[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 3rd 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) : 16490 3108 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
338/19:32:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
9
340/16:39:38
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 221
9
341/16:30:00
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
7
341/22:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
9
351/15:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2020/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5022036
79 A = 6795172
29 meter
Y = -820103
51 meter E =
0011484
Z = -4514849
19 I = 51
31374
XDOT = -1720
743685 Wp = 107
68510
YDOT = -6758
501617 meter/sec RA = 234
54825 deg
ZDOT = 3144
925064 TA = 194
07708
MA = 194
10912
Ha = 229
505 n
mi
Hp = 221
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16476498
65 X = -4990562
07
Y = -2690628
31 feet Y = -876086
86 meter
Z = -14812497
35 Z = -4539168
26
XDOT = -5645
484532 XDOT = -1660
316617
YDOT = -22173
561737 feet/sec YDOT = -6777
406816 meter/sec
ZDOT = 10317
995616 ZDOT = 3136
712003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7905471
52 X = 2409587
72
Y = -14590174
62 feet Y = -4447085
22 meter
Z = -14924975
40 Z = -4549132
50
XDOT = 21758
344680 XDOT = 6631
943458
YDOT = 1284
144725 feet/sec YDOT = 391
407312 meter/sec
ZDOT = 10280
132848 ZDOT = 3133
384492
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 20337
51050243
00016717 00000-0 10270-3 0 9002
2 25544 51
6449 235
6068 0001803 91
5709 268
5648 15
49138654 18109
Satellite: ISS
Catalog Number: 25544
Epoch time: 20337
51050243 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 235
6068 deg
Eccentricity:
0001803
Arg of perigee: 91
5709 deg
Mean anomaly: 268
5648 deg
Mean motion: 15
49138654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 305
Coasting Arc #2 (Orbit 1825)
---------------------------------------
Vector Time (GMT): 2020/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5089736
47 A = 6795226
46 meter
Y = 457412
10 meter E =
0010600
Z = 4471849
20 I = 51
33380
XDOT = 2237
260135 Wp = 72
54369
YDOT = 6589
636381 meter/sec RA = 229
57998 deg
ZDOT = -3210
984887 TA = 49
95397
MA = 49
86103
Ha = 229
340 n
mi
Hp = 221
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16698610
48 X = 5062521
42
Y = 1500695
88 feet Y = 514176
34 meter
Z = 14671421
27 Z = 4496507
32
XDOT = 7340
092306 XDOT = 2179
003794
YDOT = 21619
541931 feet/sec YDOT = 6614
329784 meter/sec
ZDOT = -10534
727319 ZDOT = -3200
257561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6591891
58 X = -2009208
55
Y = 15306288
84 feet Y = 4665356
84 meter
Z = 14785491
86 Z = 4506617
92
XDOT = -21736
029754 XDOT = -6625
141869
YDOT = 797
170729 feet/sec YDOT = 242
977638 meter/sec
ZDOT = -10485
210851 ZDOT = -3195
892267
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 20338
54265317
00016717 00000-0 10270-3 0 9017
2 25544 51
6438 230
5011 0001810 93
1029 267
0328 15
49164513 18269
Satellite: ISS
Catalog Number: 25544
Epoch time: 20338
54265317 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 230
5011 deg
Eccentricity:
0001810
Arg of perigee: 93
1029 deg
Mean anomaly: 267
0328 deg
Mean motion: 15
49164513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1826
Checksum: 280
Coasting Arc #3 (Orbit 1830)
---------------------------------------
Vector Time (GMT): 2020/338/19:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1964621
74 A = 6792579
56 meter
Y = -3972309
49 meter E =
0006495
Z = 5143758
34 I = 51
32933
XDOT = 5831
141884 Wp = 121
