[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 9th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14255 723 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
8
132/16:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 222
6
132/22:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
8
135/18:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
6
142/23:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
4
Coasting Arc #1 (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 = 1236849
03 A = 6791433
34 meter
Y = -4104246
90 meter E =
0001992
Z = 5266605
38 I = 51
59293
XDOT = 7524
163946 Wp = 48
15723
YDOT = 1165
880957 meter/sec RA = 183
68876 deg
ZDOT = -856
955823 TA = 50
05729
MA = 50
03979
Ha = 227
943 n
mi
Hp = 222
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4057903
64 X = 1257069
38
Y = -13465376
98 feet Y = -4090302
97 meter
Z = 17278889
05 Z = 5272662
38
XDOT = 24685
577250 XDOT = 7514
730184
YDOT = 3825
068755 feet/sec YDOT = 1249
968838 meter/sec
ZDOT = -2811
534854 ZDOT = -820
428508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6921937
67 X = -2109806
60
Y = -12202624
70 feet Y = -3719360
01 meter
Z = 17306810
66 Z = 5275115
89
XDOT = 19055
166327 XDOT = 5808
014697
YDOT = -14565
773250 feet/sec YDOT = -4439
647686 meter/sec
ZDOT = -2643
842904 ZDOT = -805
843317
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
54701158
00016717 00000-0 10270-3 0 9002
2 25544 51
6414 184
6720 0001383 260
6484 99
4509 15
49376723 25860
Satellite: ISS
Catalog Number: 25544
Epoch time: 20129
54701158 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 184
6720 deg
Eccentricity:
0001383
Arg of perigee: 260
6484 deg
Mean anomaly: 99
4509 deg
Mean motion: 15
49376723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2586
Checksum: 316
Coasting Arc #2 (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 = 6603427
32 A = 6802743
47 meter
Y = 1077609
63 meter E =
0008410
Z = -1205938
66 I = 51
64843
XDOT = -1814
269680 Wp = 149
64048
YDOT = 4596
903863 meter/sec RA = 181
06959 deg
ZDOT = -5851
721996 TA = 43
43227
MA = 43
36605
Ha = 228
074 n
mi
Hp = 222
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21664787
78 X = 6596744
24
Y = 3535464
66 feet Y = 1151416
60 meter
Z = -3956491
65 Z = -1173877
37
XDOT = -5952
328347 XDOT = -1837
113991
YDOT = 15081
705586 feet/sec YDOT = 4576
488266 meter/sec
ZDOT = -19198
562979 ZDOT = -5860
590179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14412785
42 X = -4393017
00
Y = 16591482
25 feet Y = 5057083
79 meter
Z = -3809291
17 Z = -1161071
95
XDOT = -8556
492373 XDOT = -2608
018875
YDOT = -11830
621549 feet/sec YDOT = -3605
973448 meter/sec
ZDOT = -19239
411339 ZDOT = -5864
172576
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
06301482
00016717 00000-0 10270-3 0 9018
2 25544 51
6418 182
1196 0001414 272
9751 87
1237 15
49329860 25943
Satellite: ISS
Catalog Number: 25544
Epoch time: 20130
06301482 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 182
1196 deg
Eccentricity:
0001414
Arg of perigee: 272
9751 deg
Mean anomaly: 87
1237 deg
Mean motion: 15
49329860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 295
Coasting Arc #3 (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 = -6641073
04 A = 6802481
45 meter
Y = -591961
62 meter E =
0012688
Z = 1315752
01 I = 51
68007
XDOT = 1581
272813 Wp = 55
55773
YDOT = -4720
795636 meter/sec RA = 176
12109 deg
ZDOT = 5824
257298 TA = 318
72881
MA = 318
82465
Ha = 227
993 n
mi
Hp = 222
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21788297
39 X = -6640351
22
Y = -1942131
30 feet Y = -666222
94 meter
Z = 4316771
67 Z = 1283493
57
XDOT = 5187
902931 XDOT = 1605
653381
YDOT = -15488
174659 feet/sec YDOT = -4702
977088 meter/sec
