[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 9th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 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
317/14:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
3
000/00:00:00
000 0
0 0
0 223
6
Coasting Arc #1 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2019/312/13:43:51
815
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5882255
74 A = 6798830
98 meter
Y = -2403939
91 meter E =
0005785
Z = -2406461
27 I = 51
69117
XDOT = 3801
353667 Wp = 200
99393
YDOT = -3932
576713 meter/sec RA = 4
82063 deg
ZDOT = -5364
689050 TA = 5
83561
MA = 5
82887
Ha = 225
694 n
mi
Hp = 223
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19298739
29 X = -5843247
52
Y = -7886941
95 feet Y = -2469501
39 meter
Z = -7895214
14 Z = -2434940
82
XDOT = 12471
632765 XDOT = 3871
105545
YDOT = -12902
154570 feet/sec YDOT = -3889
677399 meter/sec
ZDOT = -17600
685859 ZDOT = -5346
053638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13300639
34 X = 4054034
87
Y = -15989826
26 feet Y = -4873699
04 meter
Z = -8024839
39 Z = -2445971
05
XDOT = 7362
839117 XDOT = 2244
193363
YDOT = 14912
926644 feet/sec YDOT = 4545
460041 meter/sec
ZDOT = -17515
313435 ZDOT = -5338
667535
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 19312
59948365
00016717 00000-0 10270-3 0 9002
2 25544 51
6446 5
2546 0006401 254
4843 105
5601 15
50000228 37653
Satellite: ISS
Catalog Number: 25544
Epoch time: 19312
59948365 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 5
2546 deg
Eccentricity:
0006401
Arg of perigee: 254
4843 deg
Mean anomaly: 105
5601 deg
Mean motion: 15
50000228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3765
Checksum: 289
Coasting Arc #2 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2019/313/13:43:51
815
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5864419
88 A = 6798262
45 meter
Y = 2121228
94 meter E =
0007222
Z = 2698278
70 I = 51
65365
XDOT = -3873
162806 Wp = 78
48224
YDOT = 4106
146558 meter/sec RA = 359
87011 deg
ZDOT = 5179
532485 TA = 311
93719
MA = 311
99874
Ha = 225
582 n
mi
Hp = 223
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19240222
70 X = 5827156
78
Y = 6959412
55 feet Y = 2186600
72 meter
Z = 8852620
42 Z = 2726675
97
XDOT = -12707
227055 XDOT = -3943
950943
YDOT = 13471
609443 feet/sec YDOT = 4062
438403 meter/sec
ZDOT = 16993
216815 ZDOT = 5160
545672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12115832
14 X = -3692905
64
Y = 16417089
16 feet Y = 5003928
78 meter
Z = 8981885
97 Z = 2737678
84
XDOT = -8083
965552 XDOT = -2463
992700
YDOT = -15233
803166 feet/sec YDOT = -4643
263205 meter/sec
ZDOT = 16906
231410 ZDOT = 5153
019334
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 19313
63106611
00016717 00000-0 10270-3 0 9019
2 25544 51
6426
1444 0006229 258
9718 101
0732 15
49977581 37817
Satellite: ISS
Catalog Number: 25544
Epoch time: 19313
63106611 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node:
1444 deg
Eccentricity:
0006229
Arg of perigee: 258
9718 deg
Mean anomaly: 101
0732 deg
Mean motion: 15
49977581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3781
Checksum: 300
Coasting Arc #3 (Orbit 3795)
---------------------------------------
Vector Time (GMT): 2019/314/13:43:51
815
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5811406
35 A = 6797503
96 meter
Y = -1860948
95 meter E =
0003192
Z = -2990186
86 I = 51
61804
XDOT = 3934
607376 Wp = 221
16979
YDOT = -4301
455631 meter/sec RA = 354
91754 deg
ZDOT = -4969
182109 TA = 352
97925
MA = 352
98372
Ha = 225
284 n
mi
Hp = 223
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19066293
80 X = -5775639
71
Y = -6105475
56 feet Y = -1925736
23 meter
Z = -9810324
33 Z = -3018330
36
XDOT = 12908
816852 XDOT = 4006
553239
YDOT = -14112
387241 feet/sec YDOT = -4257
053821 meter/sec
ZDOT = -16303
090909 ZDOT = -4949
