[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 3rd 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19920 769 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
160/04:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 221
6
Coasting Arc #1 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2020/152/23:25:30
983
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3777061
90 A = 6791031
55 meter
Y = 1804090
68 meter E =
0002870
Z = 5345318
24 I = 51
98684
XDOT = -3041
173565 Wp = 67
04333
YDOT = -7030
457846 meter/sec RA = 67
92314 deg
ZDOT = 224
905434 TA = 20
82775
MA = 20
81605
Ha = 228
681 n
mi
Hp = 221
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12391935
37 X = -3822919
69
Y = 5918932
67 feet Y = 1761595
98 meter
Z = 17537133
33 Z = 5326859
44
XDOT = -9977
603559 XDOT = -2963
423338
YDOT = -23065
806583 feet/sec YDOT = -7064
031707 meter/sec
ZDOT = 737
878722 ZDOT = 210
320713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1033983
52 X = 315158
18
Y = -13802221
26 feet Y = -4206917
04 meter
Z = 17452061
14 Z = 5319388
24
XDOT = 23979
507490 XDOT = 7308
953883
YDOT = 2640
973625 feet/sec YDOT = 804
968761 meter/sec
ZDOT = 671
211636 ZDOT = 204
585307
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 20153
02479753
00016717 00000-0 10270-3 0 9005
2 25544 51
6442 68
4689 0001535 7
9546 352
1628 15
49444327 29506
Satellite: ISS
Catalog Number: 25544
Epoch time: 20153
02479753 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 68
4689 deg
Eccentricity:
0001535
Arg of perigee: 7
9546 deg
Mean anomaly: 352
1628 deg
Mean motion: 15
49444327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 315
Coasting Arc #2 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2020/153/23:25:30
983
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3698360
42 A = 6791125
07 meter
Y = -1970054
77 meter E =
0015306
Z = -5357323
79 I = 51
97310
XDOT = 3519
234333 Wp = 83
40917
YDOT = 6791
647900 meter/sec RA = 62
99766 deg
ZDOT = -66
498628 TA = 185
94941
MA = 185
96761
Ha = 228
651 n
mi
Hp = 222
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12133728
40 X = 3746138
35
Y = -6463434
27 feet Y = -1928429
38 meter
Z = -17576521
61 Z = -5339242
58
XDOT = 11546
044400 XDOT = 3443
349567
YDOT = 22282
309382 feet/sec YDOT = 6830
578192 meter/sec
ZDOT = -218
171352 ZDOT = -49
587023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -194891
33 X = -59402
88
Y = 13852376
73 feet Y = 4222204
43 meter
Z = -17493173
98 Z = -5331919
43
XDOT = -24080
735728 XDOT = -7339
808250
YDOT = -523
022975 feet/sec YDOT = -159
417403 meter/sec
ZDOT = -140
797946 ZDOT = -42
915214
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 20153
99227081
00016717 00000-0 10270-3 0 9017
2 25544 51
6442 63
6817 0001653 13
2274 346
8920 15
49412384 29654
Satellite: ISS
Catalog Number: 25544
Epoch time: 20153
99227081 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 63
6817 deg
Eccentricity:
0001653
Arg of perigee: 13
2274 deg
Mean anomaly: 346
8920 deg
Mean motion: 15
49412384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2965
Checksum: 305
Coasting Arc #3 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2020/154/23:25:30
983
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3608146
61 A = 6791007
99 meter
Y = 2119668
32 meter E =
0003345
Z = 5346058
36 I = 51
95695
XDOT = -3988
736392 Wp = 57
45596
YDOT = -6542
848952 meter/sec RA = 58
06995 deg
ZDOT = -96
086275 TA = 33
46683
MA = 33
44570
Ha = 228
738 n
mi
Hp = 221
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11837751
34 X = -3657549
63
Y = 6954292
39 feet Y = 2079042
58 meter
Z = 17539561
56 Z = 5328411
43
XDOT = -13086
405484 XDOT = -3914
809121
YDOT = -21466
039869 feet/sec YDOT = -6587
040477 meter/sec
ZDOT = -315
243683 ZDOT = -115
283480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -615676
16 X = -187658
09
