[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 11th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
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
018/18:05:10
953 3
0 3
2 3
2
N/A 0
8 0
0 220
9
000/00:08:17
907 -0
6 -0
0 217
9
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
9
025/12:55:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 217
5
026/08:59:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2019/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4566338
91 A = 6788521
90 meter
Y = 4544137
99 meter E =
0005200
Z = -2132661
17 I = 51
98695
XDOT = -2209
931963 Wp = 19
33295
YDOT = 4816
285216 meter/sec RA = 59
85727 deg
ZDOT = 5539
066230 TA = 317
15800
MA = 317
19850
Ha = 220
695 n
mi
Hp = 216
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14981426
86 X = 4525544
83
Y = 14908589
20 feet Y = 4594973
96 meter
Z = -6996919
86 Z = -2110578
85
XDOT = -7250
432950 XDOT = -2290
530071
YDOT = 15801
460683 feet/sec YDOT = 4791
121354 meter/sec
ZDOT = 18172
789470 ZDOT = 5528
135801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8927760
66 X = -2721181
45
Y = 19193263
71 feet Y = 5850106
78 meter
Z = -6897810
36 Z = -2102452
60
XDOT = -15966
687775 XDOT = -4866
646434
YDOT = -924
122925 feet/sec YDOT = -281
672668 meter/sec
ZDOT = 18122
813187 ZDOT = 5523
833459
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
50416252
00016717 00000-0 10270-3 0 9004
2 25544 51
6404 60
5908 0002501 271
5814 88
5052 15
53760647 30900
Satellite: ISS
Catalog Number: 25544
Epoch time: 19011
50416252 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 60
5908 deg
Eccentricity:
0002501
Arg of perigee: 271
5814 deg
Mean anomaly: 88
5052 deg
Mean motion: 15
53760647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 278
Coasting Arc #2 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2019/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4246007
44 A = 6790238
86 meter
Y = -5259917
30 meter E =
0011012
Z = 576248
24 I = 51
97546
XDOT = 3364
093521 Wp = 135
76068
YDOT = -3380
216821 meter/sec RA = 54
91038 deg
ZDOT = -6005
078287 TA = 38
04944
MA = 37
97171
Ha = 220
667 n
mi
Hp = 216
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13930470
61 X = -4189673
06
Y = -17256946
51 feet Y = -5307084
14 meter
Z = 1890578
22 Z = 555759
66
XDOT = 11037
052233 XDOT = 3430
811001
YDOT = -11089
950199 feet/sec YDOT = -3342
223967 meter/sec
ZDOT = -19701
700416 ZDOT = -5988
575042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11177279
84 X = 3406834
89
Y = -19164220
61 feet Y = -5841254
44 meter
Z = 1798767
35 Z = 548264
29
XDOT = 12938
237228 XDOT = 3943
574707
YDOT = 5684
061308 feet/sec YDOT = 1732
501887 meter/sec
ZDOT = -19626
747923 ZDOT = -5982
232767
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
53324361
00016717 00000-0 10270-3 0 9018
2 25544 51
6406 55
4636 0002475 276
7729 83
3141 15
53772113 31066
Satellite: ISS
Catalog Number: 25544
Epoch time: 19012
53324361 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 55
4636 deg
Eccentricity:
0002475
Arg of perigee: 276
7729 deg
Mean anomaly: 83
3141 deg
Mean motion: 15
53772113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3106
Checksum: 288
Coasting Arc #3 (Orbit 3121)
---------------------------------------
Vector Time (GMT): 2019/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3681934
85 A = 6790056
71 meter
Y = 5607478
93 meter E =
0012162
Z = 1007051
17 I = 51
95455
XDOT = -4486
938093 Wp = 47
27782
YDOT = 1874
392737 meter/sec RA = 49
96397 deg
ZDOT = 5930
658019 TA = 323
58818
MA = 323
67085
Ha = 220
822 n
mi
Hp = 216
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12079838
76 X = 3614065
15
Y = 18397240
59 feet Y = 5648273
38 meter
Z = 3303973
67 Z = 1024771
78
XDOT = -14720
925501 XDOT = -4536
372173
