[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 6th 2020
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ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
249/11:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
8
253/10:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 221
8
254/20:33:53
536 0
4 1
4 1
4
N/A -1
4 0
1 229
4
000/00:03:43
072 -0
1 -0
0 222
4
Coasting Arc #1 (Orbit 399)
---------------------------------------
Vector Time (GMT): 2020/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4146439
05 A = 6792917
76 meter
Y = 1978483
61 meter E =
0006976
Z = 4999048
67 I = 51
40779
XDOT = -5018
715262 Wp = 114
94336
YDOT = 5433
267967 meter/sec RA = 325
23733 deg
ZDOT = 2007
324474 TA = 315
45005
MA = 315
50611
Ha = 229
106 n
mi
Hp = 221
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13603802
65 X = 4099724
74
Y = 6491087
95 feet Y = 2024591
16 meter
Z = 16401078
31 Z = 5019076
55
XDOT = -16465
601253 XDOT = -5088
848978
YDOT = 17825
682308 feet/sec YDOT = 5376
753075 meter/sec
ZDOT = 6585
710218 ZDOT = 1982
775247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10678171
47 X = -3254706
67
Y = -10494696
92 feet Y = -3198783
62 meter
Z = 16493363
20 Z = 5027177
10
XDOT = 20610
287340 XDOT = 6282
015581
YDOT = -10772
885399 feet/sec YDOT = -3283
575470 meter/sec
ZDOT = 6472
181836 ZDOT = 1972
721024
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 20246
55183427
00016717 00000-0 10270-3 0 9006
2 25544 51
6452 325
6138 0001476 80
3768 279
7549 15
49236240 4006
Satellite: ISS
Catalog Number: 25544
Epoch time: 20246
55183427 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 325
6138 deg
Eccentricity:
0001476
Arg of perigee: 80
3768 deg
Mean anomaly: 279
7549 deg
Mean motion: 15
49236240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 400
Checksum: 306
Coasting Arc #2 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2020/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4245763
27 A = 6792947
74 meter
Y = -1702075
27 meter E =
0014534
Z = -5035309
12 I = 51
37907
XDOT = 4596
075351 Wp = 76
07268
YDOT = -5807
135072 meter/sec RA = 320
27333 deg
ZDOT = -1913
671515 TA = 175
25823
MA = 175
24445
Ha = 229
334 n
mi
Hp = 221
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13929669
53 X = -4201956
24
Y = -5584236
46 feet Y = -1749309
85 meter
Z = -16520043
04 Z = -5055826
61
XDOT = 15078
987371 XDOT = 4669
966305
YDOT = -19052
280420 feet/sec YDOT = -5755
325449 meter/sec
ZDOT = -6278
449851 ZDOT = -1891
165972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11444108
59 X = 3488164
30
Y = 9545615
20 feet Y = 2909503
51 meter
Z = -16614596
63 Z = -5064129
05
XDOT = -19530
990495 XDOT = -5953
045903
YDOT = 12675
749244 feet/sec YDOT = 3863
568370 meter/sec
ZDOT = -6174
350387 ZDOT = -1881
941998
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 20247
51943139
00016717 00000-0 10270-3 0 9018
2 25544 51
6439 320
8269 0001544 80
8223 279
3102 15
49189967 4150
Satellite: ISS
Catalog Number: 25544
Epoch time: 20247
51943139 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 320
8269 deg
Eccentricity:
0001544
Arg of perigee: 80
8223 deg
Mean anomaly: 279
3102 deg
Mean motion: 15
49189967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 312
Coasting Arc #3 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2020/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4318540
85 A = 6792720
87 meter
Y = 1404643
75 meter E =
0006705
Z = 5047087
41 I = 51
35318
XDOT = -4155
681721 Wp = 115
29927
YDOT = 6173
192348 meter/sec RA = 315
30730 deg
ZDOT = 1833
035670 TA = 316
84200
MA = 316
89454
Ha = 229
147 n
mi
Hp = 221
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14168441
10 X = 4277997
05
Y = 4608411
27 feet Y = 1452710
45 meter
Z = 16558685
73 Z = 5067966
46
XDOT = -13634
126380 XDOT = -4233
307130
YDOT = 20253
255735 feet/sec YDOT = 6126
286642 meter/sec
ZDOT = 6013
896556 ZDOT = 1812
