[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 10th 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) : 75 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 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
342/18:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 221
9
345/02:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 221
8
351/15:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
0
354/02:00:00
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
1
355/04:48:45
000 0
0 -0
0 0
1
N/A 0
0 -0
1 229
0
000/00:07:30
000 0
1 -0
0 222
1
Coasting Arc #1 (Orbit 1887)
---------------------------------------
Vector Time (GMT): 2020/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5108923
51 A = 6795588
38 meter
Y = -1070812
26 meter E =
0010852
Z = 4343671
90 I = 51
43838
XDOT = 4087
135900 Wp = 75
35892
YDOT = 5493
574408 meter/sec RA = 209
71973 deg
ZDOT = -3442
984913 TA = 49
75429
MA = 49
65941
Ha = 229
176 n
mi
Hp = 221
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16761560
08 X = 5099418
87
Y = -3513163
57 feet Y = -1013734
14 meter
Z = 14250892
05 Z = 4368465
89
XDOT = 13409
238518 XDOT = 4042
125385
YDOT = 18023
538085 feet/sec YDOT = 5539
028338 meter/sec
ZDOT = -11295
882262 ZDOT = -3423
240016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -679110
63 X = -206992
92
Y = 17016062
97 feet Y = 5186495
99 meter
Z = 14365672
58 Z = 4378657
00
XDOT = -19538
058988 XDOT = -5955
200380
YDOT = 8706
820686 feet/sec YDOT = 2653
838945 meter/sec
ZDOT = -11204
528769 ZDOT = -3415
140369
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 20342
54220293
00016717 00000-0 10270-3 0 9005
2 25544 51
6435 210
7131 0001528 100
2176 259
9147 15
49205090 18881
Satellite: ISS
Catalog Number: 25544
Epoch time: 20342
54220293 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 210
7131 deg
Eccentricity:
0001528
Arg of perigee: 100
2176 deg
Mean anomaly: 259
9147 deg
Mean motion: 15
49205090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1888
Checksum: 280
Coasting Arc #2 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2020/342/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5156829
46 A = 6802840
12 meter
Y = 4163294
09 meter E =
0010129
Z = -1517627
51 I = 51
46805
XDOT = -4092
617015 Wp = 138
43265
YDOT = 2986
379762 meter/sec RA = 208
40849 deg
ZDOT = -5743
522811 TA = 58
14626
MA = 58
04771
Ha = 229
475 n
mi
Hp = 221
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16918731
83 X = 5117262
76
Y = 13659101
35 feet Y = 4220740
36 meter
Z = -4979092
89 Z = -1492673
36
XDOT = -13427
221177 XDOT = -4097
808660
YDOT = 9797
833866 feet/sec YDOT = 2940
584642 meter/sec
ZDOT = -18843
578775 ZDOT = -5763
415527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15318460
90 X = 4669066
88
Y = 15469194
18 feet Y = 4715010
39 meter
Z = -4863608
68 Z = -1482427
92
XDOT = -13181
939054 XDOT = -4017
855024
YDOT = 7131
154804 feet/sec YDOT = 2173
575984 meter/sec
ZDOT = -18935
688733 ZDOT = -5771
597926
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 20342
80023906
00016717 00000-0 10270-3 0 9017
2 25544 51
6415 209
4311 0001930 119
3170 240
8173 15
49173981 18922
Satellite: ISS
Catalog Number: 25544
Epoch time: 20342
80023906 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 209
4311 deg
Eccentricity:
0001930
Arg of perigee: 119
3170 deg
Mean anomaly: 240
8173 deg
Mean motion: 15
49173981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 283
Coasting Arc #3 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2020/343/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5468585