66897
YDOT = 4759
140532 meter/sec RA = 228
04847 deg
ZDOT = 1443
425443 TA = 314
34522
MA = 314
39843
Ha = 229
399 n
mi
Hp = 221
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6445609
39 X = 1983909
70
Y = -13032511
46 feet Y = -3950232
61 meter
Z = 16875847
58 Z = 5153348
02
XDOT = 19131
042925 XDOT = 5770
478970
YDOT = 15613
978123 feet/sec YDOT = 4824
009141 meter/sec
ZDOT = 4735
647779 ZDOT = 1471
604409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5098062
25 X = 1553889
37
Y = -13560985
67 feet Y = -4133388
43 meter
Z = 16920280
60 Z = 5157301
53
XDOT = 19470
782909 XDOT = 5934
694631
YDOT = 13410
266478 feet/sec YDOT = 4087
449222 meter/sec
ZDOT = 4865
942911 ZDOT = 1483
139399
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 20338
86519968
00016717 00000-0 10270-3 0 9027
2 25544 51
6414 228
8997 0001866 112
3890 247
7458 15
49160577 18318
Satellite: ISS
Catalog Number: 25544
Epoch time: 20338
86519968 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 228
8997 deg
Eccentricity:
0001866
Arg of perigee: 112
3890 deg
Mean anomaly: 247
7458 deg
Mean motion: 15
49160577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1831
Checksum: 349
Coasting Arc #4 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2020/339/19:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1683130
79 A = 6792541
91 meter
Y = 4087362
13 meter E =
0015396
Z = -5171098
72 I = 51
35309
XDOT = -6186
870885 Wp = 83
77729
YDOT = -4282
532919 meter/sec RA = 223
08189 deg
ZDOT = -1373
171473 TA = 172
94424
MA = 172
92254
Ha = 229
487 n
mi
Hp = 221
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5522082
64 X = -1703593
52
Y = 13409980
73 feet Y = 4068426
46 meter
Z = -16965546
99 Z = -5179323
87
XDOT = -20298
132824 XDOT = -6131
852386
YDOT = -14050
304852 feet/sec YDOT = -4351
411131 meter/sec
ZDOT = -4505
155752 ZDOT = -1403
091919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3904123
64 X = -1189976
89
Y = 13920630
33 feet Y = 4243008
12 meter
Z = -17003665
32 Z = -5182717
19
XDOT = -20668
905468 XDOT = -6299
882387
YDOT = -11461
059953 feet/sec YDOT = -3493
331074 meter/sec
ZDOT = -4643
545722 ZDOT = -1415
352736
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 20339
83283773
00016717 00000-0 10270-3 0 9038
2 25544 51
6418 224
1133 0001925 115
0430 245
0920 15
49154811 18464
Satellite: ISS
Catalog Number: 25544
Epoch time: 20339
83283773 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 224
1133 deg
Eccentricity:
0001925
Arg of perigee: 115
0430 deg
Mean anomaly: 245
0920 deg
Mean motion: 15
49154811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 286
Coasting Arc #5 (Orbit 1859)
---------------------------------------
Vector Time (GMT): 2020/340/16:39:38
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5327955
77 A = 6796277
80 meter
Y = -42825
92 meter E =
0011430
Z = 4210611
32 I = 51
38591
XDOT = 2933
981330 Wp = 79
85597
YDOT = 6072
883076 meter/sec RA = 218
67635 deg
ZDOT = -3640
356960 TA = 47
62903
MA = 47
53232
Ha = 229
339 n
mi
Hp = 221
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17480169
84 X = 5307585
93
Y = -140505
00 feet Y = 16640
68 meter
Z = 13814341
59 Z = 4236442
97
XDOT = 9625
922998 XDOT = 2883
537227
YDOT = 19924
157074 feet/sec YDOT = 6105
411365 meter/sec
ZDOT = -11943
428346 ZDOT = -3626
226581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14136379
41 X = 4308768
44
Y = 10120358
28 feet Y = 3084685
20 meter
Z = 13933888
14 Z = 4247049
11
XDOT = -3142
053145 XDOT = -957
697799
YDOT = 20789
601754 feet/sec YDOT = 6336
670615 meter/sec
ZDOT = -11878
