[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 14th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15204 0235 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 562 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
292/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 220
1
297/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 220
7
301/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 221
2
Coasting Arc #1 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2019/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5165202
69 A = 6793200
18 meter
Y = -1099545
31 meter E =
0011450
Z = -4280551
63 I = 51
93281
XDOT = -1597
545847 Wp = 105
89044
YDOT = 6551
794042 meter/sec RA = 128
57618 deg
ZDOT = -3621
757725 TA = 127
22229
MA = 127
11776
Ha = 229
214 n
mi
Hp = 219
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16946203
06 X = 5197907
25
Y = -3607432
12 feet Y = -1041601
86 meter
Z = -14043804
55 Z = -4255380
92
XDOT = -5241
292148 XDOT = -1653
098286
YDOT = 21495
387277 feet/sec YDOT = 6533
618242 meter/sec
ZDOT = -11882
407234 ZDOT = -3629
653653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14472727
25 X = -4411287
27
Y = 9692245
40 feet Y = 2954196
40 meter
Z = -13928975
41 Z = -4245551
70
XDOT = -2504
450521 XDOT = -763
356519
YDOT = -20815
745540 feet/sec YDOT = -6344
639241 meter/sec
ZDOT = -11918
761651 ZDOT = -3632
838551
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 19287
52282763
00016717 00000-0 10270-3 0 9009
2 25544 51
6385 129
5249 0006775 149
7252 210
4292 15
50191586 33767
Satellite: ISS
Catalog Number: 25544
Epoch time: 19287
52282763 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 129
5249 deg
Eccentricity:
0006775
Arg of perigee: 149
7252 deg
Mean anomaly: 210
4292 deg
Mean motion: 15
50191586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 330
Coasting Arc #2 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2019/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4965504
15 A = 6792446
12 meter
Y = 1112278
57 meter E =
0014779
Z = 4494552
98 I = 51
95045
XDOT = 1447
314345 Wp = 128
94169
YDOT = -6782
832322 meter/sec RA = 123
63982 deg
ZDOT = 3261
292558 TA = 288
26892
MA = 288
42969
Ha = 229
189 n
mi
Hp = 219
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16291024
13 X = -4999405
52
Y = 3649207
91 feet Y = 1056561
54 meter
Z = 14745908
72 Z = 4470349
39
XDOT = 4748
406645 XDOT = 1507
212424
YDOT = -22253
386883 feet/sec YDOT = -6766
312303 meter/sec
ZDOT = 10699
778734 ZDOT = 3268
469183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13688204
43 X = 4172164
71
Y = -9725834
37 feet Y = -2964434
32 meter
Z = 14635477
94 Z = 4460893
68
XDOT = 3618
867703 XDOT = 1103
030876
YDOT = 21324
893596 feet/sec YDOT = 6499
827568 meter/sec
ZDOT = 10732
884898 ZDOT = 3271
383317
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 19288
55427249
00016717 00000-0 10270-3 0 9014
2 25544 51
6389 124
4128 0006690 153
5493 206
6000 15
50174515 33922
Satellite: ISS
Catalog Number: 25544
Epoch time: 19288
55427249 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 124
4128 deg
Eccentricity:
0006690
Arg of perigee: 153
5493 deg
Mean anomaly: 206
6000 deg
Mean motion: 15
50174515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 310
Coasting Arc #3 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2019/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4779948
12 A = 6791507
23 meter
Y = -1040039
41 meter E =
0013027
Z = -4720874
13 I = 51
96436
XDOT = -1284
460516 Wp = 102
11873
YDOT = 6986
288251 meter/sec RA = 118
70321 deg
ZDOT = -2848
949116 TA = 139
72528
MA = 139
62870
Ha = 229
071 n
mi
Hp = 219
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15682244
50 X = 4814154
89
Y = -3412202
78 feet Y = -986395
