[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 3rd 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 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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
096/04:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 231
0
000/00:00:00
000 0
0 0
0 221
7
097/14:00:43
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 222
0
100/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 231
0
000/00:00:00
000 0
0 0
0 221
9
100/08:05:06
000 0
0 0
0 0
0
N/A 0
0 0
0 230
7
000/00:00:00
000 0
0 0
0 221
8
100/14:16:50
000 0
0 0
0 0
0
N/A 0
0 0
0 230
8
000/00:00:00
000 0
0 0
0 222
0
108/01:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
5
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 2042)
---------------------------------------
Vector Time (GMT): 2020/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -263400
11 A = 6793237
22 meter
Y = -4218726
76 meter E =
0018641
Z = -5334144
33 I = 51
61007
XDOT = 7635
429343 Wp = 87
00530
YDOT = -392
150125 meter/sec RA = 357
45263 deg
ZDOT = -66
140044 TA = 182
35793
MA = 182
36673
Ha = 230
970 n
mi
Hp = 221
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -864173
59 X = -190295
47
Y = -13840967
05 feet Y = -4221263
71 meter
Z = -17500473
53 Z = -5335246
11
XDOT = 25050
621204 XDOT = 7639
568271
YDOT = -1286
581776 feet/sec YDOT = -306
742184 meter/sec
ZDOT = -216
994895 ZDOT = -29
040350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3461773
28 X = -1055148
49
Y = -13422729
08 feet Y = -4091247
82 meter
Z = -17505205
17 Z = -5335586
54
XDOT = 23326
385060 XDOT = 7109
882166
YDOT = -5951
735502 feet/sec YDOT = -1814
088981 meter/sec
ZDOT = -46
791071 ZDOT = -14
261919
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 20094
51618408
00016717 00000-0 10270-3 0 9005
2 25544 51
6453 357
9645 0003874 78
4001 281
7583 15
48691575 20431
Satellite: ISS
Catalog Number: 25544
Epoch time: 20094
51618408 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 357
9645 deg
Eccentricity:
0003874
Arg of perigee: 78
4001 deg
Mean anomaly: 281
7583 deg
Mean motion: 15
48691575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2043
Checksum: 320
Coasting Arc #2 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2020/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 749873
33 A = 6793166
53 meter
Y = 4155007
14 meter E =
0006172
Z = 5316369
69 I = 51
57613
XDOT = -7577
546697 Wp = 87
07430
YDOT = 1139
336704 meter/sec RA = 352
50801 deg
ZDOT = 178
492684 TA = 1
22310
MA = 1
22159
Ha = 230
895 n
mi
Hp = 221
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2460214
32 X = 677531
42
Y = 13631913
20 feet Y = 4162988
56 meter
Z = 17442157
77 Z = 5319836
32
XDOT = -24860
717509 XDOT = -7590
590928
YDOT = 3737
981312 feet/sec YDOT = 1054
526261 meter/sec
ZDOT = 585
605917 ZDOT = 141
652506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5206744
53 X = 1587015
73
Y = 12815129
11 feet Y = 3906051
35 meter
Z = 17457744
89 Z = 5321120
64
XDOT = -22552
373964 XDOT = -6873
963584
YDOT = 8596
076418 feet/sec YDOT = 2620
084092 meter/sec
ZDOT = 416
548351 ZDOT = 126
963937
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 20095
54864104
00016717 00000-0 10270-3 0 9016
2 25544 51
6448 352
8604 0003780 82
3162 277
8417 15
48711190 20597
Satellite: ISS
Catalog Number: 25544
Epoch time: 20095
54864104 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 352
8604 deg
Eccentricity:
0003780
Arg of perigee: 82
3162 deg
Mean anomaly: 277
8417 deg