108599 ZDOT = -3620
447501
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 20340
73596215
00016717 00000-0 10270-3 0 9048
2 25544 51
6397 219
6448 0001759 113
2272 246
9063 15
49133406 18608
Satellite: ISS
Catalog Number: 25544
Epoch time: 20340
73596215 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 219
6448 deg
Eccentricity:
0001759
Arg of perigee: 113
2272 deg
Mean anomaly: 246
9063 deg
Mean motion: 15
49133406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1860
Checksum: 310
Coasting Arc #6 (Orbit 1874)
---------------------------------------
Vector Time (GMT): 2020/341/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2433139
16 A = 6791863
95 meter
Y = 3478549
03 meter E =
0016705
Z = -5316299
39 I = 51
39886
XDOT = -6322
570378 Wp = 93
31186
YDOT = -4302
495089 meter/sec RA = 213
77015 deg
ZDOT = 77
753591 TA = 177
43780
MA = 177
42923
Ha = 229
519 n
mi
Hp = 221
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7982740
03 X = -2446032
98
Y = 11412562
44 feet Y = 3451268
39 meter
Z = -17441927
13 Z = -5328149
58
XDOT = -20743
341135 XDOT = -6274
366350
YDOT = -14115
797535 feet/sec YDOT = -4372
929093 meter/sec
ZDOT = 255
097082 ZDOT = 47
157648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13184311
86 X = -4018578
25
Y = 4269317
96 feet Y = 1301288
11 meter
Z = -17496810
77 Z = -5333027
92
XDOT = -7557
757573 XDOT = -2303
604508
YDOT = -22864
446579 feet/sec YDOT = -6969
083317 meter/sec
ZDOT = 113
526187 ZDOT = 34
602782
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 20341
70359301
00016717 00000-0 10270-3 0 9050
2 25544 51
6402 214
8575 0002009 112
7345 247
4018 15
49160744 18754
Satellite: ISS
Catalog Number: 25544
Epoch time: 20341
70359301 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 214
8575 deg
Eccentricity:
0002009
Arg of perigee: 112
7345 deg
Mean anomaly: 247
4018 deg
Mean motion: 15
49160744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1875
Checksum: 288
Coasting Arc #7 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2020/341/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1739027
35 A = 6792046
55 meter
Y = 3901853
42 meter E =
0016084
Z = -5294461
62 I = 51
40907
XDOT = -6660
339120 Wp = 88
94757
YDOT = -3719
012249 meter/sec RA = 212
50255 deg
ZDOT = -554
306912 TA = 175
73907
MA = 175
72536
Ha = 229
417 n
mi
Hp = 221
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5705470
30 X = -1756812
34
Y = 12801356
36 feet Y = 3882307
45 meter
Z = -17370280
92 Z = -5302951
94
XDOT = -21851
506299 XDOT = -6615
564482
YDOT = -12201
483758 feet/sec YDOT = -3793
242538 meter/sec
ZDOT = -1818
592230 ZDOT = -586
551858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7336261
89 X = 2236092
63
Y = 11884371
25 feet Y = 3622356
36 meter
Z = -17409616
79 Z = -5306451
20
XDOT = -21603
987248 XDOT = -6584
895313
YDOT = 10459
177933 feet/sec YDOT = 3187
957434 meter/sec
ZDOT = -1967
808464 ZDOT = -599
788020
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 20341
96162621
00016717 00000-0 10270-3 0 9066
2 25544 51
6428 213
5830 0001671 117
6196 242
5124 15
49138373 18795
Satellite: ISS
Catalog Number: 25544
Epoch time: 20341
96162621 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 213
5830 deg
Eccentricity:
0001671
Arg of perigee: 117
6196 deg
Mean anomaly: 242
5124 deg
Mean motion: 15
49138373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 305
Coasting Arc #8 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2020/342/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1459969
83 A = 6791873
45 meter
Y = -3995800
31 meter E =
