = 892008
90 feet Y = 319369
36 meter
Z = -17404646
31 Z = -5284309
27
XDOT = 1726
233041 XDOT = 437
296390
YDOT = 24908
094849 feet/sec YDOT = 7597
374418 meter/sec
ZDOT = 2650
793156 ZDOT = 810
300744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13940840
31 X = 4249168
13
Y = 1660174
56 feet Y = 506021
20 meter
Z = -17311305
73 Z = -5276485
99
XDOT = 456
887742 XDOT = 139
259384
YDOT = 23947
951671 feet/sec YDOT = 7299
335669 meter/sec
ZDOT = 2660
647865 ZDOT = 810
965469
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 19079
51472761
00016717 00000-0 10270-3 0 9028
2 25544 51
6378 82
0545 0003767 122
8396 237
3119 15
52807885 1477
Satellite: ISS
Catalog Number: 25544
Epoch time: 19079
51472761 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 82
0545 deg
Eccentricity:
0003767
Arg of perigee: 122
8396 deg
Mean anomaly: 237
3119 deg
Mean motion: 15
52807885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 329
Coasting Arc #4 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2019/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4360288
92 A = 6782757
52 meter
Y = -1504515
31 meter E =
0008464
Z = 4966161
36 I = 51
99547
XDOT = -1
333446 Wp = 81
46572
YDOT = -7342
937611 meter/sec RA = 76
31641 deg
ZDOT = -2221
295037 TA = 30
11801
MA = 30
06937
Ha = 224
374 n
mi
Hp = 215
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14305409
83 X = -4367263
63
Y = -4936073
86 feet Y = -1553313
40 meter
Z = 16293180
31 Z = 4944964
13
XDOT = -4
374824 XDOT = 91
567208
YDOT = -24091
002660 feet/sec YDOT = -7342
433400 meter/sec
ZDOT = -7287
713376 ZDOT = -2221
074826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14217198
70 X = -4333402
17
Y = -5476619
74 feet Y = -1669273
70 meter
Z = 16197382
42 Z = 4936962
16
XDOT = 556
152511 XDOT = 169
515285
YDOT = -23035
832293 feet/sec YDOT = -7021
321683 meter/sec
ZDOT = -7285
994488 ZDOT = -2220
771120
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 19080
54442112
00016717 00000-0 10270-3 0 9031
2 25544 51
6365 76
9309 0003647 127
1467 233
0018 15
52831881 1639
Satellite: ISS
Catalog Number: 25544
Epoch time: 19080
54442112 = yrday
fracday
Element set: 903
Inclination: 51
6365 deg
RA of node: 76
9309 deg
Eccentricity:
0003647
Arg of perigee: 127
1467 deg
Mean anomaly: 233
0018 deg
Mean motion: 15
52831881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 294
Coasting Arc #5 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2019/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4488779
23 A = 6785228
41 meter
Y = 2635944
91 meter E =
0012133
Z = -4364882
74 I = 51
99535
XDOT = -591
182902 Wp = 115
77823
YDOT = 6786
455521 meter/sec RA = 71
35957 deg
ZDOT = 3492
776692 TA = 189
59232
MA = 189
61551
Ha = 224
245 n
mi
Hp = 215
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14726965
99 X = 4480171
88
Y = 8648113
23 feet Y = 2686092
86 meter
Z = -14320481
44 Z = -4343099
24
XDOT = -1939
576450 XDOT = -683
992978
YDOT = 22265
274018 feet/sec YDOT = 6779
326043 meter/sec
ZDOT = 11459
241114 ZDOT = 3489
678607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14640990
87 X = 4462574
02
Y = 8951056
22 feet Y = 2728281
94 meter
Z = -14222150
23 Z = -4334911
39
XDOT = -1822
332206 XDOT = -555
446856
YDOT = 21152
067263 feet/sec YDOT = 6447
150102 meter/sec
ZDOT = 11444
535933 ZDOT = 3488
294552
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 19081
50975747
00016717 00000-0 10270-3 0 9044
2 25544 51
6373 72
1280 0003670 128
9431 231
2048 15
52810164 1780
Satellite: ISS
Catalog Number: 25544
Epoch time: 19081
50975747 = yrday
fracday
Element set: 904
Inclination: 51
6373 deg
RA of node: 72
1280 deg
Eccentricity:
0003670
Arg of perigee: 128
9431 deg
Mean anomaly: 231
2048 deg
Mean motion: 15
