[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 26th 2020
- spaceflight nasa gov will be taken offline in the next 30 days *
- *
- Current information about the International Space Station can be *
- found at www nasa gov/station *
- *
- Predicted ISS and visiting vehicle sightings opportunities can be *
- found at spotthestation nasa gov *
- *
- Updated ISS trajectory information will be made available as a CCSDS *
- Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
- system *
- Included in the OEM are a sequence of events with ISS maneuver *
- details (in the comment section), predicted post-maneuver state *
- vectors, predicted coasting state vectors at 4-minute intervals, *
- and ISS ballistic details *
- *
- OEMs will be provided in xml and txt formats *
- Links to the OEMs and more details to follow *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15144 822 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
296/18:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
8
303/01:06:42
218 1
5 1
9 1
9
N/A 1
1 -0
2 229
2
000/00:05:24
437 -0
0 0
1 222
8
303/17:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
6
Coasting Arc #1 (Orbit 1127)
---------------------------------------
Vector Time (GMT): 2020/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953675
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4182782
19 A = 6791623
03 meter
Y = -764512
38 meter E =
0015696
Z = -5309507
90 I = 52
01334
XDOT = 327
655156 Wp = 80
72783
YDOT = 7596
122470 meter/sec RA = 92
45161 deg
ZDOT = -835
285588 TA = 181
30586
MA = 181
30996
Ha = 229
002 n
mi
Hp = 221
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13723038
68 X = 4216811
54
Y = -2508242
72 feet Y = -717547
22 meter
Z = -17419645
33 Z = -5289106
40
XDOT = 1074
984106 XDOT = 246
746115
YDOT = 24921
661648 feet/sec YDOT = 7599
334158 meter/sec
ZDOT = -2740
438280 ZDOT = -833
890410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11116907
31 X = -3388433
35
Y = 8620234
21 feet Y = 2627447
39 meter
Z = -17325214
27 Z = -5280725
31
XDOT = -11855
226999 XDOT = -3613
473189
YDOT = -20786
407504 feet/sec YDOT = -6335
697007 meter/sec
ZDOT = -2734
175506 ZDOT = -833
376694
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20293
51758046
00016717 00000-0 10270-3 0 9009
2 25544 51
6408 93
2800 0001437 50
6290 309
4987 15
49321265 11285
Satellite: ISS
Catalog Number: 25544
Epoch time: 20293
51758046 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 93
2800 deg
Eccentricity:
0001437
Arg of perigee: 50
6290 deg
Mean anomaly: 309
4987 deg
Mean motion: 15
49321265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1128
Checksum: 298
Coasting Arc #2 (Orbit 1143)
---------------------------------------
Vector Time (GMT): 2020/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953675
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110576
05 A = 6791635
60 meter
Y = 981963
53 meter E =
0003981
Z = 5313144
84 I = 52
01318
XDOT = -885
795273 Wp = 96
61212
YDOT = -7578
934340 meter/sec RA = 87
52718 deg
ZDOT = 714
512065 TA = 346
58914
MA = 346
59972
Ha = 229
253 n
mi
Hp = 221
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13486141
90 X = -4147059
94
Y = 3221665
13 feet Y = 935792
00 meter
Z = 17431577
57 Z = 5293088
25
XDOT = -2906
152471 XDOT = -804
450275
YDOT = -24865
270143 feet/sec YDOT = -7588
385125 meter/sec
ZDOT = 2344
199687 ZDOT = 710
406525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10418440
39 X = 3175540
63
Y = -9324143
79 feet Y = -2841999
03 meter
Z = 17338727
99 Z = 5284844
29
XDOT = 13753
458425 XDOT = 4192
054128
YDOT = 19697
363721 feet/sec YDOT = 6003
756462 meter/sec
ZDOT = 2325
417098 ZDOT = 708
787131
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20294
54961435
00016717 00000-0 10270-3 0 9012
2 25544 51
6406 88
1714 0001530 52
6861 307