0004490
Z = 5291134
16 I = 51
43836
XDOT = 6952
261424 Wp = 116
30867
YDOT = 3187
815017 meter/sec RA = 207
54132 deg
ZDOT = 486
806632 TA = 329
01854
MA = 329
04502
Ha = 229
286 n
mi
Hp = 221
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4789927
25 X = 1478842
22
Y = -13109581
06 feet Y = -3979368
79 meter
Z = 17359364
05 Z = 5298271
64
XDOT = 22809
256641 XDOT = 6913
732971
YDOT = 10458
710687 feet/sec YDOT = 3265
344732 meter/sec
ZDOT = 1597
134618 ZDOT = 520
484751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8304488
38 X = -2531208
06
Y = -11166498
93 feet Y = -3403548
87 meter
Z = 17392435
52 Z = 5301214
35
XDOT = 20547
768520 XDOT = 6262
959845
YDOT = -12539
301987 feet/sec YDOT = -3821
979246 meter/sec
ZDOT = 1753
015465 ZDOT = 534
319114
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
99376124
00016717 00000-0 10270-3 0 9076
2 25544 51
6430 208
4768 0001698 122
1088 238
0227 15
49184354 18953
Satellite: ISS
Catalog Number: 25544
Epoch time: 20342
99376124 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 208
4768 deg
Eccentricity:
0001698
Arg of perigee: 122
1088 deg
Mean anomaly: 238
0227 deg
Mean motion: 15
49184354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 323
Coasting Arc #9 (Orbit 1909)
---------------------------------------
Vector Time (GMT): 2020/343/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1191960
67 A = 6791985
36 meter
Y = 4083148
57 meter E =
0016081
Z = -5309068
96 I = 51
46832
XDOT = -7171
263031 Wp = 90
56761
YDOT = -2627
255921 meter/sec RA = 202
58159 deg
ZDOT = -411
785552 TA = 175
49316
MA = 175
47867
Ha = 229
385 n
mi
Hp = 221
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3910632
13 X = -1211742
53
Y = 13396156
73 feet Y = 4069708
99 meter
Z = -17418205
23 Z = -5314906
82
XDOT = -23527
765851 XDOT = -7139
351046
YDOT = -8619
606039 feet/sec YDOT = -2707
271675 meter/sec
ZDOT = -1351
002468 ZDOT = -446
543618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9212395
86 X = 2807938
26
Y = 10437368
17 feet Y = 3181309
82 meter
Z = -17445258
39 Z = -5317314
76
XDOT = -19214
913474 XDOT = -5856
705627
YDOT = 14439
521857 feet/sec YDOT = 4401
166262 meter/sec
ZDOT = -1511
910267 ZDOT = -460
830249
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
96138698
00016717 00000-0 10270-3 0 9087
2 25544 51
6424 203
6895 0001680 124
3996 235
7313 15
49142663 19102
Satellite: ISS
Catalog Number: 25544
Epoch time: 20343
96138698 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 203
6895 deg
Eccentricity:
0001680
Arg of perigee: 124
3996 deg
Mean anomaly: 235
7313 deg
Mean motion: 15
49142663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1910
Checksum: 323
Coasting Arc #10 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2020/344/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 909435
46 A = 6791808
91 meter
Y = -4138389
77 meter E =
0004245
Z = 5304776
67 I = 51
50074
XDOT = 7374
148078 Wp = 114
43342
YDOT = 2058
856643 meter/sec RA = 197
62416 deg
ZDOT = 340
029245 TA = 332
30528
MA = 332
32788
Ha = 229
272 n
mi
Hp = 221
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2983712
13 X = 929876
78
Y = -13577394
26 feet Y = -4128105
91 meter
Z = 17404122
92 Z = 5309243
73
XDOT = 24193
399206 XDOT = 7348
925572
YDOT = 6754
779014 feet/sec YDOT = 2141
178612 meter/sec
ZDOT = 1115
581513 ZDOT = 375
789211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10032737
14 X = -3057978
28
Y = -9584946
27 feet Y = -2921491
62 meter
Z = 17424828
78 Z = 5311087
81
XDOT = 17780
311641 XDOT = 5419
438988
YDOT = -16270
396288 feet/sec YDOT = -4959
