[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 2nd 2020
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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) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 431 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
276/01:41:15
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 222
6
277/05:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 222
6
278/10:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 222
7
280/09:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 222
6
281/08:14:31
819 -2
2 -2
4 2
4
N/A 0
8 0
2 228
3
000/00:07:03
639 0
1 -0
0 222
7
283/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
7
288/05:45:05
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
7
288/08:50:45
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 222
7
289/02:17:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 222
6
Coasting Arc #1 (Orbit 833)
---------------------------------------
Vector Time (GMT): 2020/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1650967
75 A = 6793995
03 meter
Y = -4216106
02 meter E =
0006774
Z = 5061253
36 I = 51
58191
XDOT = 7405
949876 Wp = 121
28045
YDOT = -673
973355 meter/sec RA = 186
17374 deg
ZDOT = 1849
097023 TA = 310
75258
MA = 310
81136
Ha = 229
807 n
mi
Hp = 222
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5416560
84 X = -1628284
03
Y = -13832368
83 feet Y = -4234441
01 meter
Z = 16605161
94 Z = 5053289
08
XDOT = 24297
735815 XDOT = 7403
954137
YDOT = -2211
198670 feet/sec YDOT = -591
165692 meter/sec
ZDOT = 6066
591283 ZDOT = 1885
067564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7578675
80 X = 2309980
39
Y = 12824125
47 feet Y = 3908793
44 meter
Z = 16568356
61 Z = 5050035
09
XDOT = -22697
802888 XDOT = -6918
290320
YDOT = 5338
822398 feet/sec YDOT = 1627
273067 meter/sec
ZDOT = 6232
739040 ZDOT = 1899
738859
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 20274
55171548
00016717 00000-0 10270-3 0 9008
2 25544 51
6437 187
1175 0001176 104
8675 255
2605 15
48836744 8344
Satellite: ISS
Catalog Number: 25544
Epoch time: 20274
55171548 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 187
1175 deg
Eccentricity:
0001176
Arg of perigee: 104
8675 deg
Mean anomaly: 255
2605 deg
Mean motion: 15
48836744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 834
Checksum: 316
Coasting Arc #2 (Orbit 848)
---------------------------------------
Vector Time (GMT): 2020/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2069438
54 A = 6794075
43 meter
Y = 4052063
89 meter E =
0014041
Z = -5058309
84 I = 51
61646
XDOT = -7284
950318 Wp = 78
20847
YDOT = 1349
864762 meter/sec RA = 181
22753 deg
ZDOT = -1900
740120 TA = 173
31842
MA = 173
29968
Ha = 229
810 n
mi
Hp = 222
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6789496
53 X = 2048543
91
Y = 13294172
87 feet Y = 4075088
51 meter
Z = -16595504
74 Z = -5048308
39
XDOT = -23900
755635 XDOT = -7290
270696
YDOT = 4428
690164 feet/sec YDOT = 1268
369286 meter/sec
ZDOT = -6236
024016 ZDOT = -1936
140889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9059673
13 X = -2761388
37
Y = -11928394
55 feet Y = -3635774
66 meter
Z = -16549283
95 Z = -5044221
75
XDOT = 21889
433427 XDOT = 6671
899308
YDOT = -7754
163671 feet/sec YDOT = -2363
469087 meter/sec
ZDOT = -6399
553587 ZDOT = -1950
583933
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 20275
51956001
00016717 00000-0 10270-3 0 9011
2 25544 51
6443 182
3318 0001294 100
3462 259
7834 15
48834285 8490
Satellite: ISS
Catalog Number: 25544
Epoch time: 20275
51956001 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 182
3318 deg
Eccentricity:
0001294
Arg of perigee: 100
3462 deg
Mean anomaly: 259
7834 deg
Mean motion: 15