4428 15
49290274 11441
Satellite: ISS
Catalog Number: 25544
Epoch time: 20294
54961435 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 88
1714 deg
Eccentricity:
0001530
Arg of perigee: 52
6861 deg
Mean anomaly: 307
4428 deg
Mean motion: 15
49290274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1144
Checksum: 297
Coasting Arc #3 (Orbit 1158)
---------------------------------------
Vector Time (GMT): 2020/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953675
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4046567
39 A = 6791486
72 meter
Y = -1196063
05 meter E =
0016021
Z = -5335436
28 I = 52
01100
XDOT = 1436
151171 Wp = 83
00488
YDOT = 7489
569055 meter/sec RA = 82
60535 deg
ZDOT = -589
361417 TA = 181
38228
MA = 181
38672
Ha = 229
052 n
mi
Hp = 221
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13276139
73 X = 4085558
32
Y = -3924091
36 feet Y = -1150593
26 meter
Z = -17504712
20 Z = -5315684
63
XDOT = 4711
782058 XDOT = 1355
156641
YDOT = 24572
076953 feet/sec YDOT = 7505
176275 meter/sec
ZDOT = -1933
600448 ZDOT = -582
581545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9728396
61 X = -2965215
29
Y = 10010296
97 feet Y = 3051138
52 meter
Z = -17413258
81 Z = -5307561
28
XDOT = -15478
115288 XDOT = -4717
729540
YDOT = -18353
792662 feet/sec YDOT = -5594
236003 meter/sec
ZDOT = -1902
457930 ZDOT = -579
869177
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20295
51714333
00016717 00000-0 10270-3 0 9024
2 25544 51
6413 83
3849 0001510 58
7564 301
3734 15
49327278 11594
Satellite: ISS
Catalog Number: 25544
Epoch time: 20295
51714333 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 83
3849 deg
Eccentricity:
0001510
Arg of perigee: 58
7564 deg
Mean anomaly: 301
3734 deg
Mean motion: 15
49327278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1159
Checksum: 302
Coasting Arc #4 (Orbit 1174)
---------------------------------------
Vector Time (GMT): 2020/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938567
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3958900
50 A = 6791483
33 meter
Y = 1401202
88 meter E =
0003775
Z = 5334171
01 I = 52
00540
XDOT = -1986
028841 Wp = 91
95443
YDOT = -7387
400724 meter/sec RA = 77
68075 deg
ZDOT = 466
159327 TA = 353
61651
MA = 353
62132
Ha = 229
216 n
mi
Hp = 221
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12988518
70 X = -4000185
62
Y = 4597122
30 feet Y = 1356700
65 meter
Z = 17500561
06 Z = 5314839
74
XDOT = -6515
842655 XDOT = -1905
537455
YDOT = -24236
879015 feet/sec YDOT = -7409
159878 meter/sec
ZDOT = 1529
394118 ZDOT = 456
707177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8965545
25 X = 2732698
19
Y = -10610349
22 feet Y = -3234034
44 meter
Z = 17411038
93 Z = 5306884
67
XDOT = 17142
329479 XDOT = 5224
982025
YDOT = 16925
439398 feet/sec YDOT = 5158
873929 meter/sec
ZDOT = 1485
896073 ZDOT = 452
901123
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20296
54917464
00016717 00000-0 10270-3 0 9039
2 25544 51
6414 78
2766 0001446 58
1779 301
9511 15
49308533 11756
Satellite: ISS
Catalog Number: 25544
Epoch time: 20296
54917464 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 78
2766 deg
Eccentricity:
0001446
Arg of perigee: 58
1779 deg
Mean anomaly: 301
9511 deg
Mean motion: 15
49308533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1175
Checksum: 319
Coasting Arc #5 (Orbit 1178)
---------------------------------------
Vector Time (GMT): 2020/296/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938567
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4228349
95 A = 6791516
35 meter
Y = 159607
95 meter E =
0004571
Z = 5309185
40 I = 52
00503
XDOT = -1223
307932 Wp = 58
22262
YDOT = -7528
682535 meter/sec RA = 76
39436 deg
ZDOT = -745
126240 TA = 38
88075
MA = 38
84788
Ha = 229
138 n
mi
Hp = 221
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13872539