Mean motion: 15
48711190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 307
Coasting Arc #3 (Orbit 2068)
---------------------------------------
Vector Time (GMT): 2020/096/04:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5134216
25 A = 6798701
67 meter
Y = -2173308
86 meter E =
0010455
Z = -3901488
90 I = 51
56999
XDOT = 4890
806426 Wp = 78
19937
YDOT = -4231
885054 meter/sec RA = 349
21557 deg
ZDOT = -4085
990142 TA = 148
84634
MA = 148
78432
Ha = 231
009 n
mi
Hp = 221
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16844541
51 X = -5090581
03
Y = -7130278
41 feet Y = -2230479
61 meter
Z = -12800160
42 Z = -3926322
58
XDOT = 16045
952842 XDOT = 4957
612373
YDOT = -13884
137315 feet/sec YDOT = -4176
819329 meter/sec
ZDOT = -13405
479467 ZDOT = -4062
070149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11405440
53 X = 3476378
27
Y = -14197563
29 feet Y = -4327417
29 meter
Z = -12913894
78 Z = -3936155
13
XDOT = 7956
762692 XDOT = 2425
221268
YDOT = 18463
957106 feet/sec YDOT = 5627
814126 meter/sec
ZDOT = -13295
458305 ZDOT = -4052
455691
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 20096
19392664
00016717 00000-0 10270-3 0 9026
2 25544 51
6426 349
6695 0003946 87
0422 273
1179 15
48679384 20695
Satellite: ISS
Catalog Number: 25544
Epoch time: 20096
19392664 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 349
6695 deg
Eccentricity:
0003946
Arg of perigee: 87
0422 deg
Mean anomaly: 273
1179 deg
Mean motion: 15
48679384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2069
Checksum: 345
Coasting Arc #4 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2020/097/04:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5379605
87 A = 6798972
00 meter
Y = 1630836
71 meter E =
0015168
Z = 3812485
33 I = 51
53733
XDOT = -4393
922854 Wp = 95
27432
YDOT = 4687
098388 meter/sec RA = 344
26592 deg
ZDOT = 4179
351194 TA = 310
52018
MA = 310
65221
Ha = 230
904 n
mi
Hp = 221
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17649625
57 X = 5342450
76
Y = 5350514
14 feet Y = 1690787
89 meter
Z = 12508153
97 Z = 3838526
85
XDOT = -14415
757394 XDOT = -4466
309625
YDOT = 15377
619383 feet/sec YDOT = 4637
558055 meter/sec
ZDOT = 13711
782133 ZDOT = 4157
831090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9643637
36 X = -2939380
67
Y = 15624939
58 feet Y = 4762481
59 meter
Z = 12627459
03 Z = 3848849
51
XDOT = -10041
811984 XDOT = -3060
744293
YDOT = -17240
353988 feet/sec YDOT = -5254
859895 meter/sec
ZDOT = 13612
748813 ZDOT = 4149
165838
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 20097
22638200
00016717 00000-0 10270-3 0 9031
2 25544 51
6418 344
5650 0003878 89
4772 270
6822 15
48679022 20853
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
22638200 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 344
5650 deg
Eccentricity:
0003878
Arg of perigee: 89
4772 deg
Mean anomaly: 270
6822 deg
Mean motion: 15
48679022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2085
Checksum: 318
Coasting Arc #5 (Orbit 2090)
---------------------------------------
Vector Time (GMT): 2020/097/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6596423
51 A = 6804508
78 meter
Y = 1042255
95 meter E =
0011266
Z = -1288824
30 I = 51
54427
XDOT = 344
448389 Wp = 127
19281
YDOT = -4964
474721 meter/sec RA = 342
20504 deg
ZDOT = -5819
481861 TA = 66
81060
MA = 66
69197
Ha = 230
871 n
mi
Hp = 221
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21641809
42 X = -6601327
71
Y = 3419474
89 feet Y = 968462
50 meter
