[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 26th 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) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 431 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
270/23:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 222
5
274/02:27:04
299 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 222
7
277/05:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 222
6
277/09:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 222
6
280/09:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 222
6
281/08:14:18
140 -2
2 -2
5 2
5
N/A 1
1 -0
0 228
2
000/00:06:36
280 0
1 -0
0 222
7
283/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 222
7
Coasting Arc #1 (Orbit 755)
---------------------------------------
Vector Time (GMT): 2020/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -628911
42 A = 6793781
45 meter
Y = 4407846
26 meter E =
0014807
Z = -5144630
07 I = 51
41934
XDOT = -6967
875368 Wp = 79
63686
YDOT = -2764
569698 meter/sec RA = 210
93748 deg
ZDOT = -1517
982543 TA = 175
66202
MA = 175
64917
Ha = 229
890 n
mi
Hp = 222
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2063357
67 X = -653164
89
Y = 14461437
86 feet Y = 4400677
61 meter
Z = -16878707
59 Z = -5147744
07
XDOT = -22860
483491 XDOT = -6929
069768
YDOT = -9070
110559 feet/sec YDOT = -2842
272527 meter/sec
ZDOT = -4980
257688 ZDOT = -1551
735412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 969537
03 X = 295514
89
Y = -14559008
06 feet Y = -4437585
66 meter
Z = -16893095
69 Z = -5149015
57
XDOT = 22323
286411 XDOT = 6804
137698
YDOT = 7441
741203 feet/sec YDOT = 2268
242719 meter/sec
ZDOT = -5136
059486 ZDOT = -1565
470931
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 20269
51887007
00016717 00000-0 10270-3 0 9002
2 25544 51
6410 212
0033 0001279 90
6546 269
4751 15
48782244 7566
Satellite: ISS
Catalog Number: 25544
Epoch time: 20269
51887007 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 212
0033 deg
Eccentricity:
0001279
Arg of perigee: 90
6546 deg
Mean anomaly: 269
4751 deg
Mean motion: 15
48782244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 756
Checksum: 302
Coasting Arc #2 (Orbit 771)
---------------------------------------
Vector Time (GMT): 2020/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 162277
02 A = 6793737
14 meter
Y = -4458931
41 meter E =
0006012
Z = 5119304
86 I = 51
44985
XDOT = 7196
841048 Wp = 119
67019
YDOT = 2095
384247 meter/sec RA = 205
98093 deg
ZDOT = 1592
626073 TA = 314
89391
MA = 314
94270
Ha = 229
758 n
mi
Hp = 222
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 532404
94 X = 187259
51
Y = -14629040
07 feet Y = -4456976
86 meter
Z = 16795619
63 Z = 5120153
96
XDOT = 23611
683229 XDOT = 7165
138909
YDOT = 6874
620233 feet/sec YDOT = 2175
687277 meter/sec
ZDOT = 5225
151159 ZDOT = 1627
508316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 820084
40 X = 249961
73
Y = 14611223
32 feet Y = 4453500
87 meter
Z = 16799545
28 Z = 5120501
40
XDOT = -23006
545748 XDOT = -7012
395144
YDOT = -4917
917093 feet/sec YDOT = -1498
981130 meter/sec
ZDOT = 5386
195039 ZDOT = 1641
712248
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 20270
55125507
00016717 00000-0 10270-3 0 9019
2 25544 51
6417 206
8988 0001122 92
9751 267
1527 15
48821321 7727
Satellite: ISS
Catalog Number: 25544
Epoch time: 20270
55125507 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 206
8988 deg
Eccentricity:
0001122
Arg of perigee: 92
9751 deg
Mean anomaly: 267
1527 deg
Mean motion: 15
48821321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 772
Checksum: 300
Coasting Arc #3 (Orbit 778)
---------------------------------------
