[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 17th 2020
- spaceflight nasa gov will be taken offline in the next 30 days *
- *
- Current information about the International Space Station can be *
- found at www nasa gov/station *
- *
- Predicted ISS and visiting vehicle sightings opportunities can be *
- found at spotthestation nasa gov *
- *
- Updated ISS trajectory information will be made available as a CCSDS *
- Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
- system *
- Included in the OEM are a sequence of events with ISS maneuver *
- details (in the comment section), predicted post-maneuver state *
- vectors, predicted coasting state vectors at 4-minute intervals, *
- and ISS ballistic details *
- *
- OEMs will be provided in xml and txt formats *
- Links to the OEMs and more details to follow *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15144 822 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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
288/05:45:04
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 222
0
288/08:52:27
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
1
289/02:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
0
296/18:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
8
Coasting Arc #1 (Orbit 1019)
---------------------------------------
Vector Time (GMT): 2020/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4340860
71 A = 6792477
73 meter
Y = -922367
17 meter E =
0004833
Z = 5138805
48 I = 51
93640
XDOT = 3387
120354 Wp = 108
85274
YDOT = -6670
646734 meter/sec RA = 126
93244 deg
ZDOT = 1661
060756 TA = 325
15166
MA = 325
18330
Ha = 229
012 n
mi
Hp = 222
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14241668
98 X = -4355185
42
Y = -3026139
01 feet Y = -970989
69 meter
Z = 16859598
04 Z = 5117684
40
XDOT = 11112
599588 XDOT = 3453
393269
YDOT = -21885
323932 feet/sec YDOT = -6632
398905 meter/sec
ZDOT = 5449
674395 ZDOT = 1677
675379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14502500
93 X = 4420362
28
Y = -2223706
15 feet Y = -677785
64 meter
Z = 16761900
15 Z = 5109027
16
XDOT = -2821
674777 XDOT = -860
046472
YDOT = 23325
651861 feet/sec YDOT = 7109
658687 meter/sec
ZDOT = 5526
588469 ZDOT = 1684
504165
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 20286
55131626
00016717 00000-0 10270-3 0 9004
2 25544 51
6418 127
7592 0001444 15
0258 345
0935 15
49267220 10204
Satellite: ISS
Catalog Number: 25544
Epoch time: 20286
55131626 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 127
7592 deg
Eccentricity:
0001444
Arg of perigee: 15
0258 deg
Mean anomaly: 345
0935 deg
Mean motion: 15
49267220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1020
Checksum: 282
Coasting Arc #2 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2020/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4360062
04 A = 6792272
51 meter
Y = 669332
17 meter E =
0014323
Z = -5177742
84 I = 51
95320
XDOT = -2894
392005 Wp = 73
60819
YDOT = 6910
608031 meter/sec RA = 122
00405 deg
ZDOT = -1543
573531 TA = 181
54301
MA = 181
54743
Ha = 228
830 n
mi
Hp = 222
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14304665
50 X = 4377404
01
Y = 2195971
69 feet Y = 718186
17 meter
Z = -16987345
29 Z = -5156521
14
XDOT = -9496
036761 XDOT = -2963
955540
YDOT = 22672
598528 feet/sec YDOT = 6877
851816 meter/sec
ZDOT = -5064
217623 ZDOT = -1557
802824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14215846
66 X = -4332990
06
Y = 3268212
62 feet Y = 996151
21 meter
Z = -16889172
18 Z = -5147819
68
XDOT = 687
640003 XDOT = 209
592673
YDOT = -23526
502915 feet/sec YDOT = -7170
878088 meter/sec
ZDOT = -5130
113321 ZDOT = -1563
658540
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 20287
51885696
