[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 28th 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
358/10:50:00
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
2
361/14:12:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 222
2
364/19:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 222
3
Coasting Arc #1 (Orbit 2104)
---------------------------------------
Vector Time (GMT): 2020/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1867278
69 A = 6797768
60 meter
Y = -5349426
46 meter E =
0012342
Z = 3744904
29 I = 51
88864
XDOT = 6292
274371 Wp = 91
63823
YDOT = -820
936859 meter/sec RA = 140
47121 deg
ZDOT = -4298
237588 TA = 43
87109
MA = 43
77315
Ha = 229
138 n
mi
Hp = 222
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6126242
42 X = 1908768
36
Y = -17550611
74 feet Y = -5328313
54 meter
Z = 12286431
41 Z = 3754075
05
XDOT = 20643
944786 XDOT = 6321
864899
YDOT = -2693
362397 feet/sec YDOT = -750
406309 meter/sec
ZDOT = -14101
829358 ZDOT = -4267
600617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17508494
03 X = 5336588
98
Y = 6161085
11 feet Y = 1877898
74 meter
Z = 12329026
01 Z = 3757887
13
XDOT = 3002
082197 XDOT = 915
034654
YDOT = 19481
353257 feet/sec YDOT = 5937
916473 meter/sec
ZDOT = -13959
691943 ZDOT = -4254
914104
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
54033144
00016717 00000-0 10270-3 0 9007
2 25544 51
6410 141
4470 0001737 151
5652 208
5593 15
49189278 21057
Satellite: ISS
Catalog Number: 25544
Epoch time: 20356
54033144 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 141
4470 deg
Eccentricity:
0001737
Arg of perigee: 151
5652 deg
Mean anomaly: 208
5593 deg
Mean motion: 15
49189278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2105
Checksum: 288
Coasting Arc #2 (Orbit 2119)
---------------------------------------
Vector Time (GMT): 2020/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1469598
40 A = 6797859
19 meter
Y = 5511223
45 meter E =
0006875
Z = -3706154
61 I = 51
91541
XDOT = -6166
494994 Wp = 112
05421
YDOT = 1277
017857 meter/sec RA = 135
54153 deg
ZDOT = 4348
131271 TA = 204
13913
MA = 204
17137
Ha = 229
100 n
mi
Hp = 222
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4821517
07 X = -1513115
06
Y = 18081441
76 feet Y = 5494546
33 meter
Z = -12159299
89 Z = -3713398
55
XDOT = -20231
282790 XDOT = -6201
437328
YDOT = 4189
691132 feet/sec YDOT = 1207
863943 meter/sec
ZDOT = 14265
522542 ZDOT = 4318
092222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18129136
76 X = -5525760
88
Y = -4549731
80 feet Y = -1386758
25 meter
Z = -12192968
36 Z = -3716416
76
XDOT = -4733
246299 XDOT = -1442
693472
YDOT = -18962
052483 feet/sec YDOT = -5779
633597 meter/sec
ZDOT = 14126
138356 ZDOT = 4305
646971
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
50792658
00016717 00000-0 10270-3 0 9017
2 25544 51
6419 136
6599 0001649 151
5617 208
5623 15
49207093 21204
Satellite: ISS
Catalog Number: 25544
Epoch time: 20357
50792658 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 136
6599 deg
Eccentricity:
0001649
Arg of perigee: 151
5617 deg
Mean anomaly: 208
5623 deg
Mean motion: 15
49207093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2120
Checksum: 315
Coasting Arc #3 (Orbit 2134)
---------------------------------------
Vector Time (GMT): 2020/358/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5375513
23 A = 6797527
42 meter
Y = -1609605
55 meter E =
0006630
Z = -3842285
47 I = 51
93507
XDOT = -1109
568268 Wp = 90
27629
YDOT = 6302
533486 meter/sec RA = 130
90345 deg
ZDOT = -4198
870014 TA = 135
58088
MA = 135
52768
Ha = 229
107 n
mi
Hp = 222
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17636198
25 X = 5411776
40
Y = -5280858
11 feet Y = -1549289
60 meter
Z = -12605923
46 Z = -3816085
43
XDOT = -3640
315841 XDOT = -1159
566971
YDOT = 20677