61 meter
Z = -15488432
19 Z = -4697571
18
XDOT = -4214
109306 XDOT = -1348
648770
YDOT = 22920
893211 feet/sec YDOT = 6971
565475 meter/sec
ZDOT = -9346
945918 ZDOT = -2855
344939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13062298
58 X = -3981388
61
Y = 9499198
04 feet Y = 2895355
56 meter
Z = -15382101
43 Z = -4688464
51
XDOT = -4768
820859 XDOT = -1453
536598
YDOT = -21691
336210 feet/sec YDOT = -6611
519277 meter/sec
ZDOT = -9376
524210 ZDOT = -2857
964579
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 19289
52124806
00016717 00000-0 10270-3 0 9026
2 25544 51
6381 119
6195 0006797 156
3406 203
8058 15
50202293 34071
Satellite: ISS
Catalog Number: 25544
Epoch time: 19289
52124806 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 119
6195 deg
Eccentricity:
0006797
Arg of perigee: 156
3406 deg
Mean anomaly: 203
8058 deg
Mean motion: 15
50202293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 311
Coasting Arc #4 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2019/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4609095
20 A = 6790903
55 meter
Y = 988912
50 meter E =
0012981
Z = 4884759
19 I = 51
97679
XDOT = 1069
744944 Wp = 139
65909
YDOT = -7182
705697 meter/sec RA = 113
76861 deg
ZDOT = 2450
240494 TA = 286
32609
MA = 286
46880
Ha = 229
092 n
mi
Hp = 219
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15121703
40 X = -4643539
02
Y = 3244463
59 feet Y = 937177
88 meter
Z = 16026112
81 Z = 4862285
65
XDOT = 3509
661889 XDOT = 1138
082314
YDOT = -23565
307405 feet/sec YDOT = -7170
360894 meter/sec
ZDOT = 8038
846766 ZDOT = 2455
603216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12461846
34 X = 3798370
76
Y = -9336567
34 feet Y = -2845785
72 meter
Z = 15923556
32 Z = 4853499
97
XDOT = 6071
225890 XDOT = 1850
509651
YDOT = 21930
930030 feet/sec YDOT = 6684
547473 meter/sec
ZDOT = 8063
747542 ZDOT = 2457
830251
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 19290
55268921
00016717 00000-0 10270-3 0 9039
2 25544 51
6378 114
5078 0006745 159
9934 200
1482 15
50172617 34234
Satellite: ISS
Catalog Number: 25544
Epoch time: 19290
55268921 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 114
5078 deg
Eccentricity:
0006745
Arg of perigee: 159
9934 deg
Mean anomaly: 200
1482 deg
Mean motion: 15
50172617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 317
Coasting Arc #5 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2019/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4466688
60 A = 6790139
12 meter
Y = -862478
54 meter E =
0014717
Z = -5052219
13 I = 51
98677
XDOT = -844
509073 Wp = 103
38353
YDOT = 7335
929403 meter/sec RA = 108
83389 deg
ZDOT = -2007
187285 TA = 147
21601
MA = 147
12460
Ha = 228
960 n
mi
Hp = 219
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14654490
17 X = 4500542
58
Y = -2829654
00 feet Y = -812339
62 meter
Z = -16575522
07 Z = -5030438
87
XDOT = -2770
699059 XDOT = -916
728759
YDOT = 24068
009851 feet/sec YDOT = 7326
081687 meter/sec
ZDOT = -6585
260120 ZDOT = -2011
465154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12062600
73 X = -3676680
70
Y = 8974405
26 feet Y = 2735398
72 meter
Z = -16476124
24 Z = -5021922
67
XDOT = -7364
791871 XDOT = -2244
788562
YDOT = -21975
893548 feet/sec YDOT = -6698
252354 meter/sec
ZDOT = -6605
244731 ZDOT = -2013
278594
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 19291
51966310
00016717 00000-0 10270-3 0 9044
2 25544 51
6376 109
7154 0006941 163
2139 196
9242 15
50205626 34385
Satellite: ISS
Catalog Number: 25544
Epoch time: 19291
51966310 = yrday
fracday
Element set: 904
Inclination: 51
6376 deg
RA of node: 109
7154 deg
Eccentricity:
0006941
Arg of perigee: 163
2139 deg
Mean anomaly: 196
9242 deg
Mean motion: 15