52810164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 178
Checksum: 298
Coasting Arc #6 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2019/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4550502
71 A = 6788001
89 meter
Y = -3629323
42 meter E =
0015105
Z = 3477503
46 I = 51
99369
XDOT = 1282
586427 Wp = 98
25776
YDOT = -6015
604516 meter/sec RA = 66
40696 deg
ZDOT = -4585
052843 TA = 41
13146
MA = 41
01770
Ha = 224
198 n
mi
Hp = 215
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14929470
84 X = -4526472
20
Y = -11907229
06 feet Y = -3680075
55 meter
Z = 11409132
08 Z = 3455457
58
XDOT = 4207
960717 XDOT = 1372
030984
YDOT = -19736
235289 feet/sec YDOT = -6000
762162 meter/sec
ZDOT = -15042
824287 ZDOT = -4578
604553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14964644
91 X = -4561223
77
Y = -11957801
19 feet Y = -3644737
80 meter
Z = 11309725
54 Z = 3447204
35
XDOT = 3504
150828 XDOT = 1068
065172
YDOT = -18631
115187 feet/sec YDOT = -5678
763909 meter/sec
ZDOT = -15013
018604 ZDOT = -4575
968071
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 19082
53944537
00016717 00000-0 10270-3 0 9052
2 25544 51
6377 67
0042 0003518 132
2403 227
9048 15
52853764 1944
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
53944537 = yrday
fracday
Element set: 905
Inclination: 51
6377 deg
RA of node: 67
0042 deg
Eccentricity:
0003518
Arg of perigee: 132
2403 deg
Mean anomaly: 227
9048 deg
Mean motion: 15
52853764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 310
Coasting Arc #7 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2019/082/14:12:27
441
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4613815
00 A = 6784288
03 meter
Y = 946530
65 meter E =
0013278
Z = -4895473
00 I = 51
97728
XDOT = 1113
568904 Wp = 114
35248
YDOT = 7171
062013 meter/sec RA = 65
95715 deg
ZDOT = 2435
882096 TA = 179
47303
MA = 179
47163
Ha = 224
106 n
mi
Hp = 217
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15137188
33 X = 4626667
26
Y = 3105415
53 feet Y = 998196
85 meter
Z = -16061263
14 Z = -4873029
67
XDOT = 3653
441286 XDOT = 1021
465103
YDOT = 23527
106341 feet/sec YDOT = 7183
000017 meter/sec
ZDOT = 7991
739160 ZDOT = 2441
066873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14474880
58 X = 4411943
60
Y = -5701355
43 feet Y = -1737773
13 meter
Z = -15959781
58 Z = -4864541
42
XDOT = 15420
143057 XDOT = 4700
059604
YDOT = 16713
356001 feet/sec YDOT = 5094
230909 meter/sec
ZDOT = 8014
464439 ZDOT = 2442
808761
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 19082
60380194
00016717 00000-0 10270-3 0 9064
2 25544 51
6390 66
6835 0002159 156
3814 203
7437 15
52428969 1957
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
60380194 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 66
6835 deg
Eccentricity:
0002159
Arg of perigee: 156
3814 deg
Mean anomaly: 203
7437 deg
Mean motion: 15
52428969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 195
Checksum: 325
Coasting Arc #8 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2019/082/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1654779
96 A = 6785564
80 meter
Y = 4755126
01 meter E =
0010403
Z = 4544360
38 I = 51
97540
XDOT = -5065
395368 Wp = 121
54385
YDOT = -4804
086615 meter/sec RA = 64
29358 deg
ZDOT = 3171
760134 TA = 296
72858
MA = 296
83502
Ha = 224
119 n
mi
Hp = 217
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5429068
09 X = -1729904
18
Y = 15600807
13 feet Y = 4736201
55 meter
Z = 14909318
82 Z = 4536139
08
XDOT = -16618
751208 XDOT = -5026
704933
YDOT = -15761
439025 feet/sec YDOT = -4860
514736 meter/sec
ZDOT = 10406
037185 ZDOT = 3147
248767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11135500
73 X = 3394100
62
Y = -12246774
55 feet Y = -3732816
88 meter
Z = 14871613
49 Z = 4532867
