[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 22nd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 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
114/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
2
116/09:55:00
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
118/11:00:00
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
4
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
Coasting Arc #1 (Orbit 612)
---------------------------------------
Vector Time (GMT): 2019/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1986598
64 A = 6785271
84 meter
Y = -4685918
21 meter E =
0009527
Z = -4497015
99 I = 51
27396
XDOT = 4795
913072 Wp = 118
90070
YDOT = -5064
675275 meter/sec RA = 292
14065 deg
ZDOT = 3159
365554 TA = 183
02578
MA = 