Z = -4228426
18 Z = -1320879
09
XDOT = 1130
080018 XDOT = 428
204675
YDOT = -16287
646723 feet/sec YDOT = -4960
155103 meter/sec
ZDOT = -19092
788259 ZDOT = -5817
604764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12988433
12 X = -3958874
42
Y = 17609541
24 feet Y = 5367388
17 meter
Z = -4375496
94 Z = -1333651
47
XDOT = -9255
672493 XDOT = -2821
128976
YDOT = -11535
655596 feet/sec YDOT = -3516
067826 meter/sec
ZDOT = -19083
818620 ZDOT = -5816
747915
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 20097
61355172
00016717 00000-0 10270-3 0 9049
2 25544 51
6438 342
6517 0003544 89
4148 270
7408 15
48663378 20918
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
61355172 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 342
6517 deg
Eccentricity:
0003544
Arg of perigee: 89
4148 deg
Mean anomaly: 270
7408 deg
Mean motion: 15
48663378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2091
Checksum: 321
Coasting Arc #6 (Orbit 2106)
---------------------------------------
Vector Time (GMT): 2020/098/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6474937
08 A = 6804508
87 meter
Y = -1706373
89 meter E =
0016799
Z = 1170059
53 I = 51
51210
XDOT = 235
335368 Wp = 64
75363
YDOT = 4943
687906 meter/sec RA = 337
25005 deg
ZDOT = 5848
489724 TA = 307
95007
MA = 308
10175
Ha = 230
843 n
mi
Hp = 221
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21243231
87 X = 6487853
52
Y = -5598339
53 feet Y = -1633894
20 meter
Z = 3838777
98 Z = 1201543
90
XDOT = 772
097663 XDOT = 151
627361
YDOT = 16219
448512 feet/sec YDOT = 4945
852132 meter/sec
ZDOT = 19187
958411 ZDOT = 5849
429094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10850187
67 X = 3307137
20
Y = -19072481
47 feet Y = -5813292
35 meter
Z = 3983265
03 Z = 1214099
18
XDOT = 10644
229418 XDOT = 3244
361127
YDOT = 10102
522226 feet/sec YDOT = 3079
248774 meter/sec
ZDOT = 19191
909833 ZDOT = 5849
694117
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 20098
64600154
00016717 00000-0 10270-3 0 9057
2 25544 51
6428 337
5461 0003610 92
4119 267
7445 15
48710185 21078
Satellite: ISS
Catalog Number: 25544
Epoch time: 20098
64600154 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 337
5461 deg
Eccentricity:
0003610
Arg of perigee: 92
4119 deg
Mean anomaly: 267
7445 deg
Mean motion: 15
48710185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2107
Checksum: 299
Coasting Arc #7 (Orbit 2121)
---------------------------------------
Vector Time (GMT): 2020/099/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6298579
65 A = 6804663
17 meter
Y = 2316164
06 meter E =
0012106
Z = -1102748
80 I = 51
48038
XDOT = -771
757096 Wp = 128
77285
YDOT = -4865
712925 meter/sec RA = 332
29436 deg
ZDOT = -5862
674038 TA = 63
18804
MA = 63
06427
Ha = 230
878 n
mi
Hp = 221
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20664631
40 X = -6318654
98
Y = 7598963
44 feet Y = 2245616
51 meter
Z = -3617942
25 Z = -1133394
08
XDOT = -2532
011471 XDOT = -688
812107
YDOT = -15963
625083 feet/sec YDOT = -4873
879988 meter/sec
ZDOT = -19234
494876 ZDOT = -5866
221093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8670899
13 X = -2642890
06
Y = 20212597
40 feet Y = 6160799
69 meter
Z = -3758611
07 Z = -1145624
65
XDOT = -11770
569816 XDOT = -3587
669680
YDOT = -8599
135113 feet/sec YDOT = -2621
016382 meter/sec
ZDOT = -19250
410107 ZDOT = -5867
525001
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 20099
61392420
00016717 00000-0 10270-3 0 9060
2 25544 51
6414 332
7608 0003635 95