Vector Time (GMT): 2020/270/23:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4996791
93 A = 6796870
12 meter
Y = 1590635
45 meter E =
0010105
Z = -4334740
52 I = 51
47635
XDOT = -4609
918907 Wp = 111
35180
YDOT = -5020
458934 meter/sec RA = 203
49647 deg
ZDOT = 3474
701948 TA = 194
12210
MA = 194
15038
Ha = 229
867 n
mi
Hp = 222
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16393674
30 X = -4993151
92
Y = 5218620
25 feet Y = 1534777
92 meter
Z = -14221589
63 Z = -4359004
10
XDOT = -15124
405863 XDOT = -4570
314051
YDOT = -16471
321963 feet/sec YDOT = -5071
788763 meter/sec
ZDOT = 11399
940773 ZDOT = 3452
405261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16018175
08 X = -4882339
76
Y = 6017108
09 feet Y = 1834014
55 meter
Z = -14333619
34 Z = -4368887
17
XDOT = -15558
829523 XDOT = -4742
331239
YDOT = -14531
150397 feet/sec YDOT = -4429
094641 meter/sec
ZDOT = 11296
994784 ZDOT = 3443
324010
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 20271
00292477
00016717 00000-0 10270-3 0 9022
2 25544 51
6427 204
6619 0001374 113
6972 246
4323 15
48789530 7796
Satellite: ISS
Catalog Number: 25544
Epoch time: 20271
00292477 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 204
6619 deg
Eccentricity:
0001374
Arg of perigee: 113
6972 deg
Mean anomaly: 246
4323 deg
Mean motion: 15
48789530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 779
Checksum: 312
Coasting Arc #4 (Orbit 794)
---------------------------------------
Vector Time (GMT): 2020/271/23:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4788916
80 A = 6796831
79 meter
Y = -2049546
96 meter E =
0010571
Z = 4358538
55 I = 51
50725
XDOT = 5092
839413 Wp = 77
16994
YDOT = 4585
340526 meter/sec RA = 198
54210 deg
ZDOT = -3430
188420 TA = 47
75632
MA = 47
66669
Ha = 229
846 n
mi
Hp = 222
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15711669
29 X = 4790308
32
Y = -6724235
44 feet Y = -1995985
82 meter
Z = 14299667
16 Z = 4381804
64
XDOT = 16708
790725 XDOT = 5057
848073
YDOT = 15043
768129 feet/sec YDOT = 4642
096451 meter/sec
ZDOT = -11253
899017 ZDOT = -3405
534765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15131012
56 X = 4611932
63
Y = -7748564
37 feet Y = -2361762
42 meter
Z = 14407101
86 Z = 4391284
65
XDOT = 17185
005408 XDOT = 5237
989648
YDOT = 12788
508562 feet/sec YDOT = 3897
937410 meter/sec
ZDOT = -11140
047975 ZDOT = -3395
486623
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 20272
03530981
00016717 00000-0 10270-3 0 9032
2 25544 51
6425 199
5569 0001535 116
4722 243
6585 15
48765129 7958
Satellite: ISS
Catalog Number: 25544
Epoch time: 20272
03530981 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 199
5569 deg
Eccentricity:
0001535
Arg of perigee: 116
4722 deg
Mean anomaly: 243
6585 deg
Mean motion: 15
48765129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 795
Checksum: 324
Coasting Arc #5 (Orbit 809)
---------------------------------------
Vector Time (GMT): 2020/272/23:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4535369
07 A = 6796566
79 meter
Y = 2506274
44 meter E =
0010477
Z = -4408757
20 I = 51
54003
XDOT = -5524
952847 Wp = 112
38934
YDOT = -4084
746882 meter/sec RA = 193
59100 deg
ZDOT = 3364
061730 TA = 191
76247
MA = 191
78696
Ha = 229
822 n
mi
Hp = 222
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14879819
77 X = -4541642
72
Y = 8222685
19 feet Y = 2455521
27 meter
Z = -14464426
50 Z = -4430803
63
XDOT = -18126
485717 XDOT = -5495
206007
YDOT = -13401
400530 feet/sec YDOT = -4146
364278 meter/sec
ZDOT = 11036
947933 ZDOT = 3337
296299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14039950
74 X = -4279376
99
Y = 9431105
16 feet Y = 2874600
85 meter
Z = -14566237
00 Z = -4439789
04
XDOT = -18572
289173 XDOT = -5660
833740
