[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 20th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14632 4598 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
292/21:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 219
9
297/21:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 220
7
301/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
9
000/00:00:00
000 0
0 0
0 221
2
304/19:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
3
000/00:00:00
000 0
0 0
0 221
8
305/15:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
2
000/00:00:00
000 0
0 0
0 221
9
Coasting Arc #1 (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 = 4467247
72 A = 6790156
91 meter
Y = -867305
35 meter E =
0014738
Z = -5050922
15 I = 51
98683
XDOT = -840
757730 Wp = 103
46985
YDOT = 7335
195179 meter/sec RA = 108
83372 deg
ZDOT = -2011
403230 TA = 147
08740
MA = 146
99555
Ha = 228
982 n
mi
Hp = 219
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14656324
54 X = 4501149
33
Y = -2845490
01 feet Y = -817159
92 meter
Z = -16571266
88 Z = -5029139
06
XDOT = -2758
391501 XDOT = -912
949005
YDOT = 24065
600981 feet/sec YDOT = 7325
389572 meter/sec
ZDOT = -6599
091962 ZDOT = -2015
662808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12057335
00 X = -3675075
71
Y = 8989448
64 feet Y = 2739983
95 meter
Z = -16471855
82 Z = -5020621
65
XDOT = -7373
811019 XDOT = -2247
537599
YDOT = -21968
711492 feet/sec YDOT = -6696
063263 meter/sec
ZDOT = -6618
993094 ZDOT = -2017
469095
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
51967086
00016717 00000-0 10270-3 0 9001
2 25544 51
6376 109
7153 0006977 163
0845 197
0540 15
50201437 34384
Satellite: ISS
Catalog Number: 25544
Epoch time: 19291
51967086 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 109
7153 deg
Eccentricity:
0006977
Arg of perigee: 163
0845 deg
Mean anomaly: 197
0540 deg
Mean motion: 15
50201437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 319
Coasting Arc #2 (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 = -4343338
58 A = 6789741
14 meter
Y = 768176
65 meter E =
0011021
Z = 5159408
66 I = 51
99553
XDOT = 573
871147 Wp = 149
71704
YDOT = -7476
411878 meter/sec RA = 103
89975 deg
ZDOT = 1585
522446 TA = 285
00099
MA = 285
12295
Ha = 228
981 n
mi
Hp = 219
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14249798
49 X = -4376667
81
Y = 2520264
59 feet Y = 719419
99 meter
Z = 16927193
78 Z = 5138228
97
XDOT = 1882
779354 XDOT = 649
730154
YDOT = -24528
910360 feet/sec YDOT = -7469
570300 meter/sec
ZDOT = 5201
845294 ZDOT = 1588
494362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11686698
83 X = 3562105
80
Y = -8723112
05 feet Y = -2658804
55 meter
Z = 16830530
78 Z = 5129945
78
XDOT = 8767
116328 XDOT = 2672
217057
YDOT = 21877
627161 feet/sec YDOT = 6668
300759 meter/sec
ZDOT = 5215
903097 ZDOT = 1589
807264
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
55111230
00016717 00000-0 10270-3 0 9019
2 25544 51
6383 104
6034 0006862 167
1695 192
9632 15
50170356 34544
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
55111230 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 104
6034 deg
Eccentricity:
0006862
Arg of perigee: 167
1695 deg
Mean anomaly: 192
9632 deg
Mean motion: 15
50170356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 297
Coasting Arc #3 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2019/292/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3973819
58 A = 6794262
29 meter
Y = 3834826
28 meter E =
0015200
Z = 3953765
06 I = 52
01675
XDOT = -1923
023093 Wp = 124
25585
YDOT = -6203
791330 meter/sec RA = 102
03151 deg
ZDOT = 4064
930652 TA = 283
35376
MA = 283
52318
Ha = 228
888 n
mi
Hp = 219
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13037465
82 X = -4035611
