[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 12th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14325 6884 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
254/16:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 218
5
260/17:57:24
363 -1
0 2
2 2
2
N/A -2
0 -0
2 229
7
000/00:00:44
725 -0
5 -0
0 219
0
264/20:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 218
9
268/13:57:43
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 218
7
268/17:04:00
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
7
Coasting Arc #1 (Orbit 2863)
---------------------------------------
Vector Time (GMT): 2019/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3881207
33 A = 6788186
71 meter
Y = -1747772
16 meter E =
0019978
Z = -5303969
37 I = 51
26666
XDOT = 3005
487787 Wp = 69
38945
YDOT = -7032
330821 meter/sec RA = 292
38795 deg
ZDOT = 125
303624 TA = 201
77139
MA = 201
85642
Ha = 229
226 n
mi
Hp = 218
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12733619
84 X = -3835611
35
Y = -5734160
63 feet Y = -1790919
93 meter
Z = -17401474
32 Z = -5322711
74
XDOT = 9860
524234 XDOT = 3083
293321
YDOT = -23071
951512 feet/sec YDOT = -6998
286292 meter/sec
ZDOT = 411
101129 ZDOT = 140
092376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11335909
34 X = 3455185
17
Y = 7972119
81 feet Y = 2429902
12 meter
Z = -17486550
43 Z = -5329900
57
XDOT = -13377
898233 XDOT = -4077
583381
YDOT = 20021
016986 feet/sec YDOT = 6102
405977 meter/sec
ZDOT = 478
937312 ZDOT = 145
980093
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 19254
51588503
00016717 00000-0 10270-3 0 9003
2 25544 51
6425 293
0838 0008236 28
2688 331
8908 15
50419999 28645
Satellite: ISS
Catalog Number: 25544
Epoch time: 19254
51588503 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 293
0838 deg
Eccentricity:
0008236
Arg of perigee: 28
2688 deg
Mean anomaly: 331
8908 deg
Mean motion: 15
50419999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2864
Checksum: 342
Coasting Arc #2 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2019/254/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2435454
76 A = 6790576
38 meter
Y = -4216092
75 meter E =
0014992
Z = -4744305
34 I = 51
26985
XDOT = 4491
285401 Wp = 74
95776
YDOT = -5590
194779 meter/sec RA = 291
38317 deg
ZDOT = 2673
159651 TA = 221
58519
MA = 221
69931
Ha = 229
278 n
mi
Hp = 218
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7990337
14 X = -2365083
26
Y = -13832325
28 feet Y = -4242934
55 meter
Z = -15565306
22 Z = -4755964
53
XDOT = 14735
188322 XDOT = 4540
478205
YDOT = -18340
534052 feet/sec YDOT = -5539
694834 meter/sec
ZDOT = 8770
208828 ZDOT = 2695
096204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15922320
12 X = 4853123
17
Y = -127341
25 feet Y = -38813
61 meter
Z = -15617969
60 Z = -4760357
13
XDOT = 8830
589018 XDOT = 2691
563533
YDOT = 20601
043529 feet/sec YDOT = 6279
198067 meter/sec
ZDOT = 8870
421824 ZDOT = 2703
704572
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 19254
70925063
00016717 00000-0 10270-3 0 9011
2 25544 51
6402 292
1258 0008432 28
4904 331
6707 15
50422909 28670
Satellite: ISS
Catalog Number: 25544
Epoch time: 19254
70925063 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 292
1258 deg
Eccentricity:
0008432
Arg of perigee: 28
4904 deg
Mean anomaly: 331
6707 deg
Mean motion: 15
50422909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 305
Coasting Arc #3 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2019/255/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2429294