49 A = 6802788
13 meter
Y = -3723007
11 meter E =
0014831
Z = 1558037
50 I = 51
49957
XDOT = 3880
833509 Wp = 69
22590
YDOT = -3285
693811 meter/sec RA = 203
44966 deg
ZDOT = 5730
956608 TA = 307
80679
MA = 307
94097
Ha = 229
430 n
mi
Hp = 221
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17941553
46 X = -5434115
35
Y = -12214590
27 feet Y = -3783968
14 meter
Z = 5111671
60 Z = 1531556
57
XDOT = 12732
393403 XDOT = 3889
448861
YDOT = -10779
835337 feet/sec YDOT = -3242
247794 meter/sec
ZDOT = 18802
351075 ZDOT = 5749
828952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16738233
19 X = -5101813
48
Y = -13862366
97 feet Y = -4225249
45 meter
Z = 4989095
51 Z = 1520676
31
XDOT = 12556
733756 XDOT = 3827
292449
YDOT = -8315
938581 feet/sec YDOT = -2534
698080 meter/sec
ZDOT = 18889
745478 ZDOT = 5757
594422
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 20343
83237316
00016717 00000-0 10270-3 0 9024
2 25544 51
6428 204
3248 0001944 125
3660 234
7672 15
49177698 19088
Satellite: ISS
Catalog Number: 25544
Epoch time: 20343
83237316 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 204
3248 deg
Eccentricity:
0001944
Arg of perigee: 125
3660 deg
Mean anomaly: 234
7672 deg
Mean motion: 15
49177698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 316
Coasting Arc #4 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2020/344/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5720025
21 A = 6802666
08 meter
Y = 3288585
51 meter E =
0009776
Z = -1641756
18 I = 51
53130
XDOT = -3672
153144 Wp = 139
53146
YDOT = 3551
982751 meter/sec RA = 198
49295 deg
ZDOT = -5705
573257 TA = 58
43158
MA = 58
33617
Ha = 229
422 n
mi
Hp = 221
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18766486
90 X = 5690800
90
Y = 10789322
53 feet Y = 3352387
65 meter
Z = -5386339
18 Z = -1614041
03
XDOT = -12047
746534 XDOT = -3683
884911
YDOT = 11653
486715 feet/sec YDOT = 3510
852914 meter/sec
ZDOT = -18719
072364 ZDOT = -5723
439537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17909109
06 X = 5458696
44
Y = 12215568
78 feet Y = 3723305
36 meter
Z = -5258027
47 Z = -1602646
77
XDOT = -11896
563758 XDOT = -3626
072633
YDOT = 9386
628723 feet/sec YDOT = 2861
044435 meter/sec
ZDOT = -18801
817159 ZDOT = -5730
793870
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 20344
79999646
00016717 00000-0 10270-3 0 9032
2 25544 51
6433 199
5374 0001876 126
0787 234
0537 15
49180037 19232
Satellite: ISS
Catalog Number: 25544
Epoch time: 20344
79999646 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 199
5374 deg
Eccentricity:
0001876
Arg of perigee: 126
0787 deg
Mean anomaly: 234
0537 deg
Mean motion: 15
49180037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 338
Coasting Arc #5 (Orbit 1927)
---------------------------------------
Vector Time (GMT): 2020/345/02:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4029163
66 A = 6794248
70 meter
Y = 2731794
15 meter E =
0012963
Z = -4752238
12 I = 51
51221
XDOT = -5915
661283 Wp = 109
62033
YDOT = -4027
329375 meter/sec RA = 196
77557 deg
ZDOT = 2702
262724 TA = 187
19777
MA = 187
21640
Ha = 229
467 n
mi
Hp = 221
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13219040
88 X = -4036328
06
Y = 8962579
24 feet Y = 2686697
45 meter
Z = -15591332
42 Z = -4771827
62
XDOT = -19408
337543 XDOT = -5883
312981
YDOT = -13213
022883 feet/sec YDOT = -4093
301881 meter/sec
ZDOT = 8865
691352 ZDOT = 2673
604722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14117644
25 X = 4303057
97
Y = 7275010
37 feet Y = 2217423
16 meter
Z = -15682055
36 Z = -4779890
47
XDOT = -1838
293218 XDOT = -560
