[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 22nd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15514 9498 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
118/11:34:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
5
120/08:22:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 217
5
122/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 659)
---------------------------------------
Vector Time (GMT): 2019/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 568385
84 A = 6792539
74 meter
Y = 6539682
16 meter E =
0013588
Z = 1718093
00 I = 51
27247
XDOT = -4811
680310 Wp = 121
18650
YDOT = 1911
270046 meter/sec RA = 277
14880 deg
ZDOT = -5656
810605 TA = 39
87431
MA = 39
77456
Ha = 223
077 n
mi
Hp = 217
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1864782
93 X = 486869
34
Y = 21455650
12 feet Y = 6545582
44 meter
Z = 5636788
07 Z = 1720656
13
XDOT = -15786
352722 XDOT = -4805
217012
YDOT = 6270
571018 feet/sec YDOT = 1857
498675 meter/sec
ZDOT = -18559
089912 ZDOT = -5680
168567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12115882
08 X = 3692920
86
Y = 17801808
17 feet Y = 5425991
13 meter
Z = 5647720
30 Z = 1721425
15
XDOT = -9275
282337 XDOT = -2827
106056
YDOT = 12261
647848 feet/sec YDOT = 3737
350264 meter/sec
ZDOT = -18664
854111 ZDOT = -5689
047533
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 19112
53559131
00016717 00000-0 10270-3 0 9003
2 25544 51
6372 277
8343 0001447 222
1410 137
9631 15
52594880 6607
Satellite: ISS
Catalog Number: 25544
Epoch time: 19112
53559131 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 277
8343 deg
Eccentricity:
0001447
Arg of perigee: 222
1410 deg
Mean anomaly: 137
9631 deg
Mean motion: 15
52594880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 294
Coasting Arc #2 (Orbit 674)
---------------------------------------
Vector Time (GMT): 2019/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -195229
99 A = 6793673
13 meter
Y = -6763333
59 meter E =
0009461
Z = -561021
49 I = 51
27494
XDOT = 4795
255164 Wp = 41
92834
YDOT = -626
271614 meter/sec RA = 272
15884 deg
ZDOT = 5946
429301 TA = 311
99163
MA = 312
07217
Ha = 223
164 n
mi
Hp = 217
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -640518
35 X = -116860
80
Y = -22189414
67 feet Y = -6765078
59 meter
Z = -1840621
70 Z = -561779
69
XDOT = 15732
464448 XDOT = 4773
017137
YDOT = -2054
696896 feet/sec YDOT = -572
772214 meter/sec
ZDOT = 19509
282484 ZDOT = 5969
669091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11756586
22 X = -3583407
48
Y = -18829574
84 feet Y = -5739254
41 meter
Z = -1843384
78 Z = -561863
68
XDOT = 11051
387870 XDOT = 3368
463023
YDOT = -8799
446690 feet/sec YDOT = -2682
071351 meter/sec
ZDOT = 19614
388346 ZDOT = 5978
465568
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 19113
50108658
00016717 00000-0 10270-3 0 9016
2 25544 51
6389 273
0322 0001421 215
6249 144
4809 15
52588302 6757
Satellite: ISS
Catalog Number: 25544
Epoch time: 19113
50108658 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 273
0322 deg
Eccentricity:
0001421
Arg of perigee: 215
6249 deg
Mean anomaly: 144
4809 deg
Mean motion: 15
52588302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 675
Checksum: 297
Coasting Arc #3 (Orbit 690)
---------------------------------------
Vector Time (GMT): 2019/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -194892
68 A = 6793556
60 meter
Y = 6753176
70 meter E =
0010824
Z = -658458
45 I = 51
27353
XDOT = -4800
138244 Wp = 146
18061
YDOT = -711
726734 meter/sec RA = 267
17045 deg