50205626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 313
Coasting Arc #6 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2019/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4342818
03 A = 6789722
04 meter
Y = 761350
44 meter E =
0010969
Z = 5160844
40 I = 51
99546
XDOT = 578
906821 Wp = 149
76955
YDOT = -7477
288687 meter/sec RA = 103
89987 deg
ZDOT = 1579
552160 TA = 285
00746
MA = 285
12884
Ha = 228
959 n
mi
Hp = 219
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14248090
64 X = -4376077
94
Y = 2497868
89 feet Y = 712599
98 meter
Z = 16931904
19 Z = 5139667
40
XDOT = 1899
300594 XDOT = 654
804260
YDOT = -24531
787030 feet/sec YDOT = -7470
390582 meter/sec
ZDOT = 5182
257743 ZDOT = 1582
548632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11695294
03 X = 3564725
62
Y = -8702363
88 feet Y = -2652480
51 meter
Z = 16835253
95 Z = 5131385
41
XDOT = 8755
059532 XDOT = 2668
542145
YDOT = 21887
073396 feet/sec YDOT = 6671
179971 meter/sec
ZDOT = 5196
427613 ZDOT = 1583
871137
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 19292
55110165
00016717 00000-0 10270-3 0 9059
2 25544 51
6383 104
6035 0006825 167
2989 192
8335 15
50174734 34544
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
55110165 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 104
6035 deg
Eccentricity:
0006825
Arg of perigee: 167
2989 deg
Mean anomaly: 192
8335 deg
Mean motion: 15
50174734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 317
Coasting Arc #7 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2019/292/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4036470
87 A = 6788875
36 meter
Y = 1129345
11 meter E =
0017682
Z = -5354608
88 I = 51
99897
XDOT = -1776
214677 Wp = 113
85656
YDOT = 7437
501372 meter/sec RA = 102
12420 deg
ZDOT = 223
323107 TA = 158
30407
MA = 158
22907
Ha = 228
805 n
mi
Hp = 220
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13243014
67 X = 4049552
42
Y = 3705200
50 feet Y = 1174556
96 meter
Z = -17567614
42 Z = -5334969
05
XDOT = -5827
475973 XDOT = -1860
335762
YDOT = 24401
251220 feet/sec YDOT = 7417
168134 meter/sec
ZDOT = 732
687359 ZDOT = 214
490498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10681728
89 X = 3255790
96
Y = 8839891
17 feet Y = 2694398
83 meter
Z = -17478101
07 Z = -5327325
21
XDOT = -14648
342339 XDOT = -4464
814745
YDOT = 19109
869603 feet/sec YDOT = 5824
688255 meter/sec
ZDOT = 691
890758 ZDOT = 210
888303
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 19292
87342429
00016717 00000-0 10270-3 0 9065
2 25544 51
6417 103
0085 0006832 168
4577 191
6731 15
50187073 34596
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
87342429 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 103
0085 deg
Eccentricity:
0006832
Arg of perigee: 168
4577 deg
Mean anomaly: 191
6731 deg
Mean motion: 15
50187073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 325
Coasting Arc #8 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2019/293/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4023166
79 A = 6788874
48 meter
Y = -1274361
41 meter E =
0006547
Z = 5314052
97 I = 52
00498
XDOT = 1480
668245 Wp = 145
20125
YDOT = -7490
629651 meter/sec RA = 97
19147 deg
ZDOT = -680
157438 TA = 311
23505
MA = 311
29144
Ha = 228
783 n
mi
Hp = 220
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13199366
12 X = -4034430
61
Y = -4180975
77 feet Y = -1319414
33 meter
Z = 17434556
99 Z = 5294482
27
XDOT = 4857
835451 XDOT = 1567
624469
YDOT = -24575
556598 feet/sec YDOT = -7473
585566 meter/sec
ZDOT = -2231
487658 ZDOT = -672
753654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10604355
11 X = -3232207
44
Y = -9074887
62 feet Y = -2766025
75 meter
Z = 17345364
48 Z = 5286867
09
XDOT = 13472
953572 XDOT = 4106
556249
YDOT = -19912