893988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10960610
91 X = 3340794
20
Y = -16677384
11 feet Y = -5083266
68 meter
Z = -9938446
68 Z = -3029238
55
XDOT = 8905
676378 XDOT = 2714
450160
YDOT = 15516
978871 feet/sec YDOT = 4729
575160 meter/sec
ZDOT = -16214
718316 ZDOT = -4942
246143
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 19314
59817079
00016717 00000-0 10270-3 0 9023
2 25544 51
6428 355
3544 0006450 262
1169 97
9250 15
49993580 37969
Satellite: ISS
Catalog Number: 25544
Epoch time: 19314
59817079 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 355
3544 deg
Eccentricity:
0006450
Arg of perigee: 262
1169 deg
Mean anomaly: 97
9250 deg
Mean motion: 15
49993580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3796
Checksum: 346
Coasting Arc #4 (Orbit 3811)
---------------------------------------
Vector Time (GMT): 2019/315/13:43:51
815
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5737690
40 A = 6796765
77 meter
Y = 1611633
74 meter E =
0006247
Z = 3262038
05 I = 51
58188
XDOT = -3970
210381 Wp = 88
35258
YDOT = 4521
866097 meter/sec RA = 349
96104 deg
ZDOT = 4741
558980 TA = 309
43998
MA = 309
49524
Ha = 225
132 n
mi
Hp = 223
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18824443
56 X = 5703396
57
Y = 5287512
27 feet Y = 1675604
85 meter
Z = 10702224
57 Z = 3289827
13
XDOT = -13025
624609 XDOT = -4043
512649
YDOT = 14835
518692 feet/sec YDOT = 4477
058475 meter/sec
ZDOT = 15556
295866 ZDOT = 4722
094651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9818192
85 X = -2992585
18
Y = 16828441
33 feet Y = 5129308
92 meter
Z = 10828745
25 Z = 3300601
55
XDOT = -9845
839338 XDOT = -3001
011830
YDOT = -15713
151274 feet/sec YDOT = -4789
368508 meter/sec
ZDOT = 15467
103053 ZDOT = 4714
373011
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 19315
62974698
00016717 00000-0 10270-3 0 9030
2 25544 51
6422 350
2435 0006376 267
3610 92
6811 15
49998885 38128
Satellite: ISS
Catalog Number: 25544
Epoch time: 19315
62974698 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 350
2435 deg
Eccentricity:
0006376
Arg of perigee: 267
3610 deg
Mean anomaly: 92
6811 deg
Mean motion: 15
49998885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3812
Checksum: 342
Coasting Arc #5 (Orbit 3826)
---------------------------------------
Vector Time (GMT): 2019/316/13:43:51
815
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5638200
02 A = 6796007
83 meter
Y = -1391345
94 meter E =
0001296
Z = -3529617
03 I = 51
54573
XDOT = 3984
823853 Wp = 300
07104
YDOT = -4757
412661 meter/sec RA = 345
00252 deg
ZDOT = -4488
140483 TA = 281
47574
MA = 281
49029
Ha = 225
172 n
mi
Hp = 223
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18498031
55 X = -5605077
11
Y = -4564783
28 feet Y = -1454210
95 meter
Z = -11580108
37 Z = -3556925
71
XDOT = 13073
569073 XDOT = 4059
528004
YDOT = -15608
309256 feet/sec YDOT = -4712
433687 meter/sec
ZDOT = -14724
870350 ZDOT = -4468
601849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8746911
37 X = 2666058
58
Y = -16840744
19 feet Y = -5133058
83 meter
Z = -11704452
32 Z = -3567517
07
XDOT = 10867
315857 XDOT = 3312
357873
YDOT = 15820
262602 feet/sec YDOT = 4822
016041 meter/sec
ZDOT = -14635
319325 ZDOT = -4460
845330
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 19316
59684697
00016717 00000-0 10270-3 0 9045
2 25544 51
6414 345
4528 0006325 270
9648 89
0778 15
49993728 38272
Satellite: ISS
Catalog Number: 25544
Epoch time: 19316
59684697 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 345
4528 deg
Eccentricity:
0006325
Arg of perigee: 270
9648 deg
Mean anomaly: 89
0778 deg
Mean motion: 15
49993728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3827
Checksum: 371
Coasting Arc #6 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2019/317/13:43:51
815
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5520938
82 A = 6795188
23 meter
Y = 1188898