Y = -13818936
02 feet Y = -4212011
70 meter
Z = 17458198
91 Z = 5321259
03
XDOT = 24078
366512 XDOT = 7339
086113
YDOT = -1589
536964 feet/sec YDOT = -484
490867 meter/sec
ZDOT = -403
132820 ZDOT = -122
874884
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 20155
02423861
00016717 00000-0 10270-3 0 9028
2 25544 51
6444 58
5739 0001591 14
9565 345
1632 15
49449369 29817
Satellite: ISS
Catalog Number: 25544
Epoch time: 20155
02423861 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 58
5739 deg
Eccentricity:
0001591
Arg of perigee: 14
9565 deg
Mean anomaly: 345
1632 deg
Mean motion: 15
49449369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 319
Coasting Arc #4 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2020/155/23:25:30
983
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3524622
88 A = 6791150
62 meter
Y = -2282821
09 meter E =
0015313
Z = -5350320
81 I = 51
93806
XDOT = 4424
081324 Wp = 85
93439
YDOT = 6235
213735 meter/sec RA = 53
14211 deg
ZDOT = 255
752687 TA = 186
48941
MA = 186
50927
Ha = 228
691 n
mi
Hp = 222
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11563723
36 X = 3575877
26
Y = -7489570
50 feet Y = -2243118
88 meter
Z = -17553545
97 Z = -5333075
18
XDOT = 14514
702505 XDOT = 4352
786186
YDOT = 20456
737975 feet/sec YDOT = 6284
288288 meter/sec
ZDOT = 839
083620 ZDOT = 277
071198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1454569
75 X = 443352
86
Y = 13801572
89 feet Y = 4206719
42 meter
Z = -17474013
64 Z = -5326079
36
XDOT = -23784
781070 XDOT = -7249
601270
YDOT = 3685
675350 feet/sec YDOT = 1123
393847 meter/sec
ZDOT = 936
737490 ZDOT = 285
517587
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 20155
99170809
00016717 00000-0 10270-3 0 9036
2 25544 51
6442 53
7865 0001654 17
5320 342
5887 15
49412562 29964
Satellite: ISS
Catalog Number: 25544
Epoch time: 20155
99170809 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 53
7865 deg
Eccentricity:
0001654
Arg of perigee: 17
5320 deg
Mean anomaly: 342
5887 deg
Mean motion: 15
49412562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 324
Coasting Arc #5 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2020/156/23:25:30
983
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3432973
91 A = 6791053
07 meter
Y = 2427096
59 meter E =
0004001
Z = 5330609
97 I = 51
91794
XDOT = -4847
051180 Wp = 50
80885
YDOT = -5920
838898 meter/sec RA = 48
21179 deg
ZDOT = -423
047200 TA = 43
22841
MA = 43
19702
Ha = 228
784 n
mi
Hp = 221
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11263037
76 X = -3485752
64
Y = 7962915
33 feet Y = 2388410
60 meter
Z = 17488877
85 Z = 5313805
95
XDOT = -15902
398884 XDOT = -4778
427411
YDOT = -19425
324467 feet/sec YDOT = -5974
658300 meter/sec
ZDOT = -1387
950130 ZDOT = -446
426923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2248819
04 X = -685440
04
Y = -13708107
19 feet Y = -4178231
07 meter
Z = 17411361
20 Z = 5306982
89
XDOT = 23392
442532 XDOT = 7130
016484
YDOT = -5747
725721 feet/sec YDOT = -1751
906800 meter/sec
ZDOT = -1495
095929 ZDOT = -455
705239
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 20157
02366984
00016717 00000-0 10270-3 0 9044
2 25544 51
6451 48
6787 0001700 19
6875 340
4341 15
49455807 30121
Satellite: ISS
Catalog Number: 25544
Epoch time: 20157
02366984 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 48
6787 deg
Eccentricity:
0001700
Arg of perigee: 19
6875 deg
Mean anomaly: 340
4341 deg
Mean motion: 15
49455807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 309
Coasting Arc #6 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2020/157/23:25:30
983
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3343994
99 A = 6791248
30 meter
Y = -2589415
19 meter E =
0015354
Z = -5326739
61 I = 51
89359
XDOT = 5228
199001 Wp = 87
93537
YDOT = 5553
298522 meter/sec RA = 43
28097 deg
ZDOT = 584
577704 TA = 187