216789 meter/sec
ZDOT = 1281
153335 ZDOT = 390
495537
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
99351452
00016717 00000-0 10270-3 0 9097
2 25544 51
6431 198
5829 0001660 124
7828 235
3479 15
49191288 19268
Satellite: ISS
Catalog Number: 25544
Epoch time: 20344
99351452 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 198
5829 deg
Eccentricity:
0001660
Arg of perigee: 124
7828 deg
Mean anomaly: 235
3479 deg
Mean motion: 15
49191288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 339
Coasting Arc #11 (Orbit 1940)
---------------------------------------
Vector Time (GMT): 2020/345/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -637800
86 A = 6791913
87 meter
Y = 4189942
21 meter E =
0016201
Z = -5321362
54 I = 51
53292
XDOT = -7500
687341 Wp = 91
56593
YDOT = -1472
854742 meter/sec RA = 192
66877 deg
ZDOT = -261
815783 TA = 175
93488
MA = 175
92170
Ha = 229
382 n
mi
Hp = 221
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2092522
52 X = -658758
19
Y = 13746529
56 feet Y = 4182693
15 meter
Z = -17458538
50 Z = -5324511
30
XDOT = -24608
554269 XDOT = -7482
388196
YDOT = -4832
200596 feet/sec YDOT = -1556
630476 meter/sec
ZDOT = -858
975667 ZDOT = -298
207361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10797837
46 X = 3291180
86
Y = 8731685
66 feet Y = 2661417
79 meter
Z = -17473141
21 Z = -5325813
44
XDOT = -16109
237602 XDOT = -4910
095621
YDOT = 17872
350546 feet/sec YDOT = 5447
492446 meter/sec
ZDOT = -1027
497425 ZDOT = -313
181215
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
96113327
00016717 00000-0 10270-3 0 9104
2 25544 51
6426 193
7956 0001706 123
1553 236
9761 15
49154189 19416
Satellite: ISS
Catalog Number: 25544
Epoch time: 20345
96113327 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 193
7956 deg
Eccentricity:
0001706
Arg of perigee: 123
1553 deg
Mean anomaly: 236
9761 deg
Mean motion: 15
49154189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1941
Checksum: 314
Coasting Arc #12 (Orbit 1956)
---------------------------------------
Vector Time (GMT): 2020/346/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 355717
65 A = 6791778
06 meter
Y = -4208608
18 meter E =
0004143
Z = 5315477
38 I = 51
56516
XDOT = 7610
609322 Wp = 111
77347
YDOT = 881
455812 meter/sec RA = 187
71624 deg
ZDOT = 186
974341 TA = 336
43222
MA = 336
45120
Ha = 229
315 n
mi
Hp = 221
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1167052
67 X = 376933
21
Y = -13807769
62 feet Y = -4204512
26 meter
Z = 17439230
27 Z = 5317256
41
XDOT = 24969
190690 XDOT = 7599
278749
YDOT = 2891
915394 feet/sec YDOT = 966
499738 meter/sec
ZDOT = 613
432877 ZDOT = 223
916850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11459545
11 X = -3492869
35
Y = -7772200
91 feet Y = -2368966
84 meter
Z = 17447492
22 Z = 5317995
63
XDOT = 14352
270678 XDOT = 4374
572103
YDOT = -19388
279570 feet/sec YDOT = -5909
547613 meter/sec
ZDOT = 784
533691 ZDOT = 239
125869
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
99325571
00016717 00000-0 10270-3 0 9115
2 25544 51
6416 188
6895 0001742 126
1309 234
0002 15
49191142 19576
Satellite: ISS
Catalog Number: 25544
Epoch time: 20346
99325571 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 188
6895 deg
Eccentricity:
0001742
Arg of perigee: 126
1309 deg
Mean anomaly: 234
0002 deg
Mean motion: 15
49191142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1957
Checksum: 305
Coasting Arc #13 (Orbit 1971)
---------------------------------------
Vector Time (GMT): 2020/347/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -83597