660149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12117524
33 X = -3693421
42
Y = -8482428
76 feet Y = -2585444
29 meter
Z = 16654916
91 Z = 5076418
67
XDOT = 18336
344069 XDOT = 5588
917672
YDOT = -14541
058533 feet/sec YDOT = -4432
114641 meter/sec
ZDOT = 5919
623690 ZDOT = 1804
301301
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 20248
55153175
00016717 00000-0 10270-3 0 9027
2 25544 51
6436 315
7204 0001586 84
1134 276
0197 15
49231543 4317
Satellite: ISS
Catalog Number: 25544
Epoch time: 20248
55153175 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 315
7204 deg
Eccentricity:
0001586
Arg of perigee: 84
1134 deg
Mean anomaly: 276
0197 deg
Mean motion: 15
49231543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 288
Coasting Arc #4 (Orbit 445)
---------------------------------------
Vector Time (GMT): 2020/249/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4031443
11 A = 6792053
00 meter
Y = 1683446
47 meter E =
0005243
Z = 5196712
86 I = 51
32867
XDOT = -4162
754223 Wp = 113
62608
YDOT = 6326
381389 meter/sec RA = 310
48975 deg
ZDOT = 1176
925928 TA = 325
01315
MA = 325
04759
Ha = 229
116 n
mi
Hp = 221
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13226519
39 X = 3987076
09
Y = 5523118
34 feet Y = 1728281
26 meter
Z = 17049582
86 Z = 5216188
09
XDOT = -13657
330129 XDOT = -4238
905154
YDOT = 20755
844451 feet/sec YDOT = 6279
404786 meter/sec
ZDOT = 3861
305538 ZDOT = 1156
519546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9148068
98 X = -2788331
42
Y = -10894511
62 feet Y = -3320647
14 meter
Z = 17139322
56 Z = 5224065
52
XDOT = 20848
679103 XDOT = 6354
677391
YDOT = -11564
971046 feet/sec YDOT = -3525
003175 meter/sec
ZDOT = 3766
901239 ZDOT = 1148
151498
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 20249
51912500
00016717 00000-0 10270-3 0 9030
2 25544 51
6437 310
9326 0001529 88
8021 271
3304 15
49239958 4465
Satellite: ISS
Catalog Number: 25544
Epoch time: 20249
51912500 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 310
9326 deg
Eccentricity:
0001529
Arg of perigee: 88
8021 deg
Mean anomaly: 271
3304 deg
Mean motion: 15
49239958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 446
Checksum: 299
Coasting Arc #5 (Orbit 460)
---------------------------------------
Vector Time (GMT): 2020/250/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4118870
45 A = 6792126
52 meter
Y = -1429175
27 meter E =
0015809
Z = -5222180
05 I = 51
30679
XDOT = 3666
622940 Wp = 82
23938
YDOT = -6625
027429 meter/sec RA = 305
51972 deg
ZDOT = -1079
594055 TA = 177
34588
MA = 177
33748
Ha = 229
339 n
mi
Hp = 221
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13513354
50 X = -4077216
47
Y = -4688895
23 feet Y = -1475002
86 meter
Z = -17133136
66 Z = -5242086
67
XDOT = 12029
602820 XDOT = 3745
677532
YDOT = -21735
654296 feet/sec YDOT = -6583
582672 meter/sec
ZDOT = -3541
975245 ZDOT = -1061
590585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9958683
78 X = 3035406
82
Y = 10112822
52 feet Y = 3082388
30 meter
Z = -17224874
41 Z = -5250141
72
XDOT = -19660
724786 XDOT = -5992
588915
YDOT = 13474
091003 feet/sec YDOT = 4106
902938 meter/sec
ZDOT = -3458
655947 ZDOT = -1054
198333
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 20250
48671710
00016717 00000-0 10270-3 0 9044
2 25544 51
6431 306
1449 0001562 88
4526 271
6803 15
49196025 4616
Satellite: ISS
Catalog Number: 25544
Epoch time: 20250
48671710 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 306
1449 deg
Eccentricity:
0001562
Arg of perigee: 88
4526 deg
Mean anomaly: 271
6803 deg
Mean motion: 15
49196025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 461
Checksum: 294
Coasting Arc #6 (Orbit 476)
---------------------------------------
Vector Time (GMT): 2020/251/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4177594
93 A = 6791925
52 meter
Y = 1159780
84 meter E =
0005007
Z = 5224285
71 I = 51
28812
XDOT = -3159
