[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 28th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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
087/06:36:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 216
6
090/20:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
1
000/00:00:00
000 0
0 0
0 216
7
094/11:01:35
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
9
094/14:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
0
000/00:00:00
000 0
0 0
0 216
9
097/20:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
9
Coasting Arc #1 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2019/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4107361
51 A = 6793893
42 meter
Y = -5335796
51 meter E =
0011937
Z = -865275
78 I = 51
93988
XDOT = 4237
812275 Wp = 136
81547
YDOT = -2305
433086 meter/sec RA = 46
63732 deg
ZDOT = -5956
659535 TA = 52
50020
MA = 52
39173
Ha = 224
313 n
mi
Hp = 216
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13475595
52 X = -4043186
84
Y = -17505894
06 feet Y = -5381369
12 meter
Z = -2838831
31 Z = -885071
62
XDOT = 13903
583581 XDOT = 4292
211394
YDOT = -7563
756843 feet/sec YDOT = -2257
739042 meter/sec
ZDOT = -19542
846242 ZDOT = -5935
941642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14571340
05 X = -4441344
45
Y = -16589480
94 feet Y = -5056473
79 meter
Z = -2927820
96 Z = -892399
83
XDOT = 12300
113760 XDOT = 3749
074674
YDOT = -7403
279687 feet/sec YDOT = -2256
519649 meter/sec
ZDOT = -19448
823938 ZDOT = -5928
001536
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 19086
53050576
00016717 00000-0 10270-3 0 9002
2 25544 51
6400 47
1586 0002034 118
7833 241
3523 15
52443233 2564
Satellite: ISS
Catalog Number: 25544
Epoch time: 19086
53050576 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 47
1586 deg
Eccentricity:
0002034
Arg of perigee: 118
7833 deg
Mean anomaly: 241
3523 deg
Mean motion: 15
52443233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 280
Coasting Arc #2 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2019/087/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3278572
69 A = 6791928
32 meter
Y = -5486412
14 meter E =
0008035
Z = -2293299
26 I = 51
91715
XDOT = 5310
205910 Wp = 132
07409
YDOT = -902
525642 meter/sec RA = 42
80821 deg
ZDOT = -5449
925407 TA = 73
33440
MA = 73
24621
Ha = 224
329 n
mi
Hp = 216
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10756472
06 X = -3205838
88
Y = -18000039
82 feet Y = -5522668
87 meter
Z = -7523947
71 Z = -2309048
33
XDOT = 17421
935400 XDOT = 5346
376130
YDOT = -2961
042131 feet/sec YDOT = -842
941242 meter/sec
ZDOT = -17880
332699 ZDOT = -5424
042645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14969375
28 X = 4562665
59
Y = -14647620
90 feet Y = -4464594
85 meter
Z = -7594598
05 Z = -2314833
48
XDOT = 5945
840868 XDOT = 1812
292297
YDOT = 15256
954329 feet/sec YDOT = 4650
319679 meter/sec
ZDOT = -17763
094504 ZDOT = -5414
191205
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 19087
30296931
00016717 00000-0 10270-3 0 9016
2 25544 51
6418 43
3179 0002249 125
4430 234
6932 15
52454595 2680
Satellite: ISS
Catalog Number: 25544
Epoch time: 19087
30296931 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 43
3179 deg
Eccentricity:
0002249
Arg of perigee: 125
4430 deg
Mean anomaly: 234
6932 deg
Mean motion: 15
52454595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 310
Coasting Arc #3 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2019/088/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2669192
68 A = 6789720
49 meter
Y = 5315998
57 meter E =
0014573
Z = 3261748
19 I = 51
88323
XDOT = -6002
962019 Wp = 92
82321
YDOT = 75
017696 meter/sec RA = 37
85780 deg
ZDOT = 4771
092427 TA = 304
84684
MA = 304
98380
Ha = 224
