[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 22nd 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16491 3871 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
116/01:51:40
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 222
4
116/05:12:17
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
4
117/03:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
4
Coasting Arc #1 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2020/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3939100
86 A = 6792019
36 meter
Y = -1980597
49 meter E =
0005550
Z = 5164324
64 I = 51
23532
XDOT = 1938
426382 Wp = 141
85013
YDOT = 7295
838830 meter/sec RA = 263
15859 deg
ZDOT = 1314
476491 TA = 295
41164
MA = 295
46908
Ha = 228
553 n
mi
Hp = 222
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12923559
25 X = 3935870
04
Y = -6498023
27 feet Y = -1936565
59 meter
Z = 16943322
31 Z = 5183451
72
XDOT = 6359
666609 XDOT = 1850
313022
YDOT = 23936
479102 feet/sec YDOT = 7317
023057 meter/sec
ZDOT = 4312
586914 ZDOT = 1323
678524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7821284
79 X = 2383927
60
Y = -12045261
73 feet Y = -3671395
78 meter
Z = 17031090
26 Z = 5191076
31
XDOT = 16604
671404 XDOT = 5061
103844
YDOT = 16961
962884 feet/sec YDOT = 5170
006287 meter/sec
ZDOT = 4354
430488 ZDOT = 1327
230413
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 20113
55068095
00016717 00000-0 10270-3 0 9002
2 25544 51
6404 263
8319 0001917 183
6392 176
4744 15
49303085 23381
Satellite: ISS
Catalog Number: 25544
Epoch time: 20113
55068095 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 263
8319 deg
Eccentricity:
0001917
Arg of perigee: 183
6392 deg
Mean anomaly: 176
4744 deg
Mean motion: 15
49303085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2338
Checksum: 307
Coasting Arc #2 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2020/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3808966
70 A = 6791868
32 meter
Y = 2173653
59 meter E =
0013831
Z = -5198291
78 I = 51
24125
XDOT = -2465
519613 Wp = 88
52768
YDOT = -7144
855322 meter/sec RA = 258
18303 deg
ZDOT = -1183
430455 TA = 170
04420
MA = 170
01677
Ha = 228
651 n
mi
Hp = 222
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12496609
90 X = -3807739
30
Y = 7131409
41 feet Y = 2131065
82 meter
Z = -17054763
04 Z = -5216791
59
XDOT = -8088
975107 XDOT = -2379
691959
YDOT = -23441
126386 feet/sec YDOT = -7171
946638 meter/sec
ZDOT = -3882
645851 ZDOT = -1195
198640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6919594
04 X = -2109092
26
Y = 12499533
99 feet Y = 3809857
96 meter
Z = -17139663
65 Z = -5224169
48
XDOT = -18098
064467 XDOT = -5516
290049
YDOT = -15405
657998 feet/sec YDOT = -4695
644558 meter/sec
ZDOT = -3936
272616 ZDOT = -1199
775893
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 20114
51821749
00016717 00000-0 10270-3 0 9013
2 25544 51
6415 259
0447 0001872 182
5602 177
5539 15
49320601 23538
Satellite: ISS
Catalog Number: 25544
Epoch time: 20114
51821749 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 259
0447 deg
Eccentricity:
0001872
Arg of perigee: 182
5602 deg
Mean anomaly: 177
5539 deg
Mean motion: 15
49320601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 295
Coasting Arc #3 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2020/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3654072
29 A = 6791759
24 meter
Y = -2367437
86 meter E =
0004814
Z = 5210737
88 I = 51
24879
XDOT = 2995
292097 Wp = 144
13932
YDOT = 6972
208718 meter/sec RA = 253