911164 feet/sec YDOT = -6069
455323 meter/sec
ZDOT = -2197
185757 ZDOT = -669
702219
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 19293
90485799
00016717 00000-0 10270-3 0 9079
2 25544 51
6413 97
8979 0006766 171
3158 188
8111 15
50227017 34759
Satellite: ISS
Catalog Number: 25544
Epoch time: 19293
90485799 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 97
8979 deg
Eccentricity:
0006766
Arg of perigee: 171
3158 deg
Mean anomaly: 188
8111 deg
Mean motion: 15
50227017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 352
Coasting Arc #9 (Orbit 3489)
---------------------------------------
Vector Time (GMT): 2019/294/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4055041
51 A = 6789274
23 meter
Y = 1454771
93 meter E =
0017044
Z = -5261359
39 I = 52
00957
XDOT = -1188
452573 Wp = 121
34252
YDOT = 7470
121080 meter/sec RA = 92
25799 deg
ZDOT = 1143
655109 TA = 159
62618
MA = 159
55810
Ha = 228
591 n
mi
Hp = 220
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13303941
95 X = 4064029
51
Y = 4772873
79 feet Y = 1500168
51 meter
Z = -17261677
79 Z = -5241639
46
XDOT = -3899
122614 XDOT = -1277
452612
YDOT = 24508
271259 feet/sec YDOT = 7456
333337 meter/sec
ZDOT = 3752
149309 ZDOT = 1137
665800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10631560
81 X = 3240499
74
Y = 9478366
76 feet Y = 2889006
19 meter
Z = -17171813
94 Z = -5233968
89
XDOT = -12181
807920 XDOT = -3713
015054
YDOT = 20446
260946 feet/sec YDOT = 6232
020336 meter/sec
ZDOT = 3724
285410 ZDOT = 1135
162193
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 19294
87182781
00016717 00000-0 10270-3 0 9082
2 25544 51
6419 93
1059 0006733 175
2984 184
8231 15
50192460 34906
Satellite: ISS
Catalog Number: 25544
Epoch time: 19294
87182781 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 93
1059 deg
Eccentricity:
0006733
Arg of perigee: 175
2984 deg
Mean anomaly: 184
8231 deg
Mean motion: 15
50192460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3490
Checksum: 332
Coasting Arc #10 (Orbit 3505)
---------------------------------------
Vector Time (GMT): 2019/295/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4108259
91 A = 6789541
86 meter
Y = -1599404
20 meter E =
0005769
Z = 5158941
65 I = 52
01004
XDOT = 899
027269 Wp = 132
46735
YDOT = -7444
272518 meter/sec RA = 87
32543 deg
ZDOT = -1594
641702 TA = 332
82134
MA = 332
85152
Ha = 228
587 n
mi
Hp = 220
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13478543
01 X = -4115129
09
Y = -5247389
11 feet Y = -1645383
96 meter
Z = 16925661
57 Z = 5138968
41
XDOT = 2949
564530 XDOT = 989
950427
YDOT = -24423
466267 feet/sec YDOT = -7433
710610 meter/sec
ZDOT = -5231
764113 ZDOT = -1590
053528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10782463
26 X = -3286494
80
Y = -9798839
14 feet Y = -2986686
17 meter
Z = 16834650
91 Z = 5131201
60
XDOT = 10884
703440 XDOT = 3317
657609
YDOT = -20913
671712 feet/sec YDOT = -6374
487138 meter/sec
ZDOT = -5210
280909 ZDOT = -1588
093621
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 19295
90325938
00016717 00000-0 10270-3 0 9091
2 25544 51
6409 87
9948 0006712 178
0891 182
0286 15
50233162 35061
Satellite: ISS
Catalog Number: 25544
Epoch time: 19295
90325938 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 87
9948 deg
Eccentricity:
0006712
Arg of perigee: 178
0891 deg
Mean anomaly: 182
0286 deg
Mean motion: 15
50233162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3506
Checksum: 336
Coasting Arc #11 (Orbit 3520)
---------------------------------------
Vector Time (GMT): 2019/296/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4208257
07 A = 6790195
25 meter
Y = 1763292
02 meter E =
0015482
Z = -5042079
60 I = 52
01080
XDOT = -626
705236 Wp = 129
56323
YDOT = 7346
702339 meter/sec RA = 82