00016717 00000-0 10270-3 0 9015
2 25544 51
6396 122
9705 0001397 18
8528 341
2674 15
49297408 10355
Satellite: ISS
Catalog Number: 25544
Epoch time: 20287
51885696 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 122
9705 deg
Eccentricity:
0001397
Arg of perigee: 18
8528 deg
Mean anomaly: 341
2674 deg
Mean motion: 15
49297408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1035
Checksum: 334
Coasting Arc #3 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2020/288/05:45:04
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4742991
02 A = 6793871
03 meter
Y = 935530
88 meter E =
0007756
Z = 4768040
71 I = 51
97330
XDOT = 1366
797830 Wp = 107
31784
YDOT = -7028
494796 meter/sec RA = 118
37065 deg
ZDOT = 2732
763453 TA = 315
73640
MA = 315
79841
Ha = 228
968 n
mi
Hp = 222
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15560994
16 X = -4776260
53
Y = 3069327
04 feet Y = 882305
68 meter
Z = 15643178
20 Z = 4744920
03
XDOT = 4484
244850 XDOT = 1432
016668
YDOT = -23059
366130 feet/sec YDOT = -7012
845418 meter/sec
ZDOT = 8965
759361 ZDOT = 2739
561808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7906655
91 X = 2409948
72
Y = 13870316
15 feet Y = 4227672
36 meter
Z = 15536198
18 Z = 4735433
21
XDOT = -22253
886275 XDOT = -6782
984537
YDOT = 2585
890335 feet/sec YDOT = 788
179374 meter/sec
ZDOT = 8997
286898 ZDOT = 2742
373047
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 20288
29289072
00016717 00000-0 10270-3 0 9028
2 25544 51
6414 119
1419 0001378 21
8437 338
2772 15
49322106 10470
Satellite: ISS
Catalog Number: 25544
Epoch time: 20288
29289072 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 119
1419 deg
Eccentricity:
0001378
Arg of perigee: 21
8437 deg
Mean anomaly: 338
2772 deg
Mean motion: 15
49322106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 302
Coasting Arc #4 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2020/288/08:52:27
000
Vector Time (MET): N/A
Weight (LBS) : 953856
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579188
59 A = 6792997
92 meter
Y = 300995
41 meter E =
0006206
Z = 5004130
46 I = 51
97371
XDOT = 1862
838767 Wp = 109
24673
YDOT = -7122
608522 meter/sec RA = 117
72664 deg
ZDOT = 2128
931138 TA = 320
08115
MA = 320
12677
Ha = 229
068 n
mi
Hp = 222
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15023584
60 X = -4606521
52
Y = 987517
76 feet Y = 249635
19 meter
Z = 16417750
87 Z = 4981819
93
XDOT = 6111
675745 XDOT = 1932
006240
YDOT = -23368
138196 feet/sec YDOT = -7101
390020 meter/sec
ZDOT = 6984
682212 ZDOT = 2138
148706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14189403
56 X = 4324930
21
Y = 5359377
81 feet Y = 1633538
36 meter
Z = 16314524
97 Z = 4972667
21
XDOT = -14793
685919 XDOT = -4509
115468
YDOT = 17733
745846 feet/sec YDOT = 5405
245734 meter/sec
ZDOT = 7027
405295 ZDOT = 2141
953134
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 20288
42189682
00016717 00000-0 10270-3 0 9030
2 25544 51
6430 118
5042 0001483 24
3678 335
7542 15
49287758 10497
Satellite: ISS
Catalog Number: 25544
Epoch time: 20288
42189682 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 118
5042 deg
Eccentricity:
0001483
Arg of perigee: 24
3678 deg
Mean anomaly: 335
7542 deg
Mean motion: 15
49287758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 321
Coasting Arc #5 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2020/289/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953856
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3718785
48 A = 6791486
26 meter
Y = -1922107
44 meter E =
0003507
Z = 5345299
24 I = 51
97566
XDOT = 3283
376592 Wp = 62
60280
YDOT = -6921
372398 meter/sec RA = 114
19214 deg
ZDOT = -202
890979 TA = 29
33305
MA = 29
31337
Ha = 229
061 n
mi
Hp = 222