69 meter E =
0004948
Z = 3775410
61 I = 51
50987
XDOT = -3969
439331 Wp = 99
63851
YDOT = 5012
154299 meter/sec RA = 340
04117 deg
ZDOT = 4220
773877 TA = 305
59982
MA = 305
64592
Ha = 225
069 n
mi
Hp = 223
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18113316
35 X = 5488894
50
Y = 3900586
24 feet Y = 1250458
33 meter
Z = 12386517
76 Z = 3802152
28
XDOT = -13023
094917 XDOT = -4045
694448
YDOT = 16444
075784 feet/sec YDOT = 4967
338611 meter/sec
ZDOT = 13847
683324 ZDOT = 4201
306344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7722920
16 X = -2353946
07
Y = 16752068
07 feet Y = 5106030
35 meter
Z = 12508291
01 Z = 3812527
10
XDOT = -11983
116858 XDOT = -3652
454018
YDOT = -15810
852690 feet/sec YDOT = -4819
147900 meter/sec
ZDOT = 13758
434190 ZDOT = 4193
570741
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 19317
62841834
00016717 00000-0 10270-3 0 9059
2 25544 51
6401 340
3425 0006498 275
3150 84
7259 15
50012672 38432
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
62841834 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 340
3425 deg
Eccentricity:
0006498
Arg of perigee: 275
3150 deg
Mean anomaly: 84
7259 deg
Mean motion: 15
50012672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 305
Coasting Arc #7 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2105586
81 A = 6792831
40 meter
Y = -4611980
68 meter E =
0003710
Z = -4524596
34 I = 51
49970
XDOT = 6979
536905 Wp = 135
36935
YDOT = 96
496622 meter/sec RA = 339
76482 deg
ZDOT = 3148
660227 TA = 166
33135
MA = 166
32130
Ha = 225
322 n
mi
Hp = 223
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6908093
22 X = 2178981
44
Y = -15131170
20 feet Y = -4588023
87 meter
Z = -14844476
19 Z = -4514189
90
XDOT = 22898
743128 XDOT = 6962
644229
YDOT = 316
589967 feet/sec YDOT = 174
452092 meter/sec
ZDOT = 10330
250089 ZDOT = 3182
524162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15588119
26 X = 4751258
75
Y = 5924911
20 feet Y = 1805912
93 meter
Z = -14796570
61 Z = -4509994
72
XDOT = 1723
554074 XDOT = 525
339282
YDOT = 21657
416919 feet/sec YDOT = 6601
180677 meter/sec
ZDOT = 10484
599332 ZDOT = 3195
705876
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 19317
62841921
00016717 00000-0 10270-3 0 9067
2 25544 51
6398 340
3425 0006418 276
0521 83
9898 15
49983031 38433
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
62841921 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 340
3425 deg
Eccentricity:
0006418
Arg of perigee: 276
0521 deg
Mean anomaly: 83
9898 deg
Mean motion: 15
49983031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 334
Coasting Arc #8 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2019/318/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2101028
75 A = 6793466
34 meter
Y = 4796917
23 meter E =
0004968
Z = 4327450
80 I = 51
47127
XDOT = -6824
051571 Wp = 34
97865
YDOT = 152
316746 meter/sec RA = 334
79924 deg
ZDOT = -3476
025153 TA = 90
50621
MA = 90
44928
Ha = 225
464 n
mi
Hp = 223
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6893138
95 X = -2175534
03
Y = 15737917
43 feet Y = 4773005
12 meter
Z = 14197673
24 Z = 4317063
93
XDOT = -22388
620639 XDOT = -6808
362593
YDOT = 499
726858 feet/sec YDOT = 76
093379 meter/sec
ZDOT = -11404
281998 ZDOT = -3509
136603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16290416
67 X = -4965319
00
Y = -5583518
69 feet Y = -1701856
50 meter
Z = 14149840
24 Z = 4312871
31
XDOT = -2858
356445 XDOT = -871
227045
YDOT = -20993
747428 feet/sec YDOT = -6398
894216 meter/sec
ZDOT = -11555
221266 ZDOT = -3522
031442
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 19318
65998871
00016717 00000-0 10270-3 0 9079
2 25544 51
6399 335
2317 0006532 279
9198 80
1215 15
50015575 38596
Satellite: ISS
Catalog Number: 25544
Epoch time: 19318
65998871 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 335
2317 deg
Eccentricity:
0006532