22 X = -4255609
76
Y = 523648
14 feet Y = 112170
98 meter
Z = 17418587
26 Z = 5288579
28
XDOT = -4013
477468 XDOT = -1135
409573
YDOT = -24700
402019 feet/sec YDOT = -7541
870955 meter/sec
ZDOT = -2444
639896 ZDOT = -750
855332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8328526
20 X = -2538534
79
Y = -11254818
09 feet Y = -3430468
55 meter
Z = 17323205
68 Z = 5280113
09
XDOT = 17315
696700 XDOT = 5277
824354
YDOT = -16630
985963 feet/sec YDOT = -5069
124521 meter/sec
ZDOT = -2470
897015 ZDOT = -753
129410
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20296
80717985
00016717 00000-0 10270-3 0 9045
2 25544 51
6426 77
0038 0001444 50
3135 309
8142 15
49338451 11799
Satellite: ISS
Catalog Number: 25544
Epoch time: 20296
80717985 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 77
0038 deg
Eccentricity:
0001444
Arg of perigee: 50
3135 deg
Mean anomaly: 309
8142 deg
Mean motion: 15
49338451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1179
Checksum: 308
Coasting Arc #6 (Orbit 1193)
---------------------------------------
Vector Time (GMT): 2020/297/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938567
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4240260
46 A = 6791703
38 meter
Y = -391240
96 meter E =
0015621
Z = -5304510
42 I = 51
99714
XDOT = 1763
865008 Wp = 92
42842
YDOT = 7392
260166 meter/sec RA = 71
46956 deg
ZDOT = 866
310973 TA = 185
82634
MA = 185
84454
Ha = 229
100 n
mi
Hp = 221
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13911615
68 X = 4270086
80
Y = -1283598
95 feet Y = -343656
51 meter
Z = -17403249
40 Z = -5283840
27
XDOT = 5786
958689 XDOT = 1676
863349
YDOT = 24252
822068 feet/sec YDOT = 7411
498505 meter/sec
ZDOT = 2842
227602 ZDOT = 874
667968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9163351
19 X = 2792989
44
Y = 10702108
38 feet Y = 3262002
64 meter
Z = -17307560
14 Z = -5275344
33
XDOT = -15667
468753 XDOT = -4775
444476
YDOT = 18065
076483 feet/sec YDOT = 5506
235312 meter/sec
ZDOT = 2880
639165 ZDOT = 878
018817
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20297
77470696
00016717 00000-0 10270-3 0 9058
2 25544 51
6436 72
2152 0001615 51
9319 308
1977 15
49301761 11944
Satellite: ISS
Catalog Number: 25544
Epoch time: 20297
77470696 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 72
2152 deg
Eccentricity:
0001615
Arg of perigee: 51
9319 deg
Mean anomaly: 308
1977 deg
Mean motion: 15
49301761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1194
Checksum: 316
Coasting Arc #7 (Orbit 1209)
---------------------------------------
Vector Time (GMT): 2020/298/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938567
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230157
52 A = 6791651
60 meter
Y = 609875
81 meter E =
0005359
Z = 5274843
11 I = 51
98502
XDOT = -2293
052059 Wp = 56
90523
YDOT = -7244
484952 meter/sec RA = 66
54499 deg
ZDOT = -997
728252 TA = 42
62675
MA = 42
58518
Ha = 229
243 n
mi
Hp = 221
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13878469
55 X = -4262285
31
Y = 2000904
88 feet Y = 562391
55 meter
Z = 17305915
71 Z = 5254216
46
XDOT = -7523
136675 XDOT = -2207
025184
YDOT = -23767
995248 feet/sec YDOT = -7269
646504 meter/sec
ZDOT = -3273
386655 ZDOT = -1008
658099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9903959
59 X = -3018726
88
Y = -10090755
18 feet Y = -3075662
18 meter
Z = 17210418
36 Z = 5245735
52
XDOT = 13970
090052 XDOT = 4258
083448
YDOT = -19400
395898 feet/sec YDOT = -5913
240670 meter/sec
ZDOT = -3323
699905 ZDOT = -1013
063731
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20298
80673179
00016717 00000-0 10270-3 0 9065
2 25544 51
6431 67
1083 0001722 55
8089 304
3224 15
49344252 12105
Satellite: ISS
Catalog Number: 25544
Epoch time: 20298
80673179 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 67
