[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 12th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13861 7638 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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
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
7
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 2631)
---------------------------------------
Vector Time (GMT): 2020/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -624897
16 A = 6791838
27 meter
Y = 4321167
82 meter E =
0012815
Z = -5213854
77 I = 51
69391
XDOT = -7529
497147 Wp = 99
87349
YDOT = 454
716911 meter/sec RA = 168
84179 deg
ZDOT = 1279
840427 TA = 182
43161
MA = 182
43784
Ha = 228
097 n
mi
Hp = 222
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2050187
53 X = -647845
25
Y = 14177059
77 feet Y = 4314052
09 meter
Z = -17105822
74 Z = -5216945
51
XDOT = -24703
074628 XDOT = -7540
239079
YDOT = 1491
853383 feet/sec YDOT = 370
456501 meter/sec
ZDOT = 4198
951532 ZDOT = 1243
238864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9398735
22 X = 2864734
49
Y = 10787301
39 feet Y = 3287969
46 meter
Z = -17120145
13 Z = -5218220
24
XDOT = -14369
559111 XDOT = -4379
841617
YDOT = 18914
165423 feet/sec YDOT = 5765
037621 meter/sec
ZDOT = 4030
784303 ZDOT = 1228
583055
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
51402350
00016717 00000-0 10270-3 0 9005
2 25544 51
6408 169
9870 0001234 279
6298 80
4713 15
49338984 26329
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
51402350 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 169
9870 deg
Eccentricity:
0001234
Arg of perigee: 279
6298 deg
Mean anomaly: 80
4713 deg
Mean motion: 15
49338984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2632
Checksum: 308
Coasting Arc #2 (Orbit 2638)
---------------------------------------
Vector Time (GMT): 2020/132/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6431367
55 A = 6801351
93 meter
Y = 256838
09 meter E =
0005131
Z = -2191707
18 I = 51
74124
XDOT = -2062
318129 Wp = 147
93826
YDOT = 4930
713567 meter/sec RA = 166
71051 deg
ZDOT = -5484
013062 TA = 56
29830
MA = 56
24940
Ha = 228
062 n
mi
Hp = 222
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21100287
24 X = 6438663
61
Y = 842644
64 feet Y = 328799
27 meter
Z = -7190640
35 Z = -2160448
27
XDOT = -6766
135594 XDOT = -2090
663280
YDOT = 16176
881782 feet/sec YDOT = 4907
493412 meter/sec
ZDOT = -17992
168837 ZDOT = -5494
099295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19262286
07 X = -5871144
79
Y = 8771614
35 feet Y = 2673588
06 meter
Z = -7047027
55 Z = -2147934
00
XDOT = -712
780674 XDOT = -217
255549
YDOT = -16030
057639 feet/sec YDOT = -4885
961568 meter/sec
ZDOT = -18038
651196 ZDOT = -5498
180884
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
96552426
00016717 00000-0 10270-3 0 9015
2 25544 51
6422 167
7548 0001489 283
8069 76
2915 15
49334977 26390
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
96552426 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 167
7548 deg
Eccentricity:
0001489
Arg of perigee: 283
8069 deg
Mean anomaly: 76
2915 deg
Mean motion: 15
49334977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2639
Checksum: 339
Coasting Arc #3 (Orbit 2654)
---------------------------------------
Vector Time (GMT): 2020/133/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6391800
36 A = 6801079
27 meter
Y = 201490
00 meter E =
0012810
Z = 2295810
98 I = 51
77303
XDOT = 1797
435437 Wp = 67
38227
YDOT = -5097
112292 meter/sec RA = 161
76821 deg
ZDOT = 5432
223742 TA = 318