53 A = 6791491
77 meter
Y = 4481748
52 meter E =
0016581
Z = 4482097
43 I = 51
26214
XDOT = -4276
979027 Wp = 50
21898
YDOT = 5511
740365 meter/sec RA = 286
39782 deg
ZDOT = -3174
899667 TA = 71
94606
MA = 71
76547
Ha = 229
311 n
mi
Hp = 218
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7970126
40 X = 2357226
45
Y = 14703899
33 feet Y = 4508512
01 meter
Z = 14705044
05 Z = 4493722
50
XDOT = -14032
083421 XDOT = -4322
873287
YDOT = 18083
137680 feet/sec YDOT = 5463
655301 meter/sec
ZDOT = -10416
337491 ZDOT = -3195
787326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16678736
86 X = -5083678
99
Y = -23867
08 feet Y = -7274
69 meter
Z = 14757542
41 Z = 4498098
93
XDOT = -9325
730852 XDOT = -2842
482764
YDOT = -19639
593691 feet/sec YDOT = -5986
148157 meter/sec
ZDOT = -10511
756669 ZDOT = -3203
983433
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 19255
74053171
00016717 00000-0 10270-3 0 9029
2 25544 51
6403 287
0131 0008508 31
6097 328
5563 15
50451745 28830
Satellite: ISS
Catalog Number: 25544
Epoch time: 19255
74053171 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 287
0131 deg
Eccentricity:
0008508
Arg of perigee: 31
6097 deg
Mean anomaly: 328
5563 deg
Mean motion: 15
50451745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 303
Coasting Arc #4 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2019/256/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2508790
88 A = 6792528
09 meter
Y = -4698367
09 meter E =
0013190
Z = -4223472
07 I = 51
25636
XDOT = 4048
399775 Wp = 71
18549
YDOT = -5398
503277 meter/sec RA = 281
41342 deg
ZDOT = 3614
207785 TA = 236
00625
MA = 236
13163
Ha = 229
430 n
mi
Hp = 218
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8230941
21 X = -2435550
79
Y = -15414590
19 feet Y = -4726013
05 meter
Z = -13856535
68 Z = -4235480
42
XDOT = 13282
151493 XDOT = 4090
910827
YDOT = -17711
624923 feet/sec YDOT = -5352
993179 meter/sec
ZDOT = 11857
637089 ZDOT = 3633
977010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17430477
00 X = 5312809
39
Y = -174536
73 feet Y = -53198
80 meter
Z = -13910771
85 Z = -4240003
26
XDOT = 9686
158076 XDOT = 2952
340982
YDOT = 18575
838648 feet/sec YDOT = 5661
915620 meter/sec
ZDOT = 11947
944433 ZDOT = 3641
733463
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 19256
70735784
00016717 00000-0 10270-3 0 9034
2 25544 51
6396 282
2206 0008542 35
1259 325
0453 15
50427690 28986
Satellite: ISS
Catalog Number: 25544
Epoch time: 19256
70735784 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 282
2206 deg
Eccentricity:
0008542
Arg of perigee: 35
1259 deg
Mean anomaly: 325
0453 deg
Mean motion: 15
50427690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 324
Coasting Arc #5 (Orbit 2913)
---------------------------------------
Vector Time (GMT): 2019/257/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2578688
26 A = 6793611
70 meter
Y = 4936996
87 meter E =
0018392
Z = 3882242
93 I = 51
25522
XDOT = -3865
851367 Wp = 62
65382
YDOT = 5228
342430 meter/sec RA = 276
42864 deg
ZDOT = -4057
833303 TA = 70
19518
MA = 69
99698
Ha = 229
445 n
mi
Hp = 218
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8460263
34 X = 2504431
97
Y = 16197496
31 feet Y = 4965418
79 meter
Z = 12737017
50 Z = 3894588
32
XDOT = -12683
239392 XDOT = -3904
318249
YDOT = 17153
354429 feet/sec YDOT = 5184
896251 meter/sec
ZDOT = -13313
101387 ZDOT = -4076
706065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18231718
27 X = -5557027