48834285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 849
Checksum: 305
Coasting Arc #3 (Orbit 857)
---------------------------------------
Vector Time (GMT): 2020/276/01:41:15
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6634047
33 A = 6804178
52 meter
Y = 808273
63 meter E =
0010333
Z = -1255840
08 I = 51
66790
XDOT = -1667
362102 Wp = 139
27217
YDOT = 4665
663283 meter/sec RA = 178
40214 deg
ZDOT = -5839
857010 TA = 54
34497
MA = 54
24880
Ha = 229
846 n
mi
Hp = 222
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21765247
15 X = 6630616
13
Y = 2651816
36 feet Y = 882441
00 meter
Z = -4120210
23 Z = -1223622
55
XDOT = -5470
348104 XDOT = -1691
044043
YDOT = 15307
294234 feet/sec YDOT = 4646
884665 meter/sec
ZDOT = -19159
635860 ZDOT = -5848
014458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19254211
32 X = 5868683
61
Y = -10546934
90 feet Y = -3214705
76 meter
Z = -3971367
08 Z = -1210472
69
XDOT = 3813
422112 XDOT = 1162
331060
YDOT = 14145
681286 feet/sec YDOT = 4311
603656 meter/sec
ZDOT = -19197
300399 ZDOT = -5851
337162
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 20276
10026479
00016717 00000-0 10270-3 0 9025
2 25544 51
6428 179
4590 0001323 116
2476 243
8810 15
48821913 8588
Satellite: ISS
Catalog Number: 25544
Epoch time: 20276
10026479 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 179
4590 deg
Eccentricity:
0001323
Arg of perigee: 116
2476 deg
Mean anomaly: 243
8810 deg
Mean motion: 15
48821913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 858
Checksum: 307
Coasting Arc #4 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2020/277/01:41:15
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6691774
46 A = 6804360
84 meter
Y = -174045
70 meter E =
0014356
Z = 1184288
54 I = 51
70140
XDOT = 1170
348262 Wp = 62
18436
YDOT = -4792
861573 meter/sec RA = 173
45859 deg
ZDOT = 5860
778463 TA = 310
64126
MA = 310
76599
Ha = 229
861 n
mi
Hp = 222
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21954640
63 X = -6695083
57
Y = -571016
09 feet Y = -248896
32 meter
Z = 3885461
10 Z = 1151774
02
XDOT = 3839
725268 XDOT = 1195
387763
YDOT = -15724
611461 feet/sec YDOT = -4779
633374 meter/sec
ZDOT = 19228
275796 ZDOT = 5866
524884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17978969
32 X = -5479989
85
Y = 12658349
41 feet Y = 3858264
90 meter
Z = 3735232
93 Z = 1138499
00
XDOT = -5484
107798 XDOT = -1671
556057
YDOT = -13519
128767 feet/sec YDOT = -4120
630448 meter/sec
ZDOT = 19254
805918 ZDOT = 5868
864844
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 20277
13262915
00016717 00000-0 10270-3 0 9037
2 25544 51
6423 174
3542 0001267 114
5395 245
5887 15
48786084 8742
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
13262915 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 174
3542 deg
Eccentricity:
0001267
Arg of perigee: 114
5395 deg
Mean anomaly: 245
5887 deg
Mean motion: 15
48786084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 323
Coasting Arc #5 (Orbit 875)
---------------------------------------
Vector Time (GMT): 2020/277/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1754566
66 A = 6794204
97 meter
Y = 4236727
67 meter E =
0014099
Z = -5026212
05 I = 51
67201
XDOT = -7348
754448 Wp = 105
76154
YDOT = -648
945866 meter/sec RA = 172
54967 deg
ZDOT = 2019
307719 TA = 183
89911
MA = 183
91010
Ha = 229
841 n
mi
Hp = 222
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5756452
29 X = -1777397
77
Y = 13900025
18 feet Y = 4216978
76 meter
Z = -16490197
00 Z = -5034791
00
XDOT = -24110
086773 XDOT = -7350
760360
YDOT = -2129
087487 feet/sec YDOT = -731
135950 meter/sec
ZDOT = 6625
025324 ZDOT = 1983
604975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14726965