94
Y = 12581451
06 feet Y = 3790042
69 meter
Z = 12971670
16 Z = 3934311
31
XDOT = -6309
130882 XDOT = -1873
253129
YDOT = -20353
646096 feet/sec YDOT = -6225
017683 meter/sec
ZDOT = 13336
386654 ZDOT = 4055
709980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15985843
49 X = -4872485
09
Y = 8661542
99 feet Y = 2640038
30 meter
Z = 12882667
95 Z = 3926637
19
XDOT = -154
655902 XDOT = -47
139119
YDOT = -20154
864839 feet/sec YDOT = -6143
202803 meter/sec
ZDOT = 13294
746764 ZDOT = 4052
238814
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
93790075
00016717 00000-0 10270-3 0 9022
2 25544 51
6411 102
6891 0006894 166
5682 193
5653 15
50202666 34606
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
93790075 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 102
6891 deg
Eccentricity:
0006894
Arg of perigee: 166
5682 deg
Mean anomaly: 193
5653 deg
Mean motion: 15
50202666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3460
Checksum: 322
Coasting Arc #4 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2019/293/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3796361
28 A = 6793259
97 meter
Y = -3718365
84 meter E =
0009487
Z = -4236647
80 I = 52
02082
XDOT = 2116
441278 Wp = 115
47857
YDOT = 6361
947413 meter/sec RA = 97
10140 deg
ZDOT = -3697
584144 TA = 116
78803
MA = 116
69095
Ha = 228
767 n
mi
Hp = 220
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12455253
54 X = 3858238
56
Y = -12199363
01 feet Y = -3675566
24 meter
Z = -13899763
13 Z = -4218055
96
XDOT = 6943
704981 XDOT = 2063
103917
YDOT = 20872
530883 feet/sec YDOT = 6385
316754 meter/sec
ZDOT = -12131
181575 ZDOT = -3687
432610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15181818
06 X = 4627418
14
Y = -8707931
95 feet Y = -2654177
66 meter
Z = -13814685
49 Z = -4210716
14
XDOT = 996
103529 XDOT = 303
612356
YDOT = 20854
886876 feet/sec YDOT = 6356
569520 meter/sec
ZDOT = -12085
316650 ZDOT = -3683
604515
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
90487327
00016717 00000-0 10270-3 0 9034
2 25544 51
6426 97
8977 0006846 170
6875 189
4404 15
50212100 34757
Satellite: ISS
Catalog Number: 25544
Epoch time: 19293
90487327 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 97
8977 deg
Eccentricity:
0006846
Arg of perigee: 170
6875 deg
Mean anomaly: 189
4404 deg
Mean motion: 15
50212100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 335
Coasting Arc #5 (Orbit 3490)
---------------------------------------
Vector Time (GMT): 2019/294/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3621001
41 A = 6792468
70 meter
Y = 3622564
61 meter E =
0013760
Z = 4458765
33 I = 52
01908
XDOT = -2359
676702 Wp = 136
31563
YDOT = -6482
527349 meter/sec RA = 92
17089 deg
ZDOT = 3334
669832 TA = 280
09301
MA = 280
24821
Ha = 228
700 n
mi
Hp = 220
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11879925
88 X = -3682899
31
Y = 11885054
49 feet Y = 3581725
94 meter
Z = 14628495
19 Z = 4441025
31
XDOT = -7741
721464 XDOT = -2303
209986
YDOT = -21268
134348 feet/sec YDOT = -6508
599185 meter/sec
ZDOT = 10940
517821 ZDOT = 3323
344441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14402179
96 X = -4389784
45
Y = 8793939
19 feet Y = 2680392
66 meter
Z = 14547297
92 Z = 4434016
41
XDOT = -2044
429435 XDOT = -623
142092
YDOT = -21448
056010 feet/sec YDOT = -6537
367472 meter/sec
ZDOT = 10889
315264 ZDOT = 3319
063293
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
93631066
00016717 00000-0 10270-3 0 9040
2 25544 51
6406 92
7864 0006792 173
2904 186
8339 15
50202786 34911
Satellite: ISS
Catalog Number: 25544
Epoch time: 19294
93631066 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 92
7864 deg
Eccentricity:
0006792
Arg of perigee: 173
2904 deg
Mean anomaly: 186
8339 deg
Mean motion: 15
