[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 7th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19998 2692 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
278/06:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
5
281/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 218
7
284/20:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 219
1
Coasting Arc #1 (Orbit 3221)
---------------------------------------
Vector Time (GMT): 2019/277/13:29:50
425
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6779147
83 A = 6800993
28 meter
Y = -400081
65 meter E =
0019486
Z = 159113
57 I = 51
67406
XDOT = 432
412024 Wp = 126
35061
YDOT = 4737
309418 meter/sec RA = 177
68378 deg
ZDOT = -6010
105061 TA = 51
93837
MA = 51
76272
Ha = 229
896 n
mi
Hp = 218
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22241298
65 X = 6782344
92
Y = -1312603
83 feet Y = -324254
55 meter
Z = 522026
16 Z = 192052
29
XDOT = 1418
674618 XDOT = 408
600012
YDOT = 15542
353733 feet/sec YDOT = 4742
011629 meter/sec
ZDOT = -19718
192456 ZDOT = -6008
062521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17578152
60 X = -5357820
91
Y = 13683116
64 feet Y = 4170613
95 meter
Z = 672068
52 Z = 204846
48
XDOT = -9087
665033 XDOT = -2769
920302
YDOT = -10643
751389 feet/sec YDOT = -3244
215423 meter/sec
ZDOT = -19709
107118 ZDOT = -6007
335850
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 19277
59508336
00016717 00000-0 10270-3 0 9002
2 25544 51
6430 178
7228 0007257 114
5537 245
6371 15
50119547 32228
Satellite: ISS
Catalog Number: 25544
Epoch time: 19277
59508336 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 178
7228 deg
Eccentricity:
0007257
Arg of perigee: 114
5537 deg
Mean anomaly: 245
6371 deg
Mean motion: 15
50119547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3222
Checksum: 314
Coasting Arc #2 (Orbit 3232)
---------------------------------------
Vector Time (GMT): 2019/278/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3337481
72 A = 6791320
24 meter
Y = 3474287
66 meter E =
0017220
Z = -4801724
92 I = 51
66238
XDOT = -6634
054662 Wp = 89
18533
YDOT = 2763
962012 meter/sec RA = 174
13201 deg
ZDOT = -2619
099814 TA = 154
97360
MA = 154
89003
Ha = 229
878 n
mi
Hp = 218
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10949743
19 X = 3321707
51
Y = 11398581
56 feet Y = 3511521
39 meter
Z = -15753690
67 Z = -4785550
95
XDOT = -21765
271200 XDOT = -6651
746779
YDOT = 9068
116837 feet/sec YDOT = 2689
676331 meter/sec
ZDOT = -8592
847158 ZDOT = -2651
368913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5716870
57 X = 1742502
15
Y = -14813938
65 feet Y = -4515288
50 meter
Z = -15680176
01 Z = -4779317
65
XDOT = 16247
823530 XDOT = 4952
336612
YDOT = 15493
671893 feet/sec YDOT = 4722
471193 meter/sec
ZDOT = -8739
965415 ZDOT = -2663
941458
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 19278
30421791
00016717 00000-0 10270-3 0 9012
2 25544 51
6394 175
2065 0007359 115
6588 244
5324 15
50147176 32336
Satellite: ISS
Catalog Number: 25544
Epoch time: 19278
30421791 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 175
2065 deg
Eccentricity:
0007359
Arg of perigee: 115
6588 deg
Mean anomaly: 244
5324 deg
Mean motion: 15
50147176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 312
Coasting Arc #3 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2019/279/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3206670
41 A = 6790579
71 meter
Y = -3363177
76 meter E =
0013758
Z = 4943837
43 I = 51
69297
XDOT = 6666
364692 Wp = 121
04131
YDOT = -3065
354659 meter/sec RA = 169
