[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 28th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19912 1579 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
130/00:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
7
132/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 222
6
Coasting Arc #1 (Orbit 2414)
---------------------------------------
Vector Time (GMT): 2020/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3194294
08 A = 6791521
83 meter
Y = 2870450
67 meter E =
0013890
Z = -5273410
79 I = 51
29018
XDOT = -4453
485423 Wp = 91
14968
YDOT = -6184
371174 meter/sec RA = 238
28482 deg
ZDOT = -670
485613 TA = 172
41222
MA = 172
39118
Ha = 228
413 n
mi
Hp = 222
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10479967
44 X = -3200539
35
Y = 9417489
09 feet Y = 2834695
21 meter
Z = -17301216
50 Z = -5288942
61
XDOT = -14611
172648 XDOT = -4380
742083
YDOT = -20289
931673 feet/sec YDOT = -6233
766440 meter/sec
ZDOT = -2199
755948 ZDOT = -691
942889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3078880
81 X = -938442
87
Y = 13658914
18 feet Y = 4163237
04 meter
Z = -17372549
24 Z = -5295153
01
XDOT = -22603
059313 XDOT = -6889
412479
YDOT = -8010
137918 feet/sec YDOT = -2441
490037 meter/sec
ZDOT = -2297
907915 ZDOT = -700
402332
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 20118
51734906
00016717 00000-0 10270-3 0 9004
2 25544 51
6428 239
2547 0001712 201
5801 158
5277 15
49331711 24150
Satellite: ISS
Catalog Number: 25544
Epoch time: 20118
51734906 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 239
2547 deg
Eccentricity:
0001712
Arg of perigee: 201
5801 deg
Mean anomaly: 158
5277 deg
Mean motion: 15
49331711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2415
Checksum: 288
Coasting Arc #2 (Orbit 2430)
---------------------------------------
Vector Time (GMT): 2020/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3021626
01 A = 6791378
89 meter
Y = -3019930
77 meter E =
0003238
Z = 5278103
65 I = 51
30819
XDOT = 4906
649326 Wp = 146
32889
YDOT = 5860
218483 meter/sec RA = 233
31238 deg
ZDOT = 541
214154 TA = 298
46267
MA = 298
49529
Ha = 228
199 n
mi
Hp = 222
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9913471
17 X = 3029532
96
Y = -9907909
34 feet Y = -2986096
95 meter
Z = 17316613
02 Z = 5292800
65
XDOT = 16097
930858 XDOT = 4838
125022
YDOT = 19226
438593 feet/sec YDOT = 5914
704945 meter/sec
ZDOT = 1775
636987 ZDOT = 564
882924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2096805
98 X = 639106
46
Y = -13773315
14 feet Y = -4198106
45 meter
Z = 17384126
65 Z = 5298681
80
XDOT = 23312
266268 XDOT = 7105
578759
YDOT = 5938
426261 feet/sec YDOT = 1810
032324 meter/sec
ZDOT = 1883
965710 ZDOT = 574
232749
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 20119
54937480
00016717 00000-0 10270-3 0 9011
2 25544 51
6423 234
1470 0001751 208
1070 151
9986 15
49359091 24311
Satellite: ISS
Catalog Number: 25544
Epoch time: 20119
54937480 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 234
1470 deg
Eccentricity:
0001751
Arg of perigee: 208
1070 deg
Mean anomaly: 151
9986 deg
Mean motion: 15
49359091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2431
Checksum: 296
Coasting Arc #3 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2020/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2863303
24 A = 6791412
26 meter
Y = 3160184
41 meter E =
0013837
Z = -5297630
17 I = 51
32926
XDOT = -5314
578456 Wp = 92
76713
YDOT = -5488
485971 meter/sec RA = 228
34264 deg
ZDOT = -403
142376 TA = 173
37206
MA = 173
35374
Ha = 228
304 n
mi
Hp = 222
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9394039
50 X = -2872695
57
Y = 10368059
07 feet Y = 3128112
75 meter
Z = -17380676
40 Z = -5311561
64
XDOT = -17436
281022 XDOT = -5250
851345
YDOT = -18006
843738 feet/sec YDOT = -5547
561020 meter/sec
ZDOT = -1322
645590 ZDOT = -428