73
Y = 340265
57 feet Y = 103712
94 meter
Z = 12792780
20 Z = 3899239
40
XDOT = -9782
744592 XDOT = -2981
780552
YDOT = -17554
676351 feet/sec YDOT = -5350
665352 meter/sec
ZDOT = -13399
303697 ZDOT = -4084
107767
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 19257
73863830
00016717 00000-0 10270-3 0 9043
2 25544 51
6401 277
1079 0008531 38
5490 321
6268 15
50454810 29145
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
73863830 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 277
1079 deg
Eccentricity:
0008531
Arg of perigee: 38
5490 deg
Mean anomaly: 321
6268 deg
Mean motion: 15
50454810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2914
Checksum: 312
Coasting Arc #6 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2019/258/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2725954
90 A = 6794688
51 meter
Y = -5110235
90 meter E =
0012324
Z = -3556741
89 I = 51
25653
XDOT = 3685
353695 Wp = 62
15146
YDOT = -5039
194667 meter/sec RA = 271
44462 deg
ZDOT = 4433
140478 TA = 255
70916
MA = 255
84605
Ha = 229
512 n
mi
Hp = 218
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8943421
60 X = -2651331
47
Y = -16765865
82 feet Y = -5140302
59 meter
Z = -11669100
69 Z = -3569801
78
XDOT = 12091
055430 XDOT = 3719
895766
YDOT = -16532
790902 feet/sec YDOT = -4997
788832 meter/sec
ZDOT = 14544
424142 ZDOT = 4451
126996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18946456
99 X = 5774880
09
Y = -854477
22 feet Y = -260444
66 meter
Z = -11728111
25 Z = -3574728
31
XDOT = 9763
904141 XDOT = 2976
037982
YDOT = 16523
040805 feet/sec YDOT = 5036
222837 meter/sec
ZDOT = 14626
569141 ZDOT = 4458
178274
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 19258
70546219
00016717 00000-0 10270-3 0 9051
2 25544 51
6405 272
3150 0008507 41
8273 318
3527 15
50436346 29296
Satellite: ISS
Catalog Number: 25544
Epoch time: 19258
70546219 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 272
3150 deg
Eccentricity:
0008507
Arg of perigee: 41
8273 deg
Mean anomaly: 318
3527 deg
Mean motion: 15
50436346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2929
Checksum: 311
Coasting Arc #7 (Orbit 2944)
---------------------------------------
Vector Time (GMT): 2019/259/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2856422
08 A = 6795801
28 meter
Y = 5297126
18 meter E =
0019659
Z = 3146080
33 I = 51
26111
XDOT = -3564
154715 Wp = 74
91535
YDOT = 4792
446851 meter/sec RA = 266
46099 deg
ZDOT = -4802
877716 TA = 68
64744
MA = 68
43774
Ha = 229
600 n
mi
Hp = 217
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9371463
51 X = 2781693
79
Y = 17379022
89 feet Y = 5328651
20 meter
Z = 10321785
87 Z = 3159773
78
XDOT = -11693
420980 XDOT = -3594
150510
YDOT = 15723
250825 feet/sec YDOT = 4752
421745 meter/sec
ZDOT = -15757
472822 ZDOT = -4820
264483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19667588
30 X = -5994680
91
Y = 1326379
67 feet Y = 404280
52 meter
Z = 10383675
44 Z = 3164944
27
XDOT = -9465
104642 XDOT = -2884
963895
YDOT = -15595
788805 feet/sec YDOT = -4753
596428 meter/sec
ZDOT = -15836
862136 ZDOT = -4827
075579
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 19259
73673934
00016717 00000-0 10270-3 0 9061
2 25544 51
6409 267
2019 0008652 45
4335 314
7520 15
50456190 29457
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
73673934 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 267
2019 deg
Eccentricity:
0008652
Arg of perigee: 45
4335 deg
Mean anomaly: 314
7520 deg
Mean motion: 15