62628
MA = 187
64966
Ha = 228
795 n
mi
Hp = 221
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10971112
16 X = 3398576
52
Y = -8495456
65 feet Y = -2551714
03 meter
Z = -17476179
83 Z = -5310363
60
XDOT = 17152
883861 XDOT = 5162
872230
YDOT = 18219
483341 feet/sec YDOT = 5611
398585 meter/sec
ZDOT = 1917
905852 ZDOT = 609
816873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3090104
15 X = 941863
74
Y = 13624420
31 feet Y = 4152723
31 meter
Z = -17400614
21 Z = -5303707
21
XDOT = -22718
160344 XDOT = -6924
495273
YDOT = 7741
503553 feet/sec YDOT = 2359
610283 meter/sec
ZDOT = 2033
623753 ZDOT = 619
848520
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 20157
99113387
00016717 00000-0 10270-3 0 9058
2 25544 51
6439 43
8912 0001844 24
4215 335
7023 15
49413357 30279
Satellite: ISS
Catalog Number: 25544
Epoch time: 20157
99113387 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 43
8912 deg
Eccentricity:
0001844
Arg of perigee: 24
4215 deg
Mean anomaly: 335
7023 deg
Mean motion: 15
49413357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 301
Coasting Arc #7 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2020/158/23:25:30
983
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3248972
24 A = 6791195
52 meter
Y = 2732576
52 meter E =
0004789
Z = 5297930
06 I = 51
86845
XDOT = -5595
253398 Wp = 49
05904
YDOT = -5182
127984 meter/sec RA = 38
34791 deg
ZDOT = -754
955995 TA = 48
15589
MA = 48
11501
Ha = 228
860 n
mi
Hp = 221
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10659357
75 X = -3305021
63
Y = 8965146
05 feet Y = 2695929
72 meter
Z = 17381660
29 Z = 5282012
21
XDOT = -18357
130571 XDOT = -5533
222300
YDOT = -17001
732231 feet/sec YDOT = -5244
351096 meter/sec
ZDOT = -2476
889747 ZDOT = -781
986023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3879627
66 X = -1182510
51
Y = -13471935
07 feet Y = -4106245
81 meter
Z = 17308186
52 Z = 5275535
25
XDOT = 21956
017123 XDOT = 6692
194019
YDOT = -9679
177608 feet/sec YDOT = -2950
213335 meter/sec
ZDOT = -2600
869109 ZDOT = -792
744905
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 20159
02309173
00016717 00000-0 10270-3 0 9065
2 25544 51
6438 38
7837 0001767 27
7262 332
3982 15
49455070 30432
Satellite: ISS
Catalog Number: 25544
Epoch time: 20159
02309173 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 38
7837 deg
Eccentricity:
0001767
Arg of perigee: 27
7262 deg
Mean anomaly: 332
3982 deg
Mean motion: 15
49455070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 311
Coasting Arc #8 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2020/159/23:25:30
983
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3151325
63 A = 6791420
52 meter
Y = -2896862
24 meter E =
0015206
Z = -5285797
02 I = 51
84084
XDOT = 5913
941375 Wp = 90
50750
YDOT = 4764
468001 meter/sec RA = 33
41279 deg
ZDOT = 916
818036 TA = 188
24757
MA = 188
27260
Ha = 228
857 n
mi
Hp = 221
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10338994
85 X = 3209160
29
Y = -9504141
22 feet Y = -2861297
43 meter
Z = -17341853
76 Z = -5270349
28
XDOT = 19402
694799 XDOT = 5855
770779
YDOT = 15631
456696 feet/sec YDOT = 4830
276463 meter/sec
ZDOT = 3007
933188 ZDOT = 945
405255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4731769
40 X = 1442243
31
Y = 13315505
06 feet Y = 4058565
94 meter
Z = -17270526
62 Z = -5264056
51
XDOT = -20930
839106 XDOT = -6379
719759
YDOT = 11500
244740 feet/sec YDOT = 3505
274597 meter/sec
ZDOT = 3139
105839 ZDOT = 956
799460
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 20159
99055179
00016717 00000-0 10270-3 0 9076
2 25544 51
6430 33
9953 0001864 31
1190 329
0071 15
49414565 30589
Satellite: ISS
Catalog Number: 25544
Epoch time: 20159
99055179 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 33
9953 deg
Eccentricity:
0001864
Arg of perigee: 31
1190 deg
Mean anomaly: 329
0071 deg