ZDOT = 19108
455703 ZDOT = 5831
997253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12820127
73 X = 3907574
93
Y = -17759593
84 feet Y = -5413124
20 meter
Z = 4168626
45 Z = 1270597
34
XDOT = 9431
205867 XDOT = 2874
631548
YDOT = 11328
112591 feet/sec YDOT = 3452
808718 meter/sec
ZDOT = 19144
136058 ZDOT = 5835
132671
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
09501702
00016717 00000-0 10270-3 0 9020
2 25544 51
6402 177
0111 0001376 278
5566 81
5428 15
49383040 26108
Satellite: ISS
Catalog Number: 25544
Epoch time: 20131
09501702 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 177
0111 deg
Eccentricity:
0001376
Arg of perigee: 278
5566 deg
Mean anomaly: 81
5428 deg
Mean motion: 15
49383040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 272
Coasting Arc #4 (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 = 6640128
72 A = 6802435
39 meter
Y = 131280
72 meter E =
0007510
Z = -1454645
91 I = 51
71260
XDOT = -1358
589108 Wp = 150
15285
YDOT = 4832
068052 meter/sec RA = 171
17627 deg
ZDOT = -5784
780575 TA = 45
66521
MA = 45
60368
Ha = 228
051 n
mi
Hp = 222
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21785199
20 X = 6645233
07
Y = 430711
03 feet Y = 205564
08 meter
Z = -4772460
32 Z = -1422378
12
XDOT = -4457
313347 XDOT = -1384
422408
YDOT = 15853
241642 feet/sec YDOT = 4816
731610 meter/sec
ZDOT = -18978
938895 ZDOT = -5791
442266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11200539
90 X = -3413924
56
Y = 18727551
22 feet Y = 5708157
61 meter
Z = -4624232
37 Z = -1409466
03
XDOT = -10249
038370 XDOT = -3123
906895
YDOT = -10807
552421 feet/sec YDOT = -3294
141978 meter/sec
ZDOT = -19009
677897 ZDOT = -5794
149823
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
06252122
00016717 00000-0 10270-3 0 9038
2 25544 51
6398 172
2232 0001459 281
0600 79
0386 15
49343064 26256
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
06252122 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 172
2232 deg
Eccentricity:
0001459
Arg of perigee: 281
0600 deg
Mean anomaly: 79
0386 deg
Mean motion: 15
49343064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2625
Checksum: 278
Coasting Arc #5 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2020/132/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3855717
70 A = 6796623
44 meter
Y = -3985396
42 meter E =
0009920
Z = 3923260
66 I = 51
71300
XDOT = 6186
873508 Wp = 77
28793
YDOT = 1969
203292 meter/sec RA = 168
00377 deg
ZDOT = -4069
151017 TA = 55
33494
MA = 55
24148
Ha = 227
988 n
mi
Hp = 222
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12649992
45 X = 3880939
99
Y = -13075447
56 feet Y = -3942138
48 meter
Z = 12871590
09 Z = 3942051
09
XDOT = 20298
141430 XDOT = 6184
159157
YDOT = 6460
640723 feet/sec YDOT = 2038
374622 meter/sec
ZDOT = -13350
232995 ZDOT = -4039
103840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16451871
24 X = -5014530
35
Y = -7621862
27 feet Y = -2323143
62 meter
Z = 12958032
94 Z = 3949608
44
XDOT = -1084
593669 XDOT = -330
584150
YDOT = -20181
146843 feet/sec YDOT = -6151
213558 meter/sec
ZDOT = -13212
242763 ZDOT = -4027
091594
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
70752316
00016717 00000-0 10270-3 0 9040
2 25544 51
6380 169
0301 0001260 286
7878 73
3134 15
49368301 26357
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
70752316 = yrday
fracday
Element set: 904
Inclination: 51
6380 deg
RA of node: 169
0301 deg
Eccentricity:
0001260
Arg of perigee: 286
7878 deg
Mean anomaly: 73
3134 deg
Mean motion: 15
49368301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2635
Checksum: 291
Coasting Arc #6 (Orbit 2638)
---------------------------------------
Vector Time (GMT): 2020/132/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6431223