20661 deg
ZDOT = 1062
934138 TA = 295
58979
MA = 295
63954
Ha = 228
436 n
mi
Hp = 222
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11988426
14 X = 3654962
86
Y = -7767184
57 feet Y = -2326570
49 meter
Z = 17095596
72 Z = 5228490
39
XDOT = 9827
073810 XDOT = 2911
940960
YDOT = 22874
700520 feet/sec YDOT = 7005
238151 meter/sec
ZDOT = 3487
316726 ZDOT = 1077
281966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5935099
01 X = 1809018
18
Y = -12885396
19 feet Y = -3927468
76 meter
Z = 17177080
94 Z = 5235574
27
XDOT = 19514
958214 XDOT = 5948
159264
YDOT = 13743
689122 feet/sec YDOT = 4189
076444 meter/sec
ZDOT = 3552
789815 ZDOT = 1082
890336
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 20115
55025390
00016717 00000-0 10270-3 0 9027
2 25544 51
6412 253
9367 0001868 190
8144 169
2966 15
49324997 23698
Satellite: ISS
Catalog Number: 25544
Epoch time: 20115
55025390 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 253
9367 deg
Eccentricity:
0001868
Arg of perigee: 190
8144 deg
Mean anomaly: 169
2966 deg
Mean motion: 15
49324997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 329
Coasting Arc #4 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2020/116/01:51:40
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2538125
32 A = 6793805
67 meter
Y = -4165414
95 meter E =
0008129
Z = 4725574
07 I = 51
26224
XDOT = 4337
125768 Wp = 127
94237
YDOT = 5711
919175 meter/sec RA = 250
35038 deg
ZDOT = 2697
254701 TA = 295
18911
MA = 295
27339
Ha = 228
386 n
mi
Hp = 222
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8327182
80 X = 2561561
03
Y = -13666059
54 feet Y = -4136900
88 meter
Z = 15503851
95 Z = 4737960
35
XDOT = 14229
415248 XDOT = 4259
829094
YDOT = 18739
892307 feet/sec YDOT = 5759
987754 meter/sec
ZDOT = 8849
260830 ZDOT = 2718
135514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7860433
37 X = 2395860
09
Y = 13876140
86 feet Y = 4229447
73 meter
Z = 15560812
45 Z = 4742935
63
XDOT = -22272
603908 XDOT = -6788
689671
YDOT = 2556
395329 feet/sec YDOT = 779
189296 meter/sec
ZDOT = 8944
745365 ZDOT = 2726
358387
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 20116
13077326
00016717 00000-0 10270-3 0 9039
2 25544 51
6419 251
0688 0001487 197
3765 162
7335 15
49336009 23783
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
13077326 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 251
0688 deg
Eccentricity:
0001487
Arg of perigee: 197
3765 deg
Mean anomaly: 162
7335 deg
Mean motion: 15
49336009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 316
Coasting Arc #5 (Orbit 2379)
---------------------------------------
Vector Time (GMT): 2020/116/05:12:17
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4632296
58 A = 6794372
17 meter
Y = 1989312
65 meter E =
0007636
Z = 4549756
43 I = 51
26756
XDOT = -6
572064 Wp = 73
34192
YDOT = 7026
323138 meter/sec RA = 249
61522 deg
ZDOT = -3059
030302 TA = 47
46843
MA = 47
40398
Ha = 228
221 n
mi
Hp = 222
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15197823
44 X = 4587606
71
Y = 6526616
29 feet Y = 2040864
30 meter
Z = 14927022
42 Z = 4572150
22
XDOT = -21
561891 XDOT = -70
282715
YDOT = 23052
241267 feet/sec YDOT = 7025
893486 meter/sec
ZDOT = -10036
188655 ZDOT = -3059
216808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -725562
28 X = -221151
38
Y = 16430799
41 feet Y = 5008107
66 meter
Z = 15029602
32 Z = 4581022
79
XDOT = -20326
720170 XDOT = -6195
584308
YDOT = 8302
940669 feet/sec YDOT = 2530
736316 meter/sec
ZDOT = -10037
339932 ZDOT = -3059
381211