09295
MA = 318
19092
Ha = 228
095 n
mi
Hp = 222
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20970473
61 X = -6404730
16
Y = 661056
42 feet Y = 129939
80 meter
Z = 7532188
24 Z = 2264730
72
XDOT = 5897
097891 XDOT = 1827
912634
YDOT = -16722
809356 feet/sec YDOT = -5076
842242 meter/sec
ZDOT = 17822
256370 ZDOT = 5441
028478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18295583
26 X = 5576493
78
Y = -10373071
82 feet Y = -3161712
29 meter
Z = 7389359
43 Z = 2252276
76
XDOT = 1917
950579 XDOT = 584
591336
YDOT = 16153
769460 feet/sec YDOT = 4923
668931 meter/sec
ZDOT = 17862
863647 ZDOT = 5444
600840
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
99752381
00016717 00000-0 10270-3 0 9022
2 25544 51
6422 162
6462 0001512 297
6235 62
4762 15
49363994 26550
Satellite: ISS
Catalog Number: 25544
Epoch time: 20133
99752381 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 162
6462 deg
Eccentricity:
0001512
Arg of perigee: 297
6235 deg
Mean anomaly: 62
4762 deg
Mean motion: 15
49363994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2655
Checksum: 316
Coasting Arc #4 (Orbit 2669)
---------------------------------------
Vector Time (GMT): 2020/134/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6320922
42 A = 6800890
34 meter
Y = -628634
01 meter E =
0004218
Z = -2426385
75 I = 51
80283
XDOT = -1533
571780 Wp = 140
42584
YDOT = 5246
055159 meter/sec RA = 156
82926 deg
ZDOT = -5362
536951 TA = 66
57819
MA = 66
53384
Ha = 228
098 n
mi
Hp = 222
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20737934
45 X = 6339268
19
Y = -2062447
55 feet Y = -557846
17 meter
Z = -7960583
18 Z = -2395636
71
XDOT = -5031
403478 XDOT = -1566
072639
YDOT = 17211
467058 feet/sec YDOT = 5228
724412 meter/sec
ZDOT = -17593
625168 ZDOT = -5370
064917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17239356
16 X = -5254555
76
Y = 11804683
13 feet Y = 3598067
42 meter
Z = -7819242
62 Z = -2383305
15
XDOT = -3106
620043 XDOT = -946
897789
YDOT = -16195
252906 feet/sec YDOT = -4936
313086 meter/sec
ZDOT = -17628
376438 ZDOT = -5373
129138
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
96502328
00016717 00000-0 10270-3 0 9035
2 25544 51
6413 157
8580 0001504 295
8996 64
1999 15
49339251 26709
Satellite: ISS
Catalog Number: 25544
Epoch time: 20134
96502328 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 157
8580 deg
Eccentricity:
0001504
Arg of perigee: 295
8996 deg
Mean anomaly: 64
1999 deg
Mean motion: 15
49339251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2670
Checksum: 328
Coasting Arc #5 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2020/135/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4961230
68 A = 6794972
67 meter
Y = 1371326
17 meter E =
0008343
Z = -4444545
99 I = 51
80948
XDOT = -4445
619858 Wp = 62
06253
YDOT = 5256
900365 meter/sec RA = 152
66555 deg
ZDOT = -3341
447420 TA = 174
19398
MA = 174
18430
Ha = 228
118 n
mi
Hp = 222
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16277003
55 X = 4967116
42
Y = 4499101
62 feet Y = 1426839
43 meter
Z = -14581843
81 Z = -4420431
89
XDOT = -14585
366987 XDOT = -4487
842841
YDOT = 17247
048443 feet/sec YDOT = 5206
950445 meter/sec
ZDOT = -10962
754003 ZDOT = -3363
144649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12611857
85 X = -3844094
27
Y = -11372900
59 feet Y = -3466460
10 meter
Z = -14471043
60 Z = -4410774
09
XDOT = 19880
440530 XDOT = 6059
558274
YDOT = -7974
100468 feet/sec YDOT = -2430
505823 meter/sec
ZDOT = -11062
640845 ZDOT = -3371
892930
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