39231 deg
ZDOT = 2040
782336 TA = 160
24978
MA = 160
18976
Ha = 228
326 n
mi
Hp = 220
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13806617
70 X = 4212718
54
Y = 5785078
79 feet Y = 1810376
45 meter
Z = -16542255
91 Z = -5021626
50
XDOT = -2056
119540 XDOT = -718
724705
YDOT = 24103
354132 feet/sec YDOT = 7339
179652 meter/sec
ZDOT = 6695
480105 ZDOT = 2037
514193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11069507
27 X = 3373985
82
Y = 10228890
97 feet Y = 3117765
97 meter
Z = -16449068
60 Z = -5013676
11
XDOT = -9538
650067 XDOT = -2907
380540
YDOT = 21093
350002 feet/sec YDOT = 6429
253081 meter/sec
ZDOT = 6680
014706 ZDOT = 2036
068482
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 19296
87022451
00016717 00000-0 10270-3 0 9104
2 25544 51
6425 83
2026 0006583 182
8139 177
2975 15
50201472 35216
Satellite: ISS
Catalog Number: 25544
Epoch time: 19296
87022451 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 83
2026 deg
Eccentricity:
0006583
Arg of perigee: 182
8139 deg
Mean anomaly: 177
2975 deg
Mean motion: 15
50201472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3521
Checksum: 304
Coasting Arc #12 (Orbit 3536)
---------------------------------------
Vector Time (GMT): 2019/297/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4323668
74 A = 6790706
38 meter
Y = -1887345
09 meter E =
0006271
Z = 4878506
04 I = 52
00572
XDOT = 369
642051 Wp = 118
01015
YDOT = -7245
954185 meter/sec RA = 77
45955 deg
ZDOT = -2476
081217 TA = 356
18231
MA = 356
18710
Ha = 228
318 n
mi
Hp = 220
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14185264
89 X = -4325939
93
Y = -6192077
05 feet Y = -1935707
80 meter
Z = 16005597
24 Z = 4857497
61
XDOT = 1212
736387 XDOT = 462
668525
YDOT = -23772
815569 feet/sec YDOT = -7241
300594 meter/sec
ZDOT = -8123
626041 ZDOT = -2474
059223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11464234
70 X = -3494298
74
Y = -10544641
25 feet Y = -3214006
65 meter
Z = 15909888
90 Z = 4849334
14
XDOT = 8241
366167 XDOT = 2511
968408
YDOT = -21200
143603 feet/sec YDOT = -6461
803770 meter/sec
ZDOT = -8113
841720 ZDOT = -2473
098956
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 19297
90165158
00016717 00000-0 10270-3 0 9112
2 25544 51
6409 78
0909 0006523 185
4027 174
7054 15
50242034 35375
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
90165158 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 78
0909 deg
Eccentricity:
0006523
Arg of perigee: 185
4027 deg
Mean anomaly: 174
7054 deg
Mean motion: 15
50242034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3537
Checksum: 311
Coasting Arc #13 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2019/297/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1818957
60 A = 6794673
73 meter
Y = 5341758
25 meter E =
0013221
Z = 3782248
43 I = 52
01680
XDOT = -4446
733502 Wp = 125
96595
YDOT = -4549
186712 meter/sec RA = 77
24747 deg
ZDOT = 4268
437286 TA = 278
97543
MA = 279
12504
Ha = 228
146 n
mi
Hp = 220
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5967708
65 X = -1896927
80
Y = 17525453
57 feet Y = 5320981
65 meter
Z = 12408951
53 Z = 3773222
79
XDOT = -14589
020675 XDOT = -4416
266654
YDOT = -14925
153256 feet/sec YDOT = -4598
742612 meter/sec
ZDOT = 14004
059338 ZDOT = 4246
910721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6169157
87 X = -1880359
32
Y = 17485053
08 feet Y = 5329444
18 meter
Z = 12367358
54 Z = 3769570
88
XDOT = -13307
338329 XDOT = -4056
076723
YDOT = -14572
978477 feet/sec YDOT = -4441
843840 meter/sec
ZDOT = 13906
192542 ZDOT = 4238
607487
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 19297
96611577
00016717 00000-0 10270-3 0 9120
2 25544 51
6391 77
7719 0006537 187
2126 172
8931 15
50237040 35380