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 20116
25977628
00016717 00000-0 10270-3 0 9047
2 25544 51
6434 250
4313 0001345 204
4454 155
6633 15
49359074 23808
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
25977628 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 250
4313 deg
Eccentricity:
0001345
Arg of perigee: 204
4454 deg
Mean anomaly: 155
6633 deg
Mean motion: 15
49359074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2380
Checksum: 299
Coasting Arc #6 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2020/117/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2835154
19 A = 6803421
00 meter
Y = 6177050
65 meter E =
0012730
Z = -37401
63 I = 51
30875
XDOT = -4364
193699 Wp = 141
01023
YDOT = 1973
680490 meter/sec RA = 245
09321 deg
ZDOT = -5980
144446 TA = 39
39372
MA = 39
30122
Ha = 228
486 n
mi
Hp = 222
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9301686
96 X = 2766051
54
Y = 20265914
19 feet Y = 6208368
98 meter
Z = -122708
77 Z = -23796
91
XDOT = -14318
220796 XDOT = -4356
891008
YDOT = 6475
329690 feet/sec YDOT = 1924
918050 meter/sec
ZDOT = -19619
896476 ZDOT = -6001
326533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21504407
56 X = -6554543
42
Y = 5899194
91 feet Y = 1798074
61 meter
Z = -60586
13 Z = -18466
65
XDOT = -3662
662121 XDOT = -1116
379414
YDOT = -13477
357689 feet/sec YDOT = -4107
898624 meter/sec
ZDOT = -19717
093351 ZDOT = -6009
770054
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 20117
16280759
00016717 00000-0 10270-3 0 9051
2 25544 51
6435 245
9621 0001520 200
7554 159
3535 15
49293542 23949
Satellite: ISS
Catalog Number: 25544
Epoch time: 20117
16280759 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 245
9621 deg
Eccentricity:
0001520
Arg of perigee: 200
7554 deg
Mean anomaly: 159
3535 deg
Mean motion: 15
49293542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 304
Coasting Arc #7 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2020/118/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3289207
19 A = 6803326
46 meter
Y = -5947929
88 meter E =
0011060
Z = 138740
33 I = 51
32448
XDOT = 4251
942923 Wp = 48
96405
YDOT = -2204
753412 meter/sec RA = 240
12118 deg
ZDOT = 5978
033021 TA = 312
53389
MA = 312
62723
Ha = 228
374 n
mi
Hp = 222
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10791362
16 X = -3223125
14
Y = -19514205
63 feet Y = -5984342
65 meter
Z = 455184
82 Z = 122922
58
XDOT = 13949
943972 XDOT = 4247
242834
YDOT = -7233
442953 feet/sec YDOT = -2157
231787 meter/sec
ZDOT = 19612
969230 ZDOT = 5998
676051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20872089
50 X = 6361812
88
Y = -7853291
49 feet Y = -2393683
25 meter
Z = 382890
22 Z = 116704
94
XDOT = 4581
822331 XDOT = 1396
539446
YDOT = 13196
323331 feet/sec YDOT = 4022
239351 meter/sec
ZDOT = 19707
710610 ZDOT = 6006
910194
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 20118
19483532
00016717 00000-0 10270-3 0 9060
2 25544 51
6440 240
8545 0001298 209
3949 150
7129 15
49323766 24104
Satellite: ISS
Catalog Number: 25544
Epoch time: 20118
19483532 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 240
8545 deg
Eccentricity:
0001298
Arg of perigee: 209
3949 deg
Mean anomaly: 150
7129 deg
Mean motion: 15
49323766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 308
Coasting Arc #8 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2020/119/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3697794
34 A = 6803394
14 meter
Y = 5696550
68 meter E =
0012092
Z = -275476
99 I = 51
34158
XDOT = -4146