50202786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3491
Checksum: 335
Coasting Arc #6 (Orbit 3505)
---------------------------------------
Vector Time (GMT): 2019/295/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3497470
91 A = 6791570
78 meter
Y = -3462057
61 meter E =
0010567
Z = -4687628
68 I = 52
01715
XDOT = 2603
356882 Wp = 107
95222
YDOT = 6578
360792 meter/sec RA = 87
24004 deg
ZDOT = -2924
649885 TA = 133
09944
MA = 133
01098
Ha = 228
542 n
mi
Hp = 220
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11474642
11 X = 3558694
83
Y = -11358456
72 feet Y = -3422604
20 meter
Z = -15379359
17 Z = -4670490
33
XDOT = 8541
197121 XDOT = 2543
808721
YDOT = 21582
548529 feet/sec YDOT = 6607
140349 meter/sec
ZDOT = -9595
308023 ZDOT = -2912
148403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13744960
55 X = 4189463
97
Y = -8611903
47 feet Y = -2624908
18 meter
Z = -15300909
04 Z = -4663717
07
XDOT = 3148
850121 XDOT = 959
769517
YDOT = 21923
146361 feet/sec YDOT = 6682
175011 meter/sec
ZDOT = -9538
755131 ZDOT = -2907
412564
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
90328103
00016717 00000-0 10270-3 0 9054
2 25544 51
6414 87
9950 0006787 178
5256 181
5916 15
50211859 35065
Satellite: ISS
Catalog Number: 25544
Epoch time: 19295
90328103 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 87
9950 deg
Eccentricity:
0006787
Arg of perigee: 178
5256 deg
Mean anomaly: 181
5916 deg
Mean motion: 15
50211859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3506
Checksum: 333
Coasting Arc #7 (Orbit 3521)
---------------------------------------
Vector Time (GMT): 2019/296/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3380402
23 A = 6790878
21 meter
Y = 3325897
17 meter E =
0011855
Z = 4859568
46 I = 52
01127
XDOT = -2884
148992 Wp = 149
05654
YDOT = -6635
537781 meter/sec RA = 82
30753 deg
ZDOT = 2522
491616 TA = 276
18621
MA = 276
32126
Ha = 228
433 n
mi
Hp = 220
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11090558
50 X = -3440947
47
Y = 10911736
13 feet Y = 3287756
81 meter
Z = 15943466
07 Z = 4843000
37
XDOT = -9462
431077 XDOT = -2821
987116
YDOT = -21770
137076 feet/sec YDOT = -6667
442694 meter/sec
ZDOT = 8275
891128 ZDOT = 2508
632625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13133744
06 X = -4003165
19
Y = 8484336
17 feet Y = 2586025
66 meter
Z = 15867620
81 Z = 4836450
82
XDOT = -4409
169425 XDOT = -1343
914841
YDOT = -22263
631703 feet/sec YDOT = -6785
954943 meter/sec
ZDOT = 8213
157975 ZDOT = 2503
370551
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
93471440
00016717 00000-0 10270-3 0 9062
2 25544 51
6407 82
8827 0006629 181
4967 178
6164 15
50207087 35229
Satellite: ISS
Catalog Number: 25544
Epoch time: 19296
93471440 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 82
8827 deg
Eccentricity:
0006629
Arg of perigee: 181
4967 deg
Mean anomaly: 178
6164 deg
Mean motion: 15
50207087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3522
Checksum: 335
Coasting Arc #8 (Orbit 3536)
---------------------------------------
Vector Time (GMT): 2019/297/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3322921
33 A = 6790186
84 meter
Y = -3140250
62 meter E =
0012073
Z = -5029321
50 I = 52
00285
XDOT = 3155
238749 Wp = 105
57164
YDOT = 6656
588674 meter/sec RA = 77
37514 deg
ZDOT = -2078
894269 TA = 144
30820
MA = 144
22742
Ha = 228
300 n
mi
Hp = 220
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10901972
88 X = 3382219
53
Y = -10302659
52 feet Y = -3102760
12 meter
Z = -16500398
63 Z = -5013035
57
XDOT = 10351
833165 XDOT = 3090
666582
YDOT = 21839
201685 feet/sec YDOT = 6691
511608 meter/sec
ZDOT = -6820
519255 ZDOT = -2063
724349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12693999
87 X = 3869131
16