ZDOT = -5934
771406 TA = 40
96207
MA = 40
88081
Ha = 223
079 n
mi
Hp = 217
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -639411
68 X = -267195
69
Y = 22156091
54 feet Y = 6750593
02 meter
Z = -2160296
74 Z = -659580
57
XDOT = -15748
485053 XDOT = -4762
994708
YDOT = -2335
061463 feet/sec YDOT = -765
197370 meter/sec
ZDOT = -19471
034795 ZDOT = -5957
998669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10991042
49 X = 3350069
75
Y = 19247687
33 feet Y = 5866695
10 meter
Z = -2166019
16 Z = -660202
64
XDOT = -13150
248399 XDOT = -4008
195712
YDOT = 5326
882894 feet/sec YDOT = 1623
633906 meter/sec
ZDOT = -19575
960326 ZDOT = -5966
752708
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 19114
53094319
00016717 00000-0 10270-3 0 9029
2 25544 51
6378 267
9102 0001256 224
1737 135
9315 15
52611692 6910
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
53094319 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 267
9102 deg
Eccentricity:
0001256
Arg of perigee: 224
1737 deg
Mean anomaly: 135
9315 deg
Mean motion: 15
52611692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 691
Checksum: 303
Coasting Arc #4 (Orbit 706)
---------------------------------------
Vector Time (GMT): 2019/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 572606
22 A = 6792341
91 meter
Y = -6515029
03 meter E =
0012587
Z = 1812630
87 I = 51
27305
XDOT = 4821
216757 Wp = 68
65943
YDOT = 1994
292419 meter/sec RA = 262
18120 deg
ZDOT = 5617
855730 TA = 311
36120
MA = 311
46939
Ha = 223
053 n
mi
Hp = 217
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1878629
32 X = 636611
77
Y = -21374767
15 feet Y = -6508267
92 meter
Z = 5946951
68 Z = 1815567
67
XDOT = 15817
640279 XDOT = 4771
269137
YDOT = 6542
954132 feet/sec YDOT = 2047
927210 meter/sec
ZDOT = 18431
285203 ZDOT = 5641
154247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9876865
30 X = -3010468
54
Y = -19044475
91 feet Y = -5804756
26 meter
Z = 5960840
74 Z = 1816864
26
XDOT = 15372
072420 XDOT = 4685
407673
YDOT = -2142
698038 feet/sec YDOT = -653
094362 meter/sec
ZDOT = 18536
420691 ZDOT = 5649
901026
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 19115
56079814
00016717 00000-0 10270-3 0 9037
2 25544 51
6387 262
7887 0001496 222
2716 137
8321 15
52613864 7074
Satellite: ISS
Catalog Number: 25544
Epoch time: 19115
56079814 = yrday
fracday
Element set: 903
Inclination: 51
6387 deg
RA of node: 262
7887 deg
Eccentricity:
0001496
Arg of perigee: 222
2716 deg
Mean anomaly: 137
8321 deg
Mean motion: 15
52613864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 707
Checksum: 325
Coasting Arc #5 (Orbit 721)
---------------------------------------
Vector Time (GMT): 2019/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1012651
76 A = 6790189
04 meter
Y = 6052810
12 meter E =
0004182
Z = -2904938
57 I = 51
27171
XDOT = -4841
004904 Wp = 132
22452
YDOT = -3205
884192 meter/sec RA = 257
18816 deg
ZDOT = -4999
708634 TA = 81
03485
MA = 80
98751
Ha = 223
029 n
mi
Hp = 217
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3322348
29 X = -1066150
13
Y = 19858300
91 feet Y = 6041186
86 meter
Z = -9530638
36 Z = -2909987
49
XDOT = -15882
562022 XDOT = -4780
510128
YDOT = -10517
992757 feet/sec YDOT = -3259
681357 meter/sec
ZDOT = -16403
243550 ZDOT = -5023
077615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8183592
21 X = 2494358
91
Y = 18384034
29 feet Y = 5603453
65 meter
Z = -9554019
18 Z = -2912065
05
XDOT = -17617
268329 XDOT = -5369
743387
YDOT = -724
520316 feet/sec YDOT = -220
833792 meter/sec
ZDOT = -16508