YDOT = -10805
490949 feet/sec YDOT = -3293
513641 meter/sec
ZDOT = 10913
325310 ZDOT = 3326
381555
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 20273
00316723
00016717 00000-0 10270-3 0 9047
2 25544 51
6434 194
7720 0001370 121
2594 238
8690 15
48803748 8103
Satellite: ISS
Catalog Number: 25544
Epoch time: 20273
00316723 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 194
7720 deg
Eccentricity:
0001370
Arg of perigee: 121
2594 deg
Mean anomaly: 238
8690 deg
Mean motion: 15
48803748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 810
Checksum: 294
Coasting Arc #6 (Orbit 825)
---------------------------------------
Vector Time (GMT): 2020/273/23:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4245365
11 A = 6796498
38 meter
Y = -2910614
15 meter E =
0010101
Z = 4431120
99 I = 51
57353
XDOT = 5917
027856 Wp = 75
85108
YDOT = 3563
109559 meter/sec RA = 188
64078 deg
ZDOT = -3319
749099 TA = 47
76231
MA = 47
67666
Ha = 229
766 n
mi
Hp = 222
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13928363
23 X = 4256073
07
Y = -9549259
01 feet Y = -2863079
15 meter
Z = 14537798
52 Z = 4451769
61
XDOT = 19412
821049 XDOT = 5892
869791
YDOT = 11689
991991 feet/sec YDOT = 3629
142628 meter/sec
ZDOT = -10891
565284 ZDOT = -3291
065461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12794733
41 X = 3899834
74
Y = -10894983
58 feet Y = -3320790
99 meter
Z = 14633159
80 Z = 4460187
11
XDOT = 19772
269560 XDOT = 6026
587762
YDOT = 8730
907583 feet/sec YDOT = 2661
180631 meter/sec
ZDOT = -10759
066763 ZDOT = -3279
363549
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20274
03554720
00016717 00000-0 10270-3 0 9053
2 25544 51
6441 189
6667 0001410 119
6878 240
4413 15
48791000 8261
Satellite: ISS
Catalog Number: 25544
Epoch time: 20274
03554720 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 189
6667 deg
Eccentricity:
0001410
Arg of perigee: 119
6878 deg
Mean anomaly: 240
4413 deg
Mean motion: 15
48791000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 826
Checksum: 298
Coasting Arc #7 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2020/274/02:27:04
299
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6457645
52 A = 6804486
75 meter
Y = -1811452
66 meter E =
0014388
Z = 1109466
02 I = 51
60221
XDOT = 2245
840204 Wp = 60
96063
YDOT = -4379
184070 meter/sec RA = 188
13627 deg
ZDOT = 5871
030453 TA = 311
05877
MA = 311
18300
Ha = 229
898 n
mi
Hp = 222
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21186501
04 X = -6442298
52
Y = -5943086
16 feet Y = -1883580
77 meter
Z = 3639980
40 Z = 1078134
70
XDOT = 7368
242138 XDOT = 2266
124484
YDOT = -14367
401803 feet/sec YDOT = -4353
955512 meter/sec
ZDOT = 19261
910935 ZDOT = 5881
989556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19169372
55 X = -5842824
75
Y = 10851538
44 feet Y = 3307548
92 meter
Z = 3495257
64 Z = 1065354
53
XDOT = -4294
632345 XDOT = -1309
003939
YDOT = -13863
029594 feet/sec YDOT = -4225
451420 meter/sec
ZDOT = 19312
512392 ZDOT = 5886
453777
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20274
16459463
00016717 00000-0 10270-3 0 9066
2 25544 51
6430 189
0303 0001252 107
5978 252
5309 15
48766229 8286
Satellite: ISS
Catalog Number: 25544
Epoch time: 20274
16459463 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 189
0303 deg
Eccentricity:
0001252
Arg of perigee: 107
5978 deg
Mean anomaly: 252
5309 deg
Mean motion: 15
48766229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 316
Coasting Arc #8 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2020/275/02:27:04
299
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6603480
15 A = 6804389
98 meter
Y = 1218171
92 meter E =
0010794
Z = -1072548
06 I = 51
63613
XDOT = -1790
773654 Wp = 138