603301 feet/sec YDOT = 6289
846300 meter/sec
ZDOT = -13775
820256 ZDOT = -4204
380745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 202696
01 X = 61781
75
Y = 18491419
48 feet Y = 5636184
66 meter
Z = -12484333
27 Z = -3805224
78
XDOT = -17555
513159 XDOT = -5350
920411
YDOT = -9111
447048 feet/sec YDOT = -2777
169060 meter/sec
ZDOT = -13801
468855 ZDOT = -4206
687707
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 20358
47551994
00016717 00000-0 10270-3 0 9021
2 25544 51
6405 131
8726 0001591 151
7994 208
3243 15
49223706 21355
Satellite: ISS
Catalog Number: 25544
Epoch time: 20358
47551994 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 131
8726 deg
Eccentricity:
0001591
Arg of perigee: 151
7994 deg
Mean anomaly: 208
3243 deg
Mean motion: 15
49223706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2135
Checksum: 310
Coasting Arc #4 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2020/359/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5204150
09 A = 6797339
94 meter
Y = 1998523
51 meter E =
0012136
Z = 3881767
22 I = 51
95637
XDOT = 642
528302 Wp = 105
16085
YDOT = -6410
613853 meter/sec RA = 125
97563 deg
ZDOT = 4148
024561 TA = 301
35716
MA = 301
47586
Ha = 229
067 n
mi
Hp = 222
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17073983
24 X = -5244966
82
Y = 6556835
68 feet Y = 1940098
37 meter
Z = 12735456
75 Z = 3856388
52
XDOT = 2108
032488 XDOT = 694
017232
YDOT = -21032
197679 feet/sec YDOT = -6403
141148 meter/sec
ZDOT = 13609
004466 ZDOT = 4151
270151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1898457
24 X = -578649
77
Y = -18272806
20 feet Y = -5569551
33 meter
Z = 12617657
06 Z = 3845861
87
XDOT = 18463
471796 XDOT = 5627
666203
YDOT = 7521
184513 feet/sec YDOT = 2292
457040 meter/sec
ZDOT = 13624
159400 ZDOT = 4152
643785
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 20359
50761649
00016717 00000-0 10270-3 0 9037
2 25544 51
6410 126
7651 0001633 162
3549 197
7658 15
49240593 21514
Satellite: ISS
Catalog Number: 25544
Epoch time: 20359
50761649 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 126
7651 deg
Eccentricity:
0001633
Arg of perigee: 162
3549 deg
Mean anomaly: 197
7658 deg
Mean motion: 15
49240593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 315
Coasting Arc #5 (Orbit 2165)
---------------------------------------
Vector Time (GMT): 2020/360/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5015682
34 A = 6797152
87 meter
Y = -2339207
24 meter E =
0006751
Z = -3952241
62 I = 51
97565
XDOT = -183
107022 Wp = 87
38570
YDOT = 6478
041521 meter/sec RA = 121
04946 deg
ZDOT = -4072
224228 TA = 140
15360
MA = 140
10401
Ha = 229
009 n
mi
Hp = 222
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16455650
71 X = 5060665
06
Y = -7674564
45 feet Y = -2282866
32 meter
Z = -12966671
98 Z = -3927768
35
XDOT = -600
744823 XDOT = -235
752260
YDOT = 21253
417063 feet/sec YDOT = 6475
699984 meter/sec
ZDOT = -13360
315708 ZDOT = -4073
240832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3446206
48 X = 1050403
74
Y = 17909346
06 feet Y = 5458768
68 meter
Z = -12853052
04 Z = -3917610
26
XDOT = -19192
811562 XDOT = -5849
968964
YDOT = -5885
085931 feet/sec YDOT = -1793
774192 meter/sec
ZDOT = -13365
144485 ZDOT = -4073
696039
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 20360
47520484
00016717 00000-0 10270-3 0 9046
2 25544 51
6420 121
9773 0001529 161
5133 198
6073 15
49227066 21668
Satellite: ISS
Catalog Number: 25544
Epoch time: 20360
47520484 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 121
9773 deg
Eccentricity:
0001529
Arg of perigee: 161
5133 deg
Mean anomaly: 198
6073 deg
Mean motion: 15
49227066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2166
Checksum: 298
Coasting Arc #6 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2020/361/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4793448