311773
YDOT = 22379
740029 feet/sec YDOT = 6821
344761 meter/sec
ZDOT = 8733
011463 ZDOT = 2661
821894
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 20345
12253619
00016717 00000-0 10270-3 0 9044
2 25544 51
6414 197
9457 0001809 112
3269 247
8072 15
49146263 19288
Satellite: ISS
Catalog Number: 25544
Epoch time: 20345
12253619 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 197
9457 deg
Eccentricity:
0001809
Arg of perigee: 112
3269 deg
Mean anomaly: 247
8072 deg
Mean motion: 15
49146263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1928
Checksum: 316
Coasting Arc #6 (Orbit 1943)
---------------------------------------
Vector Time (GMT): 2020/346/02:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3848020
81 A = 6794288
48 meter
Y = -3017202
31 meter E =
0008863
Z = 4711104
74 I = 51
54398
XDOT = 6196
556191 Wp = 71
83228
YDOT = 3552
056674 meter/sec RA = 191
82065 deg
ZDOT = -2779
425119 TA = 45
79179
MA = 45
71903
Ha = 229
259 n
mi
Hp = 221
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12624740
18 X = 3858589
92
Y = -9898957
70 feet Y = -2974112
31 meter
Z = 15456380
40 Z = 4729822
58
XDOT = 20329
908763 XDOT = 6169
876517
YDOT = 11653
729247 feet/sec YDOT = 3621
202094 meter/sec
ZDOT = -9118
848817 ZDOT = -2749
388733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14765701
14 X = -4500585
71
Y = -6054739
52 feet Y = -1845484
61 meter
Z = 15543079
57 Z = 4737530
65
XDOT = -287
458029 XDOT = -87
617207
YDOT = -22409
606351 feet/sec YDOT = -6830
448016 meter/sec
ZDOT = -8979
764973 ZDOT = -2737
032364
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 20346
15466341
00016717 00000-0 10270-3 0 9057
2 25544 51
6399 192
8389 0001670 115
7647 244
3676 15
49176453 19445
Satellite: ISS
Catalog Number: 25544
Epoch time: 20346
15466341 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 192
8389 deg
Eccentricity:
0001670
Arg of perigee: 115
7647 deg
Mean anomaly: 244
3676 deg
Mean motion: 15
49176453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1944
Checksum: 336
Coasting Arc #7 (Orbit 1958)
---------------------------------------
Vector Time (GMT): 2020/347/02:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3642360
42 A = 6794474
03 meter
Y = 3312261
41 meter E =
0012465
Z = -4694805
73 I = 51
57732
XDOT = -6420
459446 Wp = 110
81216
YDOT = -3040
645006 meter/sec RA = 186
86851 deg
ZDOT = 2837
737414 TA = 187
43946
MA = 187
45798
Ha = 229
402 n
mi
Hp = 221
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11950001
39 X = -3656323
40
Y = 10866999
39 feet Y = 3271452
40 meter
Z = -15402905
93 Z = -4712532
69
XDOT = -21064
499496 XDOT = -6399
765163
YDOT = -9975
869441 feet/sec YDOT = -3112
327815 meter/sec
ZDOT = 9310
162118 ZDOT = 2806
598761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15362183
87 X = 4682393
64
Y = 4728724
46 feet Y = 1441315
22 meter
Z = -15485031
21 Z = -4719837
51
XDOT = 2414
516518 XDOT = 735
944635
YDOT = 22152
329781 feet/sec YDOT = 6752
030117 meter/sec
ZDOT = 9165
950564 ZDOT = 2793
781732
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 20347
12228213
00016717 00000-0 10270-3 0 9060
2 25544 51
6394 188
0519 0001694 117
3641 242
7681 15
49150862 19590
Satellite: ISS
Catalog Number: 25544
Epoch time: 20347
12228213 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 188
0519 deg
Eccentricity:
0001694
Arg of perigee: 117
3641 deg
Mean anomaly: 242
7681 deg
Mean motion: 15
49150862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1959
Checksum: 314
Coasting Arc #8 (Orbit 1974)
---------------------------------------