804239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1167467
40 X = -355844
06
Y = 13861906
89 feet Y = 4225109
22 meter
Z = -17444686
77 Z = -5317140
53
XDOT = -23744
117747 XDOT = -7237
207089
YDOT = -3805
678336 feet/sec YDOT = -1159
970757 meter/sec
ZDOT = -1440
154456 ZDOT = -438
959078
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 20120
51689833
00016717 00000-0 10270-3 0 9027
2 25544 51
6425 229
3601 0001710 211
2033 148
9016 15
49335550 24464
Satellite: ISS
Catalog Number: 25544
Epoch time: 20120
51689833 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 229
3601 deg
Eccentricity:
0001710
Arg of perigee: 211
2033 deg
Mean anomaly: 148
9016 deg
Mean motion: 15
49335550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2446
Checksum: 275
Coasting Arc #4 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2020/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2686487
20 A = 6791258
99 meter
Y = -3289959
11 meter E =
0002439
Z = 5297910
17 I = 51
35291
XDOT = 5711
706328 Wp = 144
27012
YDOT = 5100
288387 meter/sec RA = 223
37255 deg
ZDOT = 268
915720 TA = 303
14258
MA = 303
16598
Ha = 228
089 n
mi
Hp = 222
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8813934
39 X = 2697342
57
Y = -10793829
09 feet Y = -3259856
51 meter
Z = 17381595
04 Z = 5310986
28
XDOT = 18739
193990 XDOT = 5652
942646
YDOT = 16733
229617 feet/sec YDOT = 5163
832167 meter/sec
ZDOT = 882
269421 ZDOT = 296
518580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 209588
08 X = 63882
45
Y = -13858413
88 feet Y = -4224044
55 meter
Z = 17441687
69 Z = 5316226
41
XDOT = 24052
830735 XDOT = 7331
302808
YDOT = 1641
554738 feet/sec YDOT = 500
345884 meter/sec
ZDOT = 1008
721990 ZDOT = 307
458463
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 20121
54891719
00016717 00000-0 10270-3 0 9030
2 25544 51
6430 224
2519 0001706 217
6807 142
4224 15
49373249 24621
Satellite: ISS
Catalog Number: 25544
Epoch time: 20121
54891719 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 224
2519 deg
Eccentricity:
0001706
Arg of perigee: 217
6807 deg
Mean anomaly: 142
4224 deg
Mean motion: 15
49373249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 295
Coasting Arc #5 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2020/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2523404
84 A = 6791342
63 meter
Y = 3415233
53 meter E =
0013787
Z = -5312037
20 I = 51
37796
XDOT = -6057
142343 Wp = 93
71274
YDOT = -4671
854718 meter/sec RA = 218
40558 deg
ZDOT = -127
450719 TA = 175
07226
MA = 175
05868
Ha = 228
204 n
mi
Hp = 222
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8278887
27 X = -2535604
59
Y = 11204834
40 feet Y = 3386947
02 meter
Z = -17427943
56 Z = -5324324
41
XDOT = -19872
514250 XDOT = -6003
831018
YDOT = -15327
607342 feet/sec YDOT = -4739
291906 meter/sec
ZDOT = -418
145404 ZDOT = -156
744681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 703536
64 X = 214437
97
Y = 13842743
77 feet Y = 4219268
30 meter
Z = -17484421
24 Z = -5329251
60
XDOT = -24078
082330 XDOT = -7338
999494
YDOT = 530
811843 feet/sec YDOT = 161
791450 meter/sec
ZDOT = -552
396808 ZDOT = -168
370547
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 20122
51643336
00016717 00000-0 10270-3 0 9049
2 25544 51
6429 219
4646 0001550 222
8301 137
2728 15
49340775 24775
Satellite: ISS
Catalog Number: 25544
Epoch time: 20122
51643336 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 219
4646 deg
Eccentricity:
0001550
Arg of perigee: 222
8301 deg
Mean anomaly: 137
2728 deg
Mean motion: 15
49340775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 298
Coasting Arc #6 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2020/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2344143
28 A = 6791212
58 meter
Y = -3528166
99 meter E =
0001707
Z = 5307171
01 I = 51
40502
XDOT = 6388
871872 Wp = 132
99400
YDOT = 4229