17916 deg
ZDOT = 2227
118572 TA = 307
17187
MA = 307
29742
Ha = 229
815 n
mi
Hp = 218
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10520572
21 X = -3192838
62
Y = -11034047
77 feet Y = -3398959
50 meter
Z = 16219939
07 Z = 4928294
24
XDOT = 21871
275237 XDOT = 6689
328746
YDOT = -10056
937856 feet/sec YDOT = -2990
678188 meter/sec
ZDOT = 7306
819463 ZDOT = 2259
557354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5317979
85 X = -1620920
26
Y = 14367980
05 feet Y = 4379360
32 meter
Z = 16149282
12 Z = 4922301
19
XDOT = -17491
946175 XDOT = -5331
545194
YDOT = -14895
905505 feet/sec YDOT = -4540
271998 meter/sec
ZDOT = 7454
747747 ZDOT = 2272
207113
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 19279
33568475
00016717 00000-0 10270-3 0 9028
2 25544 51
6390 170
0964 0007178 119
7196 240
4669 15
50181468 32498
Satellite: ISS
Catalog Number: 25544
Epoch time: 19279
33568475 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 170
0964 deg
Eccentricity:
0007178
Arg of perigee: 119
7196 deg
Mean anomaly: 240
4669 deg
Mean motion: 15
50181468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 340
Coasting Arc #4 (Orbit 3263)
---------------------------------------
Vector Time (GMT): 2019/280/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3041787
40 A = 6790069
95 meter
Y = 3320745
00 meter E =
0018789
Z = -5097826
51 I = 51
72381
XDOT = -6641
170231 Wp = 92
98064
YDOT = 3344
382527 meter/sec RA = 164
22597 deg
ZDOT = -1790
793184 TA = 159
70383
MA = 159
62905
Ha = 229
746 n
mi
Hp = 218
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9979617
45 X = 3029190
31
Y = 10894832
69 feet Y = 3354689
76 meter
Z = -16725152
60 Z = -5083081
33
XDOT = -21788
616242 XDOT = -6669
375784
YDOT = 10972
383620 feet/sec YDOT = 3269
958489 meter/sec
ZDOT = -5875
305722 ZDOT = -1823
122286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5187563
77 X = 1581169
44
Y = -13914636
11 feet Y = -4241181
09 meter
Z = -16658119
86 Z = -5077394
93
XDOT = 18569
923792 XDOT = 5660
112772
YDOT = 14107
092476 feet/sec YDOT = 4299
841787 meter/sec
ZDOT = -6022
769023 ZDOT = -1835
739998
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 19280
30268476
00016717 00000-0 10270-3 0 9036
2 25544 51
6392 165
3039 0007217 123
0585 237
1260 15
50153886 32644
Satellite: ISS
Catalog Number: 25544
Epoch time: 19280
30268476 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 165
3039 deg
Eccentricity:
0007217
Arg of perigee: 123
0585 deg
Mean anomaly: 237
1260 deg
Mean motion: 15
50153886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3264
Checksum: 304
Coasting Arc #5 (Orbit 3279)
---------------------------------------
Vector Time (GMT): 2019/281/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2896651
93 A = 6789490
62 meter
Y = -3275525
52 meter E =
0011564
Z = 5187363
19 I = 51
75541
XDOT = 6601
156042 Wp = 126
64444
YDOT = -3652
634052 meter/sec RA = 159
27679 deg
ZDOT = 1370
832311 TA = 310
14728
MA = 310
24851
Ha = 229
679 n
mi
Hp = 218
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9503451
23 X = -2885006
19
Y = -10746474
81 feet Y = -3307852
52 meter
Z = 17018908
10 Z = 5173320
76
XDOT = 21657
336095 XDOT = 6634
851477
YDOT = -11983
707521 feet/sec YDOT = -3578
626786 meter/sec
ZDOT = 4497
481336 ZDOT = 1402
980412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5036722
62 X = -1535193
05
Y = 13513054
96 feet Y = 4118779
15 meter
Z = 16955067
38 Z = 5167904
54
XDOT = -19683
993141 XDOT = -5999
681109
YDOT = -13200
521101 feet/sec YDOT = -4023
518832 meter/sec
ZDOT = 4644
154288 ZDOT = 1415