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
96611577 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 77
7719 deg
Eccentricity:
0006537
Arg of perigee: 187
2126 deg
Mean anomaly: 172
8931 deg
Mean motion: 15
50237040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 334
Coasting Arc #14 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2019/298/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1698576
45 A = 6793768
08 meter
Y = -5162076
42 meter E =
0007069
Z = -4079101
87 I = 52
00485
XDOT = 4683
445477 Wp = 125
40513
YDOT = 4626
394296 meter/sec RA = 72
31592 deg
ZDOT = -3913
184686 TA = 104
21442
MA = 104
13588
Ha = 228
127 n
mi
Hp = 220
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5572757
40 X = 1775988
41
Y = -16935946
27 feet Y = -5142649
19 meter
Z = -13382880
15 Z = -4070662
29
XDOT = 15365
634766 XDOT = 4650
372124
YDOT = 15178
458977 feet/sec YDOT = 4678
582690 meter/sec
ZDOT = -12838
532434 ZDOT = -3890
514519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5485301
43 X = 1671919
88
Y = -16995100
22 feet Y = -5180106
55 meter
Z = -13343965
64 Z = -4067240
73
XDOT = 14370
665132 XDOT = 4380
178732
YDOT = 14615
101348 feet/sec YDOT = 4454
682891 meter/sec
ZDOT = -12735
465362 ZDOT = -3881
769842
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 19298
93307951
00016717 00000-0 10270-3 0 9137
2 25544 51
6389 72
9791 0006477 189
7495 170
3529 15
50208562 35533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19298
93307951 = yrday
fracday
Element set: 913
Inclination: 51
6389 deg
RA of node: 72
9791 deg
Eccentricity:
0006477
Arg of perigee: 189
7495 deg
Mean anomaly: 170
3529 deg
Mean motion: 15
50208562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 354
Coasting Arc #15 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2019/299/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1577856
33 A = 6792790
29 meter
Y = 4996420
13 meter E =
0011971
Z = 4322162
91 I = 51
99153
XDOT = -4945
043691 Wp = 140
26613
YDOT = -4648
257406 meter/sec RA = 67
38458 deg
ZDOT = 3553
756605 TA = 273
59740
MA = 273
73430
Ha = 227
877 n
mi
Hp = 221
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5176693
99 X = -1654605
63
Y = 16392454
48 feet Y = 4978346
58 meter
Z = 14180324
50 Z = 4314311
35
XDOT = -16223
896625 XDOT = -4909
960573
YDOT = -15250
188341 feet/sec YDOT = -4703
359980 meter/sec
ZDOT = 11659
306446 ZDOT = 3529
820406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4816664
19 X = -1468119
25
Y = 16532895
68 feet Y = 5039226
60 meter
Z = 14144095
38 Z = 4311120
27
XDOT = -15512
286880 XDOT = -4728
145041
YDOT = -14441
371149 feet/sec YDOT = -4401
729926 meter/sec
ZDOT = 11550
479564 ZDOT = 3520
586171
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 19299
96450342
00016717 00000-0 10270-3 0 9145
2 25544 51
6397 67
8681 0006519 195
3375 164
7579 15
50249092 35692
Satellite: ISS
Catalog Number: 25544
Epoch time: 19299
96450342 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 67
8681 deg
Eccentricity:
0006519
Arg of perigee: 195
3375 deg
Mean anomaly: 164
7579 deg
Mean motion: 15
50249092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 361
Coasting Arc #16 (Orbit 3583)
---------------------------------------
Vector Time (GMT): 2019/300/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1525934
88 A = 6791961
45 meter
Y = -4795312
19 meter E =
0007771
Z = -4566438
52 I = 51
97551
XDOT = 5204
299672 Wp = 109
52595
YDOT = 4649
661362 meter/sec RA = 62
45013 deg
ZDOT = -3150
504197 TA = 129
02087
MA = 128
95166
Ha = 227
820 n
mi
Hp = 221
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5006348
03 X = 1601625
87
Y = -15732651
55 feet Y = -4777825
12 meter
Z = -14981753
67 Z = -4558841
82
XDOT = 17074
473990 XDOT = 5167
222831
YDOT = 15254