382 n
mi
Hp = 216
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8757193
83 X = 2593705
65
Y = 17440940
20 feet Y = 5345425
46 meter
Z = 10701273
58 Z = 3274530
39
XDOT = -19694
757279 XDOT = -6026
529890
YDOT = 246
121050 feet/sec YDOT = 7
756871 meter/sec
ZDOT = 15653
190376 ZDOT = 4741
875252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14684437
13 X = -4475816
44
Y = 12806791
36 feet Y = 3903510
01 meter
Z = 10758508
10 Z = 3279193
27
XDOT = -4303
048464 XDOT = -1311
569172
YDOT = -18024
762255 feet/sec YDOT = -5493
947535 meter/sec
ZDOT = 15520
959928 ZDOT = 4730
788586
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 19088
33291910
00016717 00000-0 10270-3 0 9023
2 25544 51
6406 38
1965 0002307 125
2498 234
8870 15
52430468 2843
Satellite: ISS
Catalog Number: 25544
Epoch time: 19088
33291910 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 38
1965 deg
Eccentricity:
0002307
Arg of perigee: 125
2498 deg
Mean anomaly: 234
8870 deg
Mean motion: 15
52430468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 310
Coasting Arc #4 (Orbit 298)
---------------------------------------
Vector Time (GMT): 2019/089/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1882020
96 A = 6786974
37 meter
Y = -5066289
66 meter E =
0008799
Z = -4113644
41 I = 51
84935
XDOT = 6589
899111 Wp = 82
90544
YDOT = 667
710705 meter/sec RA = 32
90140 deg
ZDOT = -3843
252880 TA = 147
46443
MA = 147
41017
Ha = 224
264 n
mi
Hp = 216
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6174609
45 X = -1805246
77
Y = -16621685
23 feet Y = -5086906
74 meter
Z = -13496208
71 Z = -4122599
68
XDOT = 21620
403909 XDOT = 6600
611038
YDOT = 2190
651920 feet/sec YDOT = 741
463204 meter/sec
ZDOT = -12609
097374 ZDOT = -3811
215924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14372913
42 X = 4380864
01
Y = -10331793
38 feet Y = -3149130
62 meter
Z = -13536147
03 Z = -4125817
61
XDOT = 2976
659278 XDOT = 907
285748
YDOT = 20445
177756 feet/sec YDOT = 6231
690180 meter/sec
ZDOT = -12464
198158 ZDOT = -3799
087599
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 19089
29849073
00016717 00000-0 10270-3 0 9039
2 25544 51
6425 33
3956 0002182 131
1541 228
9799 15
52465464 2991
Satellite: ISS
Catalog Number: 25544
Epoch time: 19089
29849073 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 33
3956 deg
Eccentricity:
0002182
Arg of perigee: 131
1541 deg
Mean anomaly: 228
9799 deg
Mean motion: 15
52465464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 299
Checksum: 334
Coasting Arc #5 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2019/090/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 996944
70 A = 6784651
36 meter
Y = 4747454
59 meter E =
0009873
Z = 4738179
66 I = 51
81120
XDOT = -7041
279514 Wp = 120
22251
YDOT = -1280
657726 meter/sec RA = 27
93797 deg
ZDOT = 2755
565240 TA = 302
52608
MA = 302
62144
Ha = 224
283 n
mi
Hp = 216
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3270815
95 X = 920767
98
Y = 15575638
43 feet Y = 4758177
57 meter
Z = 15545208
87 Z = 4742837
01
XDOT = -23101
310743 XDOT = -7039
820406
YDOT = -4201
632960 feet/sec YDOT = -1359
389864 meter/sec
ZDOT = 9040
568373 ZDOT = 2721
365292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14023806
82 X = -4274456
32
Y = 7482856
09 feet Y = 2280774
54 meter
Z = 15565730
80 Z = 4744434
75
XDOT = -2042
147653 XDOT = -622
446605
YDOT = -22373
929633 feet/sec YDOT = -6819
573752 meter/sec
ZDOT = 8885
961436 ZDOT = 2708
441046
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 19090
32843181
00016717 00000-0 10270-3 0 9040
2 25544 51
6408 28
2740 0002228 131
2442 228
8902 15
52457758 3159
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
32843181 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 28
2740 deg