08009
YDOT = 4564
501247 meter/sec RA = 183
18852 deg
ZDOT = -5883
340711 TA = 53
52476
MA = 53
42534
Ha = 229
885 n
mi
Hp = 222
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21664961
11 X = 6594577
25
Y = 3996627
02 feet Y = 1291966
88 meter
Z = -3518858
45 Z = -1040492
49
XDOT = -5875
241648 XDOT = -1813
104107
YDOT = 14975
397793 feet/sec YDOT = 4544
350096 meter/sec
ZDOT = -19302
298920 ZDOT = -5892
094325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17907025
83 X = 5458061
47
Y = -12872537
56 feet Y = -3923549
45 meter
Z = -3370776
60 Z = -1027412
71
XDOT = 5881
937363 XDOT = 1792
814508
YDOT = 13209
650181 feet/sec YDOT = 4026
301375 meter/sec
ZDOT = -19342
714416 ZDOT = -5895
659354
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20275
13244661
00016717 00000-0 10270-3 0 9077
2 25544 51
6432 184
2446 0001334 109
1645 250
9650 15
48808698 8438
Satellite: ISS
Catalog Number: 25544
Epoch time: 20275
13244661 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 184
2446 deg
Eccentricity:
0001334
Arg of perigee: 109
1645 deg
Mean anomaly: 250
9650 deg
Mean motion: 15
48808698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 309
Coasting Arc #9 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2020/276/02:27:04
299
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6699869
74 A = 6804593
87 meter
Y = -581309
28 meter E =
0014336
Z = 994693
84 I = 51
66925
XDOT = 1293
331656 Wp = 59
89797
YDOT = -4708
763230 meter/sec RA = 178
24325 deg
ZDOT = 5902
805450 TA = 310
85199
MA = 310
97617
Ha = 229
933 n
mi
Hp = 222
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21981199
94 X = -6697703
12
Y = -1907182
68 feet Y = -656219
82 meter
Z = 3263431
22 Z = 962153
46
XDOT = 4243
214095 XDOT = 1317
217578
YDOT = -15448
698260 feet/sec YDOT = -4694
166143 meter/sec
ZDOT = 19366
159612 ZDOT = 5909
146484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16365366
79 X = -4988163
80
Y = 14830504
90 feet Y = 4520337
89 meter
Z = 3113097
15 Z = 948872
01
XDOT = -7445
212054 XDOT = -2269
300634
YDOT = -12328
023273 feet/sec YDOT = -3757
581494 meter/sec
ZDOT = 19395
432561 ZDOT = 5911
727845
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20276
16482326
00016717 00000-0 10270-3 0 9084
2 25544 51
6422 179
1403 0001332 106
2089 253
9208 15
48763320 8592
Satellite: ISS
Catalog Number: 25544
Epoch time: 20276
16482326 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 179
1403 deg
Eccentricity:
0001332
Arg of perigee: 106
2089 deg
Mean anomaly: 253
9208 deg
Mean motion: 15
48763320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 300
Coasting Arc #10 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2020/277/02:27:04
299
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6731807
13 A = 6804448
90 meter
Y = -28720
84 meter E =
0011165
Z = -958548
53 I = 51
70370
XDOT = -814
837285 Wp = 138
31474
YDOT = 4797
883121 meter/sec RA = 173
29970 deg
ZDOT = -5914
084537 TA = 52
03282
MA = 51
93200
Ha = 229
853 n
mi
Hp = 222
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22085981
39 X = 6736284
12
Y = -94228
49 feet Y = 46584
00 meter
Z = -3144844
26 Z = -925836
68
XDOT = -2673
350672 XDOT = -839
700423
YDOT = 15741
086356 feet/sec YDOT = 4788
631484 meter/sec
ZDOT = -19403
164491 ZDOT = -5918
103570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14687051
09 X = 4476613
17
Y = -16523249
10 feet Y = -5036286
33 meter
Z = -2993704
72 Z = -912481
20
XDOT = 8818
895117 XDOT = 2687
999232
YDOT = 11327
877414 feet/sec YDOT = 3452
737036 meter/sec
ZDOT = -19421
713666 ZDOT = -5919
738326
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20277
13267128
00016717 00000-0 10270-3 0 9094
2 25544 51
6429 174
3542 0001332 114