41 A = 6796930
36 meter
Y = 2687787
89 meter E =
0011730
Z = 3992610
74 I = 51
99220
XDOT = -298
966522 Wp = 107
19770
YDOT = -6518
799237 meter/sec RA = 116
12458 deg
ZDOT = 4016
366927 TA = 301
04479
MA = 301
15991
Ha = 229
001 n
mi
Hp = 222
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15726536
79 X = -4842541
68
Y = 8818201
74 feet Y = 2633909
09 meter
Z = 13099116
61 Z = 3969207
10
XDOT = -980
861292 XDOT = -245
558366
YDOT = -21387
136605 feet/sec YDOT = -6521
844393 meter/sec
ZDOT = 13177
056847 ZDOT = 4015
043533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5031978
33 X = -1533746
99
Y = -17395379
97 feet Y = -5302111
82 meter
Z = 12990436
74 Z = 3959485
12
XDOT = 19810
218125 XDOT = 6038
154485
YDOT = 4137
635722 feet/sec YDOT = 1261
151368 meter/sec
ZDOT = 13171
043242 ZDOT = 4014
533980
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 20361
50729431
00016717 00000-0 10270-3 0 9055
2 25544 51
6426 116
8702 0001538 165
5070 194
6125 15
49252523 21821
Satellite: ISS
Catalog Number: 25544
Epoch time: 20361
50729431 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 116
8702 deg
Eccentricity:
0001538
Arg of perigee: 165
5070 deg
Mean anomaly: 194
6125 deg
Mean motion: 15
49252523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 290
Coasting Arc #7 (Orbit 2183)
---------------------------------------
Vector Time (GMT): 2020/361/14:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2326552
03 A = 6793375
25 meter
Y = -4063405
39 meter E =
0006432
Z = 4917577
15 I = 51
98454
XDOT = 4698
204145 Wp = 69
97088
YDOT = -5569
397856 meter/sec RA = 115
39092 deg
ZDOT = -2374
583563 TA = 43
21394
MA = 43
16349
Ha = 228
913 n
mi
Hp = 222
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7633044
71 X = -2304827
71
Y = -13331382
51 feet Y = -4089301
75 meter
Z = 16133783
31 Z = 4906327
87
XDOT = 15414
055595 XDOT = 4771
668056
YDOT = -18272
302677 feet/sec YDOT = -5516
448084 meter/sec
ZDOT = -7790
628489 ZDOT = -2351
583780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5798657
75 X = 1767430
88
Y = -14284402
15 feet Y = -4353885
77 meter
Z = 16081651
61 Z = 4901687
41
XDOT = 22875
712967 XDOT = 6972
517312
YDOT = 618
455863 feet/sec YDOT = 188
505347 meter/sec
ZDOT = -7683
762353 ZDOT = -2342
010765
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 20361
63630436
00016717 00000-0 10270-3 0 9066
2 25544 51
6445 116
2341 0001290 168
6874 191
4305 15
49260352 21842
Satellite: ISS
Catalog Number: 25544
Epoch time: 20361
63630436 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 116
2341 deg
Eccentricity:
0001290
Arg of perigee: 168
6874 deg
Mean anomaly: 191
4305 deg
Mean motion: 15
49260352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2184
Checksum: 292
Coasting Arc #8 (Orbit 2198)
---------------------------------------
Vector Time (GMT): 2020/362/14:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2616172
65 A = 6793537
83 meter
Y = 3930878
47 meter E =
0012502
Z = -4896063
75 I = 51
99750
XDOT = -4239
438654 Wp = 112
90634
YDOT = 5876
741299 meter/sec RA = 110
46788 deg
ZDOT = 2453
176559 TA = 181
10520
MA = 181
10797
Ha = 228
841 n
mi
Hp = 222
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8583243
60 X = 2595804
22
Y = 12896582
92 feet Y = 3960021
24 meter
Z = -16063201
27 Z = -4883404
28
XDOT = -13908
919468 XDOT = -4316
755207
YDOT = 19280
647307 feet/sec YDOT = 5828
900179 meter/sec
ZDOT = 8048
479525 ZDOT = 2432
396107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4618645
13 X = -1407763
04
Y = 14850710
99 feet Y = 4526496
71 meter
Z = -16004526
15 Z = -4878179
57
XDOT = -22694
558951 XDOT = -6917
301568
YDOT = 1510
666201 feet/sec YDOT = 460
451058 meter/sec
ZDOT = 7951
882114 ZDOT = 2423
733668
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 20362
60388747
00016717 00000-0 10270-3 0 9070