50456190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2945
Checksum: 322
Coasting Arc #8 (Orbit 2959)
---------------------------------------
Vector Time (GMT): 2019/260/16:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3052681
99 A = 6796793
84 meter
Y = -5405332
38 meter E =
0013300
Z = -2765366
84 I = 51
26700
XDOT = 3455
992359 Wp = 52
71579
YDOT = -4548
942992 meter/sec RA = 261
47925 deg
ZDOT = 5101
442024 TA = 275
84160
MA = 275
99319
Ha = 229
642 n
mi
Hp = 217
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10015360
86 X = -2978578
38
Y = -17734030
12 feet Y = -5439055
54 meter
Z = -9072725
84 Z = -2780015
26
XDOT = 11338
557607 XDOT = 3481
822907
YDOT = -14924
353647 feet/sec YDOT = -4510
150742 meter/sec
ZDOT = 16737
014516 ZDOT = 5118
293249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20225962
24 X = 6164873
29
Y = -2123078
92 feet Y = -647114
45 meter
Z = -9138961
60 Z = -2785555
50
XDOT = 9107
843738 XDOT = 2776
070771
YDOT = 14739
947161 feet/sec YDOT = 4492
735895 meter/sec
ZDOT = 16813
943662 ZDOT = 5124
890028
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 19260
70356175
00016717 00000-0 10270-3 0 9076
2 25544 51
6404 262
4096 0008603 48
9646 311
2247 15
50439286 29605
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
70356175 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 262
4096 deg
Eccentricity:
0008603
Arg of perigee: 48
9646 deg
Mean anomaly: 311
2247 deg
Mean motion: 15
50439286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2960
Checksum: 315
Coasting Arc #9 (Orbit 2960)
---------------------------------------
Vector Time (GMT): 2019/260/17:57:46
725
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3644142
13 A = 6790572
02 meter
Y = 2800255
14 meter E =
0019140
Z = -5016599
85 I = 51
24399
XDOT = -2637
154118 Wp = 64
68724
YDOT = -6910
795068 meter/sec RA = 261
26556 deg
ZDOT = -1939
729303 TA = 186
31811
MA = 186
34228
Ha = 229
679 n
mi
Hp = 218
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11955846
88 X = -3650816
47
Y = 9187188
78 feet Y = 2759465
99 meter
Z = -16458660
92 Z = -5034318
35
XDOT = -8652
080441 XDOT = -2550
257398
YDOT = -22673
212166 feet/sec YDOT = -6939
799896 meter/sec
ZDOT = -6363
941284 ZDOT = -1952
328021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8104031
55 X = -2470108
82
Y = -12609785
00 feet Y = -3843462
47 meter
Z = -16539414
33 Z = -5041213
49
XDOT = 22425
896121 XDOT = 6835
413138
YDOT = -5981
581242 feet/sec YDOT = -1823
185963 meter/sec
ZDOT = -6420
755562 ZDOT = -1957
046295
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 19260
76801850
00016717 00000-0 10270-3 0 9088
2 25544 51
6419 262
0898 0006956 44
4188 315
7520 15
50037247 29613
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
76801850 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 262
0898 deg
Eccentricity:
0006956
Arg of perigee: 44
4188 deg
Mean anomaly: 315
7520 deg
Mean motion: 15
50037247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2961
Checksum: 325
Coasting Arc #10 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2019/261/17:57:46
725
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3560547
21 A = 6790079
36 meter
Y = -2696258
82 meter E =
0009152
Z = 5106245
86 I = 51
24884
XDOT = 2975
077685 Wp = 79
06530
YDOT = 6892
892319 meter/sec RA = 256
28253 deg
ZDOT = 1564
477266 TA = 355
76651
MA = 355
77425
Ha = 229
497 n
mi
Hp = 219
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11681585
32 X = 3565629
34
Y = -8845993
51 feet Y = -2656413