711739 meter/sec RA = 213
43956 deg
ZDOT = -11
182032 TA = 317
10633
MA = 317
11964
Ha = 228
024 n
mi
Hp = 222
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7690758
79 X = 2357642
82
Y = -11575351
00 feet Y = -3501877
75 meter
Z = 17411978
39 Z = 5318590
67
XDOT = 20960
865721 XDOT = 6341
153464
YDOT = 13877
007019 feet/sec YDOT = 4300
889841 meter/sec
ZDOT = -36
686458 ZDOT = 19
736855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1630215
98 X = -496889
83
Y = -13734915
68 feet Y = -4186402
30 meter
Z = 17464478
25 Z = 5323172
97
XDOT = 23977
042156 XDOT = 7308
202449
YDOT = -2707
545484 feet/sec YDOT = -825
259864 meter/sec
ZDOT = 105
058943 ZDOT = 32
021966
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 20123
54844637
00016717 00000-0 10270-3 0 9051
2 25544 51
6429 214
3570 0001589 226
9110 133
1907 15
49378455 24938
Satellite: ISS
Catalog Number: 25544
Epoch time: 20123
54844637 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 214
3570 deg
Eccentricity:
0001589
Arg of perigee: 226
9110 deg
Mean anomaly: 133
1907 deg
Mean motion: 15
49378455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 313
Coasting Arc #7 (Orbit 2507)
---------------------------------------
Vector Time (GMT): 2020/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2174836
11 A = 6791340
33 meter
Y = 3641916
36 meter E =
0013642
Z = -5315493
67 I = 51
43329
XDOT = -6664
448675 Wp = 95
36111
YDOT = -3754
258632 meter/sec RA = 208
47617 deg
ZDOT = 153
621295 TA = 176
11576
MA = 176
10516
Ha = 228
125 n
mi
Hp = 222
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7135289
08 X = -2189579
71
Y = 11948544
48 feet Y = 3617513
39 meter
Z = -17439283
70 Z = -5326094
01
XDOT = -21864
989090 XDOT = -6622
718334
YDOT = -12317
121496 feet/sec YDOT = -3828
551913 meter/sec
ZDOT = 504
006874 ZDOT = 121
349193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2530496
79 X = 771295
42
Y = 13622562
20 feet Y = 4152156
96 meter
Z = -17488026
38 Z = -5330350
44
XDOT = -23595
869618 XDOT = -7192
021060
YDOT = 4843
957788 feet/sec YDOT = 1476
438334 meter/sec
ZDOT = 356
016103 ZDOT = 108
513708
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 20124
51595839
00016717 00000-0 10270-3 0 9067
2 25544 51
6424 209
5696 0001560 232
4101 127
6907 15
49339752 25081
Satellite: ISS
Catalog Number: 25544
Epoch time: 20124
51595839 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 209
5696 deg
Eccentricity:
0001560
Arg of perigee: 232
4101 deg
Mean anomaly: 127
6907 deg
Mean motion: 15
49339752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2508
Checksum: 312
Coasting Arc #8 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2020/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1993113
44 A = 6791218
09 meter
Y = -3740703
68 meter E =
0001170
Z = 5305168
11 I = 51
46454
XDOT = 6923
173804 Wp = 106
81073
YDOT = 3269
390876 meter/sec RA = 203
51402 deg
ZDOT = -295
997881 TA = 346
01848
MA = 346
02171
Ha = 227
945 n
mi
Hp = 222
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6539086
10 X = 2009025
25
Y = -12272649
86 feet Y = -3718326
29 meter
Z = 17405407
17 Z = 5314888
61
XDOT = 22713
824815 XDOT = 6887
537762
YDOT = 10726
348019 feet/sec YDOT = 3346
611481 meter/sec
ZDOT = -971
121656 ZDOT = -262
454055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3424386
70 X = -1043753
07
Y = -13419867
37 feet Y = -4090375
58 meter
Z = 17450115
06 Z = 5318795
07
XDOT = 23091
248150 XDOT = 7038
212436
YDOT = -6953
783781 feet/sec YDOT = -2119
513297 meter/sec
ZDOT = -817
262136 ZDOT = -249
101499
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 20125
54796583
00016717 00000-0 10270-3 0 9071
2 25544 51
6435 204
4619 0001567 238
2953 121
8045 15
49383414 25249
Satellite: ISS
Catalog Number: 25544
Epoch time: 20125
54796583 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 204
4619 deg
Eccentricity:
0001567