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12200739
77 X = -3722980
27
Y = -6306126
77 feet Y = -1963716
58 meter
Z = 17537071
01 Z = 5327224
57
XDOT = 10772
232912 XDOT = 3361
514980
YDOT = -22707
914693 feet/sec YDOT = -6884
218442 meter/sec
ZDOT = -665
652819 ZDOT = -186
751041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12433008
04 X = -3789580
85
Y = 6080375
39 feet Y = 1853298
42 meter
Z = 17453466
47 Z = 5319816
58
XDOT = -11269
948133 XDOT = -3435
080191
YDOT = -21332
572343 feet/sec YDOT = -6502
168050 meter/sec
ZDOT = -590
892950 ZDOT = -180
104171
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 20289
13142640
00016717 00000-0 10270-3 0 9043
2 25544 51
6392 114
9911 0001430 28
1947 331
9280 15
49288465 10608
Satellite: ISS
Catalog Number: 25544
Epoch time: 20289
13142640 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 114
9911 deg
Eccentricity:
0001430
Arg of perigee: 28
1947 deg
Mean anomaly: 331
9280 deg
Mean motion: 15
49288465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 295
Coasting Arc #6 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2020/290/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953856
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3829851
14 A = 6791515
79 meter
Y = 1719992
60 meter E =
0015569
Z = -5351788
51 I = 51
98927
XDOT = -2756
338526 Wp = 87
60430
YDOT = 7128
087971 meter/sec RA = 109
26653 deg
ZDOT = 319
812430 TA = 185
42912
MA = 185
44602
Ha = 228
962 n
mi
Hp = 222
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12565128
43 X = 3836329
47
Y = 5643020
35 feet Y = 1762856
53 meter
Z = -17558361
25 Z = -5333168
63
XDOT = -9043
105399 XDOT = -2837
395595
YDOT = 23386
115391 feet/sec YDOT = 7096
811423 meter/sec
ZDOT = 1049
253379 ZDOT = 306
225492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12002596
97 X = 3658391
56
Y = -6977172
80 feet Y = -2126642
27 meter
Z = -17472232
45 Z = -5325536
45
XDOT = 13146
242979 XDOT = 4006
974860
YDOT = 20157
031451 feet/sec YDOT = 6143
863186 meter/sec
ZDOT = 986
284388 ZDOT = 300
619482
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 20290
09896453
00016717 00000-0 10270-3 0 9059
2 25544 51
6400 110
2026 0001514 31
0850 329
0390 15
49289382 10758
Satellite: ISS
Catalog Number: 25544
Epoch time: 20290
09896453 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 110
2026 deg
Eccentricity:
0001514
Arg of perigee: 31
0850 deg
Mean anomaly: 329
0390 deg
Mean motion: 15
49289382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 281
Coasting Arc #7 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2020/291/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953856
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3915080
74 A = 6791519
38 meter
Y = -1516388
23 meter E =
0004036
Z = 5335521
08 I = 51
99920
XDOT = 2228
260775 Wp = 57
01973
YDOT = -7318
988103 meter/sec RA = 104
34175 deg
ZDOT = -442
677320 TA = 37
19809
MA = 37
17013
Ha = 229
130 n
mi
Hp = 221
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12844753
09 X = -3923750
61
Y = -4975027
00 feet Y = -1560217
60 meter
Z = 17504990
42 Z = 5316481
72
XDOT = 7310
566848 XDOT = 2312
088626
YDOT = -24012
428161 feet/sec YDOT = -7293
601410 meter/sec
ZDOT = -1452
353413 ZDOT = -431
648948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11492353
79 X = -3502869
44
Y = 7793587
16 feet Y = 2375485
37 meter
Z = 17416919
04 Z = 5308676
92
XDOT = -14949
182713 XDOT = -4556
510891
YDOT = -18895
039670 feet/sec YDOT = -5759
208091 meter/sec
ZDOT = -1401
197213 ZDOT = -427
084911
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 20291
13100439
00016717 00000-0 10270-3 0 9068
2 25544 51
6398 105
0948 0001596 32
2409 327
8838 15
49294118 10916
Satellite: ISS
Catalog Number: 25544
Epoch time: 20291