1083 deg
Eccentricity:
0001722
Arg of perigee: 55
8089 deg
Mean anomaly: 304
3224 deg
Mean motion: 15
49344252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1210
Checksum: 294
Coasting Arc #8 (Orbit 1224)
---------------------------------------
Vector Time (GMT): 2020/299/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938567
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222773
84 A = 6791862
35 meter
Y = -847060
73 meter E =
0015490
Z = -5265188
37 I = 51
97134
XDOT = 2802
759119 Wp = 94
37767
YDOT = 7028
539970 meter/sec RA = 61
61903 deg
ZDOT = 1118
800357 TA = 186
31382
MA = 186
33336
Ha = 229
150 n
mi
Hp = 221
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13854244
88 X = 4257507
58
Y = -2779070
63 feet Y = -799644
55 meter
Z = -17274240
05 Z = -5244591
23
XDOT = 9195
403935 XDOT = 2718
521016
YDOT = 23059
514338 feet/sec YDOT = 7059
411453 meter/sec
ZDOT = 3670
604846 ZDOT = 1132
210430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10680168
76 X = 3255315
44
Y = 9427783
69 feet Y = 2873588
47 meter
Z = -17178870
57 Z = -5236119
75
XDOT = -12094
677771 XDOT = -3686
457785
YDOT = 20492
192390 feet/sec YDOT = 6246
020240 meter/sec
ZDOT = 3732
393677 ZDOT = 1137
633593
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20299
77425593
00016717 00000-0 10270-3 0 9078
2 25544 51
6437 62
3201 0001700 57
9628 302
1687 15
49306544 12255
Satellite: ISS
Catalog Number: 25544
Epoch time: 20299
77425593 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 62
3201 deg
Eccentricity:
0001700
Arg of perigee: 57
9628 deg
Mean anomaly: 302
1687 deg
Mean motion: 15
49306544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1225
Checksum: 307
Coasting Arc #9 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2020/300/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938567
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194957
34 A = 6791849
88 meter
Y = 1068688
92 meter E =
0006002
Z = 5229704
60 I = 51
95361
XDOT = -3298
672052 Wp = 57
70710
YDOT = -6803
757135 meter/sec RA = 56
69208 deg
ZDOT = -1251
484065 TA = 44
28407
MA = 44
23606
Ha = 229
308 n
mi
Hp = 221
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13762983
41 X = -4231999
16
Y = 3506197
25 feet Y = 1021570
96 meter
Z = 17157823
50 Z = 5209236
91
XDOT = -10822
414870 XDOT = -3216
266159
YDOT = -22322
037844 feet/sec YDOT = -6840
184535 meter/sec
ZDOT = -4105
918848 ZDOT = -1267
307516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11354358
66 X = -3460808
52
Y = -8719806
83 feet Y = -2657797
12 meter
Z = 17063046
25 Z = 5200816
50
XDOT = 10193
310546 XDOT = 3106
921054
YDOT = -21477
244607 feet/sec YDOT = -6546
264156 meter/sec
ZDOT = -4178
872964 ZDOT = -1273
720479
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20300
80627884
00016717 00000-0 10270-3 0 9083
2 25544 51
6428 57
2127 0001825 63
5632 296
5705 15
49344131 12410
Satellite: ISS
Catalog Number: 25544
Epoch time: 20300
80627884 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 57
2127 deg
Eccentricity:
0001825
Arg of perigee: 63
5632 deg
Mean anomaly: 296
5705 deg
Mean motion: 15
49344131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 297
Coasting Arc #10 (Orbit 1255)
---------------------------------------
Vector Time (GMT): 2020/301/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938567
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166814
95 A = 6792051
54 meter
Y = -1309814
33 meter E =
0015211
Z = -5214730
08 I = 51
93623
XDOT = 3764
572734 Wp = 96
21083
YDOT = 6515
458211 meter/sec RA = 51
76405 deg
ZDOT = 1373
387144 TA = 186
96076
MA = 186
98191
Ha = 229
164 n
mi
Hp = 221
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13670652
73 X = 4206482
55
Y = -4297291
12 feet Y = -1262996
44 meter
Z = -17108694
50 Z = -5194392
63
XDOT = 12350