Arg of perigee: 238
2953 deg
Mean anomaly: 121
8045 deg
Mean motion: 15
49383414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 314
Coasting Arc #9 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2020/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1817673
64 A = 6791379
96 meter
Y = 3843853
31 meter E =
0013523
Z = -5307394
95 I = 51
49498
XDOT = -7122
072348 Wp = 96
28823
YDOT = -2759
756907 meter/sec RA = 198
55456 deg
ZDOT = 439
943873 TA = 177
92857
MA = 177
92297
Ha = 228
081 n
mi
Hp = 222
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5963496
20 X = -1834740
99
Y = 12611067
29 feet Y = 3823431
39 meter
Z = -17412713
08 Z = -5316266
06
XDOT = -23366
379093 XDOT = -7092
819626
YDOT = -9054
320560 feet/sec YDOT = -2839
237430 meter/sec
ZDOT = 1443
385410 ZDOT = 405
418163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4306710
01 X = 1312685
21
Y = 13214821
55 feet Y = 4027877
61 meter
Z = -17453527
51 Z = -5319835
19
XDOT = -22320
332856 XDOT = -6803
237455
YDOT = 8973
423424 feet/sec YDOT = 2735
099460 meter/sec
ZDOT = 1284
988220 ZDOT = 391
664410
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 20126
51547234
00016717 00000-0 10270-3 0 9087
2 25544 51
6425 199
6743 0001410 245
3836 114
7168 15
49342221 25391
Satellite: ISS
Catalog Number: 25544
Epoch time: 20126
51547234 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 199
6743 deg
Eccentricity:
0001410
Arg of perigee: 245
3836 deg
Mean anomaly: 114
7168 deg
Mean motion: 15
49342221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 302
Coasting Arc #10 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2020/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1632581
51 A = 6791293
66 meter
Y = -3930841
49 meter E =
0001367
Z = 5290900
92 I = 51
52713
XDOT = 7302
501213 Wp = 68
26639
YDOT = 2244
626118 meter/sec RA = 193
59739 deg
ZDOT = -585
041005 TA = 27
33409
MA = 27
32690
Ha = 227
940 n
mi
Hp = 222
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5356238
54 X = 1650715
35
Y = -12896461
58 feet Y = -3912483
54 meter
Z = 17358598
83 Z = 5298875
46
XDOT = 23958
337312 XDOT = 7279
700247
YDOT = 7364
258918 feet/sec YDOT = 2326
160412 meter/sec
ZDOT = -1919
425870 ZDOT = -549
622970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5168546
61 X = -1575373
01
Y = -12923562
30 feet Y = -3939101
79 meter
Z = 17395304
81 Z = 5302088
90
XDOT = 21435
181401 XDOT = 6533
443291
YDOT = -10940
149814 feet/sec YDOT = -3334
557663 meter/sec
ZDOT = -1756
901079 ZDOT = -535
503449
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 20127
54747582
00016717 00000-0 10270-3 0 9090
2 25544 51
6423 194
5673 0001442 247
9801 112
1196 15
49383193 25554
Satellite: ISS
Catalog Number: 25544
Epoch time: 20127
54747582 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 194
5673 deg
Eccentricity:
0001442
Arg of perigee: 247
9801 deg
Mean anomaly: 112
1196 deg
Mean motion: 15
49383193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 318
Coasting Arc #11 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2020/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1447912
35 A = 6791481
70 meter
Y = 4024718
70 meter E =
0013335
Z = -5287011
83 I = 51
55908
XDOT = -7421
002909 Wp = 97
95742
YDOT = -1712
649254 meter/sec RA = 188
64189 deg
ZDOT = 728
360063 TA = 179
02518
MA = 179
02258
Ha = 228
061 n
mi
Hp = 222
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4750368
60 X = -1467128
54
Y = 13204457
67 feet Y = 4008419
96 meter
Z = -17345839
33 Z = -5294091
81
XDOT = -24347
122405 XDOT = -7404
838039
YDOT = -5618
928000 feet/sec YDOT = -1795
545847 meter/sec
ZDOT = 2389
632752 ZDOT = 692
350171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6036615
66 X = 1839960
45
Y = 12623417
35 feet Y = 3847617
61 meter
Z = -17378447
92 Z = -5296950
93
XDOT = -20304
994393 XDOT = -6188
962291
YDOT = 12773
246738 feet/sec YDOT = 3893