24 X = 4488779
01
Y = 2855809
59 feet Y = 870450
76 meter
Z = -16529818
10 Z = -5038288
56
XDOT = 2779
816651 XDOT = 847
288115
YDOT = 23037
809896 feet/sec YDOT = 7021
924456 meter/sec
ZDOT = 6460
061402 ZDOT = 1969
026715
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 20277
26167299
00016717 00000-0 10270-3 0 9041
2 25544 51
6405 173
7168 0001293 111
6774 248
4513 15
48798838 8767
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
26167299 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 173
7168 deg
Eccentricity:
0001293
Arg of perigee: 111
6774 deg
Mean anomaly: 248
4513 deg
Mean motion: 15
48798838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 876
Checksum: 342
Coasting Arc #6 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2020/278/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1324887
95 A = 6794049
60 meter
Y = -4360921
07 meter E =
0006421
Z = 5034205
24 I = 51
70511
XDOT = 7404
915293 Wp = 65
55949
YDOT = -32
373707 meter/sec RA = 167
60915 deg
ZDOT = -1972
272919 TA = 43
60918
MA = 43
55845
Ha = 229
726 n
mi
Hp = 222
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4346745
24 X = 1349100
86
Y = -14307483
84 feet Y = -4345969
47 meter
Z = 16516421
39 Z = 5040700
28
XDOT = 24294
341512 XDOT = 7414
307310
YDOT = -106
212951 feet/sec YDOT = 50
485736 meter/sec
ZDOT = -6470
711676 ZDOT = -1936
279247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14876529
97 X = -4534366
34
Y = -1138103
60 feet Y = -346893
98 meter
Z = 16546420
76 Z = 5043349
05
XDOT = -5292
917291 XDOT = -1613
281190
YDOT = -22689
285563 feet/sec YDOT = -6915
694240 meter/sec
ZDOT = -6304
387471 ZDOT = -1921
577301
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 20278
29403174
00016717 00000-0 10270-3 0 9051
2 25544 51
6405 168
6113 0001192 114
0160 246
1115 15
48827541 8929
Satellite: ISS
Catalog Number: 25544
Epoch time: 20278
29403174 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 168
6113 deg
Eccentricity:
0001192
Arg of perigee: 114
0160 deg
Mean anomaly: 246
1115 deg
Mean motion: 15
48827541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 284
Coasting Arc #7 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2020/278/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6664667
57 A = 6804779
00 meter
Y = 1304929
19 meter E =
0013159
Z = 324105
09 I = 51
74864
XDOT = -623
586047 Wp = 52
89583
YDOT = -4715
912911 meter/sec RA = 166
76551 deg
ZDOT = 6004
029828 TA = 310
58431
MA = 310
69875
Ha = 229
747 n
mi
Hp = 222
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21865707
24 X = -6680338
69
Y = 4281263
76 feet Y = 1230312
50 meter
Z = 1063336
91 Z = 291691
96
XDOT = -2045
885982 XDOT = -599
969652
YDOT = -15472
155219 feet/sec YDOT = -4722
753823 meter/sec
ZDOT = 19698
260589 ZDOT = 6001
058328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22239362
51 X = 6778557
69
Y = 1464658
08 feet Y = 446427
78 meter
Z = 913558
90 Z = 278452
75
XDOT = -1748
681531 XDOT = -532
998131
YDOT = 13891
878813 feet/sec YDOT = 4234
244662 meter/sec
ZDOT = 19684
515044 ZDOT = 5999
840185
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 20278
48760014
00016717 00000-0 10270-3 0 9062
2 25544 51
6427 167
6546 0001108 108
3553 251
7717 15
48817952 8959
Satellite: ISS
Catalog Number: 25544
Epoch time: 20278
48760014 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 167
6546 deg
Eccentricity:
0001108
Arg of perigee: 108
3553 deg
Mean anomaly: 251
7717 deg
Mean motion: 15
48817952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 895
Checksum: 325
Coasting Arc #8 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2020/279/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6522461
18 A = 6804786
98 meter
Y = -1896770
20 meter E =