Eccentricity:
0002228
Arg of perigee: 131
2442 deg
Mean anomaly: 228
8902 deg
Mean motion: 15
52457758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 293
Coasting Arc #6 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2019/090/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3529732
94 A = 6789018
85 meter
Y = 4651938
79 meter E =
0013760
Z = 3453009
66 I = 51
80610
XDOT = -6033
989707 Wp = 98
02459
YDOT = 1160
323979 meter/sec RA = 25
08541 deg
ZDOT = 4587
355172 TA = 302
33905
MA = 302
47220
Ha = 224
133 n
mi
Hp = 216
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11580488
63 X = 3460678
64
Y = 15262266
38 feet Y = 4691024
93 meter
Z = 11328771
84 Z = 3469987
51
XDOT = -19796
554157 XDOT = -6068
798962
YDOT = 3806
837201 feet/sec YDOT = 1092
653450 meter/sec
ZDOT = 15050
377861 ZDOT = 4557
959915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2893968
95 X = 882081
73
Y = -18892731
59 feet Y = -5758504
59 meter
Z = 11405051
52 Z = 3476259
70
XDOT = 15240
673617 XDOT = 4645
357318
YDOT = 11374
128484 feet/sec YDOT = 3466
834362 meter/sec
ZDOT = 14917
232934 ZDOT = 4546
772598
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 19090
90777222
00016717 00000-0 10270-3 0 9057
2 25544 51
6380 25
3900 0002231 143
2689 216
8616 15
52477646 3241
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
90777222 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 25
3900 deg
Eccentricity:
0002231
Arg of perigee: 143
2689 deg
Mean anomaly: 216
8616 deg
Mean motion: 15
52477646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 324
Checksum: 302
Coasting Arc #7 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2019/091/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2671450
80 A = 6786352
50 meter
Y = -4558995
57 meter E =
0009240
Z = -4267043
86 I = 51
76863
XDOT = 6728
112067 Wp = 82
49609
YDOT = -566
123577 meter/sec RA = 20
12305 deg
ZDOT = -3612
914693 TA = 150
61554
MA = 150
56356
Ha = 224
151 n
mi
Hp = 216
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8764602
36 X = -2599545
48
Y = -14957334
53 feet Y = -4588467
97 meter
Z = -13999487
73 Z = -4279845
59
XDOT = 22073
858487 XDOT = 6751
491994
YDOT = -1857
360818 feet/sec YDOT = -490
754750 meter/sec
ZDOT = -11853
394663 ZDOT = -3580
175428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4367233
44 X = -1331132
75
Y = 16728935
32 feet Y = 5098979
48 meter
Z = -14056875
99 Z = -4284535
80
XDOT = -15825
775912 XDOT = -4823
696498
YDOT = -13951
836123 feet/sec YDOT = -4252
519650 meter/sec
ZDOT = -11705
199254 ZDOT = -3567
744733
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 19091
87333744
00016717 00000-0 10270-3 0 9062
2 25544 51
6399 20
5894 0002215 142
3051 217
8257 15
52485597 3397
Satellite: ISS
Catalog Number: 25544
Epoch time: 19091
87333744 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 20
5894 deg
Eccentricity:
0002215
Arg of perigee: 142
3051 deg
Mean anomaly: 217
8257 deg
Mean motion: 15
52485597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 323
Coasting Arc #8 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2019/092/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1708499
06 A = 6784086
33 meter
Y = 4424146
58 meter E =
0008971
Z = 4846827
91 I = 51
72947
XDOT = -7253
886911 Wp = 126
59098
YDOT = 67
946817 meter/sec RA = 15
15257 deg
ZDOT = 2486
545026 TA = 298
96994
MA = 299
05985
Ha = 224
037 n
mi
Hp = 216
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5605311
87 X = 1635356
91
Y = 14514916
61 feet Y = 4442843
77 meter
Z = 15901666
36 Z = 4854949
00
XDOT = -23798
841573 XDOT = -7266
185799
YDOT = 222
922629 feet/sec YDOT = -13
239723 meter/sec
ZDOT = 8157
956122 ZDOT = 2451
278625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6064525
66 X = 1848467
42