055575 Wp = 111
21360
YDOT = 6912
313710 meter/sec RA = 300
54851 deg
ZDOT = 989
067511 TA = 329
25196
MA = 329
28128
Ha = 229
149 n
mi
Hp = 221
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13706020
12 X = 4138938
74
Y = 3805055
24 feet Y = 1206281
83 meter
Z = 17140044
98 Z = 5244484
95
XDOT = -10364
355562 XDOT = -3240
920699
YDOT = 22678
194587 feet/sec YDOT = 6876
529202 meter/sec
ZDOT = 3244
972150 ZDOT = 973
522807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10681264
57 X = -3255649
44
Y = -9221929
48 feet Y = -2810844
11 meter
Z = 17233141
87 Z = 5252661
64
XDOT = 18370
065164 XDOT = 5599
195862
YDOT = -15332
101238 feet/sec YDOT = -4673
224457 meter/sec
ZDOT = 3172
993995 ZDOT = 967
128570
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 20251
51881123
00016717 00000-0 10270-3 0 9051
2 25544 51
6432 301
0380 0001641 89
2550 270
8789 15
49240091 4773
Satellite: ISS
Catalog Number: 25544
Epoch time: 20251
51881123 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 301
0380 deg
Eccentricity:
0001641
Arg of perigee: 89
2550 deg
Mean anomaly: 270
8789 deg
Mean motion: 15
49240091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 477
Checksum: 288
Coasting Arc #7 (Orbit 491)
---------------------------------------
Vector Time (GMT): 2020/252/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4234252
96 A = 6792003
63 meter
Y = -901643
73 meter E =
0016145
Z = -5247702
08 I = 51
27078
XDOT = 2620
819063 Wp = 84
04307
YDOT = -7129
958687 meter/sec RA = 295
57613 deg
ZDOT = -890
366065 TA = 177
37913
MA = 177
37066
Ha = 229
396 n
mi
Hp = 221
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13891906
04 X = -4198365
35
Y = -2958148
72 feet Y = -948793
71 meter
Z = -17216870
33 Z = -5268183
32
XDOT = 8598
487738 XDOT = 2704
678529
YDOT = -23392
252911 feet/sec YDOT = -7100
181955 meter/sec
ZDOT = -2921
148508 ZDOT = -877
431153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11354232
02 X = 3460769
92
Y = 8340108
09 feet Y = 2542064
95 meter
Z = -17311277
64 Z = -5276477
43
XDOT = -16833
845794 XDOT = -5130
956198
YDOT = 16983
665967 feet/sec YDOT = 5176
621387 meter/sec
ZDOT = -2861
209694 ZDOT = -872
096715
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 20252
48640135
00016717 00000-0 10270-3 0 9065
2 25544 51
6422 296
2505 0001728 92
6543 267
4804 15
49198502 4928
Satellite: ISS
Catalog Number: 25544
Epoch time: 20252
48640135 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 296
2505 deg
Eccentricity:
0001728
Arg of perigee: 92
6543 deg
Mean anomaly: 267
4804 deg
Mean motion: 15
49198502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 307
Coasting Arc #8 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2020/253/10:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2607661
53 A = 6803584
25 meter
Y = 6272760
92 meter E =
0012886
Z = -257977
72 I = 51
29717
XDOT = -4342
034342 Wp = 131
56583
YDOT = -2042
285693 meter/sec RA = 290
82960 deg
ZDOT = -5971
384024 TA = 51
22140
MA = 51
10635
Ha = 229
333 n
mi
Hp = 221
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8555319
97 X = -2676358
50
Y = 20579924
27 feet Y = 6243216
07 meter
Z = -846383
61 Z = -270811
76
XDOT = -14245
519494 XDOT = -4289
868481
YDOT = -6700
412378 feet/sec YDOT = -2090
549874 meter/sec
ZDOT = -19591
154934 ZDOT = -5992
349279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19774918
08 X = 6027395
03
Y = -10274982
72 feet Y = -3131814
73 meter
Z = -905810
72 Z = -276091
11
XDOT = 5756
861183 XDOT = 1754
691289
YDOT = 12760
333158 feet/sec YDOT = 3889
349547 meter/sec
ZDOT = -19687
749963 ZDOT = -6000
826189
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 20253
45398845
00016717 00000-0 10270-3 0 9072
2 25544 51
6426 291
4626 0001733 96
8781 263
2566 15
49226103 5074
Satellite: ISS
Catalog Number: 25544
Epoch time: 20253
45398845 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 291
4626 deg
Eccentricity:
0001733
Arg of perigee: 96
8781 deg
Mean anomaly: 263
2566 deg
Mean motion: 15
49226103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 320
Coasting Arc #9 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2020/254/10:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2103303
12 A = 6803676
64 meter
Y = -6455847
04 meter E =
0014010
Z = 323595
65 I = 51
28664
XDOT = 4470
267395 Wp = 53
48783
YDOT = 1764
109143 meter/sec RA = 285
85627 deg
ZDOT = 5966
277022 TA = 310
00993
MA = 310
13281
Ha = 229
411 n
mi
Hp = 221
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6900600
77 X = 2173766
17
Y = -21180600
52 feet Y = -6431932
41 meter
Z = 1061665
53 Z = 333983
88
XDOT = 14666
231612 XDOT = 4421
227523
YDOT = 5787
759655 feet/sec YDOT = 1813
824713 meter/sec
ZDOT = 19574
399677 ZDOT = 5987
872765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18686164
17 X = -5695542
84
Y = 12122658
76 feet Y = 3694986
39 meter
Z = 1109809
21 Z = 338269
85
XDOT = -6766
838150 XDOT = -2062
532268
YDOT = -12281
257541 feet/sec YDOT = -3743
327299 meter/sec
ZDOT = 19673
917633 ZDOT = 5996
610095
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 20254
48608038
00016717 00000-0 10270-3 0 9085
2 25544 51
6430 286
3554 0001747 91
3566 268
7785 15
49189925 5239
Satellite: ISS
Catalog Number: 25544
Epoch time: 20254
48608038 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 286
3554 deg
Eccentricity:
0001747
Arg of perigee: 91
3566 deg
Mean anomaly: 268
7785 deg
Mean motion: 15
49189925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 338
Coasting Arc #10 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2020/254/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3927120
79 A = 6792573
85 meter
Y = -1754849
05 meter E =
0015203
Z = -5270447
45 I = 51
24493
XDOT = 2328
279768 Wp = 94
81500
YDOT = -7253
915047 meter/sec RA = 283
68099 deg
ZDOT = 680
870351 TA = 181
73692
MA = 181
74220
Ha = 229
352 n
mi
Hp = 222
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12884254
56 X = -3881604
82
Y = -5757378
77 feet Y = -1798510
44 meter
Z = -17291494
27 Z = -5289413
34
XDOT = 7638
713149 XDOT = 2405
914901
YDOT = -23798
933882 feet/sec YDOT = -7227
444468 meter/sec
ZDOT = 2233
826610 ZDOT = 692
368814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -998805
14 X = -304435
81
Y = -13968673
08 feet Y = -4257651
56 meter
Z = -17378888
36 Z = -5297085
17
XDOT = 23544
342458 XDOT = 7176
315581
YDOT = -4527
119118 feet/sec YDOT = -1379
865907 meter/sec
ZDOT = 2287
113189 ZDOT = 697
112100
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 20254
87311373
00016717 00000-0 10270-3 0 9092
2 25544 51
6443 284
4426 0000634 84
4296 275
6926 15
48972191 5291
Satellite: ISS
Catalog Number: 25544
Epoch time: 20254
87311373 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 284
4426 deg
Eccentricity:
0000634
Arg of perigee: 84
4296 deg
Mean anomaly: 275
6926 deg
Mean motion: 15
48972191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 327
Coasting Arc #11 (Orbit 544)
---------------------------------------
Vector Time (GMT): 2020/255/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4057504
90 A = 6792480
57 meter
Y = 1406005
33 meter E =
0003548
Z = 5260153
69 I = 51
23746
XDOT = -1693
411844 Wp = 66
64869
YDOT = 7442
242038 meter/sec RA = 278
70890 deg
ZDOT = -681
273344 TA = 29
90852
MA = 29
88825
Ha = 229
122 n
mi
Hp = 222
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13312023
94 X = 4015930
20
Y = 4612878
37 feet Y = 1451146
79 meter
Z = 17257722
07 Z = 5279762
44
XDOT = -5555
813136 XDOT = -1773
198145
YDOT = 24416
804586 feet/sec YDOT = 7422
858981 meter/sec
ZDOT = -2235
148768 ZDOT = -689
693033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2446293
70 X = 745630
32
Y = 13761419
89 feet Y = 4194480
78 meter
Z = 17348099
87 Z = 5287700
84
XDOT = -22994
210202 XDOT = -7008
635270
YDOT = 6961
722352 feet/sec YDOT = 2121
932973 meter/sec