06 A = 6801348
51 meter
Y = 257206
52 meter E =
0005160
Z = -2192063
26 I = 51
74130
XDOT = -2062
869143 Wp = 147
82063
YDOT = 4930
676356 meter/sec RA = 166
71096 deg
ZDOT = -5483
849089 TA = 56
42013
MA = 56
37088
Ha = 228
069 n
mi
Hp = 222
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21099813
19 X = 6438516
74
Y = 843853
42 feet Y = 329166
07 meter
Z = -7191808
60 Z = -2160805
06
XDOT = -6767
943381 XDOT = -2091
214633
YDOT = 16176
759698 feet/sec YDOT = 4907
450037 meter/sec
ZDOT = -17991
630870 ZDOT = -5493
938000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19262414
21 X = -5871183
85
Y = 8770325
24 feet Y = 2673195
13 meter
Z = -7048199
06 Z = -2148291
07
XDOT = -711
202369 XDOT = -216
774482
YDOT = -16030
755023 feet/sec YDOT = -4886
174131 meter/sec
ZDOT = -18038
125528 ZDOT = -5498
020661
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
96552360
00016717 00000-0 10270-3 0 9056
2 25544 51
6423 167
7551 0001461 283
2937 76
8050 15
49335923 26391
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
96552360 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 167
7551 deg
Eccentricity:
0001461
Arg of perigee: 283
2937 deg
Mean anomaly: 76
8050 deg
Mean motion: 15
49335923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2639
Checksum: 311
Coasting Arc #7 (Orbit 2654)
---------------------------------------
Vector Time (GMT): 2020/133/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6391598
69 A = 6801074
59 meter
Y = 200860
96 meter E =
0012823
Z = 2296433
33 I = 51
77308
XDOT = 1798
424571 Wp = 67
51906
YDOT = -5097
119203 meter/sec RA = 161
76866 deg
ZDOT = 5431
883004 TA = 317
96354
MA = 318
06186
Ha = 228
100 n
mi
Hp = 222
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20969811
97 X = -6404524
50
Y = 658992
66 feet Y = 129313
05 meter
Z = 7534230
09 Z = 2265354
07
XDOT = 5900
343080 XDOT = 1828
903427
YDOT = -16722
832031 feet/sec YDOT = -5076
838083 meter/sec
ZDOT = 17821
138464 ZDOT = 5440
692549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18295970
87 X = 5576611
92
Y = -10370943
93 feet Y = -3161063
71 meter
Z = 7391405
85 Z = 2252900
50
XDOT = 1915
237711 XDOT = 583
764454
YDOT = 16155
275812 feet/sec YDOT = 4924
128068 meter/sec
ZDOT = 17861
767838 ZDOT = 5444
266837
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 20133
99752243
00016717 00000-0 10270-3 0 9063
2 25544 51
6423 162
6465 0001481 297
3162 62
7837 15
49365192 26553
Satellite: ISS
Catalog Number: 25544
Epoch time: 20133
99752243 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 162
6465 deg
Eccentricity:
0001481
Arg of perigee: 297
3162 deg
Mean anomaly: 62
7837 deg
Mean motion: 15
49365192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2655
Checksum: 320
Coasting Arc #8 (Orbit 2669)
---------------------------------------
Vector Time (GMT): 2020/134/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6320611
33 A = 6800883
93 meter
Y = -627544
71 meter E =
0004246
Z = -2427447
74 I = 51
80289
XDOT = -1535
187138 Wp = 140
36698
YDOT = 5246
200980 meter/sec RA = 156
82970 deg
ZDOT = -5361
944207 TA = 66
64984
MA = 66
60518
Ha = 228
103 n
mi
Hp = 222
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20736913
81 X = 6338950
10
Y = -2058873
72 feet Y = -556760
39 meter
Z = -7964067
40 Z = -2396700
23
XDOT = -5036
703210 XDOT = -1567
692387
YDOT = 17211
945474 feet/sec YDOT = 5228
852144 meter/sec
ZDOT = -17591
680470 ZDOT = -5369
480030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17240200
09 X = -5254812
99
Y = 11801070
30 feet Y = 3596966
23 meter
Z = -7822733
90 Z = -2384369
29
XDOT = -3102
454989 XDOT = -945
628281
YDOT = -16198
165176 feet/sec YDOT = -4937
200746 meter/sec
ZDOT = -17626