0012640
Z = -294716
43 I = 51
78162
XDOT = 1081
112136 Wp = 134
93673
YDOT = 4625
490314 meter/sec RA = 161
82736 deg
ZDOT = -6009
274179 TA = 48
22602
MA = 48
11807
Ha = 229
791 n
mi
Hp = 222
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21399150
85 X = 6544618
26
Y = -6222999
34 feet Y = -1823707
49 meter
Z = -966917
43 Z = -262978
28
XDOT = 3546
955826 XDOT = 1058
498391
YDOT = 15175
493157 feet/sec YDOT = 4637
453321 meter/sec
ZDOT = -19715
466468 ZDOT = -6004
077624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22272716
15 X = -6788723
88
Y = 915220
76 feet Y = 278959
29 meter
Z = -820239
80 Z = -250009
09
XDOT = 126
578856 XDOT = 38
581235
YDOT = -13990
572746 feet/sec YDOT = -4264
326573 meter/sec
ZDOT = -19691
442130 ZDOT = -6001
951561
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 20279
45543346
00016717 00000-0 10270-3 0 9078
2 25544 51
6430 162
8687 0001159 113
9356 246
1915 15
48816724 9107
Satellite: ISS
Catalog Number: 25544
Epoch time: 20279
45543346 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 162
8687 deg
Eccentricity:
0001159
Arg of perigee: 113
9356 deg
Mean anomaly: 246
1915 deg
Mean motion: 15
48816724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 319
Coasting Arc #9 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2020/280/09:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3535515
37 A = 6799254
89 meter
Y = 4574859
43 meter E =
0006421
Z = -3584443
41 I = 51
79464
XDOT = -6096
048502 Wp = 101
14913
YDOT = -1218
850573 meter/sec RA = 156
90320 deg
ZDOT = 4462
788047 TA = 216
74201
MA = 216
78605
Ha = 229
687 n
mi
Hp = 222
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11599459
89 X = -3568998
52
Y = 15009381
34 feet Y = 4535135
42 meter
Z = -11759984
94 Z = -3601699
41
XDOT = -20000
159126 XDOT = -6103
644006
YDOT = -3998
853586 feet/sec YDOT = -1287
063271 meter/sec
ZDOT = 14641
693066 ZDOT = 4433
156797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15161204
76 X = 4621135
21
Y = -11317444
91 feet Y = -3449557
21 meter
Z = -11839744
70 Z = -3608754
18
XDOT = 17433
892336 XDOT = 5313
850384
YDOT = 8199
895207 feet/sec YDOT = 2499
328059 meter/sec
ZDOT = 14504
731173 ZDOT = 4421
042062
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 20280
42326553
00016717 00000-0 10270-3 0 9087
2 25544 51
6425 158
0828 0001119 116
0199 244
1066 15
48843409 9251
Satellite: ISS
Catalog Number: 25544
Epoch time: 20280
42326553 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 158
0828 deg
Eccentricity:
0001119
Arg of perigee: 116
0199 deg
Mean anomaly: 244
1066 deg
Mean motion: 15
48843409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 302
Coasting Arc #10 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2020/281/08:18:03
639
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 36131
95 A = 6792611
10 meter
Y = -4520923
81 meter E =
0004484
Z = 5067195
40 I = 51
80430
XDOT = 7133
446642 Wp = 52
11046
YDOT = -2063
748562 meter/sec RA = 152
32343 deg
ZDOT = -1888
305548 TA = 56
18581
MA = 56
14312
Ha = 228
268 n
mi
Hp = 222
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 118543
14 X = 62069
57
Y = -14832427
19 feet Y = -4520374
63 meter
Z = 16624656
81 Z = 5067434
00
XDOT = 23403
696332 XDOT = 7165
166416
YDOT = -6770
828614 feet/sec YDOT = -1983
799926 meter/sec
ZDOT = -6195
228176 ZDOT = -1853
576286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9526912
36 X = -2903802
89
Y = 11367322
45 feet Y = 3464759
88 meter
Z = 16625765
67 Z = 5067533
37
XDOT = -21492
806233 XDOT = -6551
007340
YDOT = -9168
411794 feet/sec YDOT = -2794
531915 meter/sec
ZDOT = -6034
679092 ZDOT = -1839
370187
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 20281
39107817
00016717 00000-0 10270-3 0 9095