YDOT = 6149
582471 feet/sec YDOT = 1823
940105 meter/sec
ZDOT = 19457
539434 ZDOT = 5908
742347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12605125
54 X = -3842042
26
Y = 18026695
99 feet Y = 5494536
94 meter
Z = 3383230
62 Z = 1031208
69
XDOT = -9910
897846 XDOT = -3020
841663
YDOT = -10585
729906 feet/sec YDOT = -3226
530475 meter/sec
ZDOT = 19358
350195 ZDOT = 5900
425139
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
56232475
00016717 00000-0 10270-3 0 9027
2 25544 51
6407 50
3365 0002390 285
9572 74
1317 15
53724412 31224
Satellite: ISS
Catalog Number: 25544
Epoch time: 19013
56232475 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 50
3365 deg
Eccentricity:
0002390
Arg of perigee: 285
9572 deg
Mean anomaly: 74
1317 deg
Mean motion: 15
53724412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3122
Checksum: 285
Coasting Arc #4 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2019/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2828939
94 A = 6787621
40 meter
Y = -5628401
50 meter E =
0003097
Z = -2525173
29 I = 51
92607
XDOT = 5505
966651 Wp = 146
42525
YDOT = -384
116188 meter/sec RA = 45
01326 deg
ZDOT = -5317
766372 TA = 61
78147
MA = 61
75020
Ha = 220
720 n
mi
Hp = 216
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9281299
01 X = -2753525
51
Y = -18465884
17 feet Y = -5659614
92 meter
Z = -8284689
27 Z = -2538732
15
XDOT = 18064
195049 XDOT = 5535
683314
YDOT = -1260
223715 feet/sec YDOT = -322
378301 meter/sec
ZDOT = -17446
740066 ZDOT = -5290
948466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13453328
81 X = 4100574
62
Y = -15656755
54 feet Y = -4772179
09 meter
Z = -8345143
24 Z = -2543599
66
XDOT = 7061
290277 XDOT = 2152
281276
YDOT = 15292
433163 feet/sec YDOT = 4661
133628 meter/sec
ZDOT = -17325
622021 ZDOT = -5280
849592
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
52708283
00016717 00000-0 10270-3 0 9030
2 25544 51
6420 45
5302 0002441 287
2214 72
8672 15
53772130 31376
Satellite: ISS
Catalog Number: 25544
Epoch time: 19014
52708283 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 45
5302 deg
Eccentricity:
0002441
Arg of perigee: 287
2214 deg
Mean anomaly: 72
8672 deg
Mean motion: 15
53772130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 280
Coasting Arc #5 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2019/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1734068
20 A = 6784301
71 meter
Y = 5345267
89 meter E =
0009280
Z = 3793429
34 I = 51
88851
XDOT = -6317
879818 Wp = 92
80169
YDOT = -966
142991 meter/sec RA = 40
05312 deg
ZDOT = 4240
064041 TA = 312
52256
MA = 312
60090
Ha = 220
860 n
mi
Hp = 216
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5689200
13 X = 1655740
75
Y = 17536968
14 feet Y = 5364221
32 meter
Z = 12445634
33 Z = 3801662
76
XDOT = -20727
952160 XDOT = -6327
202353
YDOT = -3169
760468 feet/sec YDOT = -1036
846246 meter/sec
ZDOT = 13910
971263 ZDOT = 4209
351612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13791059
10 X = -4203514
81
Y = 12198793
47 feet Y = 3718192
25 meter
Z = 12482074
77 Z = 3804536
39
XDOT = -4601
697899 XDOT = -1402
597520
YDOT = -19325
990766 feet/sec YDOT = -5890
561985 meter/sec
ZDOT = 13772
460937 ZDOT = 4197
846094
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
55616035
00016717 00000-0 10270-3 0 9048
2 25544 51
6401 40
4030 0002301 294
1862 65
9049 15
53746543 31536
Satellite: ISS
Catalog Number: 25544
Epoch time: 19015
55616035 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 40
4030 deg
Eccentricity:
0002301
Arg of perigee: 294
1862 deg
Mean anomaly: 65
9049 deg
Mean motion: 15
53746543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 278
Coasting Arc #6 (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 = -5936432
44 A = 6787014
29 meter
Y = -1568452