598445 ZDOT = -5031
820806
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 19116
52628527
00016717 00000-0 10270-3 0 9046
2 25544 51
6390 257
9867 0001372 230
6141 129
4890 15
52598850 7222
Satellite: ISS
Catalog Number: 25544
Epoch time: 19116
52628527 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 257
9867 deg
Eccentricity:
0001372
Arg of perigee: 230
6141 deg
Mean anomaly: 129
4890 deg
Mean motion: 15
52598850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 722
Checksum: 322
Coasting Arc #6 (Orbit 737)
---------------------------------------
Vector Time (GMT): 2019/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1481171
68 A = 6787493
62 meter
Y = -5406370
30 meter E =
0010416
Z = 3820310
65 I = 51
27210
XDOT = 4851
969981 Wp = 103
02373
YDOT = 4260
027395 meter/sec RA = 252
19106 deg
ZDOT = 4135
624751 TA = 303
18723
MA = 303
28707
Ha = 222
938 n
mi
Hp = 217
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4859487
14 X = 1522960
18
Y = -17737435
37 feet Y = -5389573
17 meter
Z = 12533827
58 Z = 3827607
09
XDOT = 15918
536683 XDOT = 4783
883926
YDOT = 13976
467832 feet/sec YDOT = 4313
904797 meter/sec
ZDOT = 13568
322674 ZDOT = 4159
028513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6050159
87 X = -1844088
73
Y = -17343201
22 feet Y = -5286207
73 meter
Z = 12567298
81 Z = 3830512
68
XDOT = 19686
811535 XDOT = 6000
540156
YDOT = 3068
728317 feet/sec YDOT = 935
348391 meter/sec
ZDOT = 13673
755886 ZDOT = 4167
760794
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 19117
55613271
00016717 00000-0 10270-3 0 9051
2 25544 51
6397 252
8646 0001379 235
1649 124
9374 15
52624197 7386
Satellite: ISS
Catalog Number: 25544
Epoch time: 19117
55613271 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 252
8646 deg
Eccentricity:
0001379
Arg of perigee: 235
1649 deg
Mean anomaly: 124
9374 deg
Mean motion: 15
52624197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 738
Checksum: 331
Coasting Arc #7 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2019/118/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4515888
42 A = 6788923
88 meter
Y = 3775351
59 meter E =
0011390
Z = 3371999
27 I = 51
28637
XDOT = -1513
886055 Wp = 94
13341
YDOT = 5938
862784 meter/sec RA = 247
23040 deg
ZDOT = -4609
121767 TA = 46
29398
MA = 46
19968
Ha = 222
967 n
mi
Hp = 217
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14815906
89 X = 4456956
39
Y = 12386324
11 feet Y = 3825521
92 meter
Z = 11062989
74 Z = 3393792
67
XDOT = -4966
817765 XDOT = -1557
794982
YDOT = 19484
457953 feet/sec YDOT = 5921
687922 meter/sec
ZDOT = -15121
790574 ZDOT = -4616
582347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18891627
02 X = 5758167
92
Y = 3722349
08 feet Y = 1134572
00 meter
Z = 11161201
08 Z = 3401934
09
XDOT = 5425
741847 XDOT = 1653
766115
YDOT = 18031
408092 feet/sec YDOT = 5495
973187 meter/sec
ZDOT = -15156
039006 ZDOT = -4619
560689
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 19118
52161458
00016717 00000-0 10270-3 0 9065
2 25544 51
6384 248
0630 0001300 235
1665 124
9365 15
52583684 7536
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
52161458 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 248
0630 deg
Eccentricity:
0001300
Arg of perigee: 235
1665 deg
Mean anomaly: 124
9365 deg
Mean motion: 15
52583684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 305
Coasting Arc #8 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2019/119/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4509417
09 A = 6791326
12 meter
Y = -4488512
25 meter E =