5524 245
5761 15
48820786 8744
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
13267128 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 174
3542 deg
Eccentricity:
0001332
Arg of perigee: 114
5524 deg
Mean anomaly: 245
5761 deg
Mean motion: 15
48820786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 312
Coasting Arc #11 (Orbit 875)
---------------------------------------
Vector Time (GMT): 2020/277/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1726187
62 A = 6794218
75 meter
Y = 4239233
04 meter E =
0014145
Z = -5033981
40 I = 51
67165
XDOT = -7357
216225 Wp = 105
51106
YDOT = -628
337240 meter/sec RA = 172
55043 deg
ZDOT = 1994
699845 TA = 183
90045
MA = 183
91148
Ha = 229
866 n
mi
Hp = 222
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5663345
20 X = -1749011
12
Y = 13908244
87 feet Y = 4219801
52 meter
Z = -16515687
00 Z = -5042422
48
XDOT = -24137
848507 XDOT = -7359
332427
YDOT = -2061
473884 feet/sec YDOT = -710
622569 meter/sec
ZDOT = 6544
290829 ZDOT = 1958
955726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14717032
36 X = 4485751
46
Y = 2762697
28 feet Y = 842070
13 meter
Z = -16554671
05 Z = -5045863
74
XDOT = 2844
615992 XDOT = 867
038955
YDOT = 23052
187416 feet/sec YDOT = 7026
306725 meter/sec
ZDOT = 6379
135828 ZDOT = 1944
360600
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20277
26171779
00016717 00000-0 10270-3 0 9106
2 25544 51
6402 173
7170 0001288 110
5989 249
5299 15
48783256 8768
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
26171779 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 173
7170 deg
Eccentricity:
0001288
Arg of perigee: 110
5989 deg
Mean anomaly: 249
5299 deg
Mean motion: 15
48783256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 876
Checksum: 338
Coasting Arc #12 (Orbit 877)
---------------------------------------
Vector Time (GMT): 2020/277/09:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5580459
21 A = 6801915
15 meter
Y = 2881200
50 meter E =
0005706
Z = -2612633
74 I = 51
70343
XDOT = -4290
172444 Wp = 63
60429
YDOT = -3567
515667 meter/sec RA = 171
87022 deg
ZDOT = 5240
719122 TA = 267
09423
MA = 267
15953
Ha = 229
760 n
mi
Hp = 222
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18308593
22 X = -5599572
02
Y = 9452757
55 feet Y = 2818688
71 meter
Z = -8571632
99 Z = -2639788
53
XDOT = -14075
368910 XDOT = -4275
417383
YDOT = -11704
447728 feet/sec YDOT = -3615
408505 meter/sec
ZDOT = 17193
960375 ZDOT = 5219
914951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20536570
14 X = 6259546
58
Y = 801262
06 feet Y = 244224
68 meter
Z = -8697089
69 Z = -2650872
94
XDOT = 6613
047493 XDOT = 2015
656876
YDOT = 15690
930559 feet/sec YDOT = 4782
595634 meter/sec
ZDOT = 17097
820916 ZDOT = 5211
415815
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20277
39076485
00016717 00000-0 10270-3 0 9119
2 25544 51
6416 173
0790 0001105 108
1770 251
9500 15
48794893 8786
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
39076485 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 173
0790 deg
Eccentricity:
0001105
Arg of perigee: 108
1770 deg
Mean anomaly: 251
9500 deg
Mean motion: 15
48794893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 878
Checksum: 319
Coasting Arc #13 (Orbit 893)
---------------------------------------
Vector Time (GMT): 2020/278/09:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5276391
88 A = 6801796
68 meter
Y = -3366782
17 meter E =
0014603
Z = 2645271
43 I = 51
73723
XDOT = 4639
137101 Wp = 102
83384
YDOT = 3150
985115 meter/sec RA = 166
92967 deg
ZDOT = -5221
873139 TA = 47
44356
MA = 47
32039
Ha = 229
712 n
mi
Hp = 222
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17310996
99 X = 5300798
64
Y = -11045873