Y = -8143389
47 feet Y = -2482105
11 meter
Z = -16425849
64 Z = -5006598
97
XDOT = 5685
303705 XDOT = 1732
880569
YDOT = 22432
766879 feet/sec YDOT = 6837
507345 meter/sec
ZDOT = -6751
817863 ZDOT = -2057
954085
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
90168140
00016717 00000-0 10270-3 0 9071
2 25544 51
6402 78
0911 0006603 185
1551 174
9532 15
50209116 35376
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
90168140 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 78
0911 deg
Eccentricity:
0006603
Arg of perigee: 185
1551 deg
Mean anomaly: 174
9532 deg
Mean motion: 15
50209116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3537
Checksum: 301
Coasting Arc #9 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2019/297/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3015806
98 A = 6791050
06 meter
Y = 3716301
06 meter E =
0011576
Z = 4817066
48 I = 52
00420
XDOT = -3524
632068 Wp = 149
81799
YDOT = -6276
939200 meter/sec RA = 77
22456 deg
ZDOT = 2623
450577 TA = 274
36325
MA = 274
49551
Ha = 228
247 n
mi
Hp = 220
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9894379
85 X = -3080538
54
Y = 12192588
78 feet Y = 3682214
54 meter
Z = 15804023
89 Z = 4802259
18
XDOT = -11563
753505 XDOT = -3466
922987
YDOT = -20593
632546 feet/sec YDOT = -6316
031291 meter/sec
ZDOT = 8607
121314 ZDOT = 2606
469567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9814993
69 X = -2991610
08
Y = 12343572
65 feet Y = 3762320
94 meter
Z = 15736176
73 Z = 4796386
67
XDOT = -11031
972147 XDOT = -3362
545110
YDOT = -19699
054163 feet/sec YDOT = -6004
271709 meter/sec
ZDOT = 8530
127674 ZDOT = 2599
982915
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
96614629
00016717 00000-0 10270-3 0 9086
2 25544 51
6389 77
7716 0006495 186
4506 173
6562 15
50204542 35380
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
96614629 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 77
7716 deg
Eccentricity:
0006495
Arg of perigee: 186
4506 deg
Mean anomaly: 173
6562 deg
Mean motion: 15
50204542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 350
Coasting Arc #10 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2019/298/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2970132
52 A = 6790329
16 meter
Y = -3526675
21 meter E =
0011308
Z = -4993319
97 I = 51
99335
XDOT = 3795
934783 Wp = 105
33777
YDOT = 6278
396992 meter/sec RA = 72
29099 deg
ZDOT = -2183
413564 TA = 143
47746
MA = 143
40029
Ha = 228
144 n
mi
Hp = 220
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9744529
26 X = 3033603
28
Y = -11570456
74 feet Y = -3493106
56 meter
Z = -16382283
35 Z = -4978737
51
XDOT = 12453
854275 XDOT = 3736
051801
YDOT = 20598
415329 feet/sec YDOT = 6320
510835 meter/sec
ZDOT = -7163
430328 ZDOT = -2165
119901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9475466
40 X = 2888122
16
Y = -11884084
37 feet Y = -3622268
92 meter
Z = -16315471
27 Z = -4972955
64
XDOT = 12294
911295 XDOT = 3747
488963
YDOT = 19491
941298 feet/sec YDOT = 5941
143708 meter/sec
ZDOT = -7080
462073 ZDOT = -2158
124840
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
93311294
00016717 00000-0 10270-3 0 9097
2 25544 51
6389 72
9792 0006496 189
4874 170
6155 15
50208242 35536
Satellite: ISS
Catalog Number: 25544
Epoch time: 19298
93311294 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 72
9792 deg
Eccentricity:
0006496
Arg of perigee: 189
4874 deg
Mean anomaly: 170
6155 deg
Mean motion: 15
50208242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 347
Coasting Arc #11 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2019/299/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2930629
80 A = 6789770
90 meter
Y = 3365915
08 meter E =
0009631
Z = 5116987
03 I = 51
98094
XDOT = -4087
538416 Wp = 163