2 25544 51
6416 153
2962 0001079 252
5711 107
5321 15
49284140 9403
Satellite: ISS
Catalog Number: 25544
Epoch time: 20281
39107817 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 153
2962 deg
Eccentricity:
0001079
Arg of perigee: 252
5711 deg
Mean anomaly: 107
5321 deg
Mean motion: 15
49284140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 292
Coasting Arc #11 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2020/282/08:18:03
639
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 239127
22 A = 6792733
74 meter
Y = 4554314
11 meter E =
0011946
Z = -5045045
87 I = 51
83485
XDOT = -6925
044367 Wp = 106
96411
YDOT = 2571
162341 meter/sec RA = 147
38640 deg
ZDOT = 1993
342376 TA = 182
38448
MA = 182
39018
Ha = 228
250 n
mi
Hp = 222
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 784538
12 X = 212688
10
Y = 14941975
43 feet Y = 4556840
34 meter
Z = -16551987
75 Z = -5043948
51
XDOT = -22719
961833 XDOT = -6962
963876
YDOT = 8435
571986 feet/sec YDOT = 2493
509522 meter/sec
ZDOT = 6539
837190 ZDOT = 1959
610527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8697051
60 X = 2650861
33
Y = -12182237
85 feet Y = -3713146
10 meter
Z = -16546927
28 Z = -5043503
43
XDOT = 22116
747940 XDOT = 6741
184772
YDOT = 7120
605490 feet/sec YDOT = 2170
360553 meter/sec
ZDOT = 6383
871666 ZDOT = 1945
804084
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 20282
35862531
00016717 00000-0 10270-3 0 9105
2 25544 51
6423 148
5073 0001025 259
5894 100
5141 15
49290350 9550
Satellite: ISS
Catalog Number: 25544
Epoch time: 20282
35862531 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 148
5073 deg
Eccentricity:
0001025
Arg of perigee: 259
5894 deg
Mean anomaly: 100
5141 deg
Mean motion: 15
49290350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 289
Coasting Arc #12 (Orbit 970)
---------------------------------------
Vector Time (GMT): 2020/283/08:18:03
639
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -506890
09 A = 6792850
43 meter
Y = -4564424
60 meter E =
0005215
Z = 5002706
88 I = 51
86303
XDOT = 6700
126093 Wp = 51
55188
YDOT = -3061
045406 meter/sec RA = 142
45331 deg
ZDOT = -2109
345652 TA = 58
96108
MA = 58
90988
Ha = 228
262 n
mi
Hp = 222
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1663025
23 X = -480112
26
Y = -14975146
33 feet Y = -4569943
28 meter
Z = 16413080
30 Z = 5000309
61
XDOT = 21982
040989 XDOT = 6744
103791
YDOT = -10042
799887 feet/sec YDOT = -2985
873900 meter/sec
ZDOT = -6920
425367 ZDOT = -2076
691801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7814909
82 X = -2381984
51
Y = 12896160
34 feet Y = 3930749
67 meter
Z = 16402015
08 Z = 4999334
19
XDOT = -22604
066122 XDOT = -6889
719354
YDOT = -5068
676382 feet/sec YDOT = -1544
932561 meter/sec
ZDOT = -6769
415986 ZDOT = -2063
317992
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 20283
39067360
00016717 00000-0 10270-3 0 9118
2 25544 51
6422 143
4011 0001007 267
6663 92
4372 15
49301508 9710
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
39067360 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 143
4011 deg
Eccentricity:
0001007
Arg of perigee: 267
6663 deg
Mean anomaly: 92
4372 deg
Mean motion: 15
49301508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 971
Checksum: 282
Coasting Arc #13 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2020/283/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2994726
75 A = 6791420
47 meter
Y = -2950392
32 meter E =
0001849
Z = 5332812
44 I = 51
87326
XDOT = 5678
894395 Wp = 135
17557
YDOT = -5131
747360 meter/sec RA = 139
94572 deg
ZDOT = 348
571553 TA = 311
50110
MA = 311
51697
Ha = 228
253 n
mi
Hp = 222
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9825219
00 X = -2987416