285606 meter/sec
ZDOT = 2224
355971 ZDOT = 677
983700
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 20128
51497956
00016717 00000-0 10270-3 0 9107
2 25544 51
6411 189
7792 0001371 253
1509 106
9491 15
49342235 25702
Satellite: ISS
Catalog Number: 25544
Epoch time: 20128
51497956 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 189
7792 deg
Eccentricity:
0001371
Arg of perigee: 253
1509 deg
Mean anomaly: 106
9491 deg
Mean motion: 15
49342235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 313
Coasting Arc #12 (Orbit 2585)
---------------------------------------
Vector Time (GMT): 2020/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1258368
06 A = 6791414
26 meter
Y = -4100852
46 meter E =
0002035
Z = 5264091
26 I = 51
59301
XDOT = 7519
666448 Wp = 48
80564
YDOT = 1180
815245 meter/sec RA = 183
68863 deg
ZDOT = -876
143161 TA = 49
59398
MA = 49
57623
Ha = 227
938 n
mi
Hp = 222
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4128504
15 X = 1278561
07
Y = -13454240
37 feet Y = -4086668
05 meter
Z = 17270640
63 Z = 5270252
73
XDOT = 24670
821680 XDOT = 7510
159224
YDOT = 3874
065764 feet/sec YDOT = 1264
852423 meter/sec
ZDOT = -2874
485435 ZDOT = -839
637870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6864752
83 X = -2092376
66
Y = -12245590
16 feet Y = -3732455
88 meter
Z = 17299041
83 Z = 5272747
95
XDOT = 19077
227754 XDOT = 5814
739019
YDOT = -14525
548673 feet/sec YDOT = -4427
387236 meter/sec
ZDOT = -2706
895014 ZDOT = -825
061600
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 20129
54697815
00016717 00000-0 10270-3 0 9118
2 25544 51
6413 184
6717 0001360 259
5067 100
5930 15
49386791 25862
Satellite: ISS
Catalog Number: 25544
Epoch time: 20129
54697815 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 184
6717 deg
Eccentricity:
0001360
Arg of perigee: 259
5067 deg
Mean anomaly: 100
5930 deg
Mean motion: 15
49386791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2586
Checksum: 324
Coasting Arc #13 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2020/130/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6597586
13 A = 6802694
81 meter
Y = 1092196
39 meter E =
0008392
Z = -1224485
56 I = 51
64841
XDOT = -1840
857909 Wp = 149
67380
YDOT = 4592
545919 meter/sec RA = 181
06975 deg
ZDOT = -5846
843575 TA = 43
60371
MA = 43
53742
Ha = 228
067 n
mi
Hp = 222
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21645623
80 X = 6590830
47
Y = 3583321
48 feet Y = 1165937
64 meter
Z = -4017341
06 Z = -1192452
82
XDOT = -6039
560069 XDOT = -1863
675209
YDOT = 15067
407870 feet/sec YDOT = 4571
833144 meter/sec
ZDOT = -19182
557661 ZDOT = -5855
840851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14443630
26 X = -4402418
50
Y = 16550371
31 feet Y = 5044553
18 meter
Z = -3870272
08 Z = -1179658
93
XDOT = -8501
404820 XDOT = -2591
228189
YDOT = -11895
144340 feet/sec YDOT = -3625
639995 meter/sec
ZDOT = -19223
998712 ZDOT = -5859
474807
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 20130
06297798
00016717 00000-0 10270-3 0 9124
2 25544 51
6418 182
1192 0001387 272
0478 88
0513 15
49340221 25946
Satellite: ISS
Catalog Number: 25544
Epoch time: 20130
06297798 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 182
1192 deg
Eccentricity:
0001387
Arg of perigee: 272
0478 deg
Mean anomaly: 88
0513 deg
Mean motion: 15
49340221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 304
Coasting Arc #14 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2020/131/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6635048
66 A = 6802425
09 meter
Y = -609714
46 meter E =
0012703
Z = 1337630
11 I = 51
68003
XDOT = 1613
032397 Wp = 56
00310
YDOT = -4717
916522 meter/sec RA = 176
12120 deg
ZDOT = 5817
900853 TA = 318
52627
MA = 318
62261
Ha = 227
985 n
mi
Hp = 222
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21768532
33 X = -6634235
03
Y = -2000375