27 feet Y = -3307641
12 meter
Z = 8678712
03 Z = 2670962
09
XDOT = 15220
266079 XDOT = 4628
922408
YDOT = 10337
877675 feet/sec YDOT = 3202
805786 meter/sec
ZDOT = -17132
129720 ZDOT = -5199
362629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20434431
64 X = -6228414
76
Y = 1428777
75 feet Y = 435491
46 meter
Z = 8797418
56 Z = 2681453
18
XDOT = -8404
446135 XDOT = -2561
675182
YDOT = -14931
988734 feet/sec YDOT = -4551
270166 meter/sec
ZDOT = -17028
098918 ZDOT = -5190
164550
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20278
42313415
00016717 00000-0 10270-3 0 9122
2 25544 51
6423 167
9736 0001105 106
8844 253
2427 15
48813510 8942
Satellite: ISS
Catalog Number: 25544
Epoch time: 20278
42313415 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 167
9736 deg
Eccentricity:
0001105
Arg of perigee: 106
8844 deg
Mean anomaly: 253
2427 deg
Mean motion: 15
48813510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 894
Checksum: 298
Coasting Arc #14 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2020/279/09:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4912501
63 A = 6801662
88 meter
Y = 3844183
67 meter E =
0005583
Z = -2712737
56 I = 51
76847
XDOT = -4954
556826 Wp = 67
02596
YDOT = -2682
133886 meter/sec RA = 161
99162 deg
ZDOT = 5182
025497 TA = 262
46340
MA = 262
52683
Ha = 229
748 n
mi
Hp = 222
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16117131
33 X = -4941946
14
Y = 12612151
15 feet Y = 3789083
77 meter
Z = -8900057
61 Z = -2736672
80
XDOT = -16255
107698 XDOT = -4949
368009
YDOT = -8799
651858 feet/sec YDOT = -2737
509999 meter/sec
ZDOT = 17001
395988 ZDOT = 5157
970444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20074677
13 X = 6118761
59
Y = -3722160
76 feet Y = -1134514
60 meter
Z = -9010669
34 Z = -2746452
01
XDOT = 10148
048431 XDOT = 3093
125162
YDOT = 13926
549052 feet/sec YDOT = 4244
812151 meter/sec
ZDOT = 16890
219037 ZDOT = 5148
138762
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20279
39097841
00016717 00000-0 10270-3 0 9132
2 25544 51
6414 163
1879 0001113 108
3034 251
8237 15
48806999 9098
Satellite: ISS
Catalog Number: 25544
Epoch time: 20279
39097841 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 163
1879 deg
Eccentricity:
0001113
Arg of perigee: 108
3034 deg
Mean anomaly: 251
8237 deg
Mean motion: 15
48806999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 909
Checksum: 324
Coasting Arc #15 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2020/280/09:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4525767
98 A = 6801582
77 meter
Y = -4260994
18 meter E =
0014474
Z = 2744388
49 I = 51
80018
XDOT = 5216
828288 Wp = 101
96942
YDOT = 2203
047940 meter/sec RA = 157
05602 deg
ZDOT = -5162
470566 TA = 47
10338
MA = 46
98197
Ha = 229
706 n
mi
Hp = 222
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14848320
15 X = 4559748
38
Y = -13979639
70 feet Y = -4210193
70 meter
Z = 9003899
24 Z = 2766456
05
XDOT = 17115
578373 XDOT = 5216
882277
YDOT = 7227
847572 feet/sec YDOT = 2261
386372 meter/sec
ZDOT = -16937
239390 ZDOT = -5137
128668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19486718
70 X = -5939551
86
Y = 5858630
15 feet Y = 1785710
47 meter
Z = 9105898
43 Z = 2775477
84
XDOT = -11729
282089 XDOT = -3575
085181
YDOT = -12769
090279 feet/sec YDOT = -3892
018717 meter/sec
ZDOT = -16820
103895 ZDOT = -5126
767667
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20280
42334491
00016717 00000-0 10270-3 0 9144
2 25544 51
6416 158
0831 0001098 113
4379 246
6886 15
48812628 9258
Satellite: ISS
Catalog Number: 25544
Epoch time: 20280
42334491 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 158
0831 deg
Eccentricity:
0001098
Arg of perigee: 113