46 meter
Z = 16752775
12 Z = 5123554
41
XDOT = 9760
753559 XDOT = 2890
178807
YDOT = 22614
476111 feet/sec YDOT = 6925
687156 meter/sec
ZDOT = 5132
799430 ZDOT = 1578
722502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7999052
74 X = 2438111
27
Y = 12168691
41 feet Y = 3709017
14 meter
Z = 16831655
17 Z = 5130288
50
XDOT = -22362
400970 XDOT = -6816
059816
YDOT = 7508
133903 feet/sec YDOT = 2288
479214 meter/sec
ZDOT = 5197
115817 ZDOT = 1584
080901
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 19261
79957917
00016717 00000-0 10270-3 0 9099
2 25544 51
6421 256
9793 0006752 47
6937 312
4785 15
50047608 29779
Satellite: ISS
Catalog Number: 25544
Epoch time: 19261
79957917 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 256
9793 deg
Eccentricity:
0006752
Arg of perigee: 47
6937 deg
Mean anomaly: 312
4785 deg
Mean motion: 15
50047608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 362
Coasting Arc #11 (Orbit 2991)
---------------------------------------
Vector Time (GMT): 2019/262/17:57:46
725
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3523791
41 A = 6789753
54 meter
Y = 2608682
51 meter E =
0020359
Z = -5202376
55 I = 51
25799
XDOT = -3295
999809 Wp = 71
14983
YDOT = -6799
075298 meter/sec RA = 251
29967 deg
ZDOT = -1174
154801 TA = 187
48092
MA = 187
51134
Ha = 229
727 n
mi
Hp = 218
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11560995
43 X = -3527430
00
Y = 8558669
64 feet Y = 2569256
34 meter
Z = -17068164
52 Z = -5219503
00
XDOT = -10813
647667 XDOT = -3214
022156
YDOT = -22306
677486 feet/sec YDOT = -6835
475194 meter/sec
ZDOT = -3852
213915 ZDOT = -1189
966214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7926890
26 X = -2416116
15
Y = -11891238
65 feet Y = -3624449
54 meter
Z = -17146210
53 Z = -5226164
97
XDOT = 21989
923698 XDOT = 6702
528743
YDOT = -8988
706654 feet/sec YDOT = -2739
757788 meter/sec
ZDOT = -3923
673085 ZDOT = -1195
935556
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 19262
76666667
00016717 00000-0 10270-3 0 9108
2 25544 51
6433 252
1882 0006905 50
6883 309
4879 15
50045061 29921
Satellite: ISS
Catalog Number: 25544
Epoch time: 19262
76666667 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 252
1882 deg
Eccentricity:
0006905
Arg of perigee: 50
6883 deg
Mean anomaly: 309
4879 deg
Mean motion: 15
50045061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2992
Checksum: 333
Coasting Arc #12 (Orbit 3007)
---------------------------------------
Vector Time (GMT): 2019/263/17:57:46
725
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3498073
89 A = 6789447
40 meter
Y = -2500842
33 meter E =
0008751
Z = 5246532
02 I = 51
26854
XDOT = 3627
872810 Wp = 74
01829
YDOT = 6711
077887 meter/sec RA = 246
31731 deg
ZDOT = 781
371637 TA = 8
48407
MA = 8
46929
Ha = 229
610 n
mi
Hp = 218
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11476620
36 X = 3500294
03
Y = -8204863
29 feet Y = -2461711
78 meter
Z = 17213031
56 Z = 5263530
03
XDOT = 11902
469849 XDOT = 3548
762454
YDOT = 22017
972070 feet/sec YDOT = 6751
205016 meter/sec
ZDOT = 2563
555241 ZDOT = 798
802252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7779829
45 X = 2371292
01
Y = 11654798
39 feet Y = 3552382
55 meter
Z = 17290488
15 Z = 5270140
79
XDOT = -21591
059646 XDOT = -6580
954980
YDOT = 10498
560854 feet/sec YDOT = 3199
961348 meter/sec
ZDOT = 2642
399988 ZDOT = 805
403516
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 19263
79822417
00016717 00000-0 10270-3 0 9110
2 25544 51
6430 247