331858 Wp = 143
09397
YDOT = 2409
648287 meter/sec RA = 235
15178 deg
ZDOT = -5974
857498 TA = 39
88108
MA = 39
79230
Ha = 228
436 n
mi
Hp = 222
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12131871
21 X = 3635157
12
Y = 18689470
75 feet Y = 5737551
84 meter
Z = -903795
89 Z = -257666
11
XDOT = -13603
450977 XDOT = -4143
946349
YDOT = 7905
670233 feet/sec YDOT = 2363
294797 meter/sec
ZDOT = -19602
550847 ZDOT = -5994
993013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20087664
68 X = -6122720
19
Y = 9649091
08 feet Y = 2941042
96 meter
Z = -822333
29 Z = -250647
19
XDOT = -5414
277167 XDOT = -1650
271681
YDOT = -12905
033120 feet/sec YDOT = -3933
454095 meter/sec
ZDOT = -19694
980230 ZDOT = -6003
029974
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 20119
16235978
00016717 00000-0 10270-3 0 9078
2 25544 51
6434 236
0673 0001405 207
7328 152
3747 15
49293478 24255
Satellite: ISS
Catalog Number: 25544
Epoch time: 20119
16235978 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 236
0673 deg
Eccentricity:
0001405
Arg of perigee: 207
7328 deg
Mean anomaly: 152
3747 deg
Mean motion: 15
49293478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 317
Coasting Arc #9 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2020/120/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4108844
61 A = 6803239
61 meter
Y = -5402240
23 meter E =
0011413
Z = 379466
88 I = 51
36112
XDOT = 4018
940977 Wp = 50
21218
YDOT = -2629
608967 meter/sec RA = 230
18244 deg
ZDOT = 5967
910851 TA = 313
88600
MA = 313
98020
Ha = 228
266 n
mi
Hp = 222
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13480461
30 X = -4049973
02
Y = -17723885
28 feet Y = -5447859
11 meter
Z = 1244970
09 Z = 359650
21
XDOT = 13185
501894 XDOT = 4019
058465
YDOT = -8627
326006 feet/sec YDOT = -2584
666065 meter/sec
ZDOT = 19579
760010 ZDOT = 5987
433525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19108662
84 X = 5824320
43
Y = -11442707
16 feet Y = -3487737
14 meter
Z = 1154276
47 Z = 351823
47
XDOT = 6293
248196 XDOT = 1918
182050
YDOT = 12533
762402 feet/sec YDOT = 3820
290780 meter/sec
ZDOT = 19669
393987 ZDOT = 5995
231287
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 20120
19438134
00016717 00000-0 10270-3 0 9083
2 25544 51
6429 230
9599 0001293 220
7246 139
3807 15
49337824 24412
Satellite: ISS
Catalog Number: 25544
Epoch time: 20120
19438134 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 230
9599 deg
Eccentricity:
0001293
Arg of perigee: 220
7246 deg
Mean anomaly: 139
3807 deg
Mean motion: 15
49337824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 309
Coasting Arc #10 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2020/121/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4471885
66 A = 6803305
23 meter
Y = 5092962
50 meter E =
0011313
Z = -517987
24 I = 51
38378
XDOT = -3900
070955 Wp = 145
92473
YDOT = 2825
898010 meter/sec RA = 225
21535 deg
ZDOT = -5957
784747 TA = 39
67219
MA = 39
58948
Ha = 228
320 n
mi
Hp = 222
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14671540
86 X = 4417118
37
Y = 16709194
57 feet Y = 5142664
12 meter
Z = -1699433
21 Z = -496397
21
XDOT = -12795
508384 XDOT = -3902
441527
YDOT = 9271
318931 feet/sec YDOT = 2782
271757 meter/sec
ZDOT = -19546
537885 ZDOT = -5976
735406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18010567
49 X = -5489620
97
Y = 13053620
07 feet Y = 3978743
40 meter
Z = -1600571
64 Z = -487854
24
XDOT = -7091
954136 XDOT = -2161
627621
YDOT = -12161
420002 feet/sec YDOT = -3706
800817 meter/sec
ZDOT = -19633