52 feet Y = -683907
90 meter
Z = 4388550
22 Z = 1305401
15
XDOT = 5292
101039 XDOT = 1637
409286
YDOT = -15478
728746 feet/sec YDOT = -4699
742835 meter/sec
ZDOT = 19087
601223 ZDOT = 5825
795076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12860333
53 X = 3919829
66
Y = -17713258
01 feet Y = -5399001
04 meter
Z = 4240540
92 Z = 1292516
87
XDOT = 9373
138492 XDOT = 2856
932612
YDOT = 11410
032836 feet/sec YDOT = 3477
778008 meter/sec
ZDOT = 19123
990049 ZDOT = 5828
992167
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 20131
09497301
00016717 00000-0 10270-3 0 9131
2 25544 51
6402 177
0107 0001348 277
6228 82
4769 15
49394217 26103
Satellite: ISS
Catalog Number: 25544
Epoch time: 20131
09497301 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 177
0107 deg
Eccentricity:
0001348
Arg of perigee: 277
6228 deg
Mean anomaly: 82
4769 deg
Mean motion: 15
49394217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 298
Coasting Arc #15 (Orbit 2624)
---------------------------------------
Vector Time (GMT): 2020/132/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6634012
37 A = 6802370
12 meter
Y = 152582
66 meter E =
0007470
Z = -1480112
44 I = 51
71254
XDOT = -1395
721422 Wp = 150
18377
YDOT = 4831
290079 meter/sec RA = 171
17632 deg
ZDOT = -5776
580365 TA = 45
91876
MA = 45
85730
Ha = 228
041 n
mi
Hp = 222
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21765132
45 X = 6639002
68
Y = 500599
27 feet Y = 226796
99 meter
Z = -4856011
96 Z = -1447874
65
XDOT = -4579
138523 XDOT = -1421
583095
YDOT = 15850
689236 feet/sec YDOT = 4815
538237 meter/sec
ZDOT = -18952
035317 ZDOT = -5783
422500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11251535
36 X = -3429467
98
Y = 18675943
39 feet Y = 5692427
55 meter
Z = -4707922
36 Z = -1434974
73
XDOT = -10190
041468 XDOT = -3105
924639
YDOT = -10908
490159 feet/sec YDOT = -3324
907800 meter/sec
ZDOT = -18983
603223 ZDOT = -5786
202262
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 20132
06247005
00016717 00000-0 10270-3 0 9144
2 25544 51
6398 172
2227 0001431 280
1915 79
9073 15
49354916 26259
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
06247005 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 172
2227 deg
Eccentricity:
0001431
Arg of perigee: 280
1915 deg
Mean anomaly: 79
9073 deg
Mean motion: 15
49354916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2625
Checksum: 297
Coasting Arc #16 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2020/132/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6667609
59 A = 6802561
73 meter
Y = -300358
74 meter E =
0008347
Z = -1293825
87 I = 51
73084
XDOT = -907
808589 Wp = 147
97416
YDOT = 4877
889936 meter/sec RA = 168
62430 deg
ZDOT = -5834
869778 TA = 46
05382
MA = 45
98498
Ha = 228
158 n
mi
Hp = 222
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21875359
55 X = 6676757
43
Y = -985428
94 feet Y = -225745
48 meter
Z = -4244835
53 Z = -1261414
90
XDOT = -2978
374635 XDOT = -933
944546
YDOT = 16003
575906 feet/sec YDOT = 4867
592742 meter/sec
ZDOT = -19143
273551 ZDOT = -5839
342469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7872776
40 X = 2399622
25
Y = -20463720
44 feet Y = -6237341
99 meter
Z = -4095923
79 Z = -1248437
57
XDOT = 12028
614271 XDOT = 3666
321630
YDOT = 8446
952221 feet/sec YDOT = 2574
631037 meter/sec
ZDOT = -19163
960822 ZDOT = -5841
175258
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 20132
57846775
00016717 00000-0 10270-3 0 9150
2 25544 51
6403 169
6681 0001059 274
1967 85
9062 15
49361599 26335
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
57846775 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 169
6681 deg
Eccentricity:
0001059
Arg of perigee: 274
1967 deg
Mean anomaly: 85
9062 deg
Mean motion: 15
49361599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 339
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