ZDOT = -2274
228137 ZDOT = -693
184736
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 20255
90538213
00016717 00000-0 10270-3 0 9103
2 25544 51
6436 279
3372 0000535 85
9083 274
2128 15
48999124 5458
Satellite: ISS
Catalog Number: 25544
Epoch time: 20255
90538213 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 279
3372 deg
Eccentricity:
0000535
Arg of perigee: 85
9083 deg
Mean anomaly: 274
2128 deg
Mean motion: 15
48999124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 545
Checksum: 315
Coasting Arc #12 (Orbit 559)
---------------------------------------
Vector Time (GMT): 2020/256/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4172742
44 A = 6792550
70 meter
Y = -1046282
71 meter E =
0015112
Z = -5269892
44 I = 51
23335
XDOT = 1037
857779 Wp = 94
98723
YDOT = -7547
801513 meter/sec RA = 273
73635 deg
ZDOT = 677
153072 TA = 181
53006
MA = 181
53469
Ha = 229
305 n
mi
Hp = 222
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13690099
86 X = -4135134
50
Y = -3432686
05 feet Y = -1092735
05 meter
Z = -17289673
38 Z = -5290070
52
XDOT = 3405
045206 XDOT = 1118
893226
YDOT = -24763
128325 feet/sec YDOT = -7535
742343 meter/sec
ZDOT = 2221
630815 ZDOT = 682
391403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3892065
07 X = -1186301
43
Y = -13447255
60 feet Y = -4098723
51 meter
Z = -17382695
98 Z = -5298245
74
XDOT = 22103
310469 XDOT = 6737
089031
YDOT = -9299
058892 feet/sec YDOT = -2834
353150 meter/sec
ZDOT = 2246
022947 ZDOT = 684
587794
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 20256
87313512
00016717 00000-0 10270-3 0 9114
2 25544 51
6434 274
5510 0000529 87
4982 272
6229 15
48978226 5606
Satellite: ISS
Catalog Number: 25544
Epoch time: 20256
87313512 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 274
5510 deg
Eccentricity:
0000529
Arg of perigee: 87
4982 deg
Mean anomaly: 272
6229 deg
Mean motion: 15
48978226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 560
Checksum: 314
Coasting Arc #13 (Orbit 575)
---------------------------------------
Vector Time (GMT): 2020/257/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4239966
40 A = 6792472
73 meter
Y = 681746
40 meter E =
0003387
Z = 5260075
65 I = 51
23273
XDOT = -381
029549 Wp = 67
02177
YDOT = 7623
042931 meter/sec RA = 268
76329 deg
ZDOT = -679
220162 TA = 29
51556
MA = 29
49644
Ha = 229
065 n
mi
Hp = 222
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13910650
92 X = 4206477
58
Y = 2236700
78 feet Y = 728973
60 meter
Z = 17257466
03 Z = 5280590
20
XDOT = -1250
096947 XDOT = -462
945156
YDOT = 25009
983368 feet/sec YDOT = 7618
323952 meter/sec
ZDOT = -2228
412605 ZDOT = -681
270147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5259222
82 X = 1603011
12
Y = 12945107
61 feet Y = 3945668
80 meter
Z = 17352058
60 Z = 5288907
46
XDOT = -21062
200071 XDOT = -6419
758582
YDOT = 11564
178039 feet/sec YDOT = 3524
761466 meter/sec
ZDOT = -2238
079892 ZDOT = -682
166751
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 20257
90540068
00016717 00000-0 10270-3 0 9128
2 25544 51
6438 269
4453 0000403 92
8482 267
2714 15
49000092 5769
Satellite: ISS
Catalog Number: 25544
Epoch time: 20257
90540068 = yrday
fracday
Element set: 912
Inclination: 51
6438 deg
RA of node: 269
4453 deg
Eccentricity:
0000403
Arg of perigee: 92
8482 deg
Mean anomaly: 267
2714 deg
Mean motion: 15
49000092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 576
Checksum: 301
Coasting Arc #14 (Orbit 590)
---------------------------------------
Vector Time (GMT): 2020/258/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4290666
31 A = 6792522
10 meter
Y = -310749
93 meter E =
0015058
Z = -5269816
75 I = 51
23417
XDOT = -280
800117 Wp = 94
79308
YDOT = -7613
626336 meter/sec RA = 263
78959 deg
ZDOT = 678
036035 TA = 181
73233
MA = 181
73755
Ha = 229
271 n
mi
Hp = 222
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14076989
20 X = -4261275
04