794496 feet/sec YDOT = 4707
652052 meter/sec
ZDOT = -10336
299859 ZDOT = -3125
313253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4396392
46 X = 1340020
42
Y = -15946815
48 feet Y = -4860589
36 meter
Z = -14946691
87 Z = -4555751
68
XDOT = 16647
998432 XDOT = 5074
309922
YDOT = 14149
183484 feet/sec YDOT = 4312
671126 meter/sec
ZDOT = -10221
765205 ZDOT = -3115
594034
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 19300
93146297
00016717 00000-0 10270-3 0 9157
2 25544 51
6406 63
0752 0006328 197
6919 162
4012 15
50220333 35848
Satellite: ISS
Catalog Number: 25544
Epoch time: 19300
93146297 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 63
0752 deg
Eccentricity:
0006328
Arg of perigee: 197
6919 deg
Mean anomaly: 162
4012 deg
Mean motion: 15
50220333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3584
Checksum: 299
Coasting Arc #17 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2019/301/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 66355
49 A = 6795062
70 meter
Y = 5744726
77 meter E =
0012026
Z = 3626933
77 I = 51
97902
XDOT = -5611
796438 Wp = 126
55520
YDOT = -2744
679254 meter/sec RA = 59
76047 deg
ZDOT = 4432
829934 TA = 276
10374
MA = 276
24076
Ha = 227
782 n
mi
Hp = 221
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 217701
73 X = -15506
79
Y = 18847528
79 feet Y = 5745011
22 meter
Z = 11899389
02 Z = 3627057
07
XDOT = -18411
405636 XDOT = -5602
220402
YDOT = -9004
853196 feet/sec YDOT = -2807
380623 meter/sec
ZDOT = 14543
405295 ZDOT = 4405
592503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6377375
40 X = -1943824
02
Y = -17737084
52 feet Y = -5406263
36 meter
Z = 11899458
39 Z = 3626954
92
XDOT = 19153
879880 XDOT = 5838
102587
YDOT = 2824
653463 feet/sec YDOT = 860
954376 meter/sec
ZDOT = 14419
379993 ZDOT = 4395
027022
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 19301
51163684
00016717 00000-0 10270-3 0 9162
2 25544 51
6421 60
1965 0006809 199
6610 160
4279 15
50256513 35935
Satellite: ISS
Catalog Number: 25544
Epoch time: 19301
51163684 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 60
1965 deg
Eccentricity:
0006809
Arg of perigee: 199
6610 deg
Mean anomaly: 160
4279 deg
Mean motion: 15
50256513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 311
Coasting Arc #18 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2019/302/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -134241
90 A = 6794154
81 meter
Y = -5536418
87 meter E =
0005730
Z = -3935540
52 I = 51
95782
XDOT = 5859
311406 Wp = 139
59997
YDOT = 2759
562423 meter/sec RA = 54
82772 deg
ZDOT = -4089
514987 TA = 87
75152
MA = 87
68591
Ha = 227
729 n
mi
Hp = 221
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -440426
18 X = -53204
85
Y = -18164103
90 feet Y = -5537466
98 meter
Z = -12911878
35 Z = -3935995
76
XDOT = 19223
462619 XDOT = 5847
882875
YDOT = 9053
682489 feet/sec YDOT = 2825
021444 meter/sec
ZDOT = -13417
043919 ZDOT = -4061
079594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6646377
12 X = 2025815
75
Y = 16908973
18 feet Y = 5153855
03 meter
Z = -12913463
73 Z = -3936023
75
XDOT = -20023
089990 XDOT = -6103
037829
YDOT = -2258
374704 feet/sec YDOT = -688
352610 meter/sec
ZDOT = -13287
565706 ZDOT = -4050
050027
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 19302
47859469
00016717 00000-0 10270-3 0 9172
2 25544 51
6420 55
4054 0006782 203
0519 157
0329 15
50227096 36087
Satellite: ISS
Catalog Number: 25544
Epoch time: 19302
47859469 = yrday
fracday
Element set: 917
Inclination: 51
6420 deg
RA of node: 55
4054 deg
Eccentricity:
0006782
Arg of perigee: 203
0519 deg
Mean anomaly: 157
0329 deg
Mean motion: 15
50227096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 313
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