46634
YDOT = -6238
917474 meter/sec RA = 67
35723 deg
ZDOT = 1753
082662 TA = 269
59466
MA = 269
70502
Ha = 227
988 n
mi
Hp = 221
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9614927
17 X = -2992906
69
Y = 11043028
47 feet Y = 3332794
83 meter
Z = 16788015
19 Z = 5102599
32
XDOT = -13410
559109 XDOT = -4025
984932
YDOT = -20468
889351 feet/sec YDOT = -6284
282932 meter/sec
ZDOT = 5751
583537 ZDOT = 1733
376396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9169058
55 X = -2794729
05
Y = 11512277
75 feet Y = 3508942
26 meter
Z = 16722098
63 Z = 5096895
66
XDOT = -13606
832980 XDOT = -4147
362692
YDOT = -19108
709503 feet/sec YDOT = -5824
334657 meter/sec
ZDOT = 5662
185001 ZDOT = 1725
833988
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
96454263
00016717 00000-0 10270-3 0 9107
2 25544 51
6396 67
8679 0006456 194
5282 165
5684 15
50211873 35698
Satellite: ISS
Catalog Number: 25544
Epoch time: 19299
96454263 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 67
8679 deg
Eccentricity:
0006456
Arg of perigee: 194
5282 deg
Mean anomaly: 165
5684 deg
Mean motion: 15
50211873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 359
Coasting Arc #12 (Orbit 3583)
---------------------------------------
Vector Time (GMT): 2019/300/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2955679
67 A = 6789295
74 meter
Y = -3178383
79 meter E =
0012482
Z = -5230355
88 I = 51
96650
XDOT = 4355
155810 Wp = 107
11383
YDOT = 6160
716326 meter/sec RA = 62
42126 deg
ZDOT = -1288
747632 TA = 150
57788
MA = 150
50756
Ha = 227
843 n
mi
Hp = 221
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9697111
77 X = 3016408
46
Y = -10427768
33 feet Y = -3144991
99 meter
Z = -17159960
25 Z = -5215850
25
XDOT = 14288
568931 XDOT = 4292
201397
YDOT = 20212
323905 feet/sec YDOT = 6209
066691 meter/sec
ZDOT = -4228
174646 ZDOT = -1267
744551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9095217
46 X = 2772222
28
Y = -11060078
67 feet Y = -3371111
98 meter
Z = -17093514
67 Z = -5210103
27
XDOT = 14826
538433 XDOT = 4519
128914
YDOT = 18548
891097 feet/sec YDOT = 5653
702006 meter/sec
ZDOT = -4132
873345 ZDOT = -1259
699796
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
93150529
00016717 00000-0 10270-3 0 9116
2 25544 51
6407 63
0755 0006357 197
5592 162
5339 15
50215077 35842
Satellite: ISS
Catalog Number: 25544
Epoch time: 19300
93150529 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 63
0755 deg
Eccentricity:
0006357
Arg of perigee: 197
5592 deg
Mean anomaly: 162
5339 deg
Mean motion: 15
50215077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3584
Checksum: 312
Coasting Arc #13 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2019/301/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3184747
91 A = 6800613
78 meter
Y = 5997208
43 meter E =
0007698
Z = 342227
38 I = 51
99744
XDOT = -4314
350472 Wp = 75
62001
YDOT = 1941
117252 meter/sec RA = 59
77311 deg
ZDOT = 6021
537411 TA = 288
04244
MA = 288
12630
Ha = 227
853 n
mi
Hp = 221
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10448648
00 X = 3115786
29
Y = 19675880
69 feet Y = 6032436
96 meter
Z = 1122793
23 Z = 357530
42
XDOT = -14154
693149 XDOT = -4364
986083
YDOT = 6368
494921 feet/sec YDOT = 1892
588234 meter/sec
ZDOT = 19755
700167 ZDOT = 6000
456253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15696413
45 X = -4784266
82
Y = -15804325
66 feet Y = -4817158
46 meter
Z = 1192093
06 Z = 363349
96
XDOT = 10675
157302 XDOT = 3253
787946
YDOT = -9093
447412 feet/sec YDOT = -2771
682771 meter/sec
ZDOT = 19659
358335 ZDOT = 5992
172421
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
51168255
00016717 00000-0 10270-3 0 9127
2 25544 51
6422 60
1967 0006798 198
5681 161
5223 15
50234257 35933
Satellite: ISS