538227
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 19281
33414628
00016717 00000-0 10270-3 0 9043
2 25544 51
6405 160
1937 0007055 127
1931 232
9865 15
50194409 32807
Satellite: ISS
Catalog Number: 25544
Epoch time: 19281
33414628 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 160
1937 deg
Eccentricity:
0007055
Arg of perigee: 127
1931 deg
Mean anomaly: 232
9865 deg
Mean motion: 15
50194409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3280
Checksum: 304
Coasting Arc #6 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2019/281/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 876947
89 A = 6788973
40 meter
Y = 4156005
08 meter E =
0020983
Z = -5314109
77 I = 51
76157
XDOT = -7254
366752 Wp = 105
39343
YDOT = 2335
155985 meter/sec RA = 158
44695 deg
ZDOT = 625
761687 TA = 170
60675
MA = 170
56744
Ha = 229
591 n
mi
Hp = 218
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2877125
63 X = 856222
15
Y = 13635187
27 feet Y = 4165695
53 meter
Z = -17434743
34 Z = -5309900
46
XDOT = -23800
415854 XDOT = -7282
979598
YDOT = 7661
272916 feet/sec YDOT = 2253
872589 meter/sec
ZDOT = 2053
023909 ZDOT = 590
452936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2310460
18 X = -704228
26
Y = -13766616
94 feet Y = -4196064
84 meter
Z = -17415754
10 Z = -5308321
85
XDOT = 23162
530996 XDOT = 7059
939447
YDOT = -6294
862776 feet/sec YDOT = -1918
674174 meter/sec
ZDOT = 1892
005314 ZDOT = 576
683220
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 19281
46307950
00016717 00000-0 10270-3 0 9057
2 25544 51
6432 159
5556 0007080 127
0636 233
1162 15
50187305 32827
Satellite: ISS
Catalog Number: 25544
Epoch time: 19281
46307950 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 159
5556 deg
Eccentricity:
0007080
Arg of perigee: 127
0636 deg
Mean anomaly: 233
1162 deg
Mean motion: 15
50187305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3282
Checksum: 298
Coasting Arc #7 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2019/282/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -762069
03 A = 6789092
33 meter
Y = -4233243
61 meter E =
0008772
Z = 5245047
70 I = 51
79298
XDOT = 7130
403038 Wp = 107
67510
YDOT = -2611
580480 meter/sec RA = 153
49896 deg
ZDOT = -1072
914809 TA = 352
57415
MA = 352
58713
Ha = 229
516 n
mi
Hp = 218
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2500226
49 X = -740152
69
Y = -13888594
51 feet Y = -4241642
67 meter
Z = 17208161
74 Z = 5241399
38
XDOT = 23393
710755 XDOT = 7164
288191
YDOT = -8568
177427 feet/sec YDOT = -2531
653896 meter/sec
ZDOT = -3520
061709 ZDOT = -1038
195333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2160416
92 X = 658495
08
Y = 13965742
55 feet Y = 4256758
33 meter
Z = 17191732
15 Z = 5240039
96
XDOT = -22666
345474 XDOT = -6908
702100
YDOT = 7640
031627 feet/sec YDOT = 2328
681640 meter/sec
ZDOT = -3361
696348 ZDOT = -1024
645047
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 19282
49453679
00016717 00000-0 10270-3 0 9062
2 25544 51
6432 154
4447 0006982 130
8875 229
2881 15
50219539 32983
Satellite: ISS
Catalog Number: 25544
Epoch time: 19282
49453679 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 154
4447 deg
Eccentricity:
0006982
Arg of perigee: 130
8875 deg
Mean anomaly: 229
2881 deg
Mean motion: 15
50219539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3298
Checksum: 349
Coasting Arc #8 (Orbit 3312)
---------------------------------------
Vector Time (GMT): 2019/283/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 659819
61 A = 6789563
30 meter
Y = 4366123
40 meter E =
0019963