467856 ZDOT = -5372
547402
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 20134
96502106
00016717 00000-0 10270-3 0 9073
2 25544 51
6413 157
8583 0001474 295
4795 64
6203 15
49340706 26701
Satellite: ISS
Catalog Number: 25544
Epoch time: 20134
96502106 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 157
8583 deg
Eccentricity:
0001474
Arg of perigee: 295
4795 deg
Mean anomaly: 64
6203 deg
Mean motion: 15
49340706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2670
Checksum: 308
Coasting Arc #9 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2020/135/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4960006
86 A = 6794964
38 meter
Y = 1372789
95 meter E =
0008355
Z = -4445456
64 I = 51
80953
XDOT = -4447
352013 Wp = 62
27898
YDOT = 5256
394940 meter/sec RA = 152
66598 deg
ZDOT = -3339
932065 TA = 173
99508
MA = 173
98506
Ha = 228
122 n
mi
Hp = 222
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16272988
38 X = 4965880
75
Y = 4503904
02 feet Y = 1428289
45 meter
Z = -14584831
50 Z = -4421348
51
XDOT = -14591
049912 XDOT = -4489
576576
YDOT = 17245
390224 feet/sec YDOT = 5206
425641 meter/sec
ZDOT = -10957
782366 ZDOT = -3361
637712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12606132
05 X = -3842349
05
Y = -11375397
54 feet Y = -3467221
17 meter
Z = -14474058
79 Z = -4411693
12
XDOT = 19884
621751 XDOT = 6060
832710
YDOT = -7970
469543 feet/sec YDOT = -2429
399117 meter/sec
ZDOT = -11057
707885 ZDOT = -3370
389363
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 20135
80352062
00016717 00000-0 10270-3 0 9082
2 25544 51
6415 153
7081 0001315 307
3009 52
8021 15
49384728 26839
Satellite: ISS
Catalog Number: 25544
Epoch time: 20135
80352062 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 153
7081 deg
Eccentricity:
0001315
Arg of perigee: 307
3009 deg
Mean anomaly: 52
8021 deg
Mean motion: 15
49384728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 285
Coasting Arc #10 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2020/136/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4969413
08 A = 6794755
95 meter
Y = -1051812
18 meter E =
0007804
Z = 4508016
84 I = 51
83813
XDOT = 4118
299149 Wp = 108
84940
YDOT = -5599
139971 meter/sec RA = 147
72945 deg
ZDOT = 3226
390238 TA = 308
73855
MA = 308
80828
Ha = 228
274 n
mi
Hp = 222
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16303848
68 X = -4979179
46
Y = -3450827
35 feet Y = -1107438
58 meter
Z = 14790081
50 Z = 4483853
56
XDOT = 13511
480149 XDOT = 4164
932336
YDOT = -18369
881796 feet/sec YDOT = -5552
825679 meter/sec
ZDOT = 10585
269809 ZDOT = 3246
508261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13285645
29 X = 4049464
68
Y = 10221928
21 feet Y = 3115643
72 meter
Z = 14679033
17 Z = 4474169
31
XDOT = -19329
872237 XDOT = -5891
745058
YDOT = 9756
222422 feet/sec YDOT = 2973
696594 meter/sec
ZDOT = 10677
923053 ZDOT = 3254
630946
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 20136
83551722
00016717 00000-0 10270-3 0 9091
2 25544 51
6417 148
6005 0001339 307
3624 52
7404 15
49368233 26993
Satellite: ISS
Catalog Number: 25544
Epoch time: 20136
83551722 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 148
6005 deg
Eccentricity:
0001339
Arg of perigee: 307
3624 deg
Mean anomaly: 52
7404 deg
Mean motion: 15
49368233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 308
Coasting Arc #11 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2020/137/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4962401
29 A = 6794403
34 meter
Y = 755286
45 meter E =
0009308
Z = -4588452
58 I = 51
86606
XDOT = -3759
035149 Wp = 62
04725
YDOT = 5903
630918 meter/sec RA = 142
79465 deg
ZDOT = -3094
164824 TA = 177
02065
MA = 177
01510
Ha = 228
139 n
mi