62 A = 6791852
49 meter
Y = 4225819
39 meter E =
0016160
Z = -5330434
66 I = 51
59945
XDOT = -7642
443096 Wp = 93
15828
YDOT = -284
363754 meter/sec RA = 182
76468 deg
ZDOT = -106
727952 TA = 175
82822
MA = 175
81473
Ha = 229
332 n
mi
Hp = 221
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -274270
39 X = -104953
22
Y = 13864236
85 feet Y = 4224765
88 meter
Z = -17488302
71 Z = -5330892
03
XDOT = -25073
632206 XDOT = -7638
176820
YDOT = -932
951948 feet/sec YDOT = -369
803171 meter/sec
ZDOT = -350
157323 ZDOT = -143
842168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12071571
13 X = 3679414
88
Y = 6818685
97 feet Y = 2078335
48 meter
Z = -17490446
28 Z = -5331088
03
XDOT = -12406
642215 XDOT = -3781
544547
YDOT = 20634
783315 feet/sec YDOT = 6289
481955 meter/sec
ZDOT = -522
085128 ZDOT = -159
131547
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
96086875
00016717 00000-0 10270-3 0 9125
2 25544 51
6421 183
9015 0001704 128
9122 231
2180 15
49166988 19728
Satellite: ISS
Catalog Number: 25544
Epoch time: 20347
96086875 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 183
9015 deg
Eccentricity:
0001704
Arg of perigee: 128
9122 deg
Mean anomaly: 231
2180 deg
Mean motion: 15
49166988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1972
Checksum: 317
Coasting Arc #14 (Orbit 1987)
---------------------------------------
Vector Time (GMT): 2020/348/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -192569
43 A = 6791737
05 meter
Y = -4209677
67 meter E =
0004023
Z = 5322962
57 I = 51
63287
XDOT = 7657
330261 Wp = 107
73860
YDOT = -313
876778 meter/sec RA = 177
81594 deg
ZDOT = 27
574581 TA = 341
99135
MA = 342
00560
Ha = 229
330 n
mi
Hp = 221
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -631789
46 X = -171337
40
Y = -13811278
46 feet Y = -4211713
29 meter
Z = 17463787
95 Z = 5322078
00
XDOT = 25122
474610 XDOT = 7660
137073
YDOT = -1029
779456 feet/sec YDOT = -228
231324 meter/sec
ZDOT = 90
467786 ZDOT = 64
778056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12563248
38 X = -3829278
11
Y = -5784247
90 feet Y = -1763038
76 meter
Z = 17459717
25 Z = 5321721
82
XDOT = 10398
098717 XDOT = 3169
340489
YDOT = -21778
987349 feet/sec YDOT = -6638
235344 meter/sec
ZDOT = 262
845115 ZDOT = 80
115191
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
99298385
00016717 00000-0 10270-3 0 9131
2 25544 51
6416 178
7946 0001759 126
0294 234
1019 15
49199338 19881
Satellite: ISS
Catalog Number: 25544
Epoch time: 20348
99298385 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 178
7946 deg
Eccentricity:
0001759
Arg of perigee: 126
0294 deg
Mean anomaly: 234
1019 deg
Mean motion: 15
49199338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1988
Checksum: 356
Coasting Arc #15 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2020/349/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 460175
64 A = 6791799
46 meter
Y = 4194337
78 meter E =
0016123
Z = -5335995
33 I = 51
66758
XDOT = -7594
524010 Wp = 94
35944
YDOT = 905
582270 meter/sec RA = 172
86939 deg
ZDOT = 55
829279 TA = 176
17989
MA = 176
16756
Ha = 229
283 n
mi
Hp = 221
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1509762
61 X = 439158
41
Y = 13760950
73 feet Y = 4199367
24 meter
Z = -17506546
36 Z = -5333810
26
XDOT = -24916
417356 XDOT = -7604
357252
YDOT = 2971
070440 feet/sec YDOT = 820
599859 meter/sec
ZDOT = 183
166926 ZDOT = 18
914167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13012667
74 X = 3966261
13
Y = 4760989
27 feet Y = 1451149
53 meter
Z = -17496450
30 Z = -5332918
05
XDOT = -8256
510050 XDOT = -2516