0776 0006866 54
4856 305
6934 15
50052810 30080
Satellite: ISS
Catalog Number: 25544
Epoch time: 19263
79822417 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 247
0776 deg
Eccentricity:
0006866
Arg of perigee: 54
4856 deg
Mean anomaly: 305
6934 deg
Mean motion: 15
50052810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3008
Checksum: 314
Coasting Arc #13 (Orbit 3022)
---------------------------------------
Vector Time (GMT): 2019/264/17:57:46
725
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514171
72 A = 6789333
70 meter
Y = 2424523
04 meter E =
0021010
Z = -5297081
98 I = 51
28214
XDOT = -3931
202239 Wp = 77
74404
YDOT = -6547
013723 meter/sec RA = 241
33650 deg
ZDOT = -385
535806 TA = 188
53287
MA = 188
56864
Ha = 229
787 n
mi
Hp = 218
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11529434
77 X = -3515291
77
Y = 7954471
91 feet Y = 2385218
68 meter
Z = -17378877
89 Z = -5314155
43
XDOT = -12897
645142 XDOT = -3855
826729
YDOT = -21479
703814 feet/sec YDOT = -6590
553757 meter/sec
ZDOT = -1264
881252 ZDOT = -404
449008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7727787
06 X = -2355429
49
Y = -11566013
28 feet Y = -3525320
85 meter
Z = -17456675
80 Z = -5320794
78
XDOT = 20885
338034 XDOT = 6365
851033
YDOT = -11901
016351 feet/sec YDOT = -3627
429784 meter/sec
ZDOT = -1350
498029 ZDOT = -411
631799
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 19264
76531037
00016717 00000-0 10270-3 0 9124
2 25544 51
6426 242
2872 0006878 57
3435 302
8379 15
50045585 30237
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
76531037 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 242
2872 deg
Eccentricity:
0006878
Arg of perigee: 57
3435 deg
Mean anomaly: 302
8379 deg
Mean motion: 15
50045585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3023
Checksum: 315
Coasting Arc #14 (Orbit 3024)
---------------------------------------
Vector Time (GMT): 2019/264/20:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -520503
96 A = 6797274
62 meter
Y = -6022243
34 meter E =
0019303
Z = 3086578
22 I = 51
30839
XDOT = 5577
710637 Wp = 75
15359
YDOT = 2019
752587 meter/sec RA = 240
92031 deg
ZDOT = 4860
665631 TA = 320
48331
MA = 320
62390
Ha = 229
783 n
mi
Hp = 218
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1707690
15 X = -468115
80
Y = -19758016
21 feet Y = -6027770
98 meter
Z = 10126568
95 Z = 3084177
19
XDOT = 18299
575582 XDOT = 5531
100037
YDOT = 6626
484866 feet/sec YDOT = 2081
865994 meter/sec
ZDOT = 15947
065719 ZDOT = 4887
647002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16118887
82 X = 4913037
01
Y = -11562460
08 feet Y = -3524237
83 meter
Z = 10116016
09 Z = 3083361
70
XDOT = 2684
897783 XDOT = 818
356844
YDOT = 17861
734143 feet/sec YDOT = 5444
256567 meter/sec
ZDOT = 16069
654359 ZDOT = 4898
030649
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 19264
89425447
00016717 00000-0 10270-3 0 9136
2 25544 51
6412 241
6477 0006832 56
8890 303
2915 15
50024037 30257
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
89425447 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 241
6477 deg
Eccentricity:
0006832
Arg of perigee: 56
8890 deg
Mean anomaly: 303
2915 deg
Mean motion: 15
50024037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3025
Checksum: 307
Coasting Arc #15 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2019/265/20:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 682770
62 A = 6796452
20 meter
Y = 5857557
69 meter E =
0011071
Z = -3391105
78 I = 51