16 meter E =
0010891
Z = 2880370
15 I = 51
87930
XDOT = -973
125420 Wp = 98
24627
YDOT = -5665
809074 meter/sec RA = 36
39825 deg
ZDOT = -5075
968900 TA = 49
08108
MA = 48
98683
Ha = 220
803 n
mi
Hp = 216
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19476484
38 X = -5932443
53
Y = -5145840
41 feet Y = -1634815
35 meter
Z = 9450033
31 Z = 2851542
91
XDOT = -3192
668700 XDOT = -885
040301
YDOT = -18588
612446 feet/sec YDOT = -5676
198422 meter/sec
ZDOT = -16653
441273 ZDOT = -5080
482355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20202278
59 X = 6157654
51
Y = -345743
50 feet Y = -105382
62 meter
Z = 9320120
62 Z = 2840772
76
XDOT = 7981
448348 XDOT = 2432
745456
YDOT = 15584
667802 feet/sec YDOT = 4750
206746 meter/sec
ZDOT = -16673
037970 ZDOT = -5081
941973
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
26365000
00016717 00000-0 10270-3 0 9051
2 25544 51
6409 36
8754 0002471 283
2585 76
8292 15
53748716 31642
Satellite: ISS
Catalog Number: 25544
Epoch time: 19016
26365000 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 36
8754 deg
Eccentricity:
0002471
Arg of perigee: 283
2585 deg
Mean anomaly: 76
8292 deg
Mean motion: 15
53748716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 317
Coasting Arc #7 (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 = 6163032
09 A = 6789597
41 meter
Y = 2449842
90 meter E =
0008337
Z = -1432329
04 I = 51
86192
XDOT = -626
903651 Wp = 20
19301
YDOT = 4963
645519 meter/sec RA = 31
44114 deg
ZDOT = 5810
015391 TA = 324
23799
MA = 324
29379
Ha = 220
841 n
mi
Hp = 216
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20219921
57 X = 6142136
64
Y = 8037542
32 feet Y = 2518645
50 meter
Z = -4699242
24 Z = -1402442
05
XDOT = -2056
770509 XDOT = -710
583608
YDOT = 16284
926243 feet/sec YDOT = 4956
166698 meter/sec
ZDOT = 19061
730287 ZDOT = 5806
767299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21706912
66 X = -6616266
98
Y = -1871865
79 feet Y = -570544
69 meter
Z = -4564674
58 Z = -1391312
81
XDOT = -2729
897484 XDOT = -832
072753
YDOT = -14643
270531 feet/sec YDOT = -4463
268858 meter/sec
ZDOT = 19046
379877 ZDOT = 5805
336587
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
22840598
00016717 00000-0 10270-3 0 9069
2 25544 51
6422 32
0689 0002525 292
9268 67
1618 15
53753076 31793
Satellite: ISS
Catalog Number: 25544
Epoch time: 19017
22840598 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 32
0689 deg
Eccentricity:
0002525
Arg of perigee: 292
9268 deg
Mean anomaly: 67
1618 deg
Mean motion: 15
53753076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3179
Checksum: 326
Coasting Arc #8 (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 = -6010596
70 A = 6790363
35 meter
Y = -3144320
54 meter E =
0009436
Z = -169954
35 I = 51
83482
XDOT = 2326
401623 Wp = 141
27220
YDOT = -4131
558123 meter/sec RA = 26
48709 deg
ZDOT = -6025
220903 TA = 40
55336
MA = 40
48310
Ha = 220
793 n
mi
Hp = 216
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19719805
45 X = -5974163
77
Y = -10316012
26 feet Y = -3211331
49 meter
Z = -557593
00 Z = -199063
14
XDOT = 7632
551257 XDOT = 2401
695888
YDOT = -13554
980717 feet/sec YDOT = -4105
121097 meter/sec
ZDOT = -19767
785115 ZDOT = -6013
737740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21919039
61 X = 6680923
27
Y = 3831886
45 feet Y = 1167958
99 meter
Z = -688545
15 Z = -209868
56
XDOT = -2994
707012 XDOT = -912
786697
YDOT = 13677
199925 feet/sec YDOT = 4168
810537 meter/sec
ZDOT = -19715
373316 ZDOT = -6009
245787
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
25747813
00016717 00000-0 10270-3 0 9070
2 25544 51
6412 26
9421 0002459 294
8943 65
1953 15
53765995 31956
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
25747813 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 26
9421 deg