4393 264
7171 15
48677905 21229
Satellite: ISS
Catalog Number: 25544
Epoch time: 20099
61392420 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 332
7608 deg
Eccentricity:
0003635
Arg of perigee: 95
4393 deg
Mean anomaly: 264
7171 deg
Mean motion: 15
48677905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2122
Checksum: 313
Coasting Arc #8 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1896527
97 A = 6797948
48 meter
Y = -5027203
10 meter E =
0011351
Z = -4175973
04 I = 51
43719
XDOT = 6666
489243 Wp = 104
79687
YDOT = -561
295663 meter/sec RA = 328
95692 deg
ZDOT = 3708
959641 TA = 203
50030
MA = 203
55220
Ha = 230
976 n
mi
Hp = 221
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6222204
63 X = 1972887
42
Y = -16493448
51 feet Y = -5005568
11 meter
Z = -13700698
94 Z = -4166574
53
XDOT = 21871
683868 XDOT = 6654
254130
YDOT = -1841
521204 feet/sec YDOT = -486
814393 meter/sec
ZDOT = 12168
502759 ZDOT = 3741
313538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17620802
15 X = 5370820
50
Y = 1202328
25 feet Y = 366469
65 meter
Z = -13657253
16 Z = -4162730
76
XDOT = 8235
068951 XDOT = 2510
049016
YDOT = 19006
666511 feet/sec YDOT = 5793
231953 meter/sec
ZDOT = 12316
871907 ZDOT = 3754
182557
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 20100
25920612
00016717 00000-0 10270-3 0 9074
2 25544 51
6404 329
5705 0003770 96
8759 263
2819 15
48674013 21322
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
25920612 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 329
5705 deg
Eccentricity:
0003770
Arg of perigee: 96
8759 deg
Mean anomaly: 263
2819 deg
Mean motion: 15
48674013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 300
Coasting Arc #9 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3806020
90 A = 6794097
67 meter
Y = 2418523
75 meter E =
0008623
Z = 5075846
73 I = 51
42421
XDOT = -5526
960996 Wp = 113
54908
YDOT = 5013
695042 meter/sec RA = 328
56603 deg
ZDOT = 1749
625180 TA = 319
44159
MA = 319
50581
Ha = 230
721 n
mi
Hp = 221
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12486945
21 X = 3754037
52
Y = 7934789
21 feet Y = 2460795
06 meter
Z = 16653040
45 Z = 5094208
69
XDOT = -18133
074135 XDOT = -5591
113622
YDOT = 16449
130714 feet/sec YDOT = 4951
530046 meter/sec
ZDOT = 5740
240093 ZDOT = 1722
620898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3986072
16 X = 1214954
79
Y = 14148880
52 feet Y = 4312578
78 meter
Z = 16737050
08 Z = 5101452
86
XDOT = -23478
142124 XDOT = -7156
137719
YDOT = -51
235583 feet/sec YDOT = -15
616606 meter/sec
ZDOT = 5616
080885 ZDOT = 1711
781454
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 20100
38826116
00016717 00000-0 10270-3 0 9083
2 25544 51
6420 328
9333 0003649 98
6797 261
4766 15
48724471 21344
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
38826116 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 328
9333 deg
Eccentricity:
0003649
Arg of perigee: 98
6797 deg
Mean anomaly: 261
4766 deg
Mean motion: 15
48724471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 321
Coasting Arc #10 (Orbit 2137)
---------------------------------------
Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3841696
27 A = 6794279
09 meter
Y = 2350598
99 meter E =
0008615
Z = 5081126
45 I = 51
41488
XDOT = -5429
477765 Wp = 113
76429
YDOT = 5126
340957 meter/sec RA = 327
28378 deg
ZDOT = 1727
825697 TA = 319
44174
MA = 319
50590
Ha = 230
839 n
mi
Hp = 221
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12603990
37 X = 3790444
13