0004365
Z = -2371807
82 I = 51
30966
XDOT = 2195
155154 Wp = 41
48061
YDOT = -5027
475354 meter/sec RA = 242
23734 deg
ZDOT = 5349
537754 TA = 291
93534
MA = 291
98172
Ha = 222
952 n
mi
Hp = 217
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14794675
48 X = -4447369
14
Y = -14726090
05 feet Y = -4538592
81 meter
Z = -7781521
70 Z = -2393562
20
XDOT = 7201
952605 XDOT = 2225
225472
YDOT = -16494
341712 feet/sec YDOT = -5002
759382 meter/sec
ZDOT = 17550
976882 ZDOT = 5360
274147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20119009
91 X = -6132274
22
Y = -5425031
54 feet Y = -1653549
61 meter
Z = -7879511
66 Z = -2401675
15
XDOT = -2469
456980 XDOT = -752
690487
YDOT = -16362
905074 feet/sec YDOT = -4987
413467 meter/sec
ZDOT = 17599
949004 ZDOT = 5364
464456
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 19119
48709140
00016717 00000-0 10270-3 0 9078
2 25544 51
6396 243
2613 0001297 245
5216 114
5801 15
52601896 7681
Satellite: ISS
Catalog Number: 25544
Epoch time: 19119
48709140 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 243
2613 deg
Eccentricity:
0001297
Arg of perigee: 245
5216 deg
Mean anomaly: 114
5801 deg
Mean motion: 15
52601896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 313
Coasting Arc #9 (Orbit 781)
---------------------------------------
Vector Time (GMT): 2019/120/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5076994
17 A = 6788530
46 meter
Y = 2860009
89 meter E =
0010880
Z = 3473266
71 I = 51
31232
XDOT = -387
711516 Wp = 89
41159
YDOT = 6186
043315 meter/sec RA = 237
90400 deg
ZDOT = -4514
673881 TA = 49
59791
MA = 49
50302
Ha = 222
800 n
mi
Hp = 217
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16656805
03 X = 5027764
08
Y = 9383234
56 feet Y = 2916509
21 meter
Z = 11395231
98 Z = 3497809
37
XDOT = -1272
019410 XDOT = -434
926876
YDOT = 20295
417699 feet/sec YDOT = 6181
443562 meter/sec
ZDOT = -14811
922183 ZDOT = -4516
672056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13017069
79 X = 3967602
87
Y = 13910927
31 feet Y = 4240050
64 meter
Z = 11505978
96 Z = 3507022
39
XDOT = -6170
920651 XDOT = -1880
896614
YDOT = 18066
833412 feet/sec YDOT = 5506
770824 meter/sec
ZDOT = -14821
468557 ZDOT = -4517
583616
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 19120
38819904
00016717 00000-0 10270-3 0 9080
2 25544 51
6373 238
7797 0001333 261
6028 98
4973 15
52613220 7829
Satellite: ISS
Catalog Number: 25544
Epoch time: 19120
38819904 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 238
7797 deg
Eccentricity:
0001333
Arg of perigee: 261
6028 deg
Mean anomaly: 98
4973 deg
Mean motion: 15
52613220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 782
Checksum: 323
Coasting Arc #10 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2019/121/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5203393
87 A = 6791020
82 meter
Y = -3584159
91 meter E =
0004374
Z = -2486707
59 I = 51
33983
XDOT = 1207
684624 Wp = 43
64404
YDOT = -5414
409234 meter/sec RA = 232
91187 deg
ZDOT = 5285
558959 TA = 288
38649
MA = 288
43405
Ha = 222
958 n
mi
Hp = 217
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17071502
21 X = -5150848
88
Y = -11759054
81 feet Y = -3642054
16 meter
Z = -8158489
45 Z = -2511856
27
XDOT = 3962
219896 XDOT = 1242
465768
YDOT = -17763
809824 feet/sec YDOT = -5400
709466 meter/sec
ZDOT = 17341
072701 ZDOT = 5291
510097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13002048
71 X = -3963024
45
Y = -16087087
68 feet Y = -4903344
33 meter
Z = -8271931
27 Z = -2521284
65
XDOT = 7533