960415 XDOT = 3684
763893
YDOT = 21376
175232 feet/sec YDOT = 6557
110183 meter/sec
ZDOT = 4505
863334 ZDOT = 1391
480116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12056330
56 X = 3674769
55
Y = 7950605
52 feet Y = 2423344
56 meter
Z = -17014512
92 Z = -5186023
54
XDOT = -8165
969187 XDOT = -2488
987408
YDOT = 22191
169054 feet/sec YDOT = 6763
868328 meter/sec
ZDOT = 4589
317602 ZDOT = 1398
824005
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 20301
77379813
00016717 00000-0 10270-3 0 9097
2 25544 51
6447 52
4248 0001740 61
6393 298
4932 15
49316620 12562
Satellite: ISS
Catalog Number: 25544
Epoch time: 20301
77379813 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 52
4248 deg
Eccentricity:
0001740
Arg of perigee: 61
6393 deg
Mean anomaly: 298
4932 deg
Mean motion: 15
49316620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1256
Checksum: 313
Coasting Arc #11 (Orbit 1271)
---------------------------------------
Vector Time (GMT): 2020/302/18:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 938567
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4120824
65 A = 6792087
91 meter
Y = 1532699
65 meter E =
0006688
Z = 5172980
58 I = 51
91343
XDOT = -4214
073416 Wp = 57
85459
YDOT = -6221
353452 meter/sec RA = 46
83435 deg
ZDOT = -1508
742277 TA = 46
65724
MA = 46
60152
Ha = 229
343 n
mi
Hp = 221
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13519765
92 X = -4162785
35
Y = 5028542
15 feet Y = 1486383
23 meter
Z = 16971721
06 Z = 5152860
87
XDOT = -13825
700184 XDOT = -4136
862417
YDOT = -20411
264605 feet/sec YDOT = -6268
046595 meter/sec
ZDOT = -4949
941853 ZDOT = -1529
025182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12651135
21 X = -3856066
01
Y = -7153548
52 feet Y = -2180401
59 meter
Z = 16878540
93 Z = 5144579
28
XDOT = 6138
484493 XDOT = 1871
010073
YDOT = -22794
065421 feet/sec YDOT = -6947
631140 meter/sec
ZDOT = -5043
526143 ZDOT = -1537
266768
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 20302
80581631
00016717 00000-0 10270-3 0 9107
2 25544 51
6433 47
3173 0001927 66
3444 293
7908 15
49346802 12727
Satellite: ISS
Catalog Number: 25544
Epoch time: 20302
80581631 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 47
3173 deg
Eccentricity:
0001927
Arg of perigee: 66
3444 deg
Mean anomaly: 293
7908 deg
Mean motion: 15
49346802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1272
Checksum: 298
Coasting Arc #12 (Orbit 1275)
---------------------------------------
Vector Time (GMT): 2020/303/01:09:24
437
Vector Time (MET): N/A
Weight (LBS) : 938366
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3200941
79 A = 6792362
26 meter
Y = -2724926
65 meter E =
0014937
Z = -5348138
99 I = 51
90581
XDOT = 5211
779813 Wp = 89
01182
YDOT = 5592
216621 meter/sec RA = 45
42447 deg
ZDOT = 270
946645 TA = 183
56255
MA = 183
57320
Ha = 229
159 n
mi
Hp = 222
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10501777
53 X = 3257153
56
Y = -8940048
05 feet Y = -2688817
33 meter
Z = -17546387
75 Z = -5332453
11
XDOT = 17099
015136 XDOT = 5147
542475
YDOT = 18347
167392 feet/sec YDOT = 5650
139322 meter/sec
ZDOT = 888
932563 ZDOT = 296
107684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1057506
05 X = -322327
84
Y = -13843408
48 feet Y = -4219470
90 meter
Z = -17473672
66 Z = -5325975
43
XDOT = 23865
343964 XDOT = 7274
156840
YDOT = -3088
020934 feet/sec YDOT = -941
228781 meter/sec
ZDOT = 1005
114971 ZDOT = 306
359043
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 20303
06382309
00016717 00000-0 10270-3 0 9118
2 25544 51
6449 46
0410 0000796 11
9017 348
2151 15
48999933 12767
Satellite: ISS
Catalog Number: 25544
Epoch time: 20303
06382309 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 46
0410 deg
Eccentricity:
0000796
Arg of perigee: 11
9017 deg
Mean anomaly: 348
2151 deg
Mean motion: 15