79
XDOT = 8395
815928 XDOT = 2559
044695
YDOT = 20178
676780 feet/sec YDOT = 6150
460683 meter/sec
ZDOT = 10295
599642 ZDOT = 3138
098771
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 19082
99003312
00016717 00000-0 10270-3 0 9071
2 25544 51
6374 64
7608 0002211 160
9739 199
1495 15
52431309 2014
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
99003312 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 64
7608 deg
Eccentricity:
0002211
Arg of perigee: 160
9739 deg
Mean anomaly: 199
1495 deg
Mean motion: 15
52431309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 299
Coasting Arc #9 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2019/083/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2266970
93 A = 6783508
75 meter
Y = -3931474
43 meter E =
0013325
Z = -5053602
36 I = 51
95290
XDOT = 5019
490188 Wp = 85
80356
YDOT = 5431
703764 meter/sec RA = 59
33724 deg
ZDOT = -1977
488762 TA = 165
06851
MA = 165
02913
Ha = 224
112 n
mi
Hp = 217
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7437568
68 X = 2335312
98
Y = -12898538
15 feet Y = -3905741
87 meter
Z = -16580060
23 Z = -5042423
91
XDOT = 16468
143660 XDOT = 4967
983851
YDOT = 17820
550407 feet/sec YDOT = 5487
547059 meter/sec
ZDOT = -6487
824021 ZDOT = -1953
231441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11796001
41 X = -3595421
23
Y = 9177856
38 feet Y = 2797410
63 meter
Z = -16529047
59 Z = -5038053
71
XDOT = -8050
949716 XDOT = -2453
929474
YDOT = -21814
362874 feet/sec YDOT = -6649
017804 meter/sec
ZDOT = -6378
618492 ZDOT = -1944
202916
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 19083
95561217
00016717 00000-0 10270-3 0 9082
2 25544 51
6371 59
9596 0002439 160
8056 199
3188 15
52446530 2165
Satellite: ISS
Catalog Number: 25544
Epoch time: 19083
95561217 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 59
9596 deg
Eccentricity:
0002439
Arg of perigee: 160
8056 deg
Mean anomaly: 199
3188 deg
Mean motion: 15
52446530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 331
Coasting Arc #10 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2019/084/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2911079
29 A = 6782515
43 meter
Y = 3065728
56 meter E =
0004918
Z = 5301210
00 I = 51
93162
XDOT = -4885
663604 Wp = 137
24641
YDOT = -5868
022495 meter/sec RA = 54
37662 deg
ZDOT = 706
730931 TA = 306
00804
MA = 306
05362
Ha = 224
197 n
mi
Hp = 217
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9550785
07 X = -2970895
16
Y = 10058164
58 feet Y = 3032840
73 meter
Z = 17392421
27 Z = 5286923
57
XDOT = -16029
080067 XDOT = -4823
115514
YDOT = -19252
042307 feet/sec YDOT = -5922
307629 meter/sec
ZDOT = 2318
671034 ZDOT = 683
150466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12608588
54 X = 3843097
79
Y = -5971951
71 feet Y = -1820250
88 meter
Z = 17327428
43 Z = 5281400
18
XDOT = 7728
610814 XDOT = 2355
680576
YDOT = 22774
465343 feet/sec YDOT = 6941
657037 meter/sec
ZDOT = 2212
591765 ZDOT = 674
397970
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 19084
98556173
00016717 00000-0 10270-3 0 9092
2 25544 51
6375 54
8377 0002377 165
2395 194
8826 15
52406905 2325
Satellite: ISS
Catalog Number: 25544
Epoch time: 19084
98556173 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 54
8377 deg
Eccentricity:
0002377
Arg of perigee: 165
2395 deg
Mean anomaly: 194
8826 deg
Mean motion: 15
52406905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 341
Coasting Arc #11 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2019/085/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3613142
06 A = 6782362
04 meter
Y = -2190061
37 meter E =
0015615
Z = -5319004
50 I = 51
91252
XDOT = 4592
186404 Wp = 103
29913
YDOT = 6093
443094 meter/sec RA = 49
41378 deg
ZDOT = 608