306163 XDOT = 2296
151718
YDOT = -15004
979352 feet/sec YDOT = -4573
517706 meter/sec
ZDOT = 17368
422330 ZDOT = 5293
895126
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 19121
35367057
00016717 00000-0 10270-3 0 9096
2 25544 51
6378 233
9773 0001052 258
3732 101
7302 15
52621217 7973
Satellite: ISS
Catalog Number: 25544
Epoch time: 19121
35367057 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 233
9773 deg
Eccentricity:
0001052
Arg of perigee: 258
3732 deg
Mean anomaly: 101
7302 deg
Mean motion: 15
52621217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 303
Coasting Arc #11 (Orbit 812)
---------------------------------------
Vector Time (GMT): 2019/122/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5194693
67 A = 6792858
04 meter
Y = 4156476
06 meter E =
0012792
Z = 1339686
53 I = 51
36629
XDOT = -2134
592484 Wp = 122
83161
YDOT = 4545
996808 meter/sec RA = 227
92638 deg
ZDOT = -5793
757368 TA = 42
53039
MA = 42
43137
Ha = 222
869 n
mi
Hp = 217
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17042958
25 X = 5141321
15
Y = 13636732
47 feet Y = 4214268
36 meter
Z = 4395297
03 Z = 1364791
04
XDOT = -7003
256180 XDOT = -2157
125229
YDOT = 14914
687690 feet/sec YDOT = 4522
000210 meter/sec
ZDOT = -19008
390314 ZDOT = -5804
181366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12774417
04 X = 3893642
31
Y = 17670007
53 feet Y = 5385818
29 meter
Z = 4508507
24 Z = 1374193
01
XDOT = -9305
254593 XDOT = -2836
241600
YDOT = 11616
674211 feet/sec YDOT = 3540
762299 meter/sec
ZDOT = -19055
894024 ZDOT = -5808
236499
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 19122
38350195
00016717 00000-0 10270-3 0 9107
2 25544 51
6370 228
8553 0001203 269
1998 90
9016 15
52641618 8133
Satellite: ISS
Catalog Number: 25544
Epoch time: 19122
38350195 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 228
8553 deg
Eccentricity:
0001203
Arg of perigee: 269
1998 deg
Mean anomaly: 90
9016 deg
Mean motion: 15
52641618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 813
Checksum: 304
Coasting Arc #12 (Orbit 814)
---------------------------------------
Vector Time (GMT): 2019/122/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 301114
67 A = 6784911
21 meter
Y = -5033470
40 meter E =
0007772
Z = 4535652
11 I = 51
34554
XDOT = 6264
106972 Wp = 118
37831
YDOT = 3164
798667 meter/sec RA = 227
41403 deg
ZDOT = 3088
620163 TA = 300
53209
MA = 300
60877
Ha = 222
856 n
mi
Hp = 217
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 987909
02 X = 335346
00
Y = -16514010
50 feet Y = -5029911
65 meter
Z = 14880748
40 Z = 4537198
06
XDOT = 20551
532060 XDOT = 6213
248719
YDOT = 10383
197726 feet/sec YDOT = 3234
563983 meter/sec
ZDOT = 10133
268250 ZDOT = 3118
925691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5955515
30 X = -1815241
06
Y = -15427260
64 feet Y = -4702229
04 meter
Z = 14888137
79 Z = 4537904
40
XDOT = 21814
480080 XDOT = 6649
053529
YDOT = 1514
234209 feet/sec YDOT = 461
538587 meter/sec
ZDOT = 10270
080833 ZDOT = 3130
320638
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 19122
51223083
00016717 00000-0 10270-3 0 9118
2 25544 51
6404 228
2152 0001258 258
3474 101
7537 15
52648505 8152
Satellite: ISS
Catalog Number: 25544
Epoch time: 19122
51223083 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 228
2152 deg
Eccentricity:
0001258
Arg of perigee: 258
3474 deg
Mean anomaly: 101
7537 deg
Mean motion: 15
52648505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 815
Checksum: 284