Mean motion: 15
49414565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 309
Coasting Arc #9 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2020/160/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2883071
08 A = 6791244
06 meter
Y = 3108160
67 meter E =
0005078
Z = 5302433
60 I = 51
83188
XDOT = -6147
233969 Wp = 50
37641
YDOT = -4524
926979 meter/sec RA = 32
30319 deg
ZDOT = -686
412437 TA = 46
18598
MA = 46
14400
Ha = 229
040 n
mi
Hp = 221
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9458894
62 X = -2943369
26
Y = 10197377
53 feet Y = 3075581
90 meter
Z = 17396435
71 Z = 5288283
00
XDOT = -20168
090451 XDOT = -6092
843833
YDOT = -14845
560955 feet/sec YDOT = -4593
365472 meter/sec
ZDOT = -2252
009307 ZDOT = -716
141989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13485680
19 X = -4110435
32
Y = 3723432
26 feet Y = 1134902
15 meter
Z = 17331060
36 Z = 5282507
20
XDOT = -9209
177419 XDOT = -2806
957277
YDOT = -22181
793848 feet/sec YDOT = -6761
010765 meter/sec
ZDOT = -2388
457279 ZDOT = -728
001779
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 20160
24854082
00016717 00000-0 10270-3 0 9087
2 25544 51
6408 32
7188 0002134 33
5837 326
5448 15
49427567 30627
Satellite: ISS
Catalog Number: 25544
Epoch time: 20160
24854082 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 32
7188 deg
Eccentricity:
0002134
Arg of perigee: 33
5837 deg
Mean anomaly: 326
5448 deg
Mean motion: 15
49427567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 308
Coasting Arc #10 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2020/161/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2767647
68 A = 6791372
71 meter
Y = -3255956
96 meter E =
0015649
Z = -5291914
10 I = 51
80364
XDOT = 6417
032730 Wp = 89
26635
YDOT = 4075
346843 meter/sec RA = 27
36553 deg
ZDOT = 851
013318 TA = 188
85817
MA = 188
88582
Ha = 229
003 n
mi
Hp = 221
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9080208
92 X = 2829555
95
Y = -10682273
48 feet Y = -3224660
02 meter
Z = -17361922
90 Z = -5278320
29
XDOT = 21053
256987 XDOT = 6366
850362
YDOT = 13370
560510 feet/sec YDOT = 4146
825926 meter/sec
ZDOT = 2792
038444 ZDOT = 882
063392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13337972
07 X = 4065413
89
Y = -4564786
58 feet Y = -1391346
95 meter
Z = -17299096
86 Z = -5272764
72
XDOT = 11051
249278 XDOT = 3368
420780
YDOT = 21199
366322 feet/sec YDOT = 6461
566855 meter/sec
ZDOT = 2934
594797 ZDOT = 894
464494
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 20161
21599611
00016717 00000-0 10270-3 0 9090
2 25544 51
6414 27
9302 0002249 36
4288 323
7015 15
49418123 30770
Satellite: ISS
Catalog Number: 25544
Epoch time: 20161
21599611 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 27
9302 deg
Eccentricity:
0002249
Arg of perigee: 36
4288 deg
Mean anomaly: 323
7015 deg
Mean motion: 15
49418123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3077
Checksum: 294
Coasting Arc #11 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2020/162/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2652102
43 A = 6791441
50 meter
Y = 3383014
78 meter E =
0005952
Z = 5254531
87 I = 51
77304
XDOT = -6672
005214 Wp = 49
61951
YDOT = -3628
532861 meter/sec RA = 22
42580 deg
ZDOT = -1026
860265 TA = 50
22702
MA = 50
17462
Ha = 229
105 n
mi
Hp = 221
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8701123
47 X = -2715258
46
Y = 11099129
85 feet Y = 3353003
08 meter
Z = 17239277
80 Z = 5241496
28
XDOT = -21889
780887 XDOT = -6625
946155
YDOT = -11904
635372 feet/sec YDOT = -3702
886272 meter/sec
ZDOT = -3368
964124 ZDOT = -1059
158685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13131064
90 X = -4002348
58
Y = 5343186
03 feet Y = 1628603
10 meter
Z = 17179011
31 Z = 5236162
65
XDOT = -12819
048707 XDOT = -3907
246046
YDOT = -20146
784118 feet/sec YDOT = -6140
739799 meter/sec