80352369
00016717 00000-0 10270-3 0 9048
2 25544 51
6415 153
7077 0001346 307
5784 52
5244 15
49383064 26836
Satellite: ISS
Catalog Number: 25544
Epoch time: 20135
80352369 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 153
7077 deg
Eccentricity:
0001346
Arg of perigee: 307
5784 deg
Mean anomaly: 52
5244 deg
Mean motion: 15
49383064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 308
Coasting Arc #6 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2020/136/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4970911
13 A = 6794766
04 meter
Y = -1049762
85 meter E =
0007783
Z = 4506856
14 I = 51
83809
XDOT = 4115
960248 Wp = 108
68637
YDOT = -5599
655836 meter/sec RA = 147
72903 deg
ZDOT = 3228
468604 TA = 308
87830
MA = 308
94771
Ha = 228
272 n
mi
Hp = 222
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16308763
55 X = -4980694
68
Y = -3444103
84 feet Y = -1105406
10 meter
Z = 14786273
42 Z = 4482685
54
XDOT = 13503
806587 XDOT = 4162
589282
YDOT = -18371
574264 feet/sec YDOT = -5553
367721 meter/sec
ZDOT = 10592
088596 ZDOT = 3248
575255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13292965
97 X = 4051696
03
Y = 10217989
77 feet Y = 3114443
28 meter
Z = 14675191
39 Z = 4472998
33
XDOT = -19323
936910 XDOT = -5889
935970
YDOT = 9760
560772 feet/sec YDOT = 2975
018923 meter/sec
ZDOT = 10684
689581 ZDOT = 3256
693384
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
83552148
00016717 00000-0 10270-3 0 9050
2 25544 51
6416 148
6002 0001370 307
7284 52
3742 15
49366301 26995
Satellite: ISS
Catalog Number: 25544
Epoch time: 20136
83552148 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 148
6002 deg
Eccentricity:
0001370
Arg of perigee: 307
7284 deg
Mean anomaly: 52
3742 deg
Mean motion: 15
49366301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 299
Coasting Arc #7 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2020/137/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4964230
84 A = 6794415
41 meter
Y = 752397
70 meter E =
0009297
Z = -4586955
73 I = 51
86601
XDOT = -3755
968033 Wp = 61
83653
YDOT = 5904
119238 meter/sec RA = 142
79424 deg
ZDOT = -3096
958619 TA = 177
20017
MA = 177
19496
Ha = 228
138 n
mi
Hp = 222
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16286846
59 X = 4977729
25
Y = 2468496
39 feet Y = 807987
00 meter
Z = -15049067
34 Z = -4562808
51
XDOT = -12322
729766 XDOT = -3806
667179
YDOT = 19370
469942 feet/sec YDOT = 5861
834028 meter/sec
ZDOT = -10160
625390 ZDOT = -3115
326524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13856341
68 X = -4223412
94
Y = -9093132
12 feet Y = -2771586
67 meter
Z = -14938072
76 Z = -4553124
58
XDOT = 18565
802078 XDOT = 5658
856473
YDOT = -11463
063766 feet/sec YDOT = -3493
941836 meter/sec
ZDOT = -10245
257733 ZDOT = -3122
754557
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
80301653
00016717 00000-0 10270-3 0 9062
2 25544 51
6427 143
8119 0001466 315
8884 44
2149 15
49390576 27145
Satellite: ISS
Catalog Number: 25544
Epoch time: 20137
80301653 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 143
8119 deg
Eccentricity:
0001466
Arg of perigee: 315
8884 deg
Mean anomaly: 44
2149 deg
Mean motion: 15
49390576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 311
Coasting Arc #8 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2020/138/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4934063
90 A = 6794238
50 meter
Y = -448581
32 meter E =
0007209
Z = 4644570
54 I = 51
89053
XDOT = 3373
297797 Wp = 109
65235
YDOT = -6202
648775 meter/sec RA = 137