Z = -5175154
44 I = 51
82303
XDOT = -6934
531978 Wp = 112
56099
YDOT = 2845
518891 meter/sec RA = 148
55307 deg
ZDOT = 1513
758975 TA = 172
03998
MA = 172
00826
Ha = 229
469 n
mi
Hp = 218
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2164762
50 X = 636085
52
Y = 14324551
84 feet Y = 4373368
81 meter
Z = -16978853
15 Z = -5172007
29
XDOT = -22751
089166 XDOT = -6973
189058
YDOT = 9335
691900 feet/sec YDOT = 2767
756045 meter/sec
ZDOT = 4966
400837 ZDOT = 1479
979248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2056598
03 X = -626851
08
Y = -14357203
19 feet Y = -4376075
53 meter
Z = -16964715
07 Z = -5170845
15
XDOT = 21879
307290 XDOT = 6668
812862
YDOT = -8831
189313 feet/sec YDOT = -2691
746503 meter/sec
ZDOT = 4812
290173 ZDOT = 1466
786045
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 19283
46152888
00016717 00000-0 10270-3 0 9079
2 25544 51
6426 149
6533 0007001 134
0902 226
0826 15
50191944 33139
Satellite: ISS
Catalog Number: 25544
Epoch time: 19283
46152888 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 149
6533 deg
Eccentricity:
0007001
Arg of perigee: 134
0902 deg
Mean anomaly: 226
0826 deg
Mean motion: 15
50191944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3313
Checksum: 302
Coasting Arc #9 (Orbit 3328)
---------------------------------------
Vector Time (GMT): 2019/284/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -583643
81 A = 6789924
14 meter
Y = -4494520
41 meter E =
0009431
Z = 5047309
64 I = 51
85274
XDOT = 6750
930664 Wp = 102
52669
YDOT = -3070
458414 meter/sec RA = 143
60957 deg
ZDOT = -1952
458510 TA = 6
36783
MA = 6
35586
Ha = 229
352 n
mi
Hp = 218
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1914841
89 X = -557858
69
Y = -14745801
86 feet Y = -4500902
47 meter
Z = 16559414
84 Z = 5044537
55
XDOT = 22148
722651 XDOT = 6794
247735
YDOT = -10073
682462 feet/sec YDOT = -2994
722728 meter/sec
ZDOT = -6405
703774 ZDOT = -1919
559177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2051220
91 X = 625212
13
Y = 14741402
44 feet Y = 4493179
46 meter
Z = 16546995
46 Z = 5043524
22
XDOT = -21099
528444 XDOT = -6431
136270
YDOT = 9961
694748 feet/sec YDOT = 3036
324559 meter/sec
ZDOT = -6255
579147 ZDOT = -1906
700524
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 19284
49298248
00016717 00000-0 10270-3 0 9085
2 25544 51
6428 144
5425 0006866 138
8565 221
3104 15
50228075 33290
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
49298248 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 144
5425 deg
Eccentricity:
0006866
Arg of perigee: 138
8565 deg
Mean anomaly: 221
3104 deg
Mean motion: 15
50228075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3329
Checksum: 329
Coasting Arc #10 (Orbit 3334)
---------------------------------------
Vector Time (GMT): 2019/284/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3788749
31 A = 6789609
24 meter
Y = 2205863
42 meter E =
0018131
Z = -5199153
22 I = 51
86140
XDOT = -5133
251146 Wp = 100
35200
YDOT = 5491
002181 meter/sec RA = 141
59204 deg
ZDOT = -1418
413356 TA = 156
05393
MA = 155
96949
Ha = 229
479 n
mi
Hp = 219
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12430279
89 X = 3789056
02
Y = 7237084
70 feet Y = 2248233
09 meter
Z = -17057589
29 Z = -5180748
14
XDOT = -16841
375152 XDOT = -5187
381662
YDOT = 18015
099018 feet/sec YDOT = 5433
295741 meter/sec
ZDOT = -4653
587127 ZDOT = -1443
481076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7082278
15 X = 2158678
38
Y = 12632510
22 feet Y = 3850389
12 meter
Z = -16973792
37 Z = -5173611
91
XDOT = -22735
550433 XDOT = -6929