2 25544 51
6436 111
4476 0001336 167
6566 192
4617 15
49252219 21992
Satellite: ISS
Catalog Number: 25544
Epoch time: 20362
60388747 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 111
4476 deg
Eccentricity:
0001336
Arg of perigee: 167
6566 deg
Mean anomaly: 192
4617 deg
Mean motion: 15
49252219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2199
Checksum: 326
Coasting Arc #9 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2020/363/14:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2882720
36 A = 6793623
28 meter
Y = -3776272
71 meter E =
0006675
Z = 4851739
72 I = 52
00973
XDOT = 3778
160570 Wp = 70
02584
YDOT = -6162
024331 meter/sec RA = 105
54448 deg
ZDOT = -2546
216937 TA = 44
93567
MA = 44
88166
Ha = 228
815 n
mi
Hp = 222
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9457743
98 X = -2863845
59
Y = -12389346
17 feet Y = -3808404
61 meter
Z = 15917781
23 Z = 4837781
86
XDOT = 12395
539928 XDOT = 3859
153423
YDOT = -20216
615259 feet/sec YDOT = -6119
320953 meter/sec
ZDOT = -8353
730109 ZDOT = -2527
668446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3414138
25 X = 1040629
34
Y = -15275605
98 feet Y = -4656004
70 meter
Z = 15853078
60 Z = 4832018
36
XDOT = 22393
907523 XDOT = 6825
663013
YDOT = -3592
183079 feet/sec YDOT = -1094
897403 meter/sec
ZDOT = -8267
461451 ZDOT = -2519
922250
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 20363
63597117
00016717 00000-0 10270-3 0 9088
2 25544 51
6446 106
3406 0001254 180
0384 180
0766 15
49273677 22153
Satellite: ISS
Catalog Number: 25544
Epoch time: 20363
63597117 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 106
3406 deg
Eccentricity:
0001254
Arg of perigee: 180
0384 deg
Mean anomaly: 180
0766 deg
Mean motion: 15
49273677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 305
Coasting Arc #10 (Orbit 2229)
---------------------------------------
Vector Time (GMT): 2020/364/14:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3157507
74 A = 6793825
36 meter
Y = 3606160
27 meter E =
0011856
Z = -4826099
71 I = 52
01788
XDOT = -3285
079961 Wp = 113
51307
YDOT = 6390
755062 meter/sec RA = 100
62231 deg
ZDOT = 2626
532145 TA = 182
30509
MA = 182
31056
Ha = 228
770 n
mi
Hp = 222
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10359277
36 X = 3140390
14
Y = 11831234
47 feet Y = 3641374
88 meter
Z = -15833660
47 Z = -4810802
86
XDOT = -10777
821394 XDOT = -3369
057266
YDOT = 20967
044166 feet/sec YDOT = 6353
548952 meter/sec
ZDOT = 8617
231446 ZDOT = 2610
371732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2140189
46 X = -652329
75
Y = 15650980
78 feet Y = 4770418
94 meter
Z = -15762738
66 Z = -4804482
74
XDOT = -21820
462581 XDOT = -6650
876995
YDOT = 5617
473093 feet/sec YDOT = 1712
205799 meter/sec
ZDOT = 8542
020061 ZDOT = 2603
607715
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 20364
60354794
00016717 00000-0 10270-3 0 9099
2 25544 51
6443 101
5536 0001157 173
2193 186
8973 15
49256001 22308
Satellite: ISS
Catalog Number: 25544
Epoch time: 20364
60354794 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 101
5536 deg
Eccentricity:
0001157
Arg of perigee: 173
2193 deg
Mean anomaly: 186
8973 deg
Mean motion: 15
49256001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2230
Checksum: 301
Coasting Arc #11 (Orbit 2233)
---------------------------------------
Vector Time (GMT): 2020/364/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2723391
73 A = 6795525
35 meter
Y = -4422273
85 meter E =
0009525
Z = 4375718
42 I = 52
02250
XDOT = 3711
071060 Wp = 77
16872
YDOT = -5733
555744 meter/sec RA = 99
49988 deg
ZDOT = -3476
419925 TA = 48
00527
MA = 47
92419
Ha = 228
873 n
mi
Hp = 222
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8935012
23 X = -2694992
66
Y = -14508772
49 feet Y = -4452570
72 meter
Z = 14356031
56 Z = 4362557
60
XDOT = 12175