Y = -14288826
26 feet Y = -4355234
24 meter
Z = 15937888
53 Z = 4857868
43
XDOT = 16344
644578 XDOT = 4981
847667
YDOT = 15889
285631 feet/sec YDOT = 4843
054260 meter/sec
ZDOT = 7998
399266 ZDOT = 2437
912096
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 19092
90326717
00016717 00000-0 10270-3 0 9070
2 25544 51
6399 15
4670 0002177 149
4306 210
6973 15
52493335 3553
Satellite: ISS
Catalog Number: 25544
Epoch time: 19092
90326717 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 15
4670 deg
Eccentricity:
0002177
Arg of perigee: 149
4306 deg
Mean anomaly: 210
6973 deg
Mean motion: 15
52493335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 317
Coasting Arc #9 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2019/093/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -627370
19 A = 6782568
10 meter
Y = -4301727
27 meter E =
0015166
Z = -5219403
88 I = 51
69240
XDOT = 7547
442317 Wp = 88
56580
YDOT = 376
043185 meter/sec RA = 10
17848 deg
ZDOT = -1219
823647 TA = 169
73243
MA = 169
70142
Ha = 224
110 n
mi
Hp = 216
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2058301
15 X = -553867
46
Y = -14113278
43 feet Y = -4308332
56 meter
Z = -17124028
46 Z = -5222272
40
XDOT = 24761
949860 XDOT = 7548
601581
YDOT = 1233
737482 feet/sec YDOT = 460
450313 meter/sec
ZDOT = -4002
046087 ZDOT = -1183
158242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8155446
77 X = -2485780
18
Y = 11682578
99 feet Y = 3560850
08 meter
Z = -17136499
60 Z = -5223205
08
XDOT = -16510
597114 XDOT = -5032
430000
YDOT = -17139
991368 feet/sec YDOT = -5224
269369 meter/sec
ZDOT = -3836
228479 ZDOT = -1169
282440
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 19093
86882332
00016717 00000-0 10270-3 0 9087
2 25544 51
6404 10
6673 0002284 148
8214 211
3074 15
52495649 3707
Satellite: ISS
Catalog Number: 25544
Epoch time: 19093
86882332 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 10
6673 deg
Eccentricity:
0002284
Arg of perigee: 148
8214 deg
Mean anomaly: 211
3074 deg
Mean motion: 15
52495649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 308
Coasting Arc #10 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2019/094/11:01:35
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2626254
75 A = 6784502
35 meter
Y = 4094192
11 meter E =
0009273
Z = 4725257
12 I = 51
68019
XDOT = -7032
458111 Wp = 123
36598
YDOT = 1314
496067 meter/sec RA = 7
16902 deg
ZDOT = 2760
734558 TA = 299
27344
MA = 299
36610
Ha = 223
872 n
mi
Hp = 216
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8616321
34 X = 2557324
41
Y = 13432388
81 feet Y = 4123175
84 meter
Z = 15502812
07 Z = 4737846
63
XDOT = -23072
369131 XDOT = -7060
044660
YDOT = 4312
651139 feet/sec YDOT = 1235
700259 meter/sec
ZDOT = 9057
528078 ZDOT = 2726
506292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7794454
02 X = 2375749
59
Y = 13862272
75 feet Y = 4225220
74 meter
Z = 15559277
79 Z = 4742467
87
XDOT = -22316
387274 XDOT = -6802
034841
YDOT = 2522
983218 feet/sec YDOT = 769
005285 meter/sec
ZDOT = 8902
546169 ZDOT = 2713
496072
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 19094
51252414
00016717 00000-0 10270-3 0 9093
2 25544 51
6414 7
4705 0001818 151
5014 208
6237 15
52512039 3803
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
51252414 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 7
4705 deg
Eccentricity:
0001818
Arg of perigee: 151
5014 deg
Mean anomaly: 208
6237 deg
Mean motion: 15
52512039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 380
Checksum: 280
Coasting Arc #11 (Orbit 381)
---------------------------------------
Vector Time (GMT): 2019/094/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4925505
34 A = 6787653
31 meter
Y = 2549071
33 meter E =
0011990
Z = 3903234
63 I = 51
68739