795772
YDOT = 6372
363276 feet/sec YDOT = 1942
296327 meter/sec
ZDOT = -4768
133993 ZDOT = -1453
327241
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 19284
87977826
00016717 00000-0 10270-3 0 9094
2 25544 51
6422 142
6221 0007234 142
9706 217
1945 15
50168365 33358
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
87977826 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 142
6221 deg
Eccentricity:
0007234
Arg of perigee: 142
9706 deg
Mean anomaly: 217
1945 deg
Mean motion: 15
50168365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3335
Checksum: 326
Coasting Arc #11 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2019/285/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3645631
13 A = 6789102
72 meter
Y = -2239762
27 meter E =
0010645
Z = 5266128
89 I = 51
88605
XDOT = 4970
103930 Wp = 138
15416
YDOT = -5753
917914 meter/sec RA = 136
65043 deg
ZDOT = 984
599513 TA = 302
40010
MA = 302
50305
Ha = 229
455 n
mi
Hp = 219
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11960732
06 X = -3645894
86
Y = -7348301
42 feet Y = -2280531
25 meter
Z = 17277325
76 Z = 5248419
07
XDOT = 16306
115257 XDOT = 5029
293803
YDOT = -18877
683444 feet/sec YDOT = -5698
007655 meter/sec
ZDOT = 3230
313362 ZDOT = 1008
887132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6837006
67 X = -2083919
63
Y = -12373018
15 feet Y = -3771295
93 meter
Z = 17196697
14 Z = 5241553
29
XDOT = 22604
373165 XDOT = 6889
812941
YDOT = -7805
965576 feet/sec YDOT = -2379
258307 meter/sec
ZDOT = 3341
333785 ZDOT = 1018
438538
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 19285
91122743
00016717 00000-0 10270-3 0 9102
2 25544 51
6426 137
5109 0007191 145
7704 214
3911 15
50217347 33516
Satellite: ISS
Catalog Number: 25544
Epoch time: 19285
91122743 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 137
5109 deg
Eccentricity:
0007191
Arg of perigee: 145
7704 deg
Mean anomaly: 214
3911 deg
Mean motion: 15
50217347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 292
Coasting Arc #12 (Orbit 3365)
---------------------------------------
Vector Time (GMT): 2019/286/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3509028
40 A = 6789002
12 meter
Y = 2345780
98 meter E =
0018991
Z = -5332784
28 I = 51
90719
XDOT = -4765
535313 Wp = 105
64195
YDOT = 5960
119618 meter/sec RA = 131
71010 deg
ZDOT = -520
558531 TA = 159
43546
MA = 159
35891
Ha = 229
325 n
mi
Hp = 219
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11512560
37 X = 3508440
63
Y = 7696131
83 feet Y = 2385017
64 meter
Z = -17496011
41 Z = -5315740
03
XDOT = -15634
958375 XDOT = -4829
300277
YDOT = 19554
198223 feet/sec YDOT = 5906
471458 meter/sec
ZDOT = -1707
869196 ZDOT = -543
863603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6489870
31 X = 1978112
47
Y = 12343422
79 feet Y = 3762275
27 meter
Z = -17418421
39 Z = -5309134
84
XDOT = -22206
642211 XDOT = -6768
584546
YDOT = 9145
578553 feet/sec YDOT = 2787
572343 meter/sec
ZDOT = -1814
439348 ZDOT = -553
041113
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 19286
87821108
00016717 00000-0 10270-3 0 9110
2 25544 51
6410 132
7194 0007128 149
0343 211
1229 15
50172901 33665
Satellite: ISS
Catalog Number: 25544
Epoch time: 19286
87821108 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 132
7194 deg
Eccentricity:
0007128
Arg of perigee: 149
0343 deg
Mean anomaly: 211
1229 deg
Mean motion: 15
50172901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3366
Checksum: 289
Coasting Arc #13 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2019/287/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3402603