Arg of perigee: 279
9198 deg
Mean anomaly: 80
1215 deg
Mean motion: 15
50015575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 349
Coasting Arc #9 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2019/319/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2062634
08 A = 6794266
57 meter
Y = -4995584
21 meter E =
0001050
Z = -4118415
54 I = 51
44490
XDOT = 6647
706800 Wp = 136
96468
YDOT = -375
316760 meter/sec RA = 329
83196 deg
ZDOT = 3784
458709 TA = 172
22562
MA = 172
22399
Ha = 225
750 n
mi
Hp = 223
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6767172
18 X = 2138348
28
Y = -16389711
97 feet Y = -4972094
66 meter
Z = -13511862
00 Z = -4108212
37
XDOT = 21810
061679 XDOT = 6633
026412
YDOT = -1231
354201 feet/sec YDOT = -301
059841 meter/sec
ZDOT = 12416
203112 ZDOT = 3816
715822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17018548
76 X = 5187253
66
Y = 5104362
14 feet Y = 1555809
58 meter
Z = -13464849
71 Z = -4104086
19
XDOT = 3870
856123 XDOT = 1179
836946
YDOT = 20236
439863 feet/sec YDOT = 6168
066870 meter/sec
ZDOT = 12563
267666 ZDOT = 3829
283985
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 19319
62708257
00016717 00000-0 10270-3 0 9085
2 25544 51
6408 330
4404 0006482 284
4049 75
6382 15
49995333 38749
Satellite: ISS
Catalog Number: 25544
Epoch time: 19319
62708257 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 330
4404 deg
Eccentricity:
0006482
Arg of perigee: 284
4049 deg
Mean anomaly: 75
6382 deg
Mean motion: 15
49995333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 338
Coasting Arc #10 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2019/320/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2009136
11 A = 6794978
71 meter
Y = 5201229
88 meter E =
0006211
Z = 3882376
42 I = 51
41897
XDOT = -6456
316066 Wp = 52
50023
YDOT = 560
260986 meter/sec RA = 324
86335 deg
ZDOT = -4083
525491 TA = 80
53209
MA = 80
46189
Ha = 225
964 n
mi
Hp = 223
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6591653
91 X = -2086007
22
Y = 17064402
49 feet Y = 5178332
11 meter
Z = 12737455
46 Z = 3872430
41
XDOT = -21182
139323 XDOT = -6442
265365
YDOT = 1838
126596 feet/sec YDOT = 488
140863 meter/sec
ZDOT = -13397
393344 ZDOT = -4114
854240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17751440
08 X = -5410638
94
Y = -4549303
36 feet Y = -1386627
66 meter
Z = 12691600
33 Z = 3868399
78
XDOT = -4724
212667 XDOT = -1439
940021
YDOT = -19415
925813 feet/sec YDOT = -5917
974188 meter/sec
ZDOT = -13540
242972 ZDOT = -4127
066058
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 19320
65864707
00016717 00000-0 10270-3 0 9094
2 25544 51
6406 325
3299 0006555 288
9395 71
1044 15
50023243 38904
Satellite: ISS
Catalog Number: 25544
Epoch time: 19320
65864707 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 325
3299 deg
Eccentricity:
0006555
Arg of perigee: 288
9395 deg
Mean anomaly: 71
1044 deg
Mean motion: 15
50023243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 322
Coasting Arc #11 (Orbit 3904)
---------------------------------------
Vector Time (GMT): 2019/321/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1912871
93 A = 6795809
01 meter
Y = -5409836
68 meter E =
0001879
Z = -3638854
33 I = 51
39474
XDOT = 6257
160240 Wp = 336
34736
YDOT = -719
275132 meter/sec RA = 319
89342 deg
ZDOT = 4359
500775 TA = 340
39206
MA = 340
39928
Ha = 226
184 n
mi
Hp = 223
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6275826
55 X = 1990899
90
Y = -17748808
01 feet Y = -5388008
98 meter
Z = -11938498
47 Z = -3629373
18
XDOT = 20528
740944 XDOT = 6243
562024
YDOT = -2359
826548 feet/sec YDOT = -649
379586 meter/sec
ZDOT = 14302
824066 ZDOT = 4389
863028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18460193
42 X = 5626666
95
Y = 3830158
61 feet Y = 1167432
35 meter
Z = -11894749
85 Z = -3625519
76
XDOT = 5452
385661 XDOT = 1661
887150
YDOT = 18560