32257
XDOT = -5784
139324 Wp = 73
48261
YDOT = -1982
902062 meter/sec RA = 235
94383 deg
ZDOT = -4599
174542 TA = 146
20050
MA = 146
12988
Ha = 229
782 n
mi
Hp = 218
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2240061
08 X = 633691
14
Y = 19217708
94 feet Y = 5864918
41 meter
Z = -11125675
14 Z = -3387908
46
XDOT = -18976
835053 XDOT = -5739
195726
YDOT = -6505
584192 feet/sec YDOT = -2047
333194 meter/sec
ZDOT = -15089
155323 ZDOT = -4627
162629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15175190
50 X = -4625398
06
Y = 12015303
46 feet Y = 3662264
49 meter
Z = -11111477
58 Z = -3386778
37
XDOT = -3438
843566 XDOT = -1048
159519
YDOT = -18386
203137 feet/sec YDOT = -5604
114716 meter/sec
ZDOT = -15216
342732 ZDOT = -4637
941265
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 19265
86133828
00016717 00000-0 10270-3 0 9144
2 25544 51
6409 236
8562 0006688 60
2622 299
9193 15
50024731 30402
Satellite: ISS
Catalog Number: 25544
Epoch time: 19265
86133828 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 236
8562 deg
Eccentricity:
0006688
Arg of perigee: 60
2622 deg
Mean anomaly: 299
9193 deg
Mean motion: 15
50024731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 320
Coasting Arc #16 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2019/266/20:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -849626
55 A = 6795706
38 meter
Y = -5666788
70 meter E =
0018062
Z = 3635824
15 I = 51
33944
XDOT = 6022
366605 Wp = 83
20753
YDOT = 1899
889891 meter/sec RA = 230
96756 deg
ZDOT = 4351
926879 TA = 320
11592
MA = 320
24850
Ha = 229
827 n
mi
Hp = 218
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2787488
69 X = -803856
55
Y = -18591826
43 feet Y = -5676033
80 meter
Z = 11928556
92 Z = 3631808
31
XDOT = 19758
420621 XDOT = 5979
534644
YDOT = 6233
234551 feet/sec YDOT = 1966
996876 meter/sec
ZDOT = 14277
975326 ZDOT = 4381
077199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14141354
21 X = 4310284
76
Y = -12404677
97 feet Y = -3780945
85 meter
Z = 11910610
35 Z = 3630354
03
XDOT = 4397
613346 XDOT = 1340
392548
YDOT = 18902
038185 feet/sec YDOT = 5761
341239 meter/sec
ZDOT = 14410
474047 ZDOT = 4392
312489
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 19266
89289282
00016717 00000-0 10270-3 0 9155
2 25544 51
6406 231
7447 0006773 63
5202 296
6643 15
50028410 30569
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
89289282 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 231
7447 deg
Eccentricity:
0006773
Arg of perigee: 63
5202 deg
Mean anomaly: 296
6643 deg
Mean motion: 15
50028410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 318
Coasting Arc #17 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2019/267/20:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 953355
43 A = 6794844
94 meter
Y = 5485612
41 meter E =
0013258
Z = -3909090
90 I = 51
35677
XDOT = -6236
630302 Wp = 71
34168
YDOT = -1796
585407 meter/sec RA = 225
99281 deg
ZDOT = -4049
322424 TA = 156
02347
MA = 155
96167
Ha = 229
883 n
mi
Hp = 218
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3127806
54 X = 910931
01
Y = 17997416
03 feet Y = 5496036
11 meter
Z = -12825101
38 Z = -3904563
15
XDOT = -20461
385504 XDOT = -6196
407540
YDOT = -5894
309079 feet/sec YDOT = -1866
103086 meter/sec
ZDOT = -13285
178558 ZDOT = -4079
519777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13238985
76 X = -4035242
86
Y = 12607130
33 feet Y = 3842653
32 meter
Z = -12804800
03 Z = -3902903
05
XDOT = -5399
107471 XDOT = -1645
647957