Eccentricity:
0002459
Arg of perigee: 294
8943 deg
Mean anomaly: 65
1953 deg
Mean motion: 15
53765995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3195
Checksum: 340
Coasting Arc #9 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/018/18:09:19
907
Vector Time (MET): N/A
Weight (LBS) : 929313
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1985793
94 A = 6780174
49 meter
Y = -3708264
46 meter E =
0010210
Z = -5326313
61 I = 51
77914
XDOT = 6908
307867 Wp = 86
96914
YDOT = 3296
327194 meter/sec RA = 23
84789 deg
ZDOT = 281
640757 TA = 185
70760
MA = 185
71925
Ha = 220
946 n
mi
Hp = 217
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6515071
99 X = 2052985
19
Y = -12166221
98 feet Y = -3685681
69 meter
Z = -17474782
17 Z = -5316504
66
XDOT = 22665
052056 XDOT = 6869
565934
YDOT = 10814
721766 feet/sec YDOT = 3373
364054 meter/sec
ZDOT = 924
018231 ZDOT = 315
104605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -173796
58 X = -52973
20
Y = -13856281
53 feet Y = -4223394
61 meter
Z = -17429985
35 Z = -5312659
53
XDOT = 24041
529992 XDOT = 7327
858342
YDOT = -1649
201451 feet/sec YDOT = -502
676602 meter/sec
ZDOT = 1074
604527 ZDOT = 327
539460
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
77201666
00016717 00000-0 10270-3 0 9089
2 25544 51
6413 24
3823 0004734 283
7007 76
3618 15
53172378 32030
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
77201666 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 24
3823 deg
Eccentricity:
0004734
Arg of perigee: 283
7007 deg
Mean anomaly: 76
3618 deg
Mean motion: 15
53172378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 303
Coasting Arc #10 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2019/019/18:09:19
907
Vector Time (MET): N/A
Weight (LBS) : 929313
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3254932
85 A = 6781240
41 meter
Y = 3112265
33 meter E =
0004620
Z = 5071334
03 I = 51
75188
XDOT = -6438
812124 Wp = 358
55429
YDOT = -3731
669608 meter/sec RA = 18
86817 deg
ZDOT = -1838
032132 TA = 109
24783
MA = 109
19784
Ha = 221
057 n
mi
Hp = 217
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10678913
54 X = -3314126
47
Y = 10210844
26 feet Y = 3075534
89 meter
Z = 16638235
01 Z = 5055379
62
XDOT = -21124
711692 XDOT = -6387
677016
YDOT = -12243
010526 feet/sec YDOT = -3803
386779 meter/sec
ZDOT = -6030
289147 ZDOT = -1869
185142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4164631
37 X = -1269379
64
Y = 14260509
53 feet Y = 4346603
30 meter
Z = 16565781
38 Z = 5049250
17
XDOT = -23341
070035 XDOT = -7114
358147
YDOT = 368
454611 feet/sec YDOT = 112
304966 meter/sec
ZDOT = -6170
380538 ZDOT = -1880
731988
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
80148956
00016717 00000-0 10270-3 0 9097
2 25544 51
6411 19
2583 0004940 287
3495 72
7117 15
53195864 32190
Satellite: ISS
Catalog Number: 25544
Epoch time: 19019
80148956 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 19
2583 deg
Eccentricity:
0004940
Arg of perigee: 287
3495 deg
Mean anomaly: 72
7117 deg
Mean motion: 15
53195864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 331
Coasting Arc #11 (Orbit 3222)
---------------------------------------
Vector Time (GMT): 2019/020/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929313
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1825433
90 A = 6780249
59 meter
Y = -3814950
60 meter E =
0010194
Z = -5308400
83 I = 51
73711
XDOT = 7153
419074 Wp = 89
90045
YDOT = 2686
402156 meter/sec RA = 17
44627 deg
ZDOT = 530
171995 TA = 185
15174
MA = 185
16223
Ha = 220
984 n
mi
Hp = 217
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5988956
37 X = 1893742
86
Y = -12516242
13 feet Y = -3794154
84 meter
Z = -17416013
21 Z = -5299368
21
XDOT = 23469
222684 XDOT = 7120
272085
YDOT = 8813
655366 feet/sec YDOT = 2766