498687 TA = 172
50956
MA = 172
48620
Ha = 224
023 n
mi
Hp = 217
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11854140
60 X = 3663200
16
Y = -7185240
71 feet Y = -2149377
08 meter
Z = -17450802
17 Z = -5301331
53
XDOT = 15066
228358 XDOT = 4520
750749
YDOT = 19991
611200 feet/sec YDOT = 6144
396744 meter/sec
ZDOT = 1996
386770 ZDOT = 630
631960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13697757
65 X = -4175076
53
Y = 2704328
85 feet Y = 824279
43 meter
Z = -17370574
85 Z = -5294551
21
XDOT = -7189
483857 XDOT = -2191
354680
YDOT = -22911
088857 feet/sec YDOT = -6983
299884 meter/sec
ZDOT = 2095
877028 ZDOT = 638
823318
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 19085
95113416
00016717 00000-0 10270-3 0 9101
2 25544 51
6387 50
0364 0002481 166
4343 193
6876 15
52458422 2473
Satellite: ISS
Catalog Number: 25544
Epoch time: 19085
95113416 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 50
0364 deg
Eccentricity:
0002481
Arg of perigee: 166
4343 deg
Mean anomaly: 193
6876 deg
Mean motion: 15
52458422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 247
Checksum: 308
Coasting Arc #12 (Orbit 262)
---------------------------------------
Vector Time (GMT): 2019/086/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4302919
03 A = 6783548
13 meter
Y = 1343639
08 meter E =
0005238
Z = 5064869
12 I = 51
89236
XDOT = -4156
885763 Wp = 81
85079
YDOT = -6159
895276 meter/sec RA = 44
45019 deg
ZDOT = -1895
001572 TA = 26
46488
MA = 26
43814
Ha = 224
195 n
mi
Hp = 217
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14117188
43 X = -4342226
41
Y = 4408264
69 feet Y = 1295301
30 meter
Z = 16617024
67 Z = 5043871
70
XDOT = -13638
076651 XDOT = -4078
490289
YDOT = -20209
630169 feet/sec YDOT = -6205
942238 meter/sec
ZDOT = -6217
196758 ZDOT = -1915
003370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14889854
49 X = 4538427
65
Y = 417334
28 feet Y = 127203
49 meter
Z = 16521845
57 Z = 5035858
53
XDOT = 6378
389151 XDOT = 1944
133013
YDOT = 22430
267909 feet/sec YDOT = 6836
745659 meter/sec
ZDOT = -6307
020531 ZDOT = -1922
379858
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 19086
98107777
00016717 00000-0 10270-3 0 9119
2 25544 51
6375 44
9146 0002528 169
6991 190
4213 15
52420361 2635
Satellite: ISS
Catalog Number: 25544
Epoch time: 19086
98107777 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 44
9146 deg
Eccentricity:
0002528
Arg of perigee: 169
6991 deg
Mean anomaly: 190
4213 deg
Mean motion: 15
52420361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 263
Checksum: 318
Coasting Arc #13 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2019/087/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3263581
27 A = 6791858
89 meter
Y = -5488021
80 meter E =
0007733
Z = -2307736
96 I = 51
91641
XDOT = 5322
718968 Wp = 144
33589
YDOT = -883
122401 meter/sec RA = 42
80827 deg
ZDOT = -5442
470872 TA = 61
24851
MA = 61
17084
Ha = 223
889 n
mi
Hp = 217
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10707287
63 X = -3190760
45
Y = -18005320
88 feet Y = -5524110
40 meter
Z = -7571315
47 Z = -2323412
99
XDOT = 17462
988740 XDOT = 5358
635076
YDOT = -2897
383207 feet/sec YDOT = -823
399493 meter/sec
ZDOT = -17855
875565 ZDOT = -5416
527945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14986179
92 X = 4567787
64
Y = -14600761
30 feet Y = -4450312
04 meter
Z = -7641635
11 Z = -2329170
38
XDOT = 5897
030825 XDOT = 1797
414995
YDOT = 15310
472699 feet/sec YDOT = 4666
632079 meter/sec
ZDOT = -17738
367295 ZDOT = -5406
654351
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 19087
30293278
00016717 00000-0 10270-3 0 9129
2 25544 51
6412 43
3178 0002273 170
4569 189
6626 15
52468875 2688
Satellite: ISS
Catalog Number: 25544
Epoch time: 19087