13100439 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 105
0948 deg
Eccentricity:
0001596
Arg of perigee: 32
2409 deg
Mean anomaly: 327
8838 deg
Mean motion: 15
49294118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 308
Coasting Arc #8 (Orbit 1105)
---------------------------------------
Vector Time (GMT): 2020/292/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953856
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4009937
91 A = 6791571
18 meter
Y = 1303388
06 meter E =
0015509
Z = -5337545
40 I = 52
00655
XDOT = -1677
005516 Wp = 89
24184
YDOT = 7442
102973 meter/sec RA = 99
41764 deg
ZDOT = 559
022045 TA = 186
06972
MA = 186
08853
Ha = 228
989 n
mi
Hp = 222
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13155964
26 X = 4020992
46
Y = 4276207
54 feet Y = 1348291
67 meter
Z = -17511631
89 Z = -5318039
35
XDOT = -5501
986602 XDOT = -1762
816203
YDOT = 24416
348338 feet/sec YDOT = 7422
869717 meter/sec
ZDOT = 1834
061826 ZDOT = 550
666885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10949931
94 X = 3337539
25
Y = -8638083
16 feet Y = -2632887
75 meter
Z = -17421397
99 Z = -5310042
11
XDOT = 16566
812081 XDOT = 5049
564322
YDOT = 17390
633900 feet/sec YDOT = 5300
665213 meter/sec
ZDOT = 1795
246552 ZDOT = 547
191149
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 20292
09854094
00016717 00000-0 10270-3 0 9078
2 25544 51
6398 100
3065 0001575 33
6039 326
5211 15
49294032 11068
Satellite: ISS
Catalog Number: 25544
Epoch time: 20292
09854094 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 100
3065 deg
Eccentricity:
0001575
Arg of perigee: 33
6039 deg
Mean anomaly: 326
5211 deg
Mean motion: 15
49294032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1106
Checksum: 290
Coasting Arc #9 (Orbit 1121)
---------------------------------------
Vector Time (GMT): 2020/293/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953856
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4078761
99 A = 6791586
85 meter
Y = -1092647
44 meter E =
0004470
Z = 5316480
90 I = 52
01237
XDOT = 1128
349455 Wp = 54
21091
YDOT = -7549
149549 meter/sec RA = 94
49448 deg
ZDOT = -682
903338 TA = 42
29833
MA = 42
26387
Ha = 229
142 n
mi
Hp = 221
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13381765
07 X = -4092065
66
Y = -3584801
31 feet Y = -1138333
43 meter
Z = 17442522
63 Z = 5296635
03
XDOT = 3701
933907 XDOT = 1215
999705
YDOT = -24767
551013 feet/sec YDOT = -7536
041456 meter/sec
ZDOT = -2240
496515 ZDOT = -677
209169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10341540
47 X = -3152101
54
Y = 9389856
48 feet Y = 2862028
26 meter
Z = 17350710
89 Z = 5288496
68
XDOT = -18093
293610 XDOT = -5514
835892
YDOT = -15818
158599 feet/sec YDOT = -4821
374741 meter/sec
ZDOT = -2213
964662 ZDOT = -674
816429
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 20293
13057941
00016717 00000-0 10270-3 0 9081
2 25544 51
6411 95
1994 0001580 35
4994 324
6261 15
49301932 11222
Satellite: ISS
Catalog Number: 25544
Epoch time: 20293
13057941 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 95
1994 deg
Eccentricity:
0001580
Arg of perigee: 35
4994 deg
Mean anomaly: 324
6261 deg
Mean motion: 15
49301932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1122
Checksum: 297
Coasting Arc #10 (Orbit 1136)
---------------------------------------
Vector Time (GMT): 2020/294/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953856
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4156084
50 A = 6791646
21 meter
Y = 870072
47 meter E =
0015385
Z = -5313894
45 I = 52
01487
XDOT = -567
732216 Wp = 90
95786
YDOT = 7586
086194 meter/sec RA = 89
57068 deg
ZDOT = 799
826496 TA = 186
65556
MA = 186
67601
Ha = 229
003 n
mi
Hp = 222