Coasting Arc #13 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2019/123/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1188777
45 A = 6782894
27 meter
Y = 4381731
79 meter E =
0011805
Z = -5050090
45 I = 51
36297
XDOT = -6368
528936 Wp = 75
34742
YDOT = -3836
530637 meter/sec RA = 222
41457 deg
ZDOT = -1830
318966 TA = 176
83630
MA = 176
82883
Ha = 222
898 n
mi
Hp = 217
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3900188
49 X = -1213155
91
Y = 14375760
47 feet Y = 4368301
72 meter
Z = -16568538
21 Z = -5055924
41
XDOT = -20894
123806 XDOT = -6316
263607
YDOT = -12587
042771 feet/sec YDOT = -3907
455759 meter/sec
ZDOT = -6004
983484 ZDOT = -1861
128471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2685049
87 X = 818403
20
Y = 14621150
60 feet Y = 4456526
70 meter
Z = -16595266
80 Z = -5058237
32
XDOT = -23160
821518 XDOT = -7059
418399
YDOT = -2717
807873 feet/sec YDOT = -828
387840 meter/sec
ZDOT = -6144
037808 ZDOT = -1872
702724
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 19123
47769556
00016717 00000-0 10270-3 0 9125
2 25544 51
6414 223
4142 0001255 265
7387 94
3621 15
52626325 8305
Satellite: ISS
Catalog Number: 25544
Epoch time: 19123
47769556 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 223
4142 deg
Eccentricity:
0001255
Arg of perigee: 265
7387 deg
Mean anomaly: 94
3621 deg
Mean motion: 15
52626325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 304
Coasting Arc #14 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2019/124/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2127906
34 A = 6781677
02 meter
Y = -3682796
44 meter E =
0001672
Z = 5280946
92 I = 51
38502
XDOT = 6304
712847 Wp = 125
43902
YDOT = 4336
878857 meter/sec RA = 217
41265 deg
ZDOT = 482
945482 TA = 319
93115
MA = 319
94348
Ha = 222
754 n
mi
Hp = 217
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6981320
01 X = 2143277
85
Y = -12082665
50 feet Y = -3658914
84 meter
Z = 17325941
35 Z = 5291320
98
XDOT = 20684
753436 XDOT = 6253
402125
YDOT = 14228
605175 feet/sec YDOT = 4407
095667 meter/sec
ZDOT = 1584
466805 ZDOT = 513
447463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 835727
29 X = 254729
68
Y = -13870580
94 feet Y = -4227753
07 meter
Z = 17373152
35 Z = 5295336
84
XDOT = 23817
581217 XDOT = 7259
598755
YDOT = 3596
363640 feet/sec YDOT = 1096
171638 meter/sec
ZDOT = 1722
107467 ZDOT = 524
898356
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 19124
50751849
00016717 00000-0 10270-3 0 9137
2 25544 51
6416 218
2917 0001223 274
1435 85
9577 15
52673602 8465
Satellite: ISS
Catalog Number: 25544
Epoch time: 19124
50751849 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 218
2917 deg
Eccentricity:
0001223
Arg of perigee: 274
1435 deg
Mean anomaly: 85
9577 deg
Mean motion: 15
52673602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 316
Coasting Arc #15 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2019/125/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3101625
33 A = 6781884
93 meter
Y = 2991559
09 meter E =
0013359
Z = -5248557
15 I = 51
41226
XDOT = -6008
128967 Wp = 96
63886
YDOT = -4660
435509 meter/sec RA = 212
41348 deg
ZDOT = 894
602097 TA = 181
95568
MA = 181
96091
Ha = 222
904 n
mi
Hp = 217
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10175936
12 X = -3109352
16
Y = 9814826
41 feet Y = 2956831
53 meter
Z = -17219675
69 Z = -5263642
66
XDOT = -19711
709209 XDOT = -5959
913684
YDOT = -15290
142747 feet/sec YDOT = -4727
353057 meter/sec
ZDOT = 2935
046249 ZDOT = 865
533180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4474999
94 X = -1363979
98
Y = 13322608