06
Y = -9679764
82 feet Y = -2983840
61 meter
Z = 17496103
79 Z = 5318282
82
XDOT = 18631
543292 XDOT = 5734
163892
YDOT = -16836
441470 feet/sec YDOT = -5067
932859 meter/sec
ZDOT = 1143
607457 ZDOT = 376
291973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3012730
66 X = -918280
31
Y = -13546305
03 feet Y = -4128913
77 meter
Z = 17428927
03 Z = 5312336
96
XDOT = 23816
989304 XDOT = 7259
418340
YDOT = -3654
877570 feet/sec YDOT = -1114
006683 meter/sec
ZDOT = 1271
826024 ZDOT = 387
652572
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 20283
90669535
00016717 00000-0 10270-3 0 9128
2 25544 51
6435 140
8443 0001310 246
4485 113
6528 15
49324346 9790
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
90669535 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 140
8443 deg
Eccentricity:
0001310
Arg of perigee: 246
4485 deg
Mean anomaly: 113
6528 deg
Mean motion: 15
49324346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 979
Checksum: 312
Coasting Arc #14 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2020/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3148043
62 A = 6791524
07 meter
Y = 2782464
39 meter E =
0013519
Z = -5347637
65 I = 51
89766
XDOT = -5279
727687 Wp = 89
81152
YDOT = 5532
093724 meter/sec RA = 135
01481 deg
ZDOT = -230
085927 TA = 178
00093
MA = 177
99552
Ha = 228
170 n
mi
Hp = 222
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10328227
10 X = 3142671
28
Y = 9128820
18 feet Y = 2817637
98 meter
Z = -17544742
96 Z = -5332358
64
XDOT = -17321
941230 XDOT = -5340
079191
YDOT = 18149
913792 feet/sec YDOT = 5472
714573 meter/sec
ZDOT = -754
875087 ZDOT = -255
879632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3964981
73 X = 1208526
43
Y = 13295134
63 feet Y = 4052357
03 meter
Z = -17474093
78 Z = -5326103
78
XDOT = -23360
641967 XDOT = -7120
323671
YDOT = 5819
794787 feet/sec YDOT = 1773
873451 meter/sec
ZDOT = -874
208951 ZDOT = -266
458888
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 20284
87423979
00016717 00000-0 10270-3 0 9136
2 25544 51
6429 136
0572 0001334 252
3364 107
7640 15
49283570 9940
Satellite: ISS
Catalog Number: 25544
Epoch time: 20284
87423979 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 136
0572 deg
Eccentricity:
0001334
Arg of perigee: 252
3364 deg
Mean anomaly: 107
7640 deg
Mean motion: 15
49283570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 994
Checksum: 320
Coasting Arc #15 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2020/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3285524
53 A = 6791365
82 meter
Y = -2599039
46 meter E =
0001250
Z = 5344423
28 I = 51
92164
XDOT = 4865
348862 Wp = 117
65491
YDOT = -5917
841897 meter/sec RA = 130
08468 deg
ZDOT = 112
527124 TA = 331
27259
MA = 331
27948
Ha = 228
207 n
mi
Hp = 222
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10779279
95 X = -3282177
42
Y = -8527032
33 feet Y = -2635761
70 meter
Z = 17534197
10 Z = 5328471
58
XDOT = 15962
430648 XDOT = 4930
615755
YDOT = -19415
491787 feet/sec YDOT = -5863
069143 meter/sec
ZDOT = 369
183477 ZDOT = 136
319907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4890901
10 X = -1490746
66
Y = -12944640
13 feet Y = -3945526
31 meter
Z = 17460429
63 Z = 5321938
95
XDOT = 22774
594749 XDOT = 6941
696480
YDOT = -7955
888371 feet/sec YDOT = -2424
954775 meter/sec
ZDOT = 479
285582 ZDOT = 146
086245
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 20285
90628219
00016717 00000-0 10270-3 0 9146
2 25544 51
6438 130
9499 0001345 258
1779 101
9221 15
49328338 10100
Satellite: ISS
Catalog Number: 25544
Epoch time: 20285
90628219 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 130
9499 deg
Eccentricity:
0001345
Arg of perigee: 258
1779 deg
Mean anomaly: 101