25 A = 6788750
39 meter
Y = -2435604
67 meter E =
0008685
Z = 5340976
44 I = 51
92832
XDOT = 4543
801724 Wp = 139
51805
YDOT = -6174
853653 meter/sec RA = 126
77138 deg
ZDOT = 72
372404 TA = 309
75668
MA = 309
83316
Ha = 229
303 n
mi
Hp = 219
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11163396
50 X = -3401058
84
Y = -7990828
97 feet Y = -2473645
93 meter
Z = 17522888
57 Z = 5324451
41
XDOT = 14907
485970 XDOT = 4612
161468
YDOT = -20258
706212 feet/sec YDOT = -6123
659426 meter/sec
ZDOT = 237
442270 ZDOT = 94
611529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6255114
54 X = -1906558
91
Y = -12327964
88 feet Y = -3757563
70 meter
Z = 17447670
81 Z = 5318050
06
XDOT = 21732
616157 XDOT = 6624
101405
YDOT = -10516
608032 feet/sec YDOT = -3205
462128 meter/sec
ZDOT = 339
184701 ZDOT = 103
383497
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 19287
90965641
00016717 00000-0 10270-3 0 9127
2 25544 51
6411 127
6083 0007147 153
0912 207
0611 15
50220332 33823
Satellite: ISS
Catalog Number: 25544
Epoch time: 19287
90965641 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 127
6083 deg
Eccentricity:
0007147
Arg of perigee: 153
0912 deg
Mean anomaly: 207
0611 deg
Mean motion: 15
50220332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 284
Coasting Arc #14 (Orbit 3396)
---------------------------------------
Vector Time (GMT): 2019/288/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3316964
79 A = 6788926
26 meter
Y = 2587866
28 meter E =
0019019
Z = -5343825
67 I = 51
94704
XDOT = -4287
666582 Wp = 112
39673
YDOT = 6321
610259 meter/sec RA = 121
83291 deg
ZDOT = 394
064638 TA = 161
38954
MA = 161
31989
Ha = 229
146 n
mi
Hp = 219
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10882430
41 X = 3313738
01
Y = 8490374
92 feet Y = 2624940
56 meter
Z = -17532236
46 Z = -5327720
68
XDOT = -14067
147579 XDOT = -4359
952188
YDOT = 20740
191137 feet/sec YDOT = 6273
258393 meter/sec
ZDOT = 1292
862984 ZDOT = 373
060270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5990268
40 X = 1825833
81
Y = 12537745
03 feet Y = 3821504
69 meter
Z = -17458943
48 Z = -5321485
97
XDOT = -21001
570800 XDOT = -6401
278780
YDOT = 11727
704451 feet/sec YDOT = 3574
604317 meter/sec
ZDOT = 1196
719484 ZDOT = 364
760099
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 19288
87663529
00016717 00000-0 10270-3 0 9135
2 25544 51
6406 122
8159 0007041 156
0326 204
1153 15
50180416 33976
Satellite: ISS
Catalog Number: 25544
Epoch time: 19288
87663529 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 122
8159 deg
Eccentricity:
0007041
Arg of perigee: 156
0326 deg
Mean anomaly: 204
1153 deg
Mean motion: 15
50180416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3397
Checksum: 305
Coasting Arc #15 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2019/289/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3261593
16 A = 6788943
62 meter
Y = -2720053
73 meter E =
0007264
Z = 5291333
94 I = 51
96486
XDOT = 4025
850163 Wp = 133
03276
YDOT = -6469
625292 meter/sec RA = 116
89660 deg
ZDOT = -848
310182 TA = 325
01883
MA = 325
06653
Ha = 229
111 n
mi
Hp = 219
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10700764
97 X = -3256637
38
Y = -8924060
80 feet Y = -2756499
25 meter
Z = 17360019
48 Z = 5275502
06
XDOT = 13208
169825 XDOT = 4102
016908
YDOT = -21225
804765 feet/sec YDOT = -6424
179552 meter/sec
ZDOT = -2783
169888 ZDOT = -828
568337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5851594
98 X = -1783566
15
Y = -12743627
64 feet Y = -3884257
70 meter