Y = -1019520
75 feet Y = -358567
12 meter
Z = -17289425
04 Z = -5290587
51
XDOT = -921
260225 XDOT = -198
934863
YDOT = -24979
089030 feet/sec YDOT = -7616
308677 meter/sec
ZDOT = 2224
527674 ZDOT = 676
871193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6598621
64 X = -2011259
88
Y = -12342517
96 feet Y = -3761999
47 meter
Z = -17385215
24 Z = -5299013
61
XDOT = 19710
684110 XDOT = 6007
816517
YDOT = -13661
843640 feet/sec YDOT = -4164
129941 meter/sec
ZDOT = 2219
342000 ZDOT = 676
455442
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 20258
87314890
00016717 00000-0 10270-3 0 9138
2 25544 51
6432 264
6581 0000481 79
6984 280
4221 15
48986738 5914
Satellite: ISS
Catalog Number: 25544
Epoch time: 20258
87314890 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 264
6581 deg
Eccentricity:
0000481
Arg of perigee: 79
6984 deg
Mean anomaly: 280
4221 deg
Mean motion: 15
48986738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 591
Checksum: 336
Coasting Arc #15 (Orbit 606)
---------------------------------------
Vector Time (GMT): 2020/259/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4293948
20 A = 6792494
71 meter
Y = -57101
72 meter E =
0003452
Z = 5260136
10 I = 51
23821
XDOT = 938
878575 Wp = 66
98098
YDOT = 7574
327611 meter/sec RA = 258
81648 deg
ZDOT = -682
515015 TA = 29
58783
MA = 29
56830
Ha = 229
099 n
mi
Hp = 222
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14087756
57 X = 4268717
12
Y = -187341
61 feet Y = -9224
43 meter
Z = 17257664
37 Z = 5280932
93
XDOT = 3080
310287 XDOT = 857
425621
YDOT = 24850
156203 feet/sec YDOT = 7584
371344 meter/sec
ZDOT = -2239
222489 ZDOT = -678
152708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7824732
37 X = 2384978
43
Y = 11573829
05 feet Y = 3527703
10 meter
Z = 17353587
70 Z = 5289373
53
XDOT = -18227
358998 XDOT = -5555
699023
YDOT = 15658
758872 feet/sec YDOT = 4772
789704 meter/sec
ZDOT = -2219
261517 ZDOT = -676
430910
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 20259
90541094
00016717 00000-0 10270-3 0 9142
2 25544 51
6424 259
5521 0000464 87
1354 272
9849 15
48991850 6079
Satellite: ISS
Catalog Number: 25544
Epoch time: 20259
90541094 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 259
5521 deg
Eccentricity:
0000464
Arg of perigee: 87
1354 deg
Mean anomaly: 272
9849 deg
Mean motion: 15
48991850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 607
Checksum: 325
Coasting Arc #16 (Orbit 621)
---------------------------------------
Vector Time (GMT): 2020/260/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4279887
68 A = 6792516
17 meter
Y = 429953
58 meter E =
0015031
Z = -5270174
00 I = 51
24518
XDOT = -1588
320339 Wp = 95
02001
YDOT = -7451
027635 meter/sec RA = 253
84329 deg
ZDOT = 682
397025 TA = 181
54682
MA = 181
55147
Ha = 229
257 n
mi
Hp = 222
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14041626
24 X = -4258778
14
Y = 1410608
87 feet Y = 382210
36 meter
Z = -17290597
12 Z = -5290912
65
XDOT = -5211
024735 XDOT = -1508
197332
YDOT = -24445
628725 feet/sec YDOT = -7468
341314 meter/sec
ZDOT = 2238
835383 ZDOT = 674
876917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9007306
36 X = -2745426
98
Y = -10710189
82 feet Y = -3264465
86 meter
Z = -17386261
81 Z = -5299332
60
XDOT = 16473
966129 XDOT = 5021
264876
YDOT = -17430
831102 feet/sec YDOT = -5312
917320 meter/sec
ZDOT = 2204
281176 ZDOT = 671
864902
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 20260
87315675
00016717 00000-0 10270-3 0 9155
2 25544 51
6416 254
7648 0000443 84
4819 275
6381 15
48988253 6221
Satellite: ISS
Catalog Number: 25544
Epoch time: 20260
87315675 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 254
7648 deg
Eccentricity:
0000443
Arg of perigee: 84
4819 deg
Mean anomaly: 275
6381 deg
Mean motion: 15
48988253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 622
Checksum: 330
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