30293278 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 43
3178 deg
Eccentricity:
0002273
Arg of perigee: 170
4569 deg
Mean anomaly: 189
6626 deg
Mean motion: 15
52468875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 331
Coasting Arc #14 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2019/088/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2646801
77 A = 6789628
96 meter
Y = 5317080
03 meter E =
0013122
Z = 3280278
19 I = 51
88241
XDOT = -6014
712493 Wp = 97
17502
YDOT = 49
734285 meter/sec RA = 37
85761 deg
ZDOT = 4754
681388 TA = 300
74062
MA = 300
86980
Ha = 223
912 n
mi
Hp = 217
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8683732
84 X = 2571214
30
Y = 17444488
29 feet Y = 5346255
97 meter
Z = 10762067
54 Z = 3292951
38
XDOT = -19733
308705 XDOT = -6037
917050
YDOT = 163
170227 feet/sec YDOT = -17
655912 meter/sec
ZDOT = 15599
348385 ZDOT = 4725
408018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14706519
88 X = -4482547
26
Y = 12736213
67 feet Y = 3881997
93 meter
Z = 10818808
61 Z = 3297572
87
XDOT = -4237
567123 XDOT = -1291
610459
YDOT = -18081
045042 feet/sec YDOT = -5511
102529 meter/sec
ZDOT = 15466
866536 ZDOT = 4714
300920
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 19088
33287298
00016717 00000-0 10270-3 0 9139
2 25544 51
6400 38
1962 0002199 170
3136 189
8059 15
52444596 2848
Satellite: ISS
Catalog Number: 25544
Epoch time: 19088
33287298 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 38
1962 deg
Eccentricity:
0002199
Arg of perigee: 170
3136 deg
Mean anomaly: 189
8059 deg
Mean motion: 15
52444596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 331
Coasting Arc #15 (Orbit 298)
---------------------------------------
Vector Time (GMT): 2019/089/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1852987
21 A = 6786879
26 meter
Y = -5062480
04 meter E =
0007256
Z = -4129566
53 I = 51
84851
XDOT = 6601
463106 Wp = 86
97518
YDOT = 696
013891 meter/sec RA = 32
90096 deg
ZDOT = -3820
825218 TA = 143
67599
MA = 143
62671
Ha = 223
774 n
mi
Hp = 217
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6079354
35 X = -1776180
43
Y = -16609186
47 feet Y = -5082772
26 meter
Z = -13548446
62 Z = -4138380
68
XDOT = 21658
343523 XDOT = 6611
748739
YDOT = 2283
510140 feet/sec YDOT = 769
893325 meter/sec
ZDOT = -12535
515807 ZDOT = -3788
733127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14386598
94 X = 4385035
36
Y = -10236353
75 feet Y = -3120040
62 meter
Z = -13587746
80 Z = -4141545
23
XDOT = 2904
253652 XDOT = 885
216513
YDOT = 20505
228411 feet/sec YDOT = 6249
993620 meter/sec
ZDOT = -12390
370367 ZDOT = -3776
584888
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 19089
29843616
00016717 00000-0 10270-3 0 9148
2 25544 51
6419 33
3952 0002175 177
8740 182
2421 15
52478409 2997
Satellite: ISS
Catalog Number: 25544
Epoch time: 19089
29843616 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 33
3952 deg
Eccentricity:
0002175
Arg of perigee: 177
8740 deg
Mean anomaly: 182
2421 deg
Mean motion: 15
52478409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 299
Checksum: 329
Coasting Arc #16 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2019/090/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 960780
40 A = 6784560
75 meter
Y = 4741604
97 meter E =
0008853
Z = 4753058
16 I = 51
81037
XDOT = -7046
529108 Wp = 129
40472
YDOT = -1311
502608 meter/sec RA = 27
93723 deg
ZDOT = 2723
856050 TA = 293
67826
MA = 293
77115
Ha = 223
764 n
mi
Hp = 217
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3152166
68 X = 884599
51
Y = 15556446
76 feet Y = 4751923
51 meter
Z = 15594022
84 Z = 4757539
83
XDOT = -23118
533820 XDOT = -7044
570669
YDOT = -4302
830078 feet/sec YDOT = -1390
290661 meter/sec
ZDOT = 8936