Vector Time (GMT): 2020/348/02:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3421139
81 A = 6794518
44 meter
Y = -3572847
87 meter E =
0009040
Z = 4651650
74 I = 51
61145
XDOT = 6619
742787 Wp = 73
25237
YDOT = 2533
030785 meter/sec RA = 181
91783 deg
ZDOT = -2915
785173 TA = 45
82177
MA = 45
74752
Ha = 229
214 n
mi
Hp = 221
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11224211
99 X = 3438242
84
Y = -11721941
85 feet Y = -3534495
28 meter
Z = 15261321
34 Z = 4668310
56
XDOT = 21718
316230 XDOT = 6605
089086
YDOT = 8310
468456 feet/sec YDOT = 2606
975991 meter/sec
ZDOT = -9566
224321 ZDOT = -2883
663824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15794439
23 X = -4814145
08
Y = -3400037
54 feet Y = -1036331
44 meter
Z = 15338520
74 Z = 4675181
12
XDOT = -4481
022243 XDOT = -1365
815580
YDOT = -21775
411776 feet/sec YDOT = -6637
145509 meter/sec
ZDOT = -9417
434668 ZDOT = -2870
434087
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 20348
15440519
00016717 00000-0 10270-3 0 9070
2 25544 51
6393 182
9447 0001589 122
3331 237
7973 15
49182702 19751
Satellite: ISS
Catalog Number: 25544
Epoch time: 20348
15440519 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 182
9447 deg
Eccentricity:
0001589
Arg of perigee: 122
3331 deg
Mean anomaly: 237
7973 deg
Mean motion: 15
49182702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1975
Checksum: 325
Coasting Arc #9 (Orbit 1989)
---------------------------------------
Vector Time (GMT): 2020/349/02:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3174944
83 A = 6794686
13 meter
Y = 3838814
82 meter E =
0011951
Z = -4632529
86 I = 51
64632
XDOT = -6757
821597 Wp = 111
75217
YDOT = -2000
262238 meter/sec RA = 176
96966 deg
ZDOT = 2975
850359 TA = 187
97666
MA = 187
99568
Ha = 229
328 n
mi
Hp = 221
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10416485
65 X = -3195133
26
Y = 12594536
80 feet Y = 3803198
21 meter
Z = -15198588
77 Z = -4648001
03
XDOT = -22171
330699 XDOT = -6749
406916
YDOT = -6562
540151 feet/sec YDOT = -2075
786504 meter/sec
ZDOT = 9763
288579 ZDOT = 2943
043286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16156233
92 X = 4924420
10
Y = 1979061
87 feet Y = 603218
06 meter
Z = -15270299
63 Z = -4654387
33
XDOT = 6491
145936 XDOT = 1978
501281
YDOT = 21122
036076 feet/sec YDOT = 6437
996596 meter/sec
ZDOT = 9611
291559 ZDOT = 2929
521667
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 20349
12201745
00016717 00000-0 10270-3 0 9085
2 25544 51
6398 178
1570 0001592 121
2688 238
8618 15
49166134 19903
Satellite: ISS
Catalog Number: 25544
Epoch time: 20349
12201745 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 178
1570 deg
Eccentricity:
0001592
Arg of perigee: 121
2688 deg
Mean anomaly: 238
8618 deg
Mean motion: 15
49166134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1990
Checksum: 322
Coasting Arc #10 (Orbit 2005)
---------------------------------------
Vector Time (GMT): 2020/350/02:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2918180
82 A = 6794759
54 meter
Y = -4069097
04 meter E =
0009325
Z = 4586518
63 I = 51
68014
XDOT = 6872
014801 Wp = 74
06207
YDOT = 1475
555945 meter/sec RA = 172
02374 deg
ZDOT = -3055
566193 TA = 46
51828
MA = 46
44078
Ha = 229
178 n
mi
Hp = 221
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9574084
05 X = 2941187
06
Y = -13350055
90 feet Y = -4036336
04 meter
Z = 15047633
31 Z = 4600749
20
XDOT = 22545
980318 XDOT = 6869
846182
YDOT = 4841
062813 feet/sec YDOT = 1552
392177 meter/sec
ZDOT = -10024
823468 ZDOT = -3022
189520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16357181