429986 XDOT = 3791
795921
YDOT = -18810
878426 feet/sec YDOT = -5691
603939 meter/sec
ZDOT = -11405
577181 ZDOT = -3458
198038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15453537
12 X = -4710238
11
Y = -7298922
63 feet Y = -2224711
62 meter
Z = 14295051
03 Z = 4357131
55
XDOT = -426
543710 XDOT = -130
010523
YDOT = -21323
178631 feet/sec YDOT = -6499
304847 meter/sec
ZDOT = -11320
807895 ZDOT = -3450
582247
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 20364
86156772
00016717 00000-0 10270-3 0 9105
2 25544 51
6419 100
2778 0000934 167
9562 192
1611 15
49253977 22349
Satellite: ISS
Catalog Number: 25544
Epoch time: 20364
86156772 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 100
2778 deg
Eccentricity:
0000934
Arg of perigee: 167
9562 deg
Mean anomaly: 192
1611 deg
Mean motion: 15
49253977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2234
Checksum: 318
Coasting Arc #12 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2020/365/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3055348
91 A = 6795777
30 meter
Y = 4256348
30 meter E =
0008982
Z = -4337323
05 I = 52
02736
XDOT = -3253
806479 Wp = 114
88728
YDOT = 5948
214643 meter/sec RA = 94
57839 deg
ZDOT = 3547
161449 TA = 191
12210
MA = 191
14197
Ha = 228
831 n
mi
Hp = 222
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10024110
59 X = 3028594
00
Y = 13964397
30 feet Y = 4290366
51 meter
Z = -14230062
51 Z = -4322545
85
XDOT = -10675
218108 XDOT = -3337
309245
YDOT = 19515
139906 feet/sec YDOT = 5911
360771 meter/sec
ZDOT = 11637
668797 ZDOT = 3531
154093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16178347
72 X = 4931160
38
Y = 5974339
44 feet Y = 1820978
66 meter
Z = -14161574
68 Z = -4316447
96
XDOT = 2353
237919 XDOT = 717
266918
YDOT = 21020
540120 feet/sec YDOT = 6407
060629 meter/sec
ZDOT = 11563
156015 ZDOT = 3524
449953
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 20365
82914017
00016717 00000-0 10270-3 0 9117
2 25544 51
6417 95
4907 0000867 165
1519 194
9657 15
49226890 22493
Satellite: ISS
Catalog Number: 25544
Epoch time: 20365
82914017 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 95
4907 deg
Eccentricity:
0000867
Arg of perigee: 165
1519 deg
Mean anomaly: 194
9657 deg
Mean motion: 15
49226890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 334
Coasting Arc #13 (Orbit 2264)
---------------------------------------
Vector Time (GMT): 2020/366/19:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3358821
46 A = 6795900
34 meter
Y = -4073069
75 meter E =
0009852
Z = 4272283
17 I = 52
02929
XDOT = 2802
208735 Wp = 78
52035
YDOT = -6135
638900 meter/sec RA = 89
65671 deg
ZDOT = -3637
484355 TA = 48
54217
MA = 48
45760
Ha = 228
814 n
mi
Hp = 222
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11019755
46 X = -3333777
47
Y = -13363089
73 feet Y = -4110491
12 meter
Z = 14016677
07 Z = 4256027
83
XDOT = 9193
598211 XDOT = 2888
279558
YDOT = -20130
048884 feet/sec YDOT = -6103
820789 meter/sec
ZDOT = -11934
003790 ZDOT = -3623
664430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16752261
86 X = -5106089
42
Y = -4634188
48 feet Y = -1412500
65 meter
Z = 13941321
07 Z = 4249314
66
XDOT = -4203
086508 XDOT = -1281
100768
YDOT = -20603
485394 feet/sec YDOT = -6279
942348 meter/sec
ZDOT = -11869
626371 ZDOT = -3617
862118
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 20366
86121404
00016717 00000-0 10270-3 0 9123
2 25544 51
6415 90
3839 0000825 177
1722 182
9433 15
49259911 22659
Satellite: ISS
Catalog Number: 25544
Epoch time: 20366
86121404 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 90
3839 deg
Eccentricity:
0000825
Arg of perigee: 177
1722 deg
Mean anomaly: 182
9433 deg
Mean motion: 15
49259911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2265
Checksum: 306
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