561126 ZDOT = -5984
309431
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 20121
16190049
00016717 00000-0 10270-3 0 9092
2 25544 51
6433 226
1722 0001445 220
7611 139
3431 15
49298409 24561
Satellite: ISS
Catalog Number: 25544
Epoch time: 20121
16190049 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 226
1722 deg
Eccentricity:
0001445
Arg of perigee: 220
7611 deg
Mean anomaly: 139
3431 deg
Mean motion: 15
49298409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 287
Coasting Arc #11 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2020/122/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4829369
43 A = 6803070
50 meter
Y = -4742385
59 meter E =
0011745
Z = 625748
14 I = 51
40808
XDOT = 3759
154659 Wp = 51
56233
YDOT = -3034
521363 meter/sec RA = 220
24820 deg
ZDOT = 5945
548535 TA = 315
20160
MA = 315
29638
Ha = 228
140 n
mi
Hp = 222
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15844387
91 X = -4779019
28
Y = -15559007
84 feet Y = -4796109
54 meter
Z = 2052979
45 Z = 602410
99
XDOT = 12333
184578 XDOT = 3763
928085
YDOT = -9955
778749 feet/sec YDOT = -2992
457415 meter/sec
ZDOT = 19506
392831 ZDOT = 5963
820506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16726432
14 X = 5098216
52
Y = -14621264
14 feet Y = -4456561
31 meter
Z = 1946067
87 Z = 593161
49
XDOT = 7926
038998 XDOT = 2415
856687
YDOT = 11706
370279 feet/sec YDOT = 3568
101661 meter/sec
ZDOT = 19590
314255 ZDOT = 5971
127785
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 20122
19391354
00016717 00000-0 10270-3 0 9100
2 25544 51
6432 221
0638 0001300 233
5790 126
5240 15
49363029 24725
Satellite: ISS
Catalog Number: 25544
Epoch time: 20122
19391354 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 221
0638 deg
Eccentricity:
0001300
Arg of perigee: 233
5790 deg
Mean anomaly: 126
5240 deg
Mean motion: 15
49363029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 269
Coasting Arc #12 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2020/123/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5137916
69 A = 6803140
99 meter
Y = 4384469
55 meter E =
0010454
Z = -766585
83 I = 51
43343
XDOT = -3627
726634 Wp = 147
53631
YDOT = 3222
841497 meter/sec RA = 215
28399 deg
ZDOT = -5927
603929 TA = 40
75633
MA = 40
67818
Ha = 228
248 n
mi
Hp = 222
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16856682
07 X = 5092230
04
Y = 14384742
62 feet Y = 4441669
96 meter
Z = -2515045
39 Z = -741738
65
XDOT = -11901
990268 XDOT = -3634
702842
YDOT = 10573
626958 feet/sec YDOT = 3182
234844 meter/sec
ZDOT = -19447
519451 ZDOT = -5945
242873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15360483
41 X = -4681875
34
Y = 15990119
67 feet Y = 4873788
48 meter
Z = -2401171
84 Z = -731877
18
XDOT = -8689
563801 XDOT = -2648
579047
YDOT = -11256
017329 feet/sec YDOT = -3430
834082 meter/sec
ZDOT = -19528
545727 ZDOT = -5952
300738
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 20123
16142659
00016717 00000-0 10270-3 0 9111
2 25544 51
6424 216
2756 0001317 232
6707 127
4324 15
49311422 24878
Satellite: ISS
Catalog Number: 25544
Epoch time: 20123
16142659 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 216
2756 deg
Eccentricity:
0001317
Arg of perigee: 232
6707 deg
Mean anomaly: 127
4324 deg
Mean motion: 15
49311422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2487
Checksum: 283
Coasting Arc #13 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2020/124/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5434897
38 A = 6802889
75 meter
Y = -3986771