Catalog Number: 25544
Epoch time: 19301
51168255 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 60
1967 deg
Eccentricity:
0006798
Arg of perigee: 198
5681 deg
Mean anomaly: 161
5223 deg
Mean motion: 15
50234257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 314
Coasting Arc #14 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2019/302/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3377119
75 A = 6800394
58 meter
Y = -5841493
45 meter E =
0014668
Z = -770504
95 I = 51
97836
XDOT = 4453
931597 Wp = 164
09292
YDOT = -1791
922109 meter/sec RA = 54
84413 deg
ZDOT = -5976
868362 TA = 24
18754
MA = 24
11874
Ha = 227
684 n
mi
Hp = 221
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11079789
22 X = -3307804
69
Y = -19165004
75 feet Y = -5878871
23 meter
Z = -2527903
37 Z = -786741
80
XDOT = 14612
636474 XDOT = 4502
671523
YDOT = -5879
009544 feet/sec YDOT = -1741
842631 meter/sec
ZDOT = -19609
148170 ZDOT = -5955
113797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16401248
04 X = 4999100
40
Y = 14855332
75 feet Y = 4527905
42 meter
Z = -2601457
95 Z = -792924
38
XDOT = -11151
421088 XDOT = -3398
953148
YDOT = 8917
995445 feet/sec YDOT = 2718
205012 meter/sec
ZDOT = -19509
744035 ZDOT = -5946
569982
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
47864420
00016717 00000-0 10270-3 0 9131
2 25544 51
6416 55
4053 0006748 202
9397 157
1453 15
50239622 36082
Satellite: ISS
Catalog Number: 25544
Epoch time: 19302
47864420 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 55
4053 deg
Eccentricity:
0006748
Arg of perigee: 202
9397 deg
Mean anomaly: 157
1453 deg
Mean motion: 15
50239622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 307
Coasting Arc #15 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2019/303/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3573304
90 A = 6800053
34 meter
Y = 5664021
23 meter E =
0008667
Z = 1167461
66 I = 51
95866
XDOT = -4602
461451 Wp = 82
10516
YDOT = 1683
043050 meter/sec RA = 49
91342 deg
ZDOT = 5885
376070 TA = 290
48993
MA = 290
58295
Ha = 227
568 n
mi
Hp = 221
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11723441
27 X = 3504031
56
Y = 18582746
83 feet Y = 5703593
10 meter
Z = 3830254
80 Z = 1184651
75
XDOT = -15099
939144 XDOT = -4649
528331
YDOT = 5521
794782 feet/sec YDOT = 1631
311812 meter/sec
ZDOT = 19308
976609 ZDOT = 5862
904133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17067414
91 X = -5202148
06
Y = -13815138
91 feet Y = -4210854
34 meter
Z = 3908157
09 Z = 1191206
28
XDOT = 11626
066090 XDOT = 3543
624944
YDOT = -8896
819472 feet/sec YDOT = -2711
750575 meter/sec
ZDOT = 19206
306228 ZDOT = 5854
082138
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 19303
51006802
00016717 00000-0 10270-3 0 9140
2 25544 51
6431 50
2942 0006796 206
5443 153
5361 15
50241092 36244
Satellite: ISS
Catalog Number: 25544
Epoch time: 19303
51006802 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 50
2942 deg
Eccentricity:
0006796
Arg of perigee: 206
5443 deg
Mean anomaly: 153
5361 deg
Mean motion: 15
50241092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 278
Coasting Arc #16 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2019/304/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3711271
20 A = 6799555
32 meter
Y = -5463276
23 meter E =
0012124
Z = -1584684
02 I = 51
93501
XDOT = 4795
078348 Wp = 172
52839
YDOT = -1590
118791 meter/sec RA = 44
98116 deg
ZDOT = -5764
513851 TA = 24
70967
MA = 24
65164
Ha = 227
379 n
mi
Hp = 221
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12176086
63 X = -3642205
73
Y = -17924134
61 feet Y = -5504392
06 meter
Z = -5199094
54 Z = -1602544
84
XDOT = 15731
884343 XDOT = 4840
504605
YDOT = -5216
925168 feet/sec YDOT = -1536
242654 meter/sec