38 X = -4985668
89
Y = -582810
12 feet Y = -177640
53 meter
Z = 15113612
93 Z = 4606629
22
XDOT = -8417
348632 XDOT = -2565
607863
YDOT = -20364
028207 feet/sec YDOT = -6206
955797 meter/sec
ZDOT = -9870
153284 ZDOT = -3008
422721
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 20350
15413456
00016717 00000-0 10270-3 0 9095
2 25544 51
6393 173
0499 0001488 123
9180 236
2111 15
49192299 20062
Satellite: ISS
Catalog Number: 25544
Epoch time: 20350
15413456 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 173
0499 deg
Eccentricity:
0001488
Arg of perigee: 123
9180 deg
Mean anomaly: 236
2111 deg
Mean motion: 15
49192299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2006
Checksum: 301
Coasting Arc #11 (Orbit 2020)
---------------------------------------
Vector Time (GMT): 2020/351/02:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 995365
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2633430
42 A = 6794939
87 meter
Y = 4301154
12 meter E =
0011353
Z = -4565095
87 I = 51
71408
XDOT = -6924
505733 Wp = 112
86924
YDOT = -934
786877 meter/sec RA = 167
08034 deg
ZDOT = 3115
631698 TA = 188
37527
MA = 188
39424
Ha = 229
242 n
mi
Hp = 221
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8639863
60 X = -2659156
97
Y = 14111398
02 feet Y = 4271562
18 meter
Z = -14977348
65 Z = -4577949
72
XDOT = -22718
194661 XDOT = -6928
671923
YDOT = -3066
886080 feet/sec YDOT = -1012
245525 meter/sec
ZDOT = 10221
888773 ZDOT = 3081
984979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16467582
25 X = 5019319
07
Y = -899026
44 feet Y = -274023
26 meter
Z = -15036962
99 Z = -4583266
32
XDOT = 10242
340216 XDOT = 3121
865298
YDOT = 19352
350055 feet/sec YDOT = 5898
596297 meter/sec
ZDOT = 10065
931853 ZDOT = 3068
096029
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 20351
12174323
00016717 00000-0 10270-3 0 9102
2 25544 51
6395 168
2624 0001451 127
9742 232
1540 15
49173412 20212
Satellite: ISS
Catalog Number: 25544
Epoch time: 20351
12174323 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 168
2624 deg
Eccentricity:
0001451
Arg of perigee: 127
9742 deg
Mean anomaly: 232
1540 deg
Mean motion: 15
49173412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2021
Checksum: 268
Coasting Arc #12 (Orbit 2029)
---------------------------------------
Vector Time (GMT): 2020/351/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 980089
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3810196
96 A = 6793929
32 meter
Y = -2888781
95 meter E =
0009051
Z = 4822101
91 I = 51
73117
XDOT = 6138
380964 Wp = 124
49175
YDOT = -3805
064756 meter/sec RA = 164
45927 deg
ZDOT = 2562
321021 TA = 300
25666
MA = 300
34622
Ha = 229
275 n
mi
Hp = 222
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12500646
20 X = -3801033
40
Y = -9477631
07 feet Y = -2931339
90 meter
Z = 15820544
31 Z = 4803615
33
XDOT = 20139
045156 XDOT = 6168
027928
YDOT = -12483
808255 feet/sec YDOT = -3736
255648 meter/sec
ZDOT = 8406
565030 ZDOT = 2592
210037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3185287
30 X = -970875
57
Y = -15448275
43 feet Y = -4708634
35 meter
Z = 15734865
73 Z = 4795987
07
XDOT = 22190
380464 XDOT = 6763
627965
YDOT = 4156
569516 feet/sec YDOT = 1266
922389 meter/sec
ZDOT = 8545
154134 ZDOT = 2604
562980
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 20351
70230612
00016717 00000-0 10270-3 0 9111
2 25544 51
6420 165
3859 0001800 146
7571 213
3692 15
49220022 20305
Satellite: ISS
Catalog Number: 25544
Epoch time: 20351
70230612 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 165
3859 deg
Eccentricity:
0001800