211277 meter/sec
ZDOT = 1739
409431 ZDOT = 564
839749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13245638
47 X = -4037270
61
Y = 4302808
09 feet Y = 1311495
91 meter
Z = -17374703
90 Z = -5295809
75
XDOT = -9639
228247 XDOT = -2938
036770
YDOT = -22030
969588 feet/sec YDOT = -6715
039531 meter/sec
ZDOT = 1895
512589 ZDOT = 577
752237
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
05885833
00016717 00000-0 10270-3 0 9100
2 25544 51
6389 17
9725 0004586 283
6838 76
3803 15
53172584 32234
Satellite: ISS
Catalog Number: 25544
Epoch time: 19020
05885833 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 17
9725 deg
Eccentricity:
0004586
Arg of perigee: 283
6838 deg
Mean anomaly: 76
3803 deg
Mean motion: 15
53172584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3223
Checksum: 328
Coasting Arc #12 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2019/021/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929313
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3138291
90 A = 6781742
84 meter
Y = 3345670
84 meter E =
0004821
Z = 4995703
82 I = 51
70917
XDOT = -6672
362362 Wp = 10
55805
YDOT = -3152
581058 meter/sec RA = 12
46219 deg
ZDOT = -2075
304990 TA = 99
64607
MA = 99
59160
Ha = 221
256 n
mi
Hp = 217
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10296233
27 X = -3199736
65
Y = 10976610
37 feet Y = 3310232
28 meter
Z = 16390104
40 Z = 4980310
61
XDOT = -21890
952630 XDOT = -6626
532984
YDOT = -10343
113707 feet/sec YDOT = -3226
939631 meter/sec
ZDOT = -6808
743407 ZDOT = -2107
605001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15120404
81 X = 4608699
39
Y = -399854
90 feet Y = -121875
77 meter
Z = 16320152
92 Z = 4974382
61
XDOT = 8096
279405 XDOT = 2467
745963
YDOT = 21660
765015 feet/sec YDOT = 6602
201177 meter/sec
ZDOT = -6954
092227 ZDOT = -2119
607311
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
08833036
00016717 00000-0 10270-3 0 9113
2 25544 51
6385 12
8465 0004499 287
8130 72
2531 15
53132449 32395
Satellite: ISS
Catalog Number: 25544
Epoch time: 19021
08833036 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 12
8465 deg
Eccentricity:
0004499
Arg of perigee: 287
8130 deg
Mean anomaly: 72
2531 deg
Mean motion: 15
53132449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 302
Coasting Arc #13 (Orbit 3253)
---------------------------------------
Vector Time (GMT): 2019/022/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929313
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4329789
35 A = 6784233
62 meter
Y = -2897581
73 meter E =
0003969
Z = -4349462
06 I = 51
68583
XDOT = 5847
637931 Wp = 108
81747
YDOT = 3532
684929 meter/sec RA = 7
48246 deg
ZDOT = 3469
080229 TA = 196
41817
MA = 196
43103
Ha = 221
250 n
mi
Hp = 217
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14205345
62 X = 4382995
80
Y = -9506501
74 feet Y = -2848865
26 meter
Z = -14269888
65 Z = -4328301
11
XDOT = 19185
163816 XDOT = 5790
849463
YDOT = 11590
173652 feet/sec YDOT = 3597
759560 meter/sec
ZDOT = 11381
496815 ZDOT = 3497
347348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16889543
44 X = -5147932
84
Y = -3104351
25 feet Y = -946206
26 meter
Z = -14173971
48 Z = -4320226
51
XDOT = -5907
914493 XDOT = -1800
732338
YDOT = -20383
519241 feet/sec YDOT = -6212
896665 meter/sec
ZDOT = 11508
587942 ZDOT = 3507
817605
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
05345737
00016717 00000-0 10270-3 0 9128
2 25544 51
6392 8
0429 0004575 291
3786 68
6878 15
53164154 32540
Satellite: ISS
Catalog Number: 25544
Epoch time: 19022
05345737 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 8
0429 deg
Eccentricity:
0004575
Arg of perigee: 291
3786 deg
Mean anomaly: 68
6878 deg
Mean motion: 15
53164154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3254