Y = 7711938
96 feet Y = 2393273
30 meter
Z = 16670362
37 Z = 5099663
52
XDOT = -17813
247261 XDOT = -5494
791389
YDOT = 16818
703928 feet/sec YDOT = 5065
259583 meter/sec
ZDOT = 5668
719477 ZDOT = 1701
292154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13803329
93 X = 4207254
96
Y = -4996762
85 feet Y = -1523013
32 meter
Z = 16755178
34 Z = 5106978
36
XDOT = 1726
235722 XDOT = 526
156648
YDOT = 23430
677217 feet/sec YDOT = 7141
670416 meter/sec
ZDOT = 5546
712982 ZDOT = 1690
638117
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 20100
64637408
00016717 00000-0 10270-3 0 9097
2 25544 51
6402 327
6550 0003679 99
4114 260
7452 15
48654593 21381
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
64637408 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 327
6550 deg
Eccentricity:
0003679
Arg of perigee: 99
4114 deg
Mean anomaly: 260
7452 deg
Mean motion: 15
48654593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2138
Checksum: 312
Coasting Arc #11 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4109873
91 A = 6794276
00 meter
Y = -1938261
48 meter E =
0016564
Z = -5066069
98 I = 51
38722
XDOT = 4878
398955 Wp = 82
12130
YDOT = -5601
231882 meter/sec RA = 322
32371 deg
ZDOT = -1817
517057 TA = 170
18622
MA = 170
15383
Ha = 230
891 n
mi
Hp = 221
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13483838
28 X = -4063285
86
Y = -6359125
60 feet Y = -1983960
67 meter
Z = -16620964
49 Z = -5085921
18
XDOT = 16005
245915 XDOT = 4949
499581
YDOT = -18376
745021 feet/sec YDOT = -5546
280657 meter/sec
ZDOT = -5962
982471 ZDOT = -1793
646561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13175738
27 X = -4015965
02
Y = 6754515
71 feet Y = 2058776
39 meter
Z = -16711830
32 Z = -5093765
88
XDOT = -4352
905599 XDOT = -1326
765627
YDOT = -22949
290168 feet/sec YDOT = -6994
943643 meter/sec
ZDOT = -5853
158881 ZDOT = -1784
042827
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 20101
61429158
00016717 00000-0 10270-3 0 9108
2 25544 51
6397 322
8681 0003715 103
9691 256
1872 15
48696257 21533
Satellite: ISS
Catalog Number: 25544
Epoch time: 20101
61429158 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 322
8681 deg
Eccentricity:
0003715
Arg of perigee: 103
9691 deg
Mean anomaly: 256
1872 deg
Mean motion: 15
48696257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 315
Coasting Arc #12 (Orbit 2168)
---------------------------------------
Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4326798
73 A = 6794491
37 meter
Y = 1472540
47 meter E =
0009256
Z = 5021485
63 I = 51
36187
XDOT = -4298
025373 Wp = 116
43232
YDOT = 6047
307831 meter/sec RA = 317
36241 deg
ZDOT = 1923
259687 TA = 314
79102
MA = 314
86626
Ha = 230
809 n
mi
Hp = 221
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14195533
91 X = 4285619
03
Y = 4831169
54 feet Y = 1520695
58 meter
Z = 16474690
38 Z = 5042403
71
XDOT = -14101
133115 XDOT = -4374
670907
YDOT = 19840
248790 feet/sec YDOT = 5998
815707 meter/sec
ZDOT = 6309
907110 ZDOT = 1902
195180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12251532
69 X = 3734267
16
Y = -8460969
82 feet Y = -2578903
60 meter
Z = 16570478
02 Z = 5050681
70
XDOT = 6945
916516 XDOT = 2117
115354
YDOT = 22268
954912 feet/sec YDOT = 6787
577457 meter/sec
ZDOT = 6212
922181 ZDOT = 1893
698681
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 20102
64673660
00016717 00000-0 10270-3 0 9112
2 25544 51
6398 317
7625 0003732 105
9199 254
2362 15
48664922 21693
Satellite: ISS
Catalog Number: 25544
Epoch time: 20102