XDOT = -5233
734895 Wp = 88
16670
YDOT = -3838
310552 meter/sec RA = 6
42185 deg
ZDOT = -4086
576572 TA = 44
65191
MA = 44
55541
Ha = 223
994 n
mi
Hp = 216
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16159794
44 X = -4972603
51
Y = 8363094
93 feet Y = 2493727
98 meter
Z = 12805887
91 Z = 3879193
64
XDOT = -17171
046243 XDOT = -5170
574457
YDOT = -12592
882390 feet/sec YDOT = -3896
485141 meter/sec
ZDOT = -13407
403450 ZDOT = -4111
846331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4660588
23 X = -1420547
29
Y = 17667488
99 feet Y = 5385050
64 meter
Z = 12696843
24 Z = 3869997
82
XDOT = -19501
463977 XDOT = -5944
046220
YDOT = 4599
428947 feet/sec YDOT = 1401
905943 meter/sec
ZDOT = -13521
254822 ZDOT = -4121
278470
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 19094
64126367
00016717 00000-0 10270-3 0 9106
2 25544 51
6429 6
8313 0001621 148
8179 211
3069 15
52523772 3822
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
64126367 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 6
8313 deg
Eccentricity:
0001621
Arg of perigee: 148
8179 deg
Mean anomaly: 211
3069 deg
Mean motion: 15
52523772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 302
Coasting Arc #12 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2019/095/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5646262
30 A = 6790306
73 meter
Y = -2253005
86 meter E =
0004815
Z = -3029112
15 I = 51
66272
XDOT = 4252
071335 Wp = 87
42924
YDOT = 4018
717449 meter/sec RA = 1
45297 deg
ZDOT = 4943
806676 TA = 237
91942
MA = 237
96618
Ha = 223
875 n
mi
Hp = 217
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18524482
62 X = 5685750
26
Y = -7391751
53 feet Y = -2189644
93 meter
Z = -9938032
00 Z = -3001588
40
XDOT = 13950
365272 XDOT = 4182
802438
YDOT = 13184
768534 feet/sec YDOT = 4065
880295 meter/sec
ZDOT = 16219
838177 ZDOT = 4964
293124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6628632
81 X = 2020407
28
Y = -18876431
80 feet Y = -5753536
41 meter
Z = -9813280
63 Z = -2991087
94
XDOT = 17656
855152 XDOT = 5381
809450
YDOT = -2267
649231 feet/sec YDOT = -691
179486 meter/sec
ZDOT = 16312
021049 ZDOT = 4971
904016
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 19095
60681262
00016717 00000-0 10270-3 0 9114
2 25544 51
6429 2
0299 0001570 158
2707 201
8511 15
52491080 3976
Satellite: ISS
Catalog Number: 25544
Epoch time: 19095
60681262 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 2
0299 deg
Eccentricity:
0001570
Arg of perigee: 158
2707 deg
Mean anomaly: 201
8511 deg
Mean motion: 15
52491080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 294
Coasting Arc #13 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2019/096/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6192837
92 A = 6792469
12 meter
Y = 1945720
11 meter E =
0015121
Z = 1974015
56 I = 51
63691
XDOT = -3118
300687 Wp = 116
28324
YDOT = -4235
025656 meter/sec RA = 356
48626 deg
ZDOT = -5581
735975 TA = 41
93575
MA = 41
82005
Ha = 223
887 n
mi
Hp = 216
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20317709
71 X = -6223724
02
Y = 6383596
15 feet Y = 1876294
94 meter
Z = 6476429
02 Z = 1943857
58
XDOT = -10230
645298 XDOT = -3043
598411
YDOT = -13894
441127 feet/sec YDOT = -4269
479499 meter/sec
ZDOT = -18312
782070 ZDOT = -5596
701840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8213754
74 X = -2503552
45
Y = 19693775
02 feet Y = 6002662
62 meter
Z = 6339812
23 Z = 1932374
77
XDOT = -15704
746164 XDOT = -4786
806631
YDOT = -604
458813 feet/sec YDOT = -184
239046 meter/sec
ZDOT = -18379
962394 ZDOT = -5602
212538
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 19096
63672619
00016717 00000-0 10270-3 0 9125
2 25544 51
6430 356
9082 0001585 156
4926 203
6298 15
52507307 4139
Satellite: ISS