Hp = 222
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16280844
12 X = 4975874
81
Y = 2477973
90 feet Y = 810855
14 meter
Z = -15053978
28 Z = -4564314
31
XDOT = -12332
792483 XDOT = -3809
742177
YDOT = 19368
867840 feet/sec YDOT = 5861
311364 meter/sec
ZDOT = -10151
459397 ZDOT = -3112
547648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13846957
37 X = -4220552
61
Y = -9099246
12 feet Y = -2773450
22 meter
Z = -14943024
92 Z = -4554634
00
XDOT = 18573
884293 XDOT = 5661
319932
YDOT = -11458
060409 feet/sec YDOT = -3492
416813 meter/sec
ZDOT = -10236
160310 ZDOT = -3119
981663
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 20137
80301100
00016717 00000-0 10270-3 0 9104
2 25544 51
6427 143
8122 0001435 315
6503 44
4532 15
49392718 27149
Satellite: ISS
Catalog Number: 25544
Epoch time: 20137
80301100 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 143
8122 deg
Eccentricity:
0001435
Arg of perigee: 315
6503 deg
Mean anomaly: 44
4532 deg
Mean motion: 15
49392718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 267
Coasting Arc #12 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2020/138/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4932036
03 A = 6794224
45 meter
Y = -452320
53 meter E =
0007223
Z = 4646347
84 I = 51
89057
XDOT = 3377
110991 Wp = 109
86574
YDOT = -6202
279677 meter/sec RA = 137
86143 deg
ZDOT = 2974
822660 TA = 310
54031
MA = 310
60320
Ha = 228
376 n
mi
Hp = 222
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16181220
56 X = -4949180
96
Y = -1483991
24 feet Y = -507570
20 meter
Z = 15243923
37 Z = 4622348
09
XDOT = 11079
760468 XDOT = 3431
765631
YDOT = -20348
686603 feet/sec YDOT = -6164
208991 meter/sec
ZDOT = 9759
916865 ZDOT = 2991
359867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14311361
07 X = 4362102
85
Y = 7910170
96 feet Y = 2411020
11 meter
Z = 15133587
43 Z = 4612717
45
XDOT = -17692
879429 XDOT = -5392
789650
YDOT = 13153
378871 feet/sec YDOT = 4009
149880 meter/sec
ZDOT = 9836
158185 ZDOT = 2998
061015
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 20138
83500462
00016717 00000-0 10270-3 0 9111
2 25544 51
6420 138
7044 0001371 321
0367 39
0685 15
49367858 27300
Satellite: ISS
Catalog Number: 25544
Epoch time: 20138
83500462 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 138
7044 deg
Eccentricity:
0001371
Arg of perigee: 321
0367 deg
Mean anomaly: 39
0685 deg
Mean motion: 15
49367858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 295
Coasting Arc #13 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2020/139/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4892305
25 A = 6793887
79 meter
Y = 172813
57 meter E =
0010153
Z = -4720822
07 I = 51
91381
XDOT = -2967
373651 Wp = 62
66693
YDOT = 6456
503413 meter/sec RA = 132
93040 deg
ZDOT = -2838
966458 TA = 179
21001
MA = 179
20840
Ha = 228
152 n
mi
Hp = 222
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16050870
23 X = 4912940
50
Y = 566973
64 feet Y = 227638
48 meter
Z = -15488261
38 Z = -4697006
77
XDOT = -9735
477856 XDOT = -3025
561417
YDOT = 21182
753979 feet/sec YDOT = 6422
994958 meter/sec
ZDOT = -9314
194417 ZDOT = -2853
521882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14681116
73 X = -4474804
38
Y = -6767336
55 feet Y = -2062684
18 meter
Z = -15378754
91 Z = -4687444
50
XDOT = 16614
772692 XDOT = 5064
182717
YDOT = -14726
293617 feet/sec YDOT = -4488
574294 meter/sec
ZDOT = -9381
349935 ZDOT = -2859
435460
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 20139
80249665
00016717 00000-0 10270-3 0 9125
2 25544 51
6420 133
9165 0001547 319
8339 40
2697 15
49392931 27453
Satellite: ISS
Catalog Number: 25544
Epoch time: 20139
80249665 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 133