64673660 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 317
7625 deg
Eccentricity:
0003732
Arg of perigee: 105
9199 deg
Mean anomaly: 254
2362 deg
Mean motion: 15
48664922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2169
Checksum: 319
Coasting Arc #13 (Orbit 2183)
---------------------------------------
Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4498626
74 A = 6794502
45 meter
Y = -1011748
69 meter E =
0016147
Z = -5004948
91 I = 51
33804
XDOT = 3669
776456 Wp = 83
08643
YDOT = -6401
623272 meter/sec RA = 312
39979 deg
ZDOT = -2008
142009 TA = 167
28253
MA = 167
24175
Ha = 230
925 n
mi
Hp = 221
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14759274
08 X = -4462667
39
Y = -3319385
46 feet Y = -1061854
41 meter
Z = -16420436
07 Z = -5026714
29
XDOT = 12039
949001 XDOT = 3750
843018
YDOT = -21002
701023 feet/sec YDOT = -6360
131926 meter/sec
ZDOT = -6588
392419 ZDOT = -1990
118744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11199765
54 X = -3413688
54
Y = 10006769
92 feet Y = 3050063
47 meter
Z = -16520139
81 Z = -5035338
61
XDOT = -9371
779553 XDOT = -2856
518408
YDOT = -21208
771765 feet/sec YDOT = -6464
433634 meter/sec
ZDOT = -6505
332068 ZDOT = -1982
825214
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 20103
61465117
00016717 00000-0 10270-3 0 9127
2 25544 51
6394 312
9767 0003931 110
9237 249
2334 15
48703233 21842
Satellite: ISS
Catalog Number: 25544
Epoch time: 20103
61465117 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 312
9767 deg
Eccentricity:
0003931
Arg of perigee: 110
9237 deg
Mean anomaly: 249
2334 deg
Mean motion: 15
48703233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2184
Checksum: 293
Coasting Arc #14 (Orbit 2199)
---------------------------------------
Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4612488
88 A = 6794691
36 meter
Y = 505214
65 meter E =
0009881
Z = 4957748
78 I = 51
31625
XDOT = -3015
503506 Wp = 119
62158
YDOT = 6721
718847 meter/sec RA = 307
43547 deg
ZDOT = 2112
551701 TA = 309
65690
MA = 309
74403
Ha = 230
741 n
mi
Hp = 221
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15132837
52 X = 4582414
65
Y = 1657528
36 feet Y = 556626
55 meter
Z = 16265579
99 Z = 4980081
45
XDOT = -9893
384206 XDOT = -3100
705223
YDOT = 22052
883357 feet/sec YDOT = 6687
520918 meter/sec
ZDOT = 6930
943902 ZDOT = 2097
696698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9867745
90 X = 3007688
95
Y = -11447185
81 feet Y = -3489102
23 meter
Z = 16367919
60 Z = 4988941
89
XDOT = 11723
322151 XDOT = 3573
268592
YDOT = 19955
278405 feet/sec YDOT = 6082
368858 meter/sec
ZDOT = 6862
395756 ZDOT = 2091
658227
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 20104
64709351
00016717 00000-0 10270-3 0 9133
2 25544 51
6389 307
8715 0003776 115
1631 244
9910 15
48686543 22009
Satellite: ISS
Catalog Number: 25544
Epoch time: 20104
64709351 = yrday
fracday
Element set: 913
Inclination: 51
6389 deg
RA of node: 307
8715 deg
Eccentricity:
0003776
Arg of perigee: 115
1631 deg
Mean anomaly: 244
9910 deg
Mean motion: 15
48686543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2200
Checksum: 306
Coasting Arc #15 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2020/105/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4680067
02 A = 6794724
38 meter
Y = -17265
04 meter E =
0015422
Z = -4939862
65 I = 51
29909
XDOT = 2336
047479 Wp = 83
98925
YDOT = -6944
178856 meter/sec RA = 302
47020 deg
ZDOT = -2193
275877 TA = 164
47451
MA = 164
42715
Ha = 230
849 n
mi