ZDOT = -3517
295609 ZDOT = -1072
071702
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 20162
24794709
00016717 00000-0 10270-3 0 9101
2 25544 51
6408 22
8222 0002268 38
4780 321
6531 15
49430453 30936
Satellite: ISS
Catalog Number: 25544
Epoch time: 20162
24794709 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 22
8222 deg
Eccentricity:
0002268
Arg of perigee: 38
4780 deg
Mean anomaly: 321
6531 deg
Mean motion: 15
49430453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 291
Coasting Arc #12 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2020/163/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2524514
69 A = 6791591
93 meter
Y = -3533146
92 meter E =
0015309
Z = -5235337
70 I = 51
74204
XDOT = 6869
229838 Wp = 91
79193
YDOT = 3147
998832 meter/sec RA = 17
48418 deg
ZDOT = 1190
461349 TA = 189
62474
MA = 189
65410
Ha = 229
022 n
mi
Hp = 221
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8282528
52 X = 2589265
80
Y = -11591689
36 feet Y = -3504553
19 meter
Z = -17176304
78 Z = -5222917
96
XDOT = 22536
843301 XDOT = 6827
734922
YDOT = 10328
080157 feet/sec YDOT = 3224
583265 meter/sec
ZDOT = 3905
713088 ZDOT = 1223
728744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12902984
20 X = 3932829
58
Y = -6200848
81 feet Y = -1890018
72 meter
Z = -17118862
69 Z = -5217829
35
XDOT = 14433
507385 XDOT = 4399
333051
YDOT = 18852
481102 feet/sec YDOT = 5746
236240 meter/sec
ZDOT = 4058
534834 ZDOT = 1237
041417
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 20163
21539974
00016717 00000-0 10270-3 0 9111
2 25544 51
6410 18
0337 0002235 40
4197 319
7119 15
49425663 31086
Satellite: ISS
Catalog Number: 25544
Epoch time: 20163
21539974 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 18
0337 deg
Eccentricity:
0002235
Arg of perigee: 40
4197 deg
Mean anomaly: 319
7119 deg
Mean motion: 15
49425663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 291
Coasting Arc #13 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2020/164/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2399899
18 A = 6791699
77 meter
Y = 3662124
35 meter E =
0006727
Z = 5188336
74 I = 51
71130
XDOT = -7050
656372 Wp = 50
53407
YDOT = -2674
692556 meter/sec RA = 12
54033 deg
ZDOT = -1368
068036 TA = 52
64204
MA = 52
58078
Ha = 229
110 n
mi
Hp = 221
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7873684
98 X = -2465873
55
Y = 12014843
67 feet Y = 3634917
40 meter
Z = 17022102
17 Z = 5176519
30
XDOT = -23132
074711 XDOT = -7013
577909
YDOT = -8775
238045 feet/sec YDOT = -2753
330520 meter/sec
ZDOT = -4488
412190 ZDOT = -1402
227394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12625459
91 X = -3848240
18
Y = 6986243
92 feet Y = 2129407
15 meter
Z = 16967424
78 Z = 5171671
07
XDOT = -15954
449536 XDOT = -4862
916219
YDOT = -17507
692071 feet/sec YDOT = -5336
344543 meter/sec
ZDOT = -4645
366734 ZDOT = -1415
907780
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 20164
24734700
00016717 00000-0 10270-3 0 9120
2 25544 51
6422 12
9258 0002253 42
9545 317
1781 15
49439180 31242
Satellite: ISS
Catalog Number: 25544
Epoch time: 20164
24734700 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 12
9258 deg
Eccentricity:
0002253
Arg of perigee: 42
9545 deg
Mean anomaly: 317
1781 deg
Mean motion: 15
49439180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3124
Checksum: 286
Coasting Arc #14 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2020/165/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2258076
44 A = 6791866
16 meter
Y = -3813219
41 meter E =
0014917
Z = -5159958
31 I = 51
67882
XDOT = 7171
319583 Wp = 93
97885
YDOT = 2177
546195 meter/sec RA = 7
59405 deg
ZDOT = 1531
888811 TA = 190
79367
MA = 190
82572
Ha = 229
055 n
mi
Hp = 221
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7408387
28 X = 2325613
16
Y = -12510562
36 feet Y = -3787589
74 meter