Checksum: 322
Coasting Arc #14 (Orbit 3269)
---------------------------------------
Vector Time (GMT): 2019/023/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929313
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5343588
91 A = 6787404
62 meter
Y = 2448469
75 meter E =
0008489
Z = 3388709
45 I = 51
66335
XDOT = -4721
192029 Wp = 78
28142
YDOT = -3874
479897 meter/sec RA = 2
50591 deg
ZDOT = -4633
778837 TA = 62
16784
MA = 62
08184
Ha = 221
346 n
mi
Hp = 217
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17531459
68 X = -5387031
24
Y = 8033037
24 feet Y = 2388471
02 meter
Z = 11117813
14 Z = 3362647
60
XDOT = -15489
475162 XDOT = -4655
007944
YDOT = -12711
548219 feet/sec YDOT = -3926
905372 meter/sec
ZDOT = -15202
686473 ZDOT = -4656
551321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18349760
74 X = 5593007
07
Y = 6146314
69 feet Y = 1873396
72 meter
Z = 10999846
87 Z = 3352753
33
XDOT = 3015
686901 XDOT = 919
181367
YDOT = 18455
755043 feet/sec YDOT = 5625
314137 meter/sec
ZDOT = -15304
928503 ZDOT = -4664
942208
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 19023
08292650
00016717 00000-0 10270-3 0 9138
2 25544 51
6393 2
9178 0004607 294
2545 65
8126 15
53153792 32705
Satellite: ISS
Catalog Number: 25544
Epoch time: 19023
08292650 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 2
9178 deg
Eccentricity:
0004607
Arg of perigee: 294
2545 deg
Mean anomaly: 65
8126 deg
Mean motion: 15
53153792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3270
Checksum: 307
Coasting Arc #15 (Orbit 3284)
---------------------------------------
Vector Time (GMT): 2019/024/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929313
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6092290
54 A = 6790114
58 meter
Y = -2012551
48 meter E =
0006914
Z = -2209446
20 I = 51
64111
XDOT = 3364
585628 Wp =
74510
YDOT = 4187
949456 meter/sec RA = 357
53445 deg
ZDOT = 5469
659567 TA = 334
72132
MA = 334
75514
Ha = 221
509 n
mi
Hp = 217
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19987829
85 X = 6125074
65
Y = -6602859
17 feet Y = -1944239
93 meter
Z = -7248839
25 Z = -2179773
30
XDOT = 11038
666758 XDOT = 3290
936872
YDOT = 13739
991655 feet/sec YDOT = 4225
162802 meter/sec
ZDOT = 17945
077319 ZDOT = 5485
824157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19298910
99 X = -5882308
07
Y = -8520011
27 feet Y = -2596899
44 meter
Z = -7114647
19 Z = -2168544
46
XDOT = 478
163055 XDOT = 145
744099
YDOT = -16109
206673 feet/sec YDOT = -4910
086194 meter/sec
ZDOT = 18017
451962 ZDOT = 5491
719358
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 19024
04805097
00016717 00000-0 10270-3 0 9141
2 25544 51
6411 358
1137 0004648 299
6688 60
4001 15
53172687 32852
Satellite: ISS
Catalog Number: 25544
Epoch time: 19024
04805097 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 358
1137 deg
Eccentricity:
0004648
Arg of perigee: 299
6688 deg
Mean anomaly: 60
4001 deg
Mean motion: 15
53172687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3285
Checksum: 317
Coasting Arc #16 (Orbit 3300)
---------------------------------------
Vector Time (GMT): 2019/025/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929313
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6554534
02 A = 6791804
66 meter
Y = 1540379
23 meter E =
0008713
Z = 857620
03 I = 51
61305
XDOT = -1837
543333 Wp = 127
31967
YDOT = -4497
510383 meter/sec RA = 352
56637 deg
ZDOT = -5929
476941 TA = 43
40388
MA = 43
33531
Ha = 221
543 n
mi
Hp = 217
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21504376
71 X = -6575437
58
Y = 5053737
64 feet Y = 1466965
00 meter
Z = 2813714
02 Z = 825730
49
XDOT = -6028
685477 XDOT = -1758
312879
YDOT = -14755
611494 feet/sec YDOT = -4517
616160 meter/sec
ZDOT = -19453
664505 ZDOT = -5938