9165 deg
Eccentricity:
0001547
Arg of perigee: 319
8339 deg
Mean anomaly: 40
2697 deg
Mean motion: 15
49392931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 322
Coasting Arc #14 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2020/140/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4828556
13 A = 6793711
42 meter
Y = 108329
35 meter E =
0006443
Z = 4773697
03 I = 51
93563
XDOT = 2538
373245 Wp = 111
45113
YDOT = -6701
580838 meter/sec RA = 127
99990 deg
ZDOT = 2714
387933 TA = 311
78386
MA = 311
83890
Ha = 228
395 n
mi
Hp = 222
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15841719
57 X = -4852596
84
Y = 355411
27 feet Y = 54198
22 meter
Z = 15661735
65 Z = 4750183
07
XDOT = 8327
996211 XDOT = 2599
938522
YDOT = -21986
813772 feet/sec YDOT = -6672
850913 meter/sec
ZDOT = 8905
472221 ZDOT = 2726
867559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14944075
65 X = 4554954
26
Y = 5580020
46 feet Y = 1700790
24 meter
Z = 15553595
54 Z = 4740735
92
XDOT = -15420
493098 XDOT = -4700
166296
YDOT = 16266
503381 feet/sec YDOT = 4958
030231 meter/sec
ZDOT = 8963
111023 ZDOT = 2731
956240
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 20140
83448776
00016717 00000-0 10270-3 0 9135
2 25544 51
6425 128
8083 0001510 325
1781 34
9270 15
49370196 27615
Satellite: ISS
Catalog Number: 25544
Epoch time: 20140
83448776 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 128
8083 deg
Eccentricity:
0001510
Arg of perigee: 325
1781 deg
Mean anomaly: 34
9270 deg
Mean motion: 15
49370196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 304
Coasting Arc #15 (Orbit 2775)
---------------------------------------
Vector Time (GMT): 2020/141/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4760912
73 A = 6793381
38 meter
Y = -366304
57 meter E =
0011077
Z = -4842709
75 I = 51
95444
XDOT = -2087
480480 Wp = 63
47445
YDOT = 6896
657854 meter/sec RA = 123
07085 deg
ZDOT = -2573
629553 TA = 181
23993
MA = 181
24268
Ha = 228
202 n
mi
Hp = 222
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15619792
41 X = 4788178
51
Y = -1201786
64 feet Y = -312911
75 meter
Z = -15888155
36 Z = -4819516
53
XDOT = -6848
689240 XDOT = -2151
944384
YDOT = 22626
830230 feet/sec YDOT = 6872
953960 meter/sec
ZDOT = -8443
666511 ZDOT = -2583
925816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15131927
31 X = -4612211
44
Y = -4452600
67 feet Y = -1357152
69 meter
Z = -15781470
46 Z = -4810192
20
XDOT = 14048
570158 XDOT = 4282
004184
YDOT = -17644
385092 feet/sec YDOT = -5378
008576 meter/sec
ZDOT = -8491
293673 ZDOT = -2588
146312
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 20141
80197541
00016717 00000-0 10270-3 0 9145
2 25544 51
6424 124
0196 0001690 327
9882 32
1165 15
49398970 27767
Satellite: ISS
Catalog Number: 25544
Epoch time: 20141
80197541 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 124
0196 deg
Eccentricity:
0001690
Arg of perigee: 327
9882 deg
Mean anomaly: 32
1165 deg
Mean motion: 15
49398970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2776
Checksum: 316
Coasting Arc #16 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2020/142/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4670102
07 A = 6793241
90 meter
Y = 621840
39 meter E =
0005802
Z = 4890163
97 I = 51
97056
XDOT = 1620
205098 Wp = 111
06583
YDOT = -7080
229712 meter/sec RA = 118
14304 deg
ZDOT = 2443
265844 TA = 315
03422
MA = 315
08118
Ha = 228
500 n
mi
Hp = 222
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15321857
17 X = -4700462
60
Y = 2040158
77 feet Y = 569445
68 meter
Z = 16043845
05 Z = 4867404
38
XDOT = 5315
633523 XDOT = 1687
389719
YDOT = -23229
100105 feet/sec YDOT = -7061
736047 meter/sec
ZDOT = 8015
964054 ZDOT = 2451