ZDOT = -18912
447019 ZDOT = -5741
110324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17496529
98 X = 5332942
34
Y = 12749692
66 feet Y = 3886106
32 meter
Z = -5280061
22 Z = -1609362
66
XDOT = -12222
794422 XDOT = -3725
507740
YDOT = 9007
731581 feet/sec YDOT = 2745
556586 meter/sec
ZDOT = -18805
532378 ZDOT = -5731
926269
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 19304
47702610
00016717 00000-0 10270-3 0 9157
2 25544 51
6435 45
5027 0006676 210
4223 149
6541 15
50242616 36391
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
47702610 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 45
5027 deg
Eccentricity:
0006676
Arg of perigee: 210
4223 deg
Mean anomaly: 149
6541 deg
Mean motion: 15
50242616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 292
Coasting Arc #17 (Orbit 3644)
---------------------------------------
Vector Time (GMT): 2019/304/19:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5287456
33 A = 6793181
97 meter
Y = -395399
70 meter E =
0006832
Z = 4239489
76 I = 51
90200
XDOT = -2476
271198 Wp = 111
19448
YDOT = -6257
429286 meter/sec RA = 43
09821 deg
ZDOT = -3669
639044 TA = 16
28697
MA = 16
26502
Ha = 227
320 n
mi
Hp = 221
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17347297
67 X = -5303235
42
Y = -1297243
10 feet Y = -454616
15 meter
Z = 13909087
13 Z = 4213766
37
XDOT = -8124
249338 XDOT = -2388
289303
YDOT = -20529
623643 feet/sec YDOT = -6284
628625 meter/sec
ZDOT = -12039
498176 ZDOT = -3681
454643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15247966
12 X = -4647580
07
Y = -8565086
30 feet Y = -2610638
31 meter
Z = 13791776
78 Z = 4203733
56
XDOT = 790
585056 XDOT = 240
970325
YDOT = -20892
184985 feet/sec YDOT = -6367
937983 meter/sec
ZDOT = -12092
807242 ZDOT = -3685
887647
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 19304
86380783
00016717 00000-0 10270-3 0 9164
2 25544 51
6408 43
5899 0006233 213
8986 146
1767 15
50242519 36459
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
86380783 = yrday
fracday
Element set: 916
Inclination: 51
6408 deg
RA of node: 43
5899 deg
Eccentricity:
0006233
Arg of perigee: 213
8986 deg
Mean anomaly: 146
1767 deg
Mean motion: 15
50242519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3645
Checksum: 337
Coasting Arc #18 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2019/305/15:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5818560
90 A = 6796527
24 meter
Y = -1529790
86 meter E =
0011120
Z = 3146501
10 I = 51
89421
XDOT = -1110
813053 Wp = 123
75179
YDOT = -5812
354525 meter/sec RA = 38
94587 deg
ZDOT = -4873
695611 TA = 20
16457
MA = 20
12068
Ha = 227
196 n
mi
Hp = 221
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19089766
74 X = -5816306
13
Y = -5018998
87 feet Y = -1594845
63 meter
Z = 10323166
33 Z = 3118241
60
XDOT = -3644
399779 XDOT = -1022
060914
YDOT = -19069
404609 feet/sec YDOT = -5824
279982 meter/sec
ZDOT = -15989
814997 ZDOT = -4878
876289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2129255
00 X = 648996
92
Y = -19690552
05 feet Y = -6001680
27 meter
Z = 10194397
49 Z = 3107252
36
XDOT = 16901
653857 XDOT = 5151
624096
YDOT = -6473
580248 feet/sec YDOT = -1973
147260 meter/sec
ZDOT = -16012
889222 ZDOT = -4880
728635
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 19305
70183606
00016717 00000-0 10270-3 0 9174
2 25544 51
6428 39
4371 0006265 216
2934 143
7793 15
50257685 36581
Satellite: ISS
Catalog Number: 25544
Epoch time: 19305
70183606 = yrday
fracday
Element set: 917
Inclination: 51
6428 deg
RA of node: 39
4371 deg
Eccentricity:
0006265
Arg of perigee: 216
2934 deg
Mean anomaly: 143
7793 deg
Mean motion: 15
50257685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 329
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