Arg of perigee: 146
7571 deg
Mean anomaly: 213
3692 deg
Mean motion: 15
49220022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2030
Checksum: 260
Coasting Arc #13 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2020/352/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 980089
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3968629
87 A = 6793867
43 meter
Y = 2611815
56 meter E =
0012100
Z = -4867546
15 I = 51
76423
XDOT = -5845
465352 Wp = 80
60779
YDOT = 4268
343615 meter/sec RA = 159
51950 deg
ZDOT = -2478
996296 TA = 165
04700
MA = 165
01119
Ha = 229
201 n
mi
Hp = 222
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13020439
21 X = 3962772
30
Y = 8568948
68 feet Y = 2656163
62 meter
Z = -15969639
59 Z = -4848282
13
XDOT = -19178
035933 XDOT = -5880
719403
YDOT = 14003
752018 feet/sec YDOT = 4202
778684 meter/sec
ZDOT = -8133
189949 ZDOT = -2507
475958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4436320
97 X = 1352190
63
Y = 15037354
02 feet Y = 4583385
51 meter
Z = -15880338
40 Z = -4840327
14
XDOT = -22540
205917 XDOT = -6870
254764
YDOT = -2067
162693 feet/sec YDOT = -630
071189 meter/sec
ZDOT = -8265
273427 ZDOT = -2519
255340
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 20352
66991102
00016717 00000-0 10270-3 0 9126
2 25544 51
6432 160
5988 0001751 147
7067 212
4191 15
49191790 20453
Satellite: ISS
Catalog Number: 25544
Epoch time: 20352
66991102 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 160
5988 deg
Eccentricity:
0001751
Arg of perigee: 147
7067 deg
Mean anomaly: 212
4191 deg
Mean motion: 15
49191790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 303
Coasting Arc #14 (Orbit 2060)
---------------------------------------
Vector Time (GMT): 2020/353/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 980089
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4113539
66 A = 6793646
60 meter
Y = -2303822
90 meter E =
0008605
Z = 4887188
57 I = 51
79562
XDOT = 5525
628169 Wp = 125
94812
YDOT = -4729
205035 meter/sec RA = 154
58157 deg
ZDOT = 2413
662792 TA = 300
37973
MA = 300
46477
Ha = 229
248 n
mi
Hp = 222
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13495865
03 X = -4111210
76
Y = -7558474
07 feet Y = -2349811
06 meter
Z = 16034083
22 Z = 4867212
20
XDOT = 18128
701342 XDOT = 5566
376854
YDOT = -15515
764552 feet/sec YDOT = -4667
185962 meter/sec
ZDOT = 7918
841182 ZDOT = 2440
602164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5703835
94 X = -1738529
19
Y = -14480911
03 feet Y = -4413781
68 meter
Z = 15941461
65 Z = 4858957
51
XDOT = 22758
892464 XDOT = 6936
910423
YDOT = -80
609681 feet/sec YDOT = -24
569831 meter/sec
ZDOT = 8043
807164 ZDOT = 2451
752423
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 20353
70201804
00016717 00000-0 10270-3 0 9136
2 25544 51
6436 155
4920 0001732 147
9148 212
2108 15
49228764 20613
Satellite: ISS
Catalog Number: 25544
Epoch time: 20353
70201804 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 155
4920 deg
Eccentricity:
0001732
Arg of perigee: 147
9148 deg
Mean anomaly: 212
2108 deg
Mean motion: 15
49228764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2061
Checksum: 283
Coasting Arc #15 (Orbit 2066)
---------------------------------------
Vector Time (GMT): 2020/354/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980089
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4125144
52 A = 6800387
45 meter
Y = 4631899
66 meter E =
0005240
Z = -2790623
04 I = 51
82848
XDOT = -5407
710911 Wp = 74
88853
YDOT = -1728
029281 meter/sec RA = 152
40114 deg
ZDOT = 5134
950907 TA = 253
65144
MA = 253
70906
Ha = 229