535597 ZDOT = 2689
631817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14039391
25 X = -4279206
45
Y = 7363357
10 feet Y = 2244351
24 meter
Z = 15613750
49 Z = 4759071
15
XDOT = -1958
590847 XDOT = -596
978490
YDOT = -22417
530888 feet/sec YDOT = -6832
863415 meter/sec
ZDOT = 8781
822364 ZDOT = 2676
699456
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 19090
32836874
00016717 00000-0 10270-3 0 9153
2 25544 51
6401 28
2735 0002100 178
1298 181
9861 15
52469946 3159
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
32836874 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 28
2735 deg
Eccentricity:
0002100
Arg of perigee: 178
1298 deg
Mean anomaly: 181
9861 deg
Mean motion: 15
52469946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 316
Coasting Arc #17 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2019/090/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3495985
41 A = 6788907
11 meter
Y = 4659112
28 meter E =
0012223
Z = 3479411
43 I = 51
80519
XDOT = -6058
176851 Wp = 102
31144
YDOT = 1127
019503 meter/sec RA = 25
08480 deg
ZDOT = 4561
833912 TA = 298
41939
MA = 298
54252
Ha = 223
626 n
mi
Hp = 217
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11469768
42 X = 3426725
16
Y = 15285801
44 feet Y = 4697819
88 meter
Z = 11415391
82 Z = 3496224
85
XDOT = -19875
908304 XDOT = -6092
487922
YDOT = 3697
570547 feet/sec YDOT = 1059
081280 meter/sec
ZDOT = 14966
646694 ZDOT = 4532
322377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2988531
62 X = 910904
44
Y = -18829491
96 feet Y = -5739229
15 meter
Z = 11490926
64 Z = 3502434
44
XDOT = 15222
072838 XDOT = 4639
687801
YDOT = 11499
934567 feet/sec YDOT = 3505
180056 meter/sec
ZDOT = 14832
979514 ZDOT = 4521
092156
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 19090
90770460
00016717 00000-0 10270-3 0 9166
2 25544 51
6373 25
3895 0002376 187
1886 172
9233 15
52489771 3241
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
90770460 = yrday
fracday
Element set: 916
Inclination: 51
6373 deg
RA of node: 25
3895 deg
Eccentricity:
0002376
Arg of perigee: 187
1886 deg
Mean anomaly: 172
9233 deg
Mean motion: 15
52489771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 324
Checksum: 331
Coasting Arc #18 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2019/091/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914829
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2630301
35 A = 6786242
78 meter
Y = -4561578
76 meter E =
0007650
Z = -4288032
24 I = 51
76773
XDOT = 6749
765343 Wp = 84
16140
YDOT = -530
969116 meter/sec RA = 20
12217 deg
ZDOT = -3580
234438 TA = 149
34100
MA = 149
29628
Ha = 223
613 n
mi
Hp = 217
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8629597
62 X = -2558268
26
Y = -14965809
58 feet Y = -4590590
29 meter
Z = -14068347
25 Z = -4300633
77
XDOT = 22144
899419 XDOT = 6772
591812
YDOT = -1742
024660 feet/sec YDOT = -455
361239 meter/sec
ZDOT = -11746
175979 ZDOT = -3547
391338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4469437
95 X = -1362284
69
Y = 16639625
13 feet Y = 5071757
74 meter
Z = -14124829
41 Z = -4305248
00
XDOT = -15801
072144 XDOT = -4816
166790
YDOT = -14075
816523 feet/sec YDOT = -4290
308876 meter/sec
ZDOT = -11597
514884 ZDOT = -3534
922537
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 19091
87326272
00016717 00000-0 10270-3 0 9172
2 25544 51
6393 20
5887 0002239 187
8346 172
2771 15
52496593 3393
Satellite: ISS
Catalog Number: 25544
Epoch time: 19091
87326272 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 20
5887 deg
Eccentricity:
0002239
Arg of perigee: 187
8346 deg
Mean anomaly: 172
2771 deg
Mean motion: 15
52496593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 339
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