48999933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1276
Checksum: 299
Coasting Arc #13 (Orbit 1286)
---------------------------------------
Vector Time (GMT): 2020/303/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 938366
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1276142
17 A = 6793244
04 meter
Y = 4266895
05 meter E =
0005078
Z = 5126321
89 I = 51
89077
XDOT = -6347
265113 Wp = 117
02540
YDOT = -3943
000317 meter/sec RA = 42
11824 deg
ZDOT = 1698
333536 TA = 316
59441
MA = 316
63439
Ha = 229
290 n
mi
Hp = 222
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4186818
13 X = -1348662
34
Y = 13998999
52 feet Y = 4252219
01 meter
Z = 16818641
36 Z = 5119946
45
XDOT = -20824
360608 XDOT = -6310
951268
YDOT = -12936
352745 feet/sec YDOT = -4013
776888 meter/sec
ZDOT = 5571
960419 ZDOT = 1667
588649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14400075
74 X = -4389143
09
Y = 2671615
04 feet Y = 814308
26 meter
Z = 16788937
50 Z = 5117268
15
XDOT = 1997
131577 XDOT = 608
725705
YDOT = -23430
903904 feet/sec YDOT = -7141
739510 meter/sec
ZDOT = 5429
874277 ZDOT = 1655
025680
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 20303
77349445
00016717 00000-0 10270-3 0 9121
2 25544 51
6432 42
5298 0000665 32
6096 327
5094 15
48994420 12870
Satellite: ISS
Catalog Number: 25544
Epoch time: 20303
77349445 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 42
5298 deg
Eccentricity:
0000665
Arg of perigee: 32
6096 deg
Mean anomaly: 327
5094 deg
Mean motion: 15
48994420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1287
Checksum: 315
Coasting Arc #14 (Orbit 1301)
---------------------------------------
Vector Time (GMT): 2020/304/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 938366
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 914533
97 A = 6793278
21 meter
Y = -4366743
21 meter E =
0013744
Z = -5135241
77 I = 51
86573
XDOT = 6650
597426 Wp = 75
19772
YDOT = 3380
343036 meter/sec RA = 37
18987 deg
ZDOT = -1690
433207 TA = 178
48740
MA = 178
48324
Ha = 229
188 n
mi
Hp = 222
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3000439
53 X = 988240
97
Y = -14326585
33 feet Y = -4356104
23 meter
Z = -16847906
08 Z = -5130620
09
XDOT = 21819
545361 XDOT = 6620
514493
YDOT = 11090
364292 feet/sec YDOT = 3454
546548 meter/sec
ZDOT = -5546
040705 ZDOT = -1658
199503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14072284
90 X = 4289232
44
Y = -4117264
87 feet Y = -1254942
33 meter
Z = -16826305
34 Z = -5128657
87
XDOT = 415
862610 XDOT = 126
754924
YDOT = 23472
940687 feet/sec YDOT = 7154
552321 meter/sec
ZDOT = -5397
056830 ZDOT = -1645
022922
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 20304
74122779
00016717 00000-0 10270-3 0 9139
2 25544 51
6441 37
7440 0000568 20
5940 339
5233 15
48982529 13024
Satellite: ISS
Catalog Number: 25544
Epoch time: 20304
74122779 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 37
7440 deg
Eccentricity:
0000568
Arg of perigee: 20
5940 deg
Mean anomaly: 339
5233 deg
Mean motion: 15
48982529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1302
Checksum: 297
Coasting Arc #15 (Orbit 1317)
---------------------------------------
Vector Time (GMT): 2020/305/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 938366
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -536222
35 A = 6793229
63 meter
Y = 4423575
18 meter E =
0005001
Z = 5124278
77 I = 51
83742
XDOT = -6928
879737 Wp = 115
90798
YDOT = -2802
199641 meter/sec RA = 32
25850 deg
ZDOT = 1690
548099 TA = 317
77746
MA = 317
81596
Ha = 229
267 n
mi
Hp = 222
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1759259
68 X = -610539
78
Y = 14513041
94 feet Y = 4417163
25 meter
Z = 16811938
22 Z = 5121493
41
XDOT = -22732
545068 XDOT = -6905
241673
YDOT = -9193
568376 feet/sec YDOT = -2879
551169 meter/sec
ZDOT = 5546