140 n
mi
Hp = 222
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13533938
70 X = -4163078
16
Y = 15196521
19 feet Y = 4585557
56 meter
Z = -9155587
42 Z = -2810752
72
XDOT = -17741
833699 XDOT = -5412
927994
YDOT = -5669
387404 feet/sec YDOT = -1788
531970 meter/sec
ZDOT = 16846
951796 ZDOT = 5108
669812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19675578
98 X = 5997116
47
Y = 5025385
82 feet Y = 1531737
60 meter
Z = -9248979
58 Z = -2819088
98
XDOT = 3496
211378 XDOT = 1065
645228
YDOT = 17037
124592 feet/sec YDOT = 5192
915576 meter/sec
ZDOT = 16725
079998 ZDOT = 5097
804384
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 20354
08905915
00016717 00000-0 10270-3 0 9143
2 25544 51
6409 153
5805 0001304 133
2526 226
8733 15
49184769 20674
Satellite: ISS
Catalog Number: 25544
Epoch time: 20354
08905915 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 153
5805 deg
Eccentricity:
0001304
Arg of perigee: 133
2526 deg
Mean anomaly: 226
8733 deg
Mean motion: 15
49184769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2067
Checksum: 311
Coasting Arc #16 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2020/355/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980089
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3791106
87 A = 6800522
47 meter
Y = -4942894
03 meter E =
0014518
Z = 2710585
32 I = 51
85929
XDOT = 5475
741074 Wp = 104
59835
YDOT = 1342
248576 meter/sec RA = 147
46719 deg
ZDOT = -5191
207247 TA = 44
91701
MA = 44
79963
Ha = 229
074 n
mi
Hp = 222
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12438014
67 X = 3832931
73
Y = -16216843
94 feet Y = -4900265
56 meter
Z = 8892996
45 Z = 2729101
91
XDOT = 17965
029769 XDOT = 5485
540301
YDOT = 4403
702678 feet/sec YDOT = 1403
537557 meter/sec
ZDOT = -17031
519838 ZDOT = -5164
584606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20140973
95 X = -6138968
86
Y = -3239709
95 feet Y = -987463
59 meter
Z = 8978923
66 Z = 2736775
93
XDOT = -4904
706458 XDOT = -1494
954528
YDOT = -16546
041971 feet/sec YDOT = -5043
233593 meter/sec
ZDOT = -16908
044700 ZDOT = -5153
572024
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 20355
12116507
00016717 00000-0 10270-3 0 9151
2 25544 51
6416 148
4739 0001303 137
4587 222
6665 15
49205563 20835
Satellite: ISS
Catalog Number: 25544
Epoch time: 20355
12116507 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 148
4739 deg
Eccentricity:
0001303
Arg of perigee: 137
4587 deg
Mean anomaly: 222
6665 deg
Mean motion: 15
49205563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 300
Coasting Arc #17 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2020/355/04:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 980089
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1482222
29 A = 6791800
19 meter
Y = -3993722
09 meter E =
0003572
Z = 5286786
65 I = 51
83579
XDOT = 6715
386098 Wp = 81
73707
YDOT = -3596
910424 meter/sec RA = 146
89307 deg
ZDOT = -833
431834 TA = 16
21934
MA = 16
20791
Ha = 229
049 n
mi
Hp = 222
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4862934
04 X = -1463133
02
Y = -13102762
76 feet Y = -4010191
15 meter
Z = 17345100
57 Z = 5279632
65
XDOT = 22032
106620 XDOT = 6759
157032
YDOT = -11800
887219 feet/sec YDOT = -3521
569331 meter/sec
ZDOT = -2734
356410 ZDOT = -800
705520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 556549
32 X = 169636
23
Y = 14006058
62 feet Y = 4269046
67 meter
Z = 17311949
86 Z = 5276682
32
XDOT = -23637
202889 XDOT = -7204
619441
YDOT = 4135
332800 feet/sec YDOT = 1260
449438 meter/sec
ZDOT = -2582
527516 ZDOT = -787
154387