Hp = 221
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15354550
60 X = -4655531
14
Y = -56643
82 feet Y = -69463
65 meter
Z = -16206898
46 Z = -4962536
96
XDOT = 7664
197766 XDOT = 2424
179384
YDOT = -22782
739028 feet/sec YDOT = -6917
562716 meter/sec
ZDOT = -7195
786999 ZDOT = -2181
714295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8456571
39 X = -2577562
96
Y = 12683532
14 feet Y = 3865940
60 meter
Z = -16310836
98 Z = -4971543
11
XDOT = -13824
326623 XDOT = -4213
654755
YDOT = -18383
860877 feet/sec YDOT = -5603
400795 meter/sec
ZDOT = -7142
335101 ZDOT = -2176
983739
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 20105
61500556
00016717 00000-0 10270-3 0 9148
2 25544 51
6408 303
0862 0003919 118
3617 241
7928 15
48718153 22153
Satellite: ISS
Catalog Number: 25544
Epoch time: 20105
61500556 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 303
0862 deg
Eccentricity:
0003919
Arg of perigee: 118
3617 deg
Mean anomaly: 241
7928 deg
Mean motion: 15
48718153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 295
Coasting Arc #16 (Orbit 2230)
---------------------------------------
Vector Time (GMT): 2020/106/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4683646
77 A = 6794871
11 meter
Y = -505361
96 meter E =
0010415
Z = 4891031
91 I = 51
28197
XDOT = -1636
535978 Wp = 121
70561
YDOT = 7126
734391 meter/sec RA = 297
50245 deg
ZDOT = 2294
513262 TA = 305
68116
MA = 305
77805
Ha = 230
651 n
mi
Hp = 221
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15366295
19 X = 4665192
04
Y = -1658011
69 feet Y = -453089
26 meter
Z = 16046692
63 Z = 4913738
33
XDOT = -5369
212525 XDOT = -1727
252990
YDOT = 23381
674512 feet/sec YDOT = 7107
926259 meter/sec
ZDOT = 7527
930651 ZDOT = 2286
343283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6797758
83 X = 2071956
89
Y = -13759002
54 feet Y = -4193743
97 meter
Z = 16150811
09 Z = 4922767
22
XDOT = 15807
306867 XDOT = 4818
067133
YDOT = 16636
230810 feet/sec YDOT = 5070
723151 meter/sec
ZDOT = 7490
031090 ZDOT = 2282
961476
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 20106
64744239
00016717 00000-0 10270-3 0 9151
2 25544 51
6401 297
9804 0003808 122
7566 237
3952 15
48720240 22318
Satellite: ISS
Catalog Number: 25544
Epoch time: 20106
64744239 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 297
9804 deg
Eccentricity:
0003808
Arg of perigee: 122
7566 deg
Mean anomaly: 237
3952 deg
Mean motion: 15
48720240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2231
Checksum: 303
Coasting Arc #17 (Orbit 2245)
---------------------------------------
Vector Time (GMT): 2020/107/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4644419
53 A = 6794998
59 meter
Y = 997136
26 meter E =
0014689
Z = -4871953
12 I = 51
26814
XDOT = 933
550371 Wp = 84
93452
YDOT = -7211
456238 meter/sec RA = 292
53557 deg
ZDOT = -2370
849629 TA = 161
67813
MA = 161
62516
Ha = 230
798 n
mi
Hp = 221
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15237596
87 X = -4631559
56
Y = 3271444
41 feet Y = 945270
87 meter
Z = -15984098
15 Z = -4894482
57
XDOT = 3062
829301 XDOT = 1025
637806
YDOT = -23659
633327 feet/sec YDOT = -7200
501763 meter/sec
ZDOT = -7778
378049 ZDOT = -2366
091035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5117444
19 X = -1559796
99
Y = 14607681
51 feet Y = 4452421
32 meter
Z = -16087433
19 Z = -4903449
64
XDOT = -17478
971679 XDOT = -5327
590568
YDOT = -14647
420942 feet/sec YDOT = -4464
533903 meter/sec
ZDOT = -7756
129975 ZDOT = -2364
068417