298687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15210705
13 X = 4636222
92
Y = 3302272
22 feet Y = 1006532
57 meter
Z = 15939133
18 Z = 4858247
79
XDOT = -12571
897810 XDOT = -3831
914452
YDOT = 18967
748496 feet/sec YDOT = 5781
369742 meter/sec
ZDOT = 8053
211892 ZDOT = 2454
618985
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 20142
83396338
00016717 00000-0 10270-3 0 9155
2 25544 51
6419 118
9116 0001613 335
9416 24
1659 15
49367528 27924
Satellite: ISS
Catalog Number: 25544
Epoch time: 20142
83396338 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 118
9116 deg
Eccentricity:
0001613
Arg of perigee: 335
9416 deg
Mean anomaly: 24
1659 deg
Mean motion: 15
49367528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 323
Coasting Arc #17 (Orbit 2793)
---------------------------------------
Vector Time (GMT): 2020/142/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1199101
89 A = 6800888
97 meter
Y = 6279973
36 meter E =
0006214
Z = -2312444
41 I = 51
99530
XDOT = -5293
780817 Wp = 34
40788
YDOT = 989
566195 meter/sec RA = 117
22731 deg
ZDOT = 5444
557851 TA = 300
01950
MA = 300
08114
Ha = 228
295 n
mi
Hp = 222
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3934061
33 X = -1258004
58
Y = 20603587
15 feet Y = 6266235
08 meter
Z = -7586759
88 Z = -2318411
62
XDOT = -17368
047301 XDOT = -5330
899994
YDOT = 3246
608251 feet/sec YDOT = 930
159191 meter/sec
ZDOT = 17862
722607 ZDOT = 5418
752247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11562425
20 X = -3524227
20
Y = -17489243
53 feet Y = -5330721
43 meter
Z = -7614476
46 Z = -2320892
43
XDOT = 9013
739531 XDOT = 2747
387809
YDOT = -13667
279227 feet/sec YDOT = -4165
786708 meter/sec
ZDOT = 17743
982043 ZDOT = 5408
365727
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 20142
96296163
00016717 00000-0 10270-3 0 9165
2 25544 51
6381 118
2683 0001204 329
9139 30
1941 15
49381575 27946
Satellite: ISS
Catalog Number: 25544
Epoch time: 20142
96296163 = yrday
fracday
Element set: 916
Inclination: 51
6381 deg
RA of node: 118
2683 deg
Eccentricity:
0001204
Arg of perigee: 329
9139 deg
Mean anomaly: 30
1941 deg
Mean motion: 15
49381575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2794
Checksum: 315
Coasting Arc #18 (Orbit 2809)
---------------------------------------
Vector Time (GMT): 2020/143/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 784925
22 A = 6801116
14 meter
Y = -6390002
38 meter E =
0012821
Z = 2175184
28 I = 52
01058
XDOT = 5168
927345 Wp = 105
54430
YDOT = -1250
658759 meter/sec RA = 112
30266 deg
ZDOT = -5515
611015 TA = 50
49311
MA = 50
37983
Ha = 228
249 n
mi
Hp = 222
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2575213
99 X = 845755
82
Y = -20964574
73 feet Y = -6380884
96 meter
Z = 7136431
36 Z = 2179144
08
XDOT = 16958
423048 XDOT = 5209
320532
YDOT = -4103
211150 feet/sec YDOT = -1192
629532 meter/sec
ZDOT = -18095
836663 ZDOT = -5490
404037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13073935
52 X = 3984935
55
Y = 16581701
37 feet Y = 5054102
58 meter
Z = 7154939
76 Z = 2180825
64
XDOT = -7933
862835 XDOT = -2418
241392
YDOT = 14047
130019 feet/sec YDOT = 4281
565230 meter/sec
ZDOT = -17979
823623 ZDOT = -5480
250240
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 20143
99494680
00016717 00000-0 10270-3 0 9174
2 25544 51
6381 113
1605 0001373 328
8658 31
2410 15
49396873 28104
Satellite: ISS
Catalog Number: 25544
Epoch time: 20143
99494680 = yrday
fracday
Element set: 917
Inclination: 51
6381 deg
RA of node: 113
1605 deg
Eccentricity:
0001373
Arg of perigee: 328
8658 deg
Mean anomaly: 31
2410 deg
Mean motion: 15
49396873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2810
Checksum: 312
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list