Z = -16928997
07 Z = -5148825
94
XDOT = 23527
951388 XDOT = 7138
995628
YDOT = 7144
180431 feet/sec YDOT = 2257
560078 meter/sec
ZDOT = 5025
881925 ZDOT = 1566
645857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12306913
76 X = 3751147
31
Y = -7853687
54 feet Y = -2393803
96 meter
Z = -16877463
68 Z = -5144250
93
XDOT = 17283
080386 XDOT = 5267
882902
YDOT = 15959
131344 feet/sec YDOT = 4864
343234 meter/sec
ZDOT = 5185
614968 ZDOT = 1580
575442
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 20165
21479439
00016717 00000-0 10270-3 0 9134
2 25544 51
6423 8
1370 0002310 44
7645 315
3691 15
49441086 31394
Satellite: ISS
Catalog Number: 25544
Epoch time: 20165
21479439 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 8
1370 deg
Eccentricity:
0002310
Arg of perigee: 44
7645 deg
Mean anomaly: 315
3691 deg
Mean motion: 15
49441086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 292
Coasting Arc #15 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2020/166/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2121016
15 A = 6792050
47 meter
Y = 3943937
43 meter E =
0007686
Z = 5102630
89 I = 51
64578
XDOT = -7276
726816 Wp = 52
62442
YDOT = -1691
607671 meter/sec RA = 2
64637 deg
ZDOT = -1710
910226 TA = 53
95026
MA = 53
87908
Ha = 229
170 n
mi
Hp = 221
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6958714
40 X = -2189746
40
Y = 12939427
25 feet Y = 3919833
81 meter
Z = 16740915
00 Z = 5092161
38
XDOT = -23873
775644 XDOT = -7248
959329
YDOT = -5549
893934 feet/sec YDOT = -1772
825753 meter/sec
ZDOT = -5613
222526 ZDOT = -1746
190415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11947111
93 X = -3641479
72
Y = 8645241
00 feet Y = 2635069
46 meter
Z = 16692424
73 Z = 5087851
06
XDOT = -18506
420658 XDOT = -5640
757016
YDOT = -14383
078739 feet/sec YDOT = -4383
962400 meter/sec
ZDOT = -5775
388669 ZDOT = -1760
338466
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 20166
24673770
00016717 00000-0 10270-3 0 9143
2 25544 51
6421 3
0298 0002382 48
2819 311
8535 15
49443526 31553
Satellite: ISS
Catalog Number: 25544
Epoch time: 20166
24673770 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 3
0298 deg
Eccentricity:
0002382
Arg of perigee: 48
2819 deg
Mean anomaly: 311
8535 deg
Mean motion: 15
49443526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 300
Coasting Arc #16 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2020/167/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980095
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1959049
30 A = 6792233
57 meter
Y = -4094992
56 meter E =
0014409
Z = -5065357
82 I = 51
61275
XDOT = 7321
022468 Wp = 96
43246
YDOT = 1190
004349 meter/sec RA = 357
69581 deg
ZDOT = 1872
418637 TA = 191
74678
MA = 191
78043
Ha = 229
082 n
mi
Hp = 221
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6427327
11 X = 2029299
77
Y = -13435014
95 feet Y = -4072691
65 meter
Z = -16618628
02 Z = -5055671
39
XDOT = 24019
102586 XDOT = 7298
076222
YDOT = 3904
213742 feet/sec YDOT = 1271
744707 meter/sec
ZDOT = 6143
105765 ZDOT = 1907
925768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11517452
49 X = 3510519
52
Y = -9520959
44 feet Y = -2901988
44 meter
Z = -16573731
54 Z = -5051673
37
XDOT = 19512
640051 XDOT = 5947
452688
YDOT = 12643
767440 feet/sec YDOT = 3853
820316 meter/sec
ZDOT = 6306
343137 ZDOT = 1922
173388
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 20167
21418279
00016717 00000-0 10270-3 0 9153
2 25544 51
6422 358
2412 0002304 50
8950 309
2405 15
49450717 31700
Satellite: ISS
Catalog Number: 25544
Epoch time: 20167
21418279 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 358
2412 deg
Eccentricity:
0002304
Arg of perigee: 50
8950 deg
Mean anomaly: 309
2405 deg
Mean motion: 15
49450717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 287
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