41 meter E =
0012035
Z = 875822
15 I = 51
46085
XDOT = 3471
435559 Wp = 53
75606
YDOT = -3423
143225 meter/sec RA = 210
32108 deg
ZDOT = 5909
755996 TA = 315
72585
MA = 315
82206
Ha = 228
080 n
mi
Hp = 222
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17831028
14 X = -5394166
44
Y = -13079958
69 feet Y = -4047320
57 meter
Z = 2873432
27 Z = 849520
34
XDOT = 11389
224274 XDOT = 3480
749848
YDOT = -11230
784860 feet/sec YDOT = -3384
271152 meter/sec
ZDOT = 19388
963241 ZDOT = 5926
641509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13820694
40 X = 4212547
65
Y = -17282873
31 feet Y = -5267819
79 meter
Z = 2752851
85 Z = 839069
24
XDOT = 9484
901891 XDOT = 2890
998096
YDOT = 10712
740514 feet/sec YDOT = 3265
243309 meter/sec
ZDOT = 19466
540727 ZDOT = 5933
401614
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 20124
19343498
00016717 00000-0 10270-3 0 9120
2 25544 51
6419 211
1678 0001320 240
8140 119
2878 15
49374269 25035
Satellite: ISS
Catalog Number: 25544
Epoch time: 20124
19343498 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 211
1678 deg
Eccentricity:
0001320
Arg of perigee: 240
8140 deg
Mean anomaly: 119
2878 deg
Mean motion: 15
49374269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2503
Checksum: 299
Coasting Arc #14 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2020/125/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5682825
59 A = 6802905
18 meter
Y = 3589408
25 meter E =
0009510
Z = -1017281
07 I = 51
49069
XDOT = -3324
846113 Wp = 149
87837
YDOT = 3605
398662 meter/sec RA = 205
36071 deg
ZDOT = -5884
151369 TA = 41
14655
MA = 41
07488
Ha = 228
122 n
mi
Hp = 222
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18644440
90 X = 5647206
81
Y = 11776273
77 feet Y = 3652758
49 meter
Z = -3337536
32 Z = -989762
43
XDOT = -10908
287772 XDOT = -3336
333585
YDOT = 11828
735769 feet/sec YDOT = 3568
153640 meter/sec
ZDOT = -19304
958559 ZDOT = -5900
330188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12238443
28 X = -3730277
51
Y = 18366892
27 feet Y = 5598228
77 meter
Z = -3211342
94 Z = -978817
33
XDOT = -10215
636199 XDOT = -3113
725913
YDOT = -10176
275764 feet/sec YDOT = -3101
728853 meter/sec
ZDOT = -19379
300813 ZDOT = -5906
810888
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 20125
16094321
00016717 00000-0 10270-3 0 9137
2 25544 51
6425 206
3796 0001413 246
3371 113
7631 15
49330983 25186
Satellite: ISS
Catalog Number: 25544
Epoch time: 20125
16094321 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 206
3796 deg
Eccentricity:
0001413
Arg of perigee: 246
3371 deg
Mean anomaly: 113
7631 deg
Mean motion: 15
49330983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 287
Coasting Arc #15 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2020/126/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5912596
12 A = 6802676
57 meter
Y = -3156120
34 meter E =
0012306
Z = 1128638
84 I = 51
52065
XDOT = 3152
910166 Wp = 55
71088
YDOT = -3797
020896 meter/sec RA = 200
40098 deg
ZDOT = 5860
146295 TA = 316
53611
MA = 316
63305
Ha = 228
028 n
mi
Hp = 222
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19398281
23 X = -5882346
36
Y = -10354725
52 feet Y = -3222070
06 meter
Z = 3702883
35 Z = 1099990
87
XDOT = 10344
193458 XDOT = 3166
669648
YDOT = -12457
417638 feet/sec YDOT = -3761
685885 meter/sec
ZDOT = 19226
201754 ZDOT = 5875
495505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10505045
64 X = 3201937
91
Y = -19342015
13 feet Y = -5895446
21 meter
Z = 3571479
69 Z = 1088587
01
XDOT = 10966
258868 XDOT = 3342