417648 ZDOT = 1656
946774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13549088
57 X = -4129762
20
Y = 5530496
26 feet Y = 1685695
26 meter
Z = 16798823
11 Z = 5120281
28
XDOT = -2834
426847 XDOT = -863
933303
YDOT = -23353
438075 feet/sec YDOT = -7118
127925 meter/sec
ZDOT = 5391
094275 ZDOT = 1643
205535
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 20305
77347352
00016717 00000-0 10270-3 0 9140
2 25544 51
6435 32
6377 0000753 28
2039 331
9151 15
48994852 13184
Satellite: ISS
Catalog Number: 25544
Epoch time: 20305
77347352 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 32
6377 deg
Eccentricity:
0000753
Arg of perigee: 28
2039 deg
Mean anomaly: 331
9151 deg
Mean motion: 15
48994852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1318
Checksum: 308
Coasting Arc #16 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2020/306/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 938366
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 166321
74 A = 6793242
23 meter
Y = -4460217
43 meter E =
0014015
Z = -5133844
14 I = 51
80763
XDOT = 7131
641943 Wp = 74
86808
YDOT = 2198
259000 meter/sec RA = 27
32653 deg
ZDOT = -1679
043551 TA = 178
91577
MA = 178
91273
Ha = 229
261 n
mi
Hp = 222
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 545675
00 X = 241122
90
Y = -14633259
28 feet Y = -4457939
19 meter
Z = -16843320
68 Z = -5132854
57
XDOT = 23397
775404 XDOT = 7114
686380
YDOT = 7212
135828 feet/sec YDOT = 2277
915358 meter/sec
ZDOT = -5508
673067 ZDOT = -1644
440944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12938788
83 X = 3943742
84
Y = -6868772
11 feet Y = -2093601
74 meter
Z = -16838503
59 Z = -5132375
89
XDOT = 5199
448839 XDOT = 1584
792006
YDOT = 22904
212600 feet/sec YDOT = 6981
204000 meter/sec
ZDOT = -5348
700975 ZDOT = -1630
284057
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 20306
74120192
00016717 00000-0 10270-3 0 9150
2 25544 51
6430 27
8520 0000801 31
2865 328
8333 15
48989584 13330
Satellite: ISS
Catalog Number: 25544
Epoch time: 20306
74120192 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 27
8520 deg
Eccentricity:
0000801
Arg of perigee: 31
2865 deg
Mean anomaly: 328
8333 deg
Mean motion: 15
48989584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 294
Coasting Arc #17 (Orbit 1348)
---------------------------------------
Vector Time (GMT): 2020/307/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 938366
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 213489
02 A = 6793231
02 meter
Y = 4452101
35 meter E =
0004925
Z = 5123170
73 I = 51
77544
XDOT = -7307
816260 Wp = 114
78148
YDOT = -1582
634094 meter/sec RA = 22
39163 deg
ZDOT = 1676
576547 TA = 319
02898
MA = 319
06598
Ha = 229
257 n
mi
Hp = 222
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 700423
28 X = 138802
25
Y = 14606631
72 feet Y = 4454070
96 meter
Z = 16808302
91 Z = 5124026
55
XDOT = -23975
775130 XDOT = -7297
719719
YDOT = -5192
369076 feet/sec YDOT = -1664
298944 meter/sec
ZDOT = 5500
579222 ZDOT = 1641
101463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12144205
59 X = -3701553
86
Y = 8138657
03 feet Y = 2480662
66 meter
Z = 16812015
40 Z = 5124302
29
XDOT = -7539
985414 XDOT = -2298
187554
YDOT = -22296
812434 feet/sec YDOT = -6796
068430 meter/sec
ZDOT = 5336
550184 ZDOT = 1626
580496
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 20307
77344441
00016717 00000-0 10270-3 0 9160
2 25544 51
6415 22
7461 0000842 25
4494 334
6697 15
48988408 13498
Satellite: ISS
Catalog Number: 25544
Epoch time: 20307
77344441 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 22
7461 deg
Eccentricity:
0000842
Arg of perigee: 25
4494 deg
Mean anomaly: 334
6697 deg
Mean motion: 15
48988408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1349
Checksum: 322
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