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 20107
61535168
00016717 00000-0 10270-3 0 9169
2 25544 51
6403 293
1959 0003939 124
9821 235
1699 15
48720166 22469
Satellite: ISS
Catalog Number: 25544
Epoch time: 20107
61535168 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 293
1959 deg
Eccentricity:
0003939
Arg of perigee: 124
9821 deg
Mean anomaly: 235
1699 deg
Mean motion: 15
48720166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2246
Checksum: 322
Coasting Arc #18 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2020/108/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 916536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4613037
86 A = 6795435
54 meter
Y = -1518047
68 meter E =
0011054
Z = 4747264
24 I = 51
26268
XDOT = -371
507076 Wp = 119
86536
YDOT = 7182
045048 meter/sec RA = 290
13862 deg
ZDOT = 2647
563476 TA = 303
79262
MA = 303
89784
Ha = 230
543 n
mi
Hp = 222
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15134638
64 X = 4606610
86
Y = -4980471
38 feet Y = -1466497
22 meter
Z = 15575013
90 Z = 4769656
90
XDOT = -1218
855236 XDOT = -464
651515
YDOT = 23563
139921 feet/sec YDOT = 7177
369854 meter/sec
ZDOT = 8686
231875 ZDOT = 2645
532438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5064108
14 X = -1543540
16
Y = 15000212
51 feet Y = 4572064
77 meter
Z = 15677750
89 Z = 4778578
47
XDOT = -16959
245295 XDOT = -5169
177966
YDOT = -14828
171450 feet/sec YDOT = -4519
626658 meter/sec
ZDOT = 8676
498080 ZDOT = 2644
596615
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 20108
13156822
00016717 00000-0 10270-3 0 9174
2 25544 51
6393 290
6472 0003542 124
0542 236
0945 15
48729767 22549
Satellite: ISS
Catalog Number: 25544
Epoch time: 20108
13156822 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 290
6472 deg
Eccentricity:
0003542
Arg of perigee: 124
0542 deg
Mean anomaly: 236
0945 deg
Mean motion: 15
48729767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 307
Coasting Arc #19 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2020/109/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 916536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4470030
10 A = 6795644
54 meter
Y = 1999104
37 meter E =
0013382
Z = -4724274
81 I = 51
25295
XDOT = -325
185370 Wp = 83
72425
YDOT = -7141
873108 meter/sec RA = 285
16817 deg
ZDOT = -2719
686305 TA = 159
18083
MA = 159
12627
Ha = 230
692 n
mi
Hp = 221
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14665453
09 X = -4469104
68
Y = 6558741
37 feet Y = 1949122
31 meter
Z = -15499589
27 Z = -4745986
24
XDOT = -1066
881135 XDOT = -232
088011
YDOT = -23431
342218 feet/sec YDOT = -7144
989124 meter/sec
ZDOT = -8922
855331 ZDOT = -2721
039541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3253024
77 X = 991521
95
Y = -15633677
38 feet Y = -4765144
86 meter
Z = -15599225
36 Z = -4754643
89
XDOT = 18407
782137 XDOT = 5610
691995
YDOT = 12722
171412 feet/sec YDOT = 3877
717846 meter/sec
ZDOT = -8928
656617 ZDOT = -2721
454537
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 20109
09947626
00016717 00000-0 10270-3 0 9181
2 25544 51
6396 285
8606 0003602 126
3247 233
8235 15
48704720 22696
Satellite: ISS
Catalog Number: 25544
Epoch time: 20109
09947626 = yrday
fracday
Element set: 918
Inclination: 51
6396 deg
RA of node: 285
8606 deg
Eccentricity:
0003602
Arg of perigee: 126
3247 deg
Mean anomaly: 233
8235 deg
Mean motion: 15
48704720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 321
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