210336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19545410
25 X = 5957441
04
Y = 10331779
15 feet Y = 3149126
29 meter
Z = 2669596
60 Z = 813693
04
XDOT = -4496
209292 XDOT = -1370
444592
YDOT = 13574
849579 feet/sec YDOT = 4137
614152 meter/sec
ZDOT = -19492
460777 ZDOT = -5941
302045
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 19025
07751575
00016717 00000-0 10270-3 0 9157
2 25544 51
6404 352
9896 0004645 303
4948 56
5760 15
53180707 33017
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
07751575 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 352
9896 deg
Eccentricity:
0004645
Arg of perigee: 303
4948 deg
Mean anomaly: 56
5760 deg
Mean motion: 15
53180707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3301
Checksum: 318
Coasting Arc #17 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2019/025/12:55:30
000
Vector Time (MET): N/A
Weight (LBS) : 914879
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4051376
84 A = 6783088
98 meter
Y = 2966101
75 meter E =
0003965
Z = 4557313
78 I = 51
56764
XDOT = -6063
440241 Wp = 94
40431
YDOT = 3538
643412 meter/sec RA = 350
13635 deg
ZDOT = 3084
578061 TA = 324
68470
MA = 324
71096
Ha = 221
592 n
mi
Hp = 217
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13291918
76 X = 3995771
50
Y = 9731304
96 feet Y = 3011096
25 meter
Z = 14951816
87 Z = 4576858
34
XDOT = -19893
176645 XDOT = -6117
542567
YDOT = 11609
722481 feet/sec YDOT = 3470
535347 meter/sec
ZDOT = 10120
006761 ZDOT = 3054
993276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3161203
90 X = 963534
95
Y = 16085621
79 feet Y = 4902897
52 meter
Z = 15039607
37 Z = 4584072
33
XDOT = -21390
396550 XDOT = -6519
792869
YDOT = -5140
909520 feet/sec YDOT = -1566
949222 meter/sec
ZDOT = 9986
024074 ZDOT = 3043
740138
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 19025
59224657
00016717 00000-0 10270-3 0 9161
2 25544 51
6398 350
4317 0004970 309
1357 50
9353 15
53210893 33092
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
59224657 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 350
4317 deg
Eccentricity:
0004970
Arg of perigee: 309
1357 deg
Mean anomaly: 50
9353 deg
Mean motion: 15
53210893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 317
Coasting Arc #18 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2019/026/08:59:00
000
Vector Time (MET): N/A
Weight (LBS) : 914879
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4583677
07 A = 6783928
52 meter
Y = 2429604
64 meter E =
0005338
Z = 4366589
90 I = 51
54178
XDOT = -5462
135101 Wp = 87
67057
YDOT = 4160
569885 meter/sec RA = 345
97299 deg
ZDOT = 3415
314543 TA = 327
65098
MA = 327
68370
Ha = 221
787 n
mi
Hp = 217
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15038310
60 X = 4534957
78
Y = 7971143
84 feet Y = 2480590
18 meter
Z = 14326082
36 Z = 4388736
94
XDOT = -17920
390751 XDOT = -5524
843230
YDOT = 13650
163664 feet/sec YDOT = 4099
137915 meter/sec
ZDOT = 11205
100207 ZDOT = 3388
629620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10622663
52 X = -3237787
84
Y = 13190345
49 feet Y = 4020417
30 meter
Z = 14425684
08 Z = 4396948
51
XDOT = -9087
974993 XDOT = -2770
014778
YDOT = -19453
201365 feet/sec YDOT = -5929
335776 meter/sec
ZDOT = 11084
129505 ZDOT = 3378
442673
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 19026
42868633
00016717 00000-0 10270-3 0 9173
2 25544 51
6388 346
2678 0004848 313
5188 46
5561 15
53167193 33220
Satellite: ISS
Catalog Number: 25544
Epoch time: 19026
42868633 = yrday
fracday
Element set: 917
Inclination: 51
6388 deg
RA of node: 346
2678 deg
Eccentricity:
0004848
Arg of perigee: 313
5188 deg
Mean anomaly: 46
5561 deg
Mean motion: 15
53167193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3322
Checksum: 337
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