584263
YDOT = 22623
650780 feet/sec YDOT = 6895
688758 meter/sec
ZDOT = 12
086918 ZDOT = 3
684093
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
96058928
00016717 00000-0 10270-3 0 9147
2 25544 51
6425 174
0070 0001654 130
7380 229
3914 15
49182218 20038
Satellite: ISS
Catalog Number: 25544
Epoch time: 20349
96058928 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 174
0070 deg
Eccentricity:
0001654
Arg of perigee: 130
7380 deg
Mean anomaly: 229
3914 deg
Mean motion: 15
49182218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 299
Coasting Arc #16 (Orbit 2018)
---------------------------------------
Vector Time (GMT): 2020/350/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -728456
55 A = 6791724
84 meter
Y = -4146081
08 meter E =
0003898
Z = 5326529
06 I = 51
69937
XDOT = 7515
033353 Wp = 104
67743
YDOT = -1496
317427 meter/sec RA = 167
92513 deg
ZDOT = -137
831879 TA = 346
63058
MA = 346
64091
Ha = 229
328 n
mi
Hp = 221
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2389949
32 X = -707912
84
Y = -13602628
20 feet Y = -4154113
29 meter
Z = 17475489
04 Z = 5323039
66
XDOT = 24655
621237 XDOT = 7531
876603
YDOT = -4909
177909 feet/sec YDOT = -1412
184727 meter/sec
ZDOT = -452
204329 ZDOT = -101
286228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13334071
90 X = -4064225
12
Y = -3675571
70 feet Y = -1120314
25 meter
Z = 17459346
15 Z = 5321608
71
XDOT = 6071
980694 XDOT = 1850
739716
YDOT = -23357
244970 feet/sec YDOT = -7119
288267 meter/sec
ZDOT = -282
797334 ZDOT = -86
196627
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
99269948
00016717 00000-0 10270-3 0 9159
2 25544 51
6408 168
9001 0001767 129
8145 230
3161 15
49203694 20193
Satellite: ISS
Catalog Number: 25544
Epoch time: 20350
99269948 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 168
9001 deg
Eccentricity:
0001767
Arg of perigee: 129
8145 deg
Mean anomaly: 230
3161 deg
Mean motion: 15
49203694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2019
Checksum: 316
Coasting Arc #17 (Orbit 2029)
---------------------------------------
Vector Time (GMT): 2020/351/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 982624
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3792929
13 A = 6793871
15 meter
Y = -2899468
37 meter E =
0008988
Z = 4829296
33 I = 51
73107
XDOT = 6151
929901 Wp = 125
07156
YDOT = -3794
718304 meter/sec RA = 164
45887 deg
ZDOT = 2545
013488 TA = 299
85886
MA = 299
94815
Ha = 229
244 n
mi
Hp = 222
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12443993
22 X = -3783682
31
Y = -9512691
49 feet Y = -2941832
75 meter
Z = 15844148
08 Z = 4810893
84
XDOT = 20183
497050 XDOT = 6181
544231
YDOT = -12449
863202 feet/sec YDOT = -3725
757861 meter/sec
ZDOT = 8349
781786 ZDOT = 2574
968242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3119732
68 X = -950894
52
Y = -15437192
58 feet Y = -4705256
30 meter
Z = 15758859
36 Z = 4803300
33
XDOT = 22202
357439 XDOT = 6767
278547
YDOT = 4206
907280 feet/sec YDOT = 1282
265339 meter/sec
ZDOT = 8488
675561 ZDOT = 2587
348311
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
70227307
00016717 00000-0 10270-3 0 9163
2 25544 51
6419 165
3855 0001805 148
9253 211
2004 15
49229778 20306
Satellite: ISS
Catalog Number: 25544
Epoch time: 20351
70227307 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 165
3855 deg
Eccentricity:
0001805
Arg of perigee: 148
9253 deg
Mean anomaly: 211
2004 deg
Mean motion: 15
49229778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2030
Checksum: 293
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