YDOT = -19278
656776 feet/sec YDOT = -5876
134585 meter/sec
ZDOT = -13422
466952 ZDOT = -4091
167927
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 19267
85997390
00016717 00000-0 10270-3 0 9169
2 25544 51
6388 226
9531 0006843 67
9430 292
2446 15
50034527 30713
Satellite: ISS
Catalog Number: 25544
Epoch time: 19267
85997390 = yrday
fracday
Element set: 916
Inclination: 51
6388 deg
RA of node: 226
9531 deg
Eccentricity:
0006843
Arg of perigee: 67
9430 deg
Mean anomaly: 292
2446 deg
Mean motion: 15
50034527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3071
Checksum: 336
Coasting Arc #18 (Orbit 3082)
---------------------------------------
Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1035358
41 A = 6790538
79 meter
Y = -4463141
75 meter E =
0011419
Z = 5002434
45 I = 51
36228
XDOT = 6418
904863 Wp = 95
68600
YDOT = 3705
254455 meter/sec RA = 222
27700 deg
ZDOT = 1972
277385 TA = 335
06486
MA = 335
11998
Ha = 229
784 n
mi
Hp = 218
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3396845
17 X = 1060890
65
Y = -14642853
51 feet Y = -4451420
57 meter
Z = 16412186
53 Z = 5007526
11
XDOT = 21059
399157 XDOT = 6367
414379
YDOT = 12156
346638 feet/sec YDOT = 3776
747397 meter/sec
ZDOT = 6470
726330 ZDOT = 2003
332604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5129422
62 X = 1563448
01
Y = 14102200
69 feet Y = 4298350
77 meter
Z = 16435587
67 Z = 5009567
12
XDOT = -23225
023781 XDOT = -7078
987249
YDOT = 722
744285 feet/sec YDOT = 220
292458 meter/sec
ZDOT = 6611
832961 ZDOT = 2015
286687
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 19268
63363911
00016717 00000-0 10270-3 0 9173
2 25544 51
6406 223
1217 0006795 71
1486 289
0400 15
50067426 30839
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
63363911 = yrday
fracday
Element set: 917
Inclination: 51
6406 deg
RA of node: 223
1217 deg
Eccentricity:
0006795
Arg of perigee: 71
1486 deg
Mean anomaly: 289
0400 deg
Mean motion: 15
50067426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3083
Checksum: 306
Coasting Arc #19 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916741
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1219050
09 A = 6790349
79 meter
Y = -4338334
09 meter E =
0011002
Z = 5070241
92 I = 51
36610
XDOT = 6408
799750 Wp = 94
75015
YDOT = 3837
475679 meter/sec RA = 221
63265 deg
ZDOT = 1738
480285 TA = 338
35790
MA = 338
40436
Ha = 229
883 n
mi
Hp = 218
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3999508
16 X = 1242843
67
Y = -14233379
57 feet Y = -4324568
44 meter
Z = 16634651
98 Z = 5076221
66
XDOT = 21026
245900 XDOT = 6356
967134
YDOT = 12590
143305 feet/sec YDOT = 3908
853697 meter/sec
ZDOT = 5703
675475 ZDOT = 1769
485562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13267217
97 X = 4043848
04
Y = 6453883
55 feet Y = 1967143
71 meter
Z = 16662086
32 Z = 5078603
91
XDOT = -15786
186874 XDOT = -4811
629759
YDOT = 17327
454889 feet/sec YDOT = 5281
408250 meter/sec
ZDOT = 5844
551186 ZDOT = 1781
419202
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 19268
76258386
00016717 00000-0 10270-3 0 9187
2 25544 51
6422 222
4834 0006918 71
6009 288
5893 15
50031022 30852
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
76258386 = yrday
fracday
Element set: 918
Inclination: 51
6422 deg
RA of node: 222
4834 deg
Eccentricity:
0006918
Arg of perigee: 71
6009 deg
Mean anomaly: 288
5893 deg
Mean motion: 15
50031022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 323
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