86104 deg
ZDOT = 2978
370883 TA = 310
71505
MA = 310
77764
Ha = 228
377 n
mi
Hp = 222
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16187873
68 X = -4951241
86
Y = -1471723
48 feet Y = -503853
84 meter
Z = 15238092
33 Z = 4620560
86
XDOT = 11067
249989 XDOT = 3427
939613
YDOT = -20349
897556 feet/sec YDOT = -6164
620804 meter/sec
ZDOT = 9771
558016 ZDOT = 2994
889535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14322351
42 X = 4365452
71
Y = 7901601
35 feet Y = 2408408
09 meter
Z = 15127710
61 Z = 4610926
19
XDOT = -17682
466032 XDOT = -5389
615646
YDOT = 13158
751018 feet/sec YDOT = 4010
787310 meter/sec
ZDOT = 9847
714036 ZDOT = 3001
583238
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
83501166
00016717 00000-0 10270-3 0 9078
2 25544 51
6419 138
7040 0001403 321
2671 38
8379 15
49365446 27308
Satellite: ISS
Catalog Number: 25544
Epoch time: 20138
83501166 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 138
7040 deg
Eccentricity:
0001403
Arg of perigee: 321
2671 deg
Mean anomaly: 38
8379 deg
Mean motion: 15
49365446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 300
Coasting Arc #9 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2020/139/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4894532
63 A = 6793903
94 meter
Y = 167954
00 meter E =
0010142
Z = -4718700
70 I = 51
91377
XDOT = -2962
712046 Wp = 62
45546
YDOT = 6456
684071 meter/sec RA = 132
93003 deg
ZDOT = -2843
418890 TA = 179
37326
MA = 179
37198
Ha = 228
153 n
mi
Hp = 222
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16058177
91 X = 4915211
75
Y = 551030
19 feet Y = 222804
07 meter
Z = -15481301
51 Z = -4694874
47
XDOT = -9720
183877 XDOT = -3020
880552
YDOT = 21183
346691 feet/sec YDOT = 6423
227854 meter/sec
ZDOT = -9328
802134 ZDOT = -2857
951623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14693975
47 X = -4478723
72
Y = -6755439
32 feet Y = -2059057
90 meter
Z = -15371744
63 Z = -4685307
76
XDOT = 16601
672664 XDOT = 5060
189828
YDOT = -14731
852168 feet/sec YDOT = -4490
268541 meter/sec
ZDOT = -9395
853316 ZDOT = -2863
856091
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
80250524
00016717 00000-0 10270-3 0 9086
2 25544 51
6419 133
9162 0001579 320
1299 39
9735 15
49390296 27453
Satellite: ISS
Catalog Number: 25544
Epoch time: 20139
80250524 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 133
9162 deg
Eccentricity:
0001579
Arg of perigee: 320
1299 deg
Mean anomaly: 39
9735 deg
Mean motion: 15
49390296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 323
Coasting Arc #10 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2020/140/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4830816
34 A = 6793729
67 meter
Y = 114316
31 meter E =
0006435
Z = 4771283
72 I = 51
93560
XDOT = 2532
851536 Wp = 111
17889
YDOT = -6701
473886 meter/sec RA = 127
99954 deg
ZDOT = 2719
803124 TA = 311
99861
MA = 312
05340
Ha = 228
398 n
mi
Hp = 222
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15849134
97 X = -4854912
12
Y = 375053
51 feet Y = 60159
59 meter
Z = 15653817
97 Z = 4747758
65
XDOT = 8309
880369 XDOT = 2594
389724
YDOT = -21986
462880 feet/sec YDOT = -6672
805860 meter/sec
ZDOT = 8923
238595 ZDOT = 2732
255861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14958192
74 X = 4559257
15
Y = 5564506
01 feet Y = 1696061
43 meter
Z = 15545626
53 Z = 4738306
97
XDOT = -15404
556587 XDOT = -4695
308848
YDOT = 16271
906224 feet/sec YDOT = 4959
677017 meter/sec
ZDOT = 8980
753739 ZDOT = 2737
333740
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