074291 feet/sec YDOT = 5657
110644 meter/sec
ZDOT = 14441
282236 ZDOT = 4401
702826
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 19321
62573785
00016717 00000-0 10270-3 0 9107
2 25544 51
6405 320
5390 0006597 292
3301 67
7144 15
50000523 39059
Satellite: ISS
Catalog Number: 25544
Epoch time: 19321
62573785 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 320
5390 deg
Eccentricity:
0006597
Arg of perigee: 292
3301 deg
Mean anomaly: 67
7144 deg
Mean motion: 15
50000523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3905
Checksum: 290
Coasting Arc #12 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2019/322/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1803642
81 A = 6796523
40 meter
Y = 5619457
11 meter E =
0007093
Z = 3367853
80 I = 51
37372
XDOT = -6049
926886 Wp = 67
31929
YDOT = 835
168216 meter/sec RA = 314
92214 deg
ZDOT = -4623
047049 TA = 73
30406
MA = 73
22622
Ha = 226
346 n
mi
Hp = 223
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5917463
28 X = -1882706
49
Y = 18436539
06 feet Y = 5598845
16 meter
Z = 11049389
11 Z = 3358900
70
XDOT = -19848
841489 XDOT = -6036
359921
YDOT = 2740
053201 feet/sec YDOT = 767
589881 meter/sec
ZDOT = -15167
477196 ZDOT = -4652
402602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19145825
44 X = -5835647
59
Y = -3044964
16 feet Y = -928105
08 meter
Z = 11008038
23 Z = 3355250
05
XDOT = -6005
422589 XDOT = -1830
452805
YDOT = -17681
542476 feet/sec YDOT = -5389
334147 meter/sec
ZDOT = -15301
355321 ZDOT = -4663
853102
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 19322
65729916
00016717 00000-0 10270-3 0 9111
2 25544 51
6416 315
4286 0006637 296
3609 63
6859 15
50029814 39218
Satellite: ISS
Catalog Number: 25544
Epoch time: 19322
65729916 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 315
4286 deg
Eccentricity:
0006637
Arg of perigee: 296
3609 deg
Mean anomaly: 63
6859 deg
Mean motion: 15
50029814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 333
Coasting Arc #13 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2019/323/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1649237
87 A = 6797309
89 meter
Y = -5820311
69 meter E =
0004884
Z = -3092653
72 I = 51
35338
XDOT = 5847
414998 Wp = 342
41956
YDOT = -925
582914 meter/sec RA = 309
94935 deg
ZDOT = 4862
762727 TA = 341
93098
MA = 341
94834
Ha = 226
560 n
mi
Hp = 223
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5410885
41 X = 1729222
24
Y = -19095510
81 feet Y = -5801421
35 meter
Z = -10146501
71 Z = -3084448
34
XDOT = 19184
432409 XDOT = 5833
709741
YDOT = -3036
689350 feet/sec YDOT = -860
269900 meter/sec
ZDOT = 15953
945954 ZDOT = 4891
134181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19755763
00 X = 6021556
56
Y = 2096350
60 feet Y = 638967
66 meter
Z = -10108553
46 Z = -3081087
09
XDOT = 6439
931938 XDOT = 1962
891255
YDOT = 16823
866966 feet/sec YDOT = 5127
914651 meter/sec
ZDOT = 16083
343043 ZDOT = 4902
202960
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 19323
62438464
00016717 00000-0 10270-3 0 9125
2 25544 51
6416 310
6376 0006689 300
3340 59
7149 15
50013495 39362
Satellite: ISS
Catalog Number: 25544
Epoch time: 19323
62438464 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 310
6376 deg
Eccentricity:
0006689
Arg of perigee: 300
3340 deg
Mean anomaly: 59
7149 deg
Mean motion: 15
50013495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 311
Coasting Arc #14 (Orbit 3951)
---------------------------------------
Vector Time (GMT): 2019/324/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1485078
23 A = 6798003
32 meter
Y = 6016590
19 meter E =
0007838
Z = 2789541
70 I = 51
33514
XDOT = -5644
971029 Wp = 79
69644
YDOT = 970
730408 meter/sec RA = 304
97589 deg
ZDOT = -5085
328837 TA = 68
58895
MA = 68
50535
Ha = 226
745 n
mi
Hp = 223
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4872303
90 X = -1565797
29