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13635447
83 X = 4171858
67
Y = 2854568
46 feet Y = 916637
07 meter
Z = -17434036
91 Z = -5293667
01
XDOT = -1862
638503 XDOT = -656
405117
YDOT = 24888
734231 feet/sec YDOT = 7579
241589 meter/sec
ZDOT = 2624
102678 ZDOT = 796
853363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9692657
58 X = 2954322
03
Y = -10167634
00 feet Y = -3099094
84 meter
Z = -17340451
25 Z = -5285369
54
XDOT = 19392
529474 XDOT = 5910
842984
YDOT = 14044
982278 feet/sec YDOT = 4280
910598 meter/sec
ZDOT = 2610
135408 ZDOT = 795
569272
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 20294
09811264
00016717 00000-0 10270-3 0 9094
2 25544 51
6420 90
4108 0001612 36
6332 323
4928 15
49305776 11375
Satellite: ISS
Catalog Number: 25544
Epoch time: 20294
09811264 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 90
4108 deg
Eccentricity:
0001612
Arg of perigee: 36
6332 deg
Mean anomaly: 323
4928 deg
Mean motion: 15
49305776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1137
Checksum: 293
Coasting Arc #11 (Orbit 1152)
---------------------------------------
Vector Time (GMT): 2020/295/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953856
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4208289
46 A = 6791690
69 meter
Y = -653805
48 meter E =
0005127
Z = 5287467
32 I = 52
01384
XDOT = 13
713276 Wp = 52
37929
YDOT = -7607
436434 meter/sec RA = 84
64830 deg
ZDOT = -926
103526 TA = 46
46164
MA = 46
41906
Ha = 229
198 n
mi
Hp = 221
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13806723
94 X = -4226349
62
Y = -2145031
11 feet Y = -700966
72 meter
Z = 17347333
72 Z = 5266980
82
XDOT = 44
991062 XDOT = 103
279473
YDOT = -24958
780953 feet/sec YDOT = -7606
782260 meter/sec
ZDOT = -3038
397395 ZDOT = -925
819580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8995358
10 X = -2741785
15
Y = 10843901
24 feet Y = 3305221
10 meter
Z = 17252539
24 Z = 5258573
96
XDOT = -20586
677397 XDOT = -6274
819271
YDOT = -12226
507892 feet/sec YDOT = -3726
639605 meter/sec
ZDOT = -3036
851661 ZDOT = -925
632386
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 20295
13014746
00016717 00000-0 10270-3 0 9102
2 25544 51
6422 85
3044 0001730 39
3831 320
7445 15
49311908 11530
Satellite: ISS
Catalog Number: 25544
Epoch time: 20295
13014746 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 85
3044 deg
Eccentricity:
0001730
Arg of perigee: 39
3831 deg
Mean anomaly: 320
7445 deg
Mean motion: 15
49311908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1153
Checksum: 276
Coasting Arc #12 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2020/296/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4267355
63 A = 6791791
30 meter
Y = 420073
16 meter E =
0015283
Z = -5280305
10 I = 52
00970
XDOT = 543
065021 Wp = 92
71542
YDOT = 7558
440432 meter/sec RA = 79
72482 deg
ZDOT = 1042
093062 TA = 187
22779
MA = 187
24985
Ha = 229
061 n
mi
Hp = 221
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14000510
60 X = 4287990
16
Y = 1378192
78 feet Y = 467909
31 meter
Z = -17323835
64 Z = -5259525
53
XDOT = 1781
709386 XDOT = 453
441932
YDOT = 24798
032914 feet/sec YDOT = 7564
012232 meter/sec
ZDOT = 3418
940493 ZDOT = 1044
513622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8239608
84 X = 2511432
77
Y = -11547515
27 feet Y = -3519682
65 meter
Z = -17227673
40 Z = -5250994
85
XDOT = 21524
816733 XDOT = 6560
764140
YDOT = 10251
108058 feet/sec YDOT = 3124
537736 meter/sec
ZDOT = 3429
894115 ZDOT = 1045
431726
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 20296
09767961
00016717 00000-0 10270-3 0 9113
2 25544 51
6422 80
5163 0001688 42
4287 317
6993 15
49308130 11683
Satellite: ISS
Catalog Number: 25544
Epoch time: 20296
09767961 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 80