83449818
00016717 00000-0 10270-3 0 9098
2 25544 51
6425 128
8080 0001542 325
4655 34
6395 15
49367287 27612
Satellite: ISS
Catalog Number: 25544
Epoch time: 20140
83449818 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 128
8080 deg
Eccentricity:
0001542
Arg of perigee: 325
4655 deg
Mean anomaly: 34
6395 deg
Mean motion: 15
49367287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 324
Coasting Arc #11 (Orbit 2775)
---------------------------------------
Vector Time (GMT): 2020/141/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4763147
28 A = 6793401
89 meter
Y = -373698
42 meter E =
0011066
Z = -4839964
13 I = 51
95442
XDOT = -2081
015526 Wp = 63
25845
YDOT = 6896
169395 meter/sec RA = 123
07052 deg
ZDOT = -2580
158711 TA = 181
38708
MA = 181
39015
Ha = 228
207 n
mi
Hp = 222
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15627123
63 X = 4790482
24
Y = -1226044
70 feet Y = -320280
23 meter
Z = -15879147
41 Z = -4816759
89
XDOT = -6827
478761 XDOT = -2145
442733
YDOT = 22625
227673 feet/sec YDOT = 6872
538002 meter/sec
ZDOT = -8465
087634 ZDOT = -2590
423480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15147326
57 X = -4616905
14
Y = -4432497
40 feet Y = -1351025
21 meter
Z = -15772411
53 Z = -4807431
03
XDOT = 14029
499514 XDOT = 4276
191452
YDOT = -17649
335555 feet/sec YDOT = -5379
517477 meter/sec
ZDOT = -8512
569931 ZDOT = -2594
631315
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
80198772
00016717 00000-0 10270-3 0 9108
2 25544 51
6423 124
0193 0001723 328
2523 31
8523 15
49395788 27764
Satellite: ISS
Catalog Number: 25544
Epoch time: 20141
80198772 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 124
0193 deg
Eccentricity:
0001723
Arg of perigee: 328
2523 deg
Mean anomaly: 31
8523 deg
Mean motion: 15
49395788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2776
Checksum: 306
Coasting Arc #12 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2020/142/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672106
98 A = 6793264
48 meter
Y = 630636
10 meter E =
0005803
Z = 4887135
13 I = 51
97054
XDOT = 1612
788865 Wp = 110
73669
YDOT = -7079
255084 meter/sec RA = 118
14274 deg
ZDOT = 2450
989748 TA = 315
28324
MA = 315
33002
Ha = 228
506 n
mi
Hp = 222
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15328434
97 X = -4702551
01
Y = 2069016
08 feet Y = 578218
50 meter
Z = 16033907
91 Z = 4864365
60
XDOT = 5291
302050 XDOT = 1679
925619
YDOT = -23225
902508 feet/sec YDOT = -7060
844622 meter/sec
ZDOT = 8041
304948 ZDOT = 2458
986449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15226598
13 X = 4641067
11
Y = 3277322
14 feet Y = 998927
79 meter
Z = 15929149
94 Z = 4855204
90
XDOT = -12549
577409 XDOT = -3825
111194
YDOT = 18971
873070 feet/sec YDOT = 5782
626912 meter/sec
ZDOT = 8078
386506 ZDOT = 2462
292207
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
83397788
00016717 00000-0 10270-3 0 9111
2 25544 51
6418 118
9112 0001646 336
1578 23
9495 15
49364084 27926
Satellite: ISS
Catalog Number: 25544
Epoch time: 20142
83397788 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 118
9112 deg
Eccentricity:
0001646
Arg of perigee: 336
1578 deg
Mean anomaly: 23
9495 deg
Mean motion: 15
49364084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 331
Coasting Arc #13 (Orbit 2793)
---------------------------------------
Vector Time (GMT): 2020/142/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1192280
33 A = 6800885
49 meter
Y = 6278700
12 meter E =
0006215
Z = -2319398
53 I = 51
99520
XDOT = -5295
731619 Wp = 34
27941