515703
YDOT = 9543
630076 feet/sec YDOT = 2908
898447 meter/sec
ZDOT = 19296
745944 ZDOT = 5881
648164
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 20126
19294610
00016717 00000-0 10270-3 0 9145
2 25544 51
6419 201
2709 0001332 252
2023 107
8982 15
49378022 25344
Satellite: ISS
Catalog Number: 25544
Epoch time: 20126
19294610 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 201
2709 deg
Eccentricity:
0001332
Arg of perigee: 252
2023 deg
Mean anomaly: 107
8982 deg
Mean motion: 15
49378022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2534
Checksum: 283
Coasting Arc #16 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2020/127/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6094734
25 A = 6802617
10 meter
Y = 2730750
57 meter E =
0008614
Z = -1270797
55 I = 51
55082
XDOT = -2989
881381 Wp = 150
35448
YDOT = 3973
101733 meter/sec RA = 195
44523 deg
ZDOT = -5826
116251 TA = 43
45435
MA = 43
38649
Ha = 228
101 n
mi
Hp = 222
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19995847
28 X = 6069918
13
Y = 8959155
42 feet Y = 2798767
49 meter
Z = -4169283
31 Z = -1241251
43
XDOT = -9809
322116 XDOT = -3005
787134
YDOT = 13035
110671 feet/sec YDOT = 3939
577914 meter/sec
ZDOT = -19114
554630 ZDOT = -5840
678744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8769580
73 X = -2672968
21
Y = 20107380
86 feet Y = 6128729
69 meter
Z = -4033731
04 Z = -1229481
22
XDOT = -11658
586637 XDOT = -3553
537207
YDOT = -8916
231214 feet/sec YDOT = -2717
667274 meter/sec
ZDOT = -19181
499314 ZDOT = -5846
520991
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 20127
16044927
00016717 00000-0 10270-3 0 9158
2 25544 51
6407 196
4832 0001293 256
8028 103
2978 15
49349526 25492
Satellite: ISS
Catalog Number: 25544
Epoch time: 20127
16044927 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 196
4832 deg
Eccentricity:
0001293
Arg of perigee: 256
8028 deg
Mean anomaly: 103
2978 deg
Mean motion: 15
49349526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 324
Coasting Arc #17 (Orbit 2564)
---------------------------------------
Vector Time (GMT): 2020/128/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6254157
58 A = 6802446
38 meter
Y = -2272694
51 meter E =
0012476
Z = 1381946
39 I = 51
58212
XDOT = 2798
367248 Wp = 58
47727
YDOT = -4156
768254 meter/sec RA = 190
49030 deg
ZDOT = 5795
984295 TA = 316
56469
MA = 316
66291
Ha = 228
029 n
mi
Hp = 222
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20518889
69 X = -6234991
65
Y = -7456346
82 feet Y = -2342525
85 meter
Z = 4533944
85 Z = 1351611
98
XDOT = 9180
994907 XDOT = 2816
487341
YDOT = -13637
691122 feet/sec YDOT = -4125
373858 meter/sec
ZDOT = 19015
696505 ZDOT = 5809
621770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6906116
19 X = 2104984
21
Y = -20740548
90 feet Y = -6321719
31 meter
Z = 4394745
56 Z = 1339518
45
XDOT = 12360
494039 XDOT = 3767
478583
YDOT = 8181
466731 feet/sec YDOT = 2493
711060 meter/sec
ZDOT = 19078
409465 ZDOT = 5815
099205
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 20128
19244991
00016717 00000-0 10270-3 0 9166
2 25544 51
6396 191
3749 0001355 257
2507 102
8492 15
49369027 25658
Satellite: ISS
Catalog Number: 25544
Epoch time: 20128
19244991 = yrday
fracday
Element set: 916
Inclination: 51
6396 deg
RA of node: 191
3749 deg
Eccentricity:
0001355
Arg of perigee: 257
2507 deg
Mean anomaly: 102
8492 deg
Mean motion: 15
49369027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2565
Checksum: 328
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