Y = 19739469
14 feet Y = 5999531
57 meter
Z = 9152039
70 Z = 2782131
84
XDOT = -18520
246157 XDOT = -5630
704531
YDOT = 3184
811050 feet/sec YDOT = 907
684309 meter/sec
ZDOT = -16684
149727 ZDOT = -5112
715569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20317629
23 X = -6192813
39
Y = -1098657
37 feet Y = -334870
77 meter
Z = 9117714
20 Z = 2779079
29
XDOT = -6698
847228 XDOT = -2041
808635
YDOT = -15986
997507 feet/sec YDOT = -4872
836840 meter/sec
ZDOT = -16809
057313 ZDOT = -5123
400669
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 19324
65594093
00016717 00000-0 10270-3 0 9131
2 25544 51
6414 305
5273 0006659 305
0029 55
0496 15
50033449 39525
Satellite: ISS
Catalog Number: 25544
Epoch time: 19324
65594093 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 305
5273 deg
Eccentricity:
0006659
Arg of perigee: 305
0029 deg
Mean anomaly: 55
0496 deg
Mean motion: 15
50033449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 310
Coasting Arc #15 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2019/325/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1274728
86 A = 6798696
29 meter
Y = -6191789
20 meter E =
0007759
Z = -2488175
35 I = 51
31855
XDOT = 5459
833257 Wp = 350
35751
YDOT = -996
950876 meter/sec RA = 300
00129 deg
ZDOT = 5283
154794 TA = 341
66217
MA = 341
69013
Ha = 226
873 n
mi
Hp = 223
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4182181
31 X = 1355958
84
Y = -20314269
04 feet Y = -6177080
04 meter
Z = -8163304
97 Z = -2481785
96
XDOT = 17912
838771 XDOT = 5444
912707
YDOT = -3270
836206 feet/sec YDOT = -935
978706 meter/sec
ZDOT = 17333
185019 ZDOT = 5309
640694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20751894
66 X = 6325177
49
Y = -51492
98 feet Y = -15695
06 meter
Z = -8133629
65 Z = -2479130
32
XDOT = 6872
211050 XDOT = 2094
649928
YDOT = 15222
548817 feet/sec YDOT = 4639
832880 meter/sec
ZDOT = 17453
983107 ZDOT = 5319
974051
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 19325
62302314
00016717 00000-0 10270-3 0 9143
2 25544 51
6408 300
7365 0006714 307
8047 52
2495 15
50022241 39671
Satellite: ISS
Catalog Number: 25544
Epoch time: 19325
62302314 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 300
7365 deg
Eccentricity:
0006714
Arg of perigee: 307
8047 deg
Mean anomaly: 52
2495 deg
Mean motion: 15
50022241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 288
Coasting Arc #16 (Orbit 3982)
---------------------------------------
Vector Time (GMT): 2019/326/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1060262
22 A = 6799291
56 meter
Y = 6357449
00 meter E =
0008017
Z = 2158127
12 I = 51
30606
XDOT = -5282
417241 Wp = 91
13997
YDOT = 978
177695 meter/sec RA = 295
02547 deg
ZDOT = -5459
221570 TA = 64
85549
MA = 64
77235
Ha = 227
041 n
mi
Hp = 222
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3478550
58 X = -1141757
42
Y = 20857772
30 feet Y = 6345136
69 meter
Z = 7080469
55 Z = 2152778
85
XDOT = -17330
765228 XDOT = -5266
444592
YDOT = 3209
244406 feet/sec YDOT = 919
195385 meter/sec
ZDOT = -17910
831922 ZDOT = -5484
843194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21118809
91 X = -6437013
26
Y = 1222814
69 feet Y = 372713
92 meter
Z = 7055538
32 Z = 2150528
08
XDOT = -6882
677017 XDOT = -2097
839955
YDOT = -14517
655642 feet/sec YDOT = -4424
981440 meter/sec
ZDOT = -18027
683599 ZDOT = -5494
837961
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 19326
65457458
00016717 00000-0 10270-3 0 9158
2 25544 51
6419 295
6257 0006746 311
7600 48
2973 15
50039465 39839
Satellite: ISS
Catalog Number: 25544
Epoch time: 19326
65457458 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 295
6257 deg
Eccentricity:
0006746
Arg of perigee: 311
7600 deg
Mean anomaly: 48
2973 deg
Mean motion: 15
50039465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3983
Checksum: 341
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