Catalog Number: 25544
Epoch time: 19096
63672619 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 356
9082 deg
Eccentricity:
0001585
Arg of perigee: 156
4926 deg
Mean anomaly: 203
6298 deg
Mean motion: 15
52507307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 318
Coasting Arc #14 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2019/097/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6528683
35 A = 6793772
84 meter
Y = -1658672
10 meter E =
0009482
Z = -855408
99 I = 51
60625
XDOT = 1905
285895 Wp = 46
96075
YDOT = 4466
271791 meter/sec RA = 351
52039 deg
ZDOT = 5929
229262 TA = 303
78974
MA = 303
88001
Ha = 223
814 n
mi
Hp = 217
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21419564
79 X = 6550901
02
Y = -5441837
59 feet Y = -1585539
63 meter
Z = -2806459
95 Z = -823640
61
XDOT = 6250
937975 XDOT = 1826
399896
YDOT = 14653
122675 feet/sec YDOT = 4487
137388 meter/sec
ZDOT = 19452
851908 ZDOT = 5938
292615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9284058
12 X = 2829780
91
Y = -20074968
56 feet Y = -6118850
42 meter
Z = -2662606
16 Z = -811562
36
XDOT = 13771
601347 XDOT = 4197
584091
YDOT = 3805
462671 feet/sec YDOT = 1159
905022 meter/sec
ZDOT = 19493
305941 ZDOT = 5941
559651
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 19097
60226586
00016717 00000-0 10270-3 0 9132
2 25544 51
6410 352
1066 0001550 162
9015 197
2190 15
52503886 4283
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
60226586 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 352
1066 deg
Eccentricity:
0001550
Arg of perigee: 162
9015 deg
Mean anomaly: 197
2190 deg
Mean motion: 15
52503886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 299
Coasting Arc #15 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2019/097/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2021294
27 A = 6782482
04 meter
Y = -3854304
00 meter E =
0014582
Z = -5214663
21 I = 51
56052
XDOT = 7238
025151 Wp = 89
22607
YDOT = -2190
275822 meter/sec RA = 350
33509 deg
ZDOT = -1189
381674 TA = 169
34817
MA = 169
31725
Ha = 223
869 n
mi
Hp = 216
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6631542
89 X = -1952713
85
Y = -12645354
33 feet Y = -3876524
43 meter
Z = -17108475
09 Z = -5224315
19
XDOT = 23746
801675 XDOT = 7267
756923
YDOT = -7185
944298 feet/sec YDOT = -2109
169000 meter/sec
ZDOT = -3902
170847 ZDOT = -1154
149236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3637277
43 X = -1108642
16
Y = 13754015
81 feet Y = 4192224
02 meter
Z = -17151662
58 Z = -5227826
75
XDOT = -21457
975456 XDOT = -6540
390919
YDOT = -10330
744199 feet/sec YDOT = -3148
810832 meter/sec
ZDOT = -3742
592285 ZDOT = -1140
742129
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 19097
85974417
00016717 00000-0 10270-3 0 9143
2 25544 51
6408 350
8225 0002158 165
0205 195
1011 15
52517464 4323
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
85974417 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 350
8225 deg
Eccentricity:
0002158
Arg of perigee: 165
0205 deg
Mean anomaly: 195
1011 deg
Mean motion: 15
52517464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 300
Coasting Arc #16 (Orbit 447)
---------------------------------------
Vector Time (GMT): 2019/098/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 921484
36 A = 6782014
93 meter
Y = 4118011
37 meter E =
0003232
Z = 5306859
42 I = 51
52708
XDOT = -7444
150166 Wp = 121
00185
YDOT = 1836
530711 meter/sec RA = 345
34522 deg
ZDOT = -134
075258 TA = 330
26861
MA = 330
28698
Ha = 223
728 n
mi
Hp = 217
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3023242
64 X = 849588
97
Y = 13510536
00 feet Y = 4127914
31 meter
Z = 17410956
10 Z = 5311160
89
XDOT = -24423
064848 XDOT = -7463
482236
YDOT = 6025
363226 feet/sec YDOT = 1753