4379 deg
Mean anomaly: 246
6886 deg
Mean motion: 15
48812628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 316
Coasting Arc #16 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2020/280/09:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3493751
00 A = 6799215
69 meter
Y = 4583079
04 meter E =
0006528
Z = -3614888
87 I = 51
79408
XDOT = -6126
453435 Wp = 101
72559
YDOT = -1179
281089 meter/sec RA = 156
90406 deg
ZDOT = 4431
510167 TA = 215
72424
MA = 215
76793
Ha = 229
719 n
mi
Hp = 222
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11462437
66 X = -3527181
27
Y = 15036348
56 feet Y = 4543822
36 meter
Z = -11859871
62 Z = -3631941
86
XDOT = -20099
912845 XDOT = -6134
337224
YDOT = -3869
032444 feet/sec YDOT = -1247
835409 meter/sec
ZDOT = 14539
075352 ZDOT = 4401
730518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15035996
40 X = 4582971
70
Y = -11380783
39 feet Y = -3468862
78 meter
Z = -11938693
04 Z = -3638913
64
XDOT = 17559
849683 XDOT = 5352
242183
YDOT = 8110
979742 feet/sec YDOT = 2472
226625 meter/sec
ZDOT = 14401
427537 ZDOT = 4389
555113
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20280
42334478
00016717 00000-0 10270-3 0 9150
2 25544 51
6423 158
0831 0001119 114
5514 245
5752 15
48825485 9258
Satellite: ISS
Catalog Number: 25544
Epoch time: 20280
42334478 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 158
0831 deg
Eccentricity:
0001119
Arg of perigee: 114
5514 deg
Mean anomaly: 245
5752 deg
Mean motion: 15
48825485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 302
Coasting Arc #17 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2020/281/08:17:36
280
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -214524
25 A = 6792319
82 meter
Y = -4444902
86 meter E =
0003839
Z = 5129582
58 I = 51
80312
XDOT = 7129
458264 Wp = 50
00985
YDOT = -2263
643689 meter/sec RA = 152
32819 deg
ZDOT = -1660
110911 TA = 56
01155
MA = 55
97508
Ha = 228
218 n
mi
Hp = 222
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -703819
72 X = -189721
14
Y = -14583014
65 feet Y = -4447163
05 meter
Z = 16829339
16 Z = 5128600
81
XDOT = 23390
611103 XDOT = 7162
305161
YDOT = -7426
652522 feet/sec YDOT = -2183
733347 meter/sec
ZDOT = -5446
558106 ZDOT = -1625
398281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8758588
56 X = -2669617
79
Y = 11687572
53 feet Y = 3562372
11 meter
Z = 16824806
38 Z = 5128200
99
XDOT = -21857
873348 XDOT = -6662
279797
YDOT = -8755
326696 feet/sec YDOT = -2668
623577 meter/sec
ZDOT = -5286
085676 ZDOT = -1611
198914
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20281
39116770
00016717 00000-0 10270-3 0 9161
2 25544 51
6413 153
2970 0001196 253
0347 107
0672 15
49294451 9400
Satellite: ISS
Catalog Number: 25544
Epoch time: 20281
39116770 = yrday
fracday
Element set: 916
Inclination: 51
6413 deg
RA of node: 153
2970 deg
Eccentricity:
0001196
Arg of perigee: 253
0347 deg
Mean anomaly: 107
0672 deg
Mean motion: 15
49294451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 295
Coasting Arc #18 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2020/282/08:17:36
280
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 479544
30 A = 6792448
15 meter
Y = 4461455
88 meter E =
0012261
Z = -5110377
71 I = 51
83364
XDOT = -6909
381280 Wp = 105
50415
YDOT = 2769
188823 meter/sec RA = 147
39099 deg
ZDOT = 1769
545222 TA = 181
60149
MA = 181
60542
Ha = 228
203 n
mi
Hp = 222
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1573308
09 X = 454443
04
Y = 14637322
45 feet Y = 4466678
11 meter
Z = -16766331
07 Z = -5108109
23
XDOT = -22668
573752 XDOT = -6948
429248
YDOT = 9085
265167 feet/sec YDOT = 2691
704848 meter/sec
ZDOT = 5805
594561 ZDOT = 1735
886718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7915841