9221 deg
Mean motion: 15
49328338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1010
Checksum: 310
Coasting Arc #16 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2020/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3422475
04 A = 6791490
42 meter
Y = 2421359
09 meter E =
0013580
Z = -5354753
61 I = 51
94151
XDOT = -4410
359682 Wp = 90
30911
YDOT = 6251
452864 meter/sec RA = 125
15632 deg
ZDOT = 7
914071 TA = 179
76648
MA = 179
76584
Ha = 228
163 n
mi
Hp = 222
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11228592
65 X = 3421154
80
Y = 7944091
49 feet Y = 2459624
03 meter
Z = -17568089
28 Z = -5338131
79
XDOT = -14469
683997 XDOT = -4479
975969
YDOT = 20510
015959 feet/sec YDOT = 6201
743809 meter/sec
ZDOT = 25
964800 ZDOT = -13
679232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5794985
44 X = 1766311
56
Y = 12581858
41 feet Y = 3834950
44 meter
Z = -17491215
68 Z = -5331322
54
XDOT = -21919
731473 XDOT = -6681
134153
YDOT = 9993
243545 feet/sec YDOT = 3045
940633 meter/sec
ZDOT = -73
983048 ZDOT = -22
550033
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
87382140
00016717 00000-0 10270-3 0 9154
2 25544 51
6429 126
1623 0001255 267
7708 92
3298 15
49287118 10257
Satellite: ISS
Catalog Number: 25544
Epoch time: 20286
87382140 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 126
1623 deg
Eccentricity:
0001255
Arg of perigee: 267
7708 deg
Mean anomaly: 92
3298 deg
Mean motion: 15
49287118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1025
Checksum: 315
Coasting Arc #17 (Orbit 1040)
---------------------------------------
Vector Time (GMT): 2020/287/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3541601
19 A = 6791361
06 meter
Y = -2231523
92 meter E =
0001188
Z = 5346887
07 I = 51
95979
XDOT = 3943
660514 Wp = 79
88936
YDOT = -6567
872872 meter/sec RA = 120
22931 deg
ZDOT = -128
724966 TA = 11
33429
MA = 11
33161
Ha = 228
237 n
mi
Hp = 222
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11619426
47 X = -3542356
72
Y = -7321272
70 feet Y = -2271132
51 meter
Z = 17542280
41 Z = 5329681
53
XDOT = 12938
518747 XDOT = 4017
436626
YDOT = -21548
139343 feet/sec YDOT = -6523
359530 meter/sec
ZDOT = -422
326004 ZDOT = -109
388425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6655988
92 X = -2028745
42
Y = -12128296
43 feet Y = -3696704
75 meter
Z = 17462701
52 Z = 5322631
42
XDOT = 20945
271111 XDOT = 6384
118635
YDOT = -11974
983979 feet/sec YDOT = -3649
975117 meter/sec
ZDOT = -332
800003 ZDOT = -101
437441
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
90585977
00016717 00000-0 10270-3 0 9163
2 25544 51
6427 121
0554 0001251 270
6485 89
4522 15
49328809 10411
Satellite: ISS
Catalog Number: 25544
Epoch time: 20287
90585977 = yrday
fracday
Element set: 916
Inclination: 51
6427 deg
RA of node: 121
0554 deg
Eccentricity:
0001251
Arg of perigee: 270
6485 deg
Mean anomaly: 89
4522 deg
Mean motion: 15
49328809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1041
Checksum: 318
Coasting Arc #18 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2020/288/05:45:05
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4741139
85 A = 6793824
78 meter
Y = 921688
82 meter E =
0006591
Z = 4774374
89 I = 51
97330
XDOT = 1378
621342 Wp = 119
81970
YDOT = -7029
525278 meter/sec RA = 118
37055 deg
ZDOT = 2720
070404 TA = 303
36355
MA = 303
42661
Ha = 228
295 n
mi
Hp = 222
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15554920
78 X = -4774285
49
Y = 3023913
47 feet Y = 868485
02 meter
Z = 15663959
61 Z = 4751263
50
XDOT = 4523
035898 XDOT = 1443
912480
YDOT = -23062
746974 feet/sec YDOT = -7013
743277 meter/sec
ZDOT = 8924
115499 ZDOT = 2726
926370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7862735