5163 deg
Eccentricity:
0001688
Arg of perigee: 42
4287 deg
Mean anomaly: 317
6993 deg
Mean motion: 15
49308130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1168
Checksum: 320
Coasting Arc #13 (Orbit 1178)
---------------------------------------
Vector Time (GMT): 2020/296/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4226162
50 A = 6791524
52 meter
Y = 173073
46 meter E =
0004516
Z = 5310543
81 I = 52
00502
XDOT = -1232
794815 Wp = 58
30585
YDOT = -7528
300205 meter/sec RA = 76
39587 deg
ZDOT = -732
949632 TA = 38
68088
MA = 38
64855
Ha = 229
134 n
mi
Hp = 221
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13865362
53 X = -4253579
65
Y = 567826
30 feet Y = 125660
06 meter
Z = 17423043
99 Z = 5289947
93
XDOT = -4044
602410 XDOT = -1144
959174
YDOT = -24699
147654 feet/sec YDOT = -7541
595065 meter/sec
ZDOT = -2404
690395 ZDOT = -738
724960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8360965
54 X = -2548422
30
Y = -11223988
16 feet Y = -3421071
59 meter
Z = 17327709
35 Z = 5281485
81
XDOT = 17299
189653 XDOT = 5272
793006
YDOT = -16653
832203 feet/sec YDOT = -5076
088056 meter/sec
ZDOT = -2431
161540 ZDOT = -741
018037
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 20296
80720076
00016717 00000-0 10270-3 0 9129
2 25544 51
6427 77
0049 0001412 49
8685 310
2588 15
49333596 11795
Satellite: ISS
Catalog Number: 25544
Epoch time: 20296
80720076 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 77
0049 deg
Eccentricity:
0001412
Arg of perigee: 49
8685 deg
Mean anomaly: 310
2588 deg
Mean motion: 15
49333596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1179
Checksum: 318
Coasting Arc #14 (Orbit 1193)
---------------------------------------
Vector Time (GMT): 2020/297/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4236591
11 A = 6791710
92 meter
Y = -406494
40 meter E =
0015603
Z = -5306291
64 I = 51
99712
XDOT = 1774
820171 Wp = 92
38003
YDOT = 7391
268533 meter/sec RA = 71
47112 deg
ZDOT = 852
348840 TA = 185
74078
MA = 185
75868
Ha = 229
096 n
mi
Hp = 221
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13899577
14 X = 4266596
94
Y = -1333643
04 feet Y = -358949
98 meter
Z = -17409093
32 Z = -5285638
88
XDOT = 5822
900825 XDOT = 1687
896607
YDOT = 24249
568677 feet/sec YDOT = 7410
629817 meter/sec
ZDOT = 2796
420080 ZDOT = 860
759241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9197233
80 X = 2803316
86
Y = 10663373
83 feet Y = 3250196
34 meter
Z = -17313483
99 Z = -5277149
92
XDOT = -15646
666784 XDOT = -4769
104036
YDOT = 18090
296846 feet/sec YDOT = 5513
922479 meter/sec
ZDOT = 2835
078883 ZDOT = 864
132043
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 20297
77473103
00016717 00000-0 10270-3 0 9133
2 25544 51
6437 72
2163 0001583 51
5184 308
6108 15
49296433 11947
Satellite: ISS
Catalog Number: 25544
Epoch time: 20297
77473103 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 72
2163 deg
Eccentricity:
0001583
Arg of perigee: 51
5184 deg
Mean anomaly: 308
6108 deg
Mean motion: 15
49296433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1194
Checksum: 304
Coasting Arc #15 (Orbit 1209)
---------------------------------------
Vector Time (GMT): 2020/298/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224698
29 A = 6791658
21 meter
Y = 627094
62 meter E =
0005295
Z = 5277238
87 I = 51
98500
XDOT = -2305
700471 Wp = 56
93020
YDOT = -7242
631219 meter/sec RA = 66
54660 deg
ZDOT = -981
666444 TA = 42
44701
MA = 42
40607
Ha = 229
240 n
mi
Hp = 221
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13860558
71 X = -4257030
68
Y = 2057397
05 feet Y = 579670
26 meter
Z = 17313775
81 Z = 5256638
24
XDOT = -7564
634090 XDOT = -2219
771405
YDOT = -23761
913447 feet/sec YDOT = -7267
934762 meter/sec