YDOT = 999
790994 meter/sec RA = 117
22691 deg
ZDOT = 5440
799490 TA = 300
06542
MA = 300
12705
Ha = 228
300 n
mi
Hp = 222
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3911680
88 X = -1251135
50
Y = 20599409
84 feet Y = 6265038
38 meter
Z = -7609575
23 Z = -2325332
48
XDOT = -17374
447568 XDOT = -5332
946731
YDOT = 3280
154179 feet/sec YDOT = 940
361639 meter/sec
ZDOT = 17850
392028 ZDOT = 5414
984178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11575687
07 X = -3528269
42
Y = -17470550
87 feet Y = -5325023
91 meter
Z = -7637138
80 Z = -2327799
91
XDOT = 8996
273657 XDOT = 2742
064211
YDOT = -13694
784049 feet/sec YDOT = -4174
170178 meter/sec
ZDOT = 17731
606371 ZDOT = 5404
593622
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
96297641
00016717 00000-0 10270-3 0 9123
2 25544 51
6380 118
2680 0001236 330
3710 29
7370 15
49378142 27944
Satellite: ISS
Catalog Number: 25544
Epoch time: 20142
96297641 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 118
2680 deg
Eccentricity:
0001236
Arg of perigee: 330
3710 deg
Mean anomaly: 29
7370 deg
Mean motion: 15
49378142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2794
Checksum: 301
Coasting Arc #14 (Orbit 2809)
---------------------------------------
Vector Time (GMT): 2020/143/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 777252
45 A = 6801112
36 meter
Y = -6388185
58 meter E =
0012806
Z = 2183328
75 I = 52
01047
XDOT = 5170
368933 Wp = 105
28656
YDOT = -1262
677826 meter/sec RA = 112
30227 deg
ZDOT = -5511
482848 TA = 50
65551
MA = 50
54209
Ha = 228
256 n
mi
Hp = 222
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2550040
85 X = 838023
74
Y = -20958614
12 feet Y = -6379154
30 meter
Z = 7163152
06 Z = 2187251
13
XDOT = 16963
152667 XDOT = 5210
876361
YDOT = -4142
643787 feet/sec YDOT = -1204
631841 meter/sec
ZDOT = -18082
292809 ZDOT = -5486
268591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13087599
05 X = 3989100
19
Y = 16559527
13 feet Y = 5047343
87 meter
Z = 7181488
27 Z = 2188917
62
XDOT = -7910
807702 XDOT = -2411
214188
YDOT = 14077
240995 feet/sec YDOT = 4290
743055 meter/sec
ZDOT = -17966
245735 ZDOT = -5476
111700
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
99496397
00016717 00000-0 10270-3 0 9137
2 25544 51
6380 113
1602 0001404 329
3756 30
7312 15
49393065 28105
Satellite: ISS
Catalog Number: 25544
Epoch time: 20143
99496397 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 113
1602 deg
Eccentricity:
0001404
Arg of perigee: 329
3756 deg
Mean anomaly: 30
7312 deg
Mean motion: 15
49393065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2810
Checksum: 296
Coasting Arc #15 (Orbit 2824)
---------------------------------------
Vector Time (GMT): 2020/144/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -323868
46 A = 6801312
53 meter
Y = 6465137
07 meter E =
0007149
Z = -2077809
66 I = 52
02513
XDOT = -5032
228767 Wp = 32
49390
YDOT = 1532
110106 meter/sec RA = 107
37810 deg
ZDOT = 5566
282224 TA = 304
69390
MA = 304
76124
Ha = 228
358 n
mi
Hp = 222
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1062560
57 X = -386046
52
Y = 21211079
62 feet Y = 6461168
00 meter
Z = -6816960
83 Z = -2079532
94
XDOT = -16509
936900 XDOT = -5076
025458
YDOT = 5026
607958 feet/sec YDOT = 1475
590406 meter/sec
ZDOT = 18262
080789 ZDOT = 5541
731142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14582015
66 X = -4444598
37
Y = -15436686
81 feet Y = -4705102
14 meter
Z = -6825203
90 Z = -2080322
15
XDOT = 6782
362680 XDOT = 2067
264145
YDOT = -14409
972304 feet/sec YDOT = -4392