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 20355
25017674
00016717 00000-0 10270-3 0 9161
2 25544 51
6434 147
8369 0001227 144
4697 215
6535 15
49247116 20852
Satellite: ISS
Catalog Number: 25544
Epoch time: 20355
25017674 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 147
8369 deg
Eccentricity:
0001227
Arg of perigee: 144
4697 deg
Mean anomaly: 215
6535 deg
Mean motion: 15
49247116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2085
Checksum: 317
Coasting Arc #18 (Orbit 2099)
---------------------------------------
Vector Time (GMT): 2020/356/04:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 980089
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1741394
70 A = 6791916
17 meter
Y = 3908642
13 meter E =
0015257
Z = -5287815
25 I = 51
86474
XDOT = -6397
508264 Wp = 100
56821
YDOT = 4091
431055 meter/sec RA = 141
95973 deg
ZDOT = 916
986898 TA = 178
20136
MA = 178
19587
Ha = 228
997 n
mi
Hp = 222
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5713237
21 X = 1723242
61
Y = 12823629
05 feet Y = 3928014
62 meter
Z = -17348475
23 Z = -5279400
06
XDOT = -20989
200342 XDOT = -6447
238573
YDOT = 13423
330232 feet/sec YDOT = 4019
611380 meter/sec
ZDOT = 3008
487199 ZDOT = 885
790143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1692291
31 X = -515810
39
Y = -13984793
48 feet Y = -4262565
05 meter
Z = -17309472
43 Z = -5275927
20
XDOT = 23060
206091 XDOT = 7028
750817
YDOT = -6336
960009 feet/sec YDOT = -1931
505411 meter/sec
ZDOT = 2863
728480 ZDOT = 872
864441
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 20356
21777307
00016717 00000-0 10270-3 0 9175
2 25544 51
6445 143
0492 0001209 145
8910 214
2318 15
49228210 21008
Satellite: ISS
Catalog Number: 25544
Epoch time: 20356
21777307 = yrday
fracday
Element set: 917
Inclination: 51
6445 deg
RA of node: 143
0492 deg
Eccentricity:
0001209
Arg of perigee: 145
8910 deg
Mean anomaly: 214
2318 deg
Mean motion: 15
49228210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2100
Checksum: 277
Coasting Arc #19 (Orbit 2115)
---------------------------------------
Vector Time (GMT): 2020/357/04:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 980089
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1986218
78 A = 6791867
96 meter
Y = -3795980
92 meter E =
0003670
Z = 5267238
10 I = 51
89110
XDOT = 6066
649955 Wp = 76
48714
YDOT = -4572
793480 meter/sec RA = 137
02829 deg
ZDOT = -1006
418110 TA = 23
12908
MA = 23
11256
Ha = 228
988 n
mi
Hp = 222
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6516465
81 X = -1969208
44
Y = -12454005
64 feet Y = -3818097
57 meter
Z = 17280964
90 Z = 5257630
88
XDOT = 19903
707200 XDOT = 6122
222011
YDOT = -15002
603280 feet/sec YDOT = -4504
641033 meter/sec
ZDOT = -3301
896686 ZDOT = -976
814262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2807425
39 X = 855703
26
Y = 13828309
07 feet Y = 4214868
60 meter
Z = 17236431
25 Z = 5253664
25
XDOT = -22368
921379 XDOT = -6818
047236
YDOT = 8491
604231 feet/sec YDOT = 2588
240970 meter/sec
ZDOT = -3164
502649 ZDOT = -964
540408
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 20357
24986989
00016717 00000-0 10270-3 0 9188
2 25544 51
6447 137
9423 0001117 150
7614 209
3599 15
49259074 21165
Satellite: ISS
Catalog Number: 25544
Epoch time: 20357
24986989 = yrday
fracday
Element set: 918
Inclination: 51
6447 deg
RA of node: 137
9423 deg
Eccentricity:
0001117
Arg of perigee: 150
7614 deg
Mean anomaly: 209
3599 deg
Mean motion: 15
49259074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2116
Checksum: 337
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