25 X = 2412748
41
Y = -12426468
60 feet Y = -3787587
63 meter
Z = -16755855
69 Z = -5107184
81
XDOT = 22449
146087 XDOT = 6842
499727
YDOT = 6683
560134 feet/sec YDOT = 2037
149129 meter/sec
ZDOT = 5649
967592 ZDOT = 1722
110122
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20282
35871082
00016717 00000-0 10270-3 0 9173
2 25544 51
6421 148
5080 0001137 259
3813 100
7209 15
49295212 9558
Satellite: ISS
Catalog Number: 25544
Epoch time: 20282
35871082 = yrday
fracday
Element set: 917
Inclination: 51
6421 deg
RA of node: 148
5080 deg
Eccentricity:
0001137
Arg of perigee: 259
3813 deg
Mean anomaly: 100
7209 deg
Mean motion: 15
49295212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 295
Coasting Arc #19 (Orbit 970)
---------------------------------------
Vector Time (GMT): 2020/283/08:17:36
280
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -737197
86 A = 6792534
54 meter
Y = -4455631
04 meter E =
0004586
Z = 5071586
73 I = 51
86178
XDOT = 6672
924928 Wp = 48
67822
YDOT = -3258
133721 meter/sec RA = 142
45777 deg
ZDOT = -1888
402188 TA = 59
60564
MA = 59
56032
Ha = 228
208 n
mi
Hp = 222
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2418628
14 X = -711954
06
Y = -14618212
07 feet Y = -4463733
76 meter
Z = 16639064
07 Z = 5068066
98
XDOT = 21892
798321 XDOT = 6718
035316
YDOT = -10689
415094 feet/sec YDOT = -3183
260064 meter/sec
ZDOT = -6195
545236 ZDOT = -1855
877720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7024531
93 X = -2141077
33
Y = 13066696
22 feet Y = 3982729
01 meter
Z = 16622807
84 Z = 5066631
83
XDOT = -22905
077601 XDOT = -6981
467653
YDOT = -4606
277991 feet/sec YDOT = -1403
993532 meter/sec
ZDOT = -6045
133295 ZDOT = -1842
556628
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20283
39075495
00016717 00000-0 10270-3 0 9183
2 25544 51
6419 143
4018 0001131 267
1849 92
9171 15
49311723 9714
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
39075495 = yrday
fracday
Element set: 918
Inclination: 51
6419 deg
RA of node: 143
4018 deg
Eccentricity:
0001131
Arg of perigee: 267
1849 deg
Mean anomaly: 92
9171 deg
Mean motion: 15
49311723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 971
Checksum: 311
Coasting Arc #20 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2020/283/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3033950
06 A = 6791419
06 meter
Y = -2914864
49 meter E =
0001875
Z = 5330259
81 I = 51
87302
XDOT = 5652
438575 Wp = 139
20714
YDOT = -5157
377268 meter/sec RA = 139
94745 deg
ZDOT = 395
547854 TA = 307
02143
MA = 307
03858
Ha = 228
210 n
mi
Hp = 222
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9953904
38 X = -3027021
33
Y = -9563203
70 feet Y = -2948753
54 meter
Z = 17487729
02 Z = 5315538
73
XDOT = 18544
745980 XDOT = 5707
768452
YDOT = -16920
529093 feet/sec YDOT = -5093
858276 meter/sec
ZDOT = 1297
729180 ZDOT = 423
139907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3184201
43 X = -970544
60
Y = -13519312
78 feet Y = -4120686
54 meter
Z = 17419666
67 Z = 5309514
40
XDOT = 23791
564374 XDOT = 7251
668821
YDOT = -3760
850321 feet/sec YDOT = -1146
307178 meter/sec
ZDOT = 1425
354243 ZDOT = 434
447973
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20283
90677509
00016717 00000-0 10270-3 0 9195
2 25544 51
6432 140
8450 0001411 247
4945 112
6056 15
49329254 9797
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
90677509 = yrday
fracday
Element set: 919
Inclination: 51
6432 deg
RA of node: 140
8450 deg
Eccentricity:
0001411
Arg of perigee: 247
4945 deg
Mean anomaly: 112
6056 deg
Mean motion: 15
49329254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 979
Checksum: 316
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