159558 meter/sec
ZDOT = 18149
056401 ZDOT = 5531
832391
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 20144
96245251
00016717 00000-0 10270-3 0 9147
2 25544 51
6404 108
3714 0001226 338
8695 21
2404 15
49389259 28254
Satellite: ISS
Catalog Number: 25544
Epoch time: 20144
96245251 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 108
3714 deg
Eccentricity:
0001226
Arg of perigee: 338
8695 deg
Mean anomaly: 21
2404 deg
Mean motion: 15
49389259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2825
Checksum: 305
Coasting Arc #16 (Orbit 2840)
---------------------------------------
Vector Time (GMT): 2020/145/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -108930
76 A = 6801571
04 meter
Y = -6513230
41 meter E =
0013126
Z = 1936493
04 I = 52
03418
XDOT = 4888
485968 Wp = 108
32271
YDOT = -1763
674919 meter/sec RA = 102
45501 deg
ZDOT = -5629
781400 TA = 50
48866
MA = 50
37270
Ha = 228
398 n
mi
Hp = 222
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -357384
39 X = -45496
26
Y = -21368866
18 feet Y = -6514094
19 meter
Z = 6353323
63 Z = 1936116
88
XDOT = 16038
339789 XDOT = 4935
191116
YDOT = -5786
335037 feet/sec YDOT = -1708
746313 meter/sec
ZDOT = -18470
411417 ZDOT = -5605
921653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15925451
61 X = 4854077
65
Y = 14253206
25 feet Y = 4344377
27 meter
Z = 6351927
99 Z = 1936067
65
XDOT = -5724
748412 XDOT = -1744
903316
YDOT = 14618
542456 feet/sec YDOT = 4455
731741 meter/sec
ZDOT = -18360
540549 ZDOT = -5596
292759
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 20145
99443695
00016717 00000-0 10270-3 0 9154
2 25544 51
6397 103
2635 0001296 343
3483 16
7624 15
49386572 28410
Satellite: ISS
Catalog Number: 25544
Epoch time: 20145
99443695 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 103
2635 deg
Eccentricity:
0001296
Arg of perigee: 343
3483 deg
Mean anomaly: 16
7624 deg
Mean motion: 15
49386572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2841
Checksum: 328
Coasting Arc #17 (Orbit 2855)
---------------------------------------
Vector Time (GMT): 2020/146/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922720
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 575840
46 A = 6801736
03 meter
Y = 6522612
38 meter E =
0008125
Z = -1827958
37 I = 52
04209
XDOT = -4733
176239 Wp = 32
24610
YDOT = 2004
055725 meter/sec RA = 97
53326 deg
ZDOT = 5678
207791 TA = 307
81478
MA = 307
88830
Ha = 228
449 n
mi
Hp = 222
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1889240
34 X = 511739
10
Y = 21399646
92 feet Y = 6528693
74 meter
Z = -5997238
75 Z = -1825315
72
XDOT = -15528
793436 XDOT = -4782
816048
YDOT = 6574
985976 feet/sec YDOT = 1950
847457 meter/sec
ZDOT = 18629
290654 ZDOT = 5655
095511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17212906
25 X = -5246493
83
Y = -12859684
03 feet Y = -3919631
69 meter
Z = -5985430
22 Z = -1824359
13
XDOT = 4627
409135 XDOT = 1410
434304
YDOT = -14787
200540 feet/sec YDOT = -4507
138724 meter/sec
ZDOT = 18522
831493 ZDOT = 5645
759039
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 20146
96192250
00016717 00000-0 10270-3 0 9161
2 25544 51
6409 98
4759 0001224 349
1541 10
9582 15
49388474 28564
Satellite: ISS
Catalog Number: 25544
Epoch time: 20146
96192250 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 98
4759 deg
Eccentricity:
0001224
Arg of perigee: 349
1541 deg
Mean anomaly: 10
9582 deg
Mean motion: 15
49388474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2856
Checksum: 329
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