Z = 17287981
35 Z = 5269376
72
XDOT = 20221
437609 XDOT = 6163
494183
YDOT = -12919
935481 feet/sec YDOT = -3937
996335 meter/sec
ZDOT = -2692
750261 ZDOT = -820
750280
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 19289
90807405
00016717 00000-0 10270-3 0 9144
2 25544 51
6412 117
7047 0006986 159
3458 200
7976 15
50228401 34132
Satellite: ISS
Catalog Number: 25544
Epoch time: 19289
90807405 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 117
7047 deg
Eccentricity:
0006986
Arg of perigee: 159
3458 deg
Mean anomaly: 200
7976 deg
Mean motion: 15
50228401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 320
Coasting Arc #16 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2019/290/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3239827
42 A = 6789405
95 meter
Y = 2899715
98 meter E =
0018330
Z = -5230004
82 I = 51
97935
XDOT = -3739
488249 Wp = 119
50924
YDOT = 6543
263625 meter/sec RA = 111
96100 deg
ZDOT = 1306
011053 TA = 163
03926
MA = 162
97791
Ha = 228
984 n
mi
Hp = 219
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10629355
05 X = 3232566
28
Y = 9513503
87 feet Y = 2935905
32 meter
Z = -17158808
47 Z = -5214284
24
XDOT = -12268
662233 XDOT = -3818
723033
YDOT = 21467
400346 feet/sec YDOT = 6501
003023 meter/sec
ZDOT = 4284
813166 ZDOT = 1287
652982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5756349
06 X = 1754535
19
Y = 13145477
94 feet Y = 4006741
68 meter
Z = -17087290
84 Z = -5208206
25
XDOT = -19217
502230 XDOT = -5857
494680
YDOT = 13898
371515 feet/sec YDOT = 4236
223638 meter/sec
ZDOT = 4200
674343 ZDOT = 1280
365540
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 19290
87504865
00016717 00000-0 10270-3 0 9157
2 25544 51
6405 112
9127 0006953 161
5728 198
5676 15
50187793 34284
Satellite: ISS
Catalog Number: 25544
Epoch time: 19290
87504865 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 112
9127 deg
Eccentricity:
0006953
Arg of perigee: 161
5728 deg
Mean anomaly: 198
5676 deg
Mean motion: 15
50187793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3428
Checksum: 345
Coasting Arc #17 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2019/291/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3246621
59 A = 6789702
52 meter
Y = -3053037
12 meter E =
0007080
Z = 5116204
75 I = 51
99233
XDOT = 3459
008910 Wp = 122
25520
YDOT = -6614
099948 meter/sec RA = 107
02732 deg
ZDOT = -1753
793808 TA = 344
61015
MA = 344
63167
Ha = 228
950 n
mi
Hp = 219
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10651645
62 X = -3237092
60
Y = -10016525
98 feet Y = -3089289
85 meter
Z = 16785448
65 Z = 5100456
66
XDOT = 11348
454428 XDOT = 3541
231765
YDOT = -21699
802980 feet/sec YDOT = -6574
959135 meter/sec
ZDOT = -5753
916692 ZDOT = -1736
791132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5796325
56 X = -1766720
03
Y = -13512607
29 feet Y = -4118642
70 meter
Z = 16713817
26 Z = 5094371
50
XDOT = 18202
889726 XDOT = 5548
240789
YDOT = -14821
061951 feet/sec YDOT = -4517
459683 meter/sec
ZDOT = -5675
930343 ZDOT = -1730
023568
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 19291
90648364
00016717 00000-0 10270-3 0 9166
2 25544 51
6406 107
8019 0006960 166
0410 194
0934 15
50231241 34448
Satellite: ISS
Catalog Number: 25544
Epoch time: 19291
90648364 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 107
8019 deg
Eccentricity:
0006960
Arg of perigee: 166
0410 deg
Mean anomaly: 194
0934 deg
Mean motion: 15
50231241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3444
Checksum: 298
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