32 X = 2396561
72
Y = 13878605
13 feet Y = 4230198
84 meter
Z = 15557022
74 Z = 4741780
53
XDOT = -22268
722220 XDOT = -6787
506533
YDOT = 2554
835138 feet/sec YDOT = 778
713750 meter/sec
ZDOT = 8955
909587 ZDOT = 2729
761242
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
29287529
00016717 00000-0 10270-3 0 9179
2 25544 51
6416 119
1416 0001180 285
2447 74
8573 15
49330741 10473
Satellite: ISS
Catalog Number: 25544
Epoch time: 20288
29287529 = yrday
fracday
Element set: 917
Inclination: 51
6416 deg
RA of node: 119
1416 deg
Eccentricity:
0001180
Arg of perigee: 285
2447 deg
Mean anomaly: 74
8573 deg
Mean motion: 15
49330741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 316
Coasting Arc #19 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2020/288/08:50:45
000
Vector Time (MET): N/A
Weight (LBS) : 951926
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4738094
44 A = 6794001
98 meter
Y = 1016626
47 meter E =
0006713
Z = 4758158
36 I = 51
97712
XDOT = 1264
643651 Wp = 118
06815
YDOT = -7036
722290 meter/sec RA = 117
73630 deg
ZDOT = 2756
742804 TA = 304
72613
MA = 304
78934
Ha = 228
396 n
mi
Hp = 222
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15544929
26 X = -4772223
16
Y = 3335388
68 feet Y = 963451
23 meter
Z = 15610755
78 Z = 4735059
36
XDOT = 4149
093344 XDOT = 1329
845597
YDOT = -23086
359219 feet/sec YDOT = -7022
215360 meter/sec
ZDOT = 9044
431773 ZDOT = 2763
044907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15603985
59 X = 4756094
81
Y = 3551176
91 feet Y = 1082398
72 meter
Z = 15503874
21 Z = 4725580
86
XDOT = -13152
684886 XDOT = -4008
938353
YDOT = 18092
147108 feet/sec YDOT = 5514
486438 meter/sec
ZDOT = 9073
665109 ZDOT = 2765
653125
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
42188082
00016717 00000-0 10270-3 0 9189
2 25544 51
6431 118
5038 0001122 292
2397 67
8634 15
49292311 10493
Satellite: ISS
Catalog Number: 25544
Epoch time: 20288
42188082 = yrday
fracday
Element set: 918
Inclination: 51
6431 deg
RA of node: 118
5038 deg
Eccentricity:
0001122
Arg of perigee: 292
2397 deg
Mean anomaly: 67
8634 deg
Mean motion: 15
49292311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 306
Coasting Arc #20 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2020/289/02:17:30
000
Vector Time (MET): N/A
Weight (LBS) : 951926
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1297940
68 A = 6801904
81 meter
Y = -6412513
76 meter E =
0012768
Z = 1838166
35 I = 52
01123
XDOT = 5118
689139 Wp = 113
89922
YDOT = -596
703654 meter/sec RA = 114
11735 deg
ZDOT = -5669
954421 TA = 46
02912
MA = 45
92389
Ha = 228
204 n
mi
Hp = 222
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4258335
56 X = 1360621
99
Y = -21038430
97 feet Y = -6397648
63 meter
Z = 6030729
48 Z = 1844624
10
XDOT = 16793
599536 XDOT = 5152
523002
YDOT = -1957
689153 feet/sec YDOT = -539
274095 meter/sec
ZDOT = -18602
212667 ZDOT = -5645
007267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15490667
44 X = -4721555
44
Y = -14846750
69 feet Y = -4525289
61 meter
Z = 6060685
89 Z = 1847297
06
XDOT = 6343
459862 XDOT = 1933
486566
YDOT = -14199
845834 feet/sec YDOT = -4328
113010 meter/sec
ZDOT = -18486
779874 ZDOT = -5634
770506
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
13140520
00016717 00000-0 10270-3 0 9194
2 25544 51
6396 114
9906 0001144 294
7303 65
3728 15
49320784 10601
Satellite: ISS
Catalog Number: 25544
Epoch time: 20289
13140520 = yrday
fracday
Element set: 919
Inclination: 51
6396 deg
RA of node: 114
9906 deg
Eccentricity:
0001144
Arg of perigee: 294
7303 deg
Mean anomaly: 65
3728 deg
Mean motion: 15
49320784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 299
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