ZDOT = -3220
690434 ZDOT = -992
657970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9938895
59 X = -3029375
37
Y = -10042903
93 feet Y = -3061077
12 meter
Z = 17218398
25 Z = 5248167
79
XDOT = 13943
882382 XDOT = 4250
095350
YDOT = -19427
966840 feet/sec YDOT = -5921
644293 meter/sec
ZDOT = -3271
289253 ZDOT = -997
088964
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 20298
80675955
00016717 00000-0 10270-3 0 9148
2 25544 51
6432 67
1095 0001690 55
4556 304
6753 15
49338337 12105
Satellite: ISS
Catalog Number: 25544
Epoch time: 20298
80675955 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 67
1095 deg
Eccentricity:
0001690
Arg of perigee: 55
4556 deg
Mean anomaly: 304
6753 deg
Mean motion: 15
49338337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1210
Checksum: 317
Coasting Arc #16 (Orbit 1224)
---------------------------------------
Vector Time (GMT): 2020/299/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4215144
88 A = 6791867
15 meter
Y = -866082
26 meter E =
0015481
Z = -5268206
92 I = 51
97131
XDOT = 2817
100784 Wp = 94
30086
YDOT = 7025
674834 meter/sec RA = 61
62071 deg
ZDOT = 1100
641883 TA = 186
21510
MA = 186
23433
Ha = 229
147 n
mi
Hp = 221
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13829215
49 X = 4250106
55
Y = -2841477
24 feet Y = -818750
12 meter
Z = -17284143
44 Z = -5247646
28
XDOT = 9242
456641 XDOT = 2732
981858
YDOT = 23050
114284 feet/sec YDOT = 7056
707361 meter/sec
ZDOT = 3611
029801 ZDOT = 1114
121913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10714674
31 X = 3265832
73
Y = 9370102
99 feet Y = 2856007
39 meter
Z = -17188942
16 Z = -5239189
57
XDOT = -12062
637968 XDOT = -3676
692053
YDOT = 20521
723665 feet/sec YDOT = 6255
021373 meter/sec
ZDOT = 3673
142551 ZDOT = 1119
573850
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 20299
77428747
00016717 00000-0 10270-3 0 9151
2 25544 51
6438 62
3213 0001667 57
5986 302
5325 15
49300283 12251
Satellite: ISS
Catalog Number: 25544
Epoch time: 20299
77428747 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 62
3213 deg
Eccentricity:
0001667
Arg of perigee: 57
5986 deg
Mean anomaly: 302
5325 deg
Mean motion: 15
49300283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1225
Checksum: 316
Coasting Arc #17 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2020/300/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4184788
96 A = 6791853
29 meter
Y = 1089612
73 meter E =
0005927
Z = 5233572
96 I = 51
95356
XDOT = -3314
932846 Wp = 57
68836
YDOT = -6799
572114 meter/sec RA = 56
69383 deg
ZDOT = -1230
888110 TA = 44
10271
MA = 44
05546
Ha = 229
306 n
mi
Hp = 221
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13729622
56 X = -4222084
30
Y = 3574844
91 feet Y = 1042607
06 meter
Z = 17170514
96 Z = 5213154
05
XDOT = -10875
763929 XDOT = -3232
672586
YDOT = -22308
307461 feet/sec YDOT = -6836
182168 meter/sec
ZDOT = -4038
346816 ZDOT = -1246
790904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11387613
66 X = -3470944
64
Y = -8651149
76 feet Y = -2636870
45 meter
Z = 17075962
60 Z = 5204753
40
XDOT = 10154
190561 XDOT = 3094
997283
YDOT = -21508
539237 feet/sec YDOT = -6555
802760 meter/sec
ZDOT = -4111
668346 ZDOT = -1253
236512
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 20300
80631475
00016717 00000-0 10270-3 0 9163
2 25544 51
6429 57
2140 0001793 63
2880 296
8453 15
49337081 12411
Satellite: ISS
Catalog Number: 25544
Epoch time: 20300
80631475 = yrday
fracday
Element set: 916
Inclination: 51
6429 deg
RA of node: 57
2140 deg
Eccentricity:
0001793
Arg of perigee: 63
2880 deg
Mean anomaly: 296
8453 deg
Mean motion: 15
49337081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 298
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