176916 meter/sec
ZDOT = -439
879454 ZDOT = -170
283682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6689776
63 X = 2039043
92
Y = -12093838
01 feet Y = -3686201
83 meter
Z = 17429915
16 Z = 5312638
14
XDOT = 21482
772831 XDOT = 6547
949159
YDOT = 11020
499353 feet/sec YDOT = 3359
048203 meter/sec
ZDOT = -603
818426 ZDOT = -184
043856
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 19098
88964864
00016717 00000-0 10270-3 0 9153
2 25544 51
6414 345
7001 0002082 171
1412 188
9777 15
52529729 4482
Satellite: ISS
Catalog Number: 25544
Epoch time: 19098
88964864 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 345
7001 deg
Eccentricity:
0002082
Arg of perigee: 171
1412 deg
Mean anomaly: 188
9777 deg
Mean motion: 15
52529729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 448
Checksum: 339
Coasting Arc #17 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2019/099/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 176956
36 A = 6782734
02 meter
Y = -4418344
36 meter E =
0014551
Z = -5156156
45 I = 51
49809
XDOT = 7382
486104 Wp = 108
69374
YDOT = -1405
241732 meter/sec RA = 340
35481 deg
ZDOT = 1456
340679 TA = 175
38284
MA = 175
36940
Ha = 223
757 n
mi
Hp = 216
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 580565
49 X = 251396
44
Y = -14495880
45 feet Y = -4415949
43 meter
Z = -16916523
79 Z = -5155115
93
XDOT = 24220
754933 XDOT = 7390
577053
YDOT = -4610
373135 feet/sec YDOT = -1322
640329 meter/sec
ZDOT = 4778
020602 ZDOT = 1492
222155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9869348
56 X = -3008177
44
Y = 10641452
82 feet Y = 3243514
82 meter
Z = -16911292
80 Z = -5154562
05
XDOT = -20694
681581 XDOT = -6307
738946
YDOT = -11335
713687 feet/sec YDOT = -3455
125532 meter/sec
ZDOT = 4940
421252 ZDOT = 1505
840397
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 19099
85518081
00016717 00000-0 10270-3 0 9168
2 25544 51
6419 340
8995 0002090 170
8133 189
3057 15
52541584 4636
Satellite: ISS
Catalog Number: 25544
Epoch time: 19099
85518081 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 340
8995 deg
Eccentricity:
0002090
Arg of perigee: 170
8133 deg
Mean anomaly: 189
3057 deg
Mean motion: 15
52541584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 328
Coasting Arc #18 (Orbit 478)
---------------------------------------
Vector Time (GMT): 2019/100/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1219786
92 A = 6784595
12 meter
Y = 4702763
73 meter E =
0007418
Z = 4730102
82 I = 51
47257
XDOT = -7118
209332 Wp = 77
80245
YDOT = 887
833093 meter/sec RA = 335
36346 deg
ZDOT = -2713
186044 TA = 39
11013
MA = 39
05654
Ha = 223
816 n
mi
Hp = 217
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4001925
57 X = -1295260
32
Y = 15429014
88 feet Y = 4688701
28 meter
Z = 15518710
03 Z = 4723994
13
XDOT = -23353
705157 XDOT = -7114
429024
YDOT = 2912
838230 feet/sec YDOT = 808
253403 meter/sec
ZDOT = -8901
529017 ZDOT = -2747
754775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12920642
81 X = 3938211
93
Y = -9380866
26 feet Y = -2859288
04 meter
Z = 15490532
82 Z = 4721514
40
XDOT = 19225
499118 XDOT = 5859
932131
YDOT = 11494
880446 feet/sec YDOT = 3503
639560 meter/sec
ZDOT = -9057
926267 ZDOT = -2760
855926
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 19100
88507925
00016717 00000-0 10270-3 0 9170
2 25544 51
6415 335
7775 0002077 171
8008 188
3178 15
52507650 4794
Satellite: ISS
Catalog Number: 25544
Epoch time: 19100
88507925 = yrday
fracday
Element set: 917
Inclination: 51
6415 deg
RA of node: 335
7775 deg
Eccentricity:
0002077
Arg of perigee: 171
8008 deg
Mean anomaly: 188
3178 deg
Mean motion: 15
52507650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 479
Checksum: 328
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