74 feet Y = 4060731
14 meter
Z = -17288151
90 Z = -5269428
70
XDOT = -23562
041117 XDOT = -7181
710133
YDOT = -4277
803142 feet/sec YDOT = -1303
874398 meter/sec
ZDOT = 2803
896160 ZDOT = 854
627550
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 19125
47297725
00016717 00000-0 10270-3 0 9143
2 25544 51
6412 213
4914 0001129 280
9801 79
1223 15
52657455 8610
Satellite: ISS
Catalog Number: 25544
Epoch time: 19125
47297725 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 213
4914 deg
Eccentricity:
0001129
Arg of perigee: 280
9801 deg
Mean anomaly: 79
1223 deg
Mean motion: 15
52657455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 307
Coasting Arc #16 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2019/126/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4049629
80 A = 6783218
73 meter
Y = -2317706
68 meter E =
0005683
Z = 4921068
09 I = 51
44556
XDOT = 5498
186659 Wp = 49
02938
YDOT = 4855
998853 meter/sec RA = 207
41586 deg
ZDOT = -2232
148107 TA = 62
85449
MA = 62
79656
Ha = 222
765 n
mi
Hp = 217
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13286187
02 X = 4051341
78
Y = -7604024
54 feet Y = -2272411
60 meter
Z = 16145236
51 Z = 4940744
10
XDOT = 18038
670140 XDOT = 5454
319616
YDOT = 15931
754768 feet/sec YDOT = 4917
238280 meter/sec
ZDOT = -7323
320560 ZDOT = -2205
545689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8036624
91 X = 2449563
27
Y = -12917749
41 feet Y = -3937330
02 meter
Z = 16234439
53 Z = 4948257
17
XDOT = 22520
038469 XDOT = 6864
107725
YDOT = 4935
858333 feet/sec YDOT = 1504
449620 meter/sec
ZDOT = -7203
326760 ZDOT = -2195
573996
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 19126
50279624
00016717 00000-0 10270-3 0 9157
2 25544 51
6412 208
3689 0001186 286
7915 73
3106 15
52662341 8778
Satellite: ISS
Catalog Number: 25544
Epoch time: 19126
50279624 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 208
3689 deg
Eccentricity:
0001186
Arg of perigee: 286
7915 deg
Mean anomaly: 73
3106 deg
Mean motion: 15
52662341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 319
Coasting Arc #17 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2019/127/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4925635
18 A = 6785446
09 meter
Y = 1712261
58 meter E =
0007697
Z = -4349399
21 I = 51
48289
XDOT = -4749
509317 Wp = 110
79397
YDOT = -4924
154521 meter/sec RA = 202
42513 deg
ZDOT = 3442
492938 TA = 194
25849
MA = 194
28022
Ha = 222
873 n
mi
Hp = 217
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16160220
40 X = -4923288
75
Y = 5617656
10 feet Y = 1657193
14 meter
Z = -14269682
46 Z = -4373320
70
XDOT = -15582
379648 XDOT = -4710
815044
YDOT = -16155
362603 feet/sec YDOT = -4977
050778 meter/sec
ZDOT = 11294
268169 ZDOT = 3419
514776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11301476
97 X = -3444690
18
Y = 12723305
89 feet Y = 3878063
63 meter
Z = -14378064
08 Z = -4382433
93
XDOT = -20611
783020 XDOT = -6282
471464
YDOT = -5670
676369 feet/sec YDOT = -1728
422157 meter/sec
ZDOT = 11190
661156 ZDOT = 3410
913520
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 19127
46824849
00016717 00000-0 10270-3 0 9169
2 25544 51
6409 203
5678 0001173 291
7236 68
3791 15
52672878 8924
Satellite: ISS
Catalog Number: 25544
Epoch time: 19127
46824849 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 203
5678 deg
Eccentricity:
0001173
Arg of perigee: 291
7236 deg
Mean anomaly: 68
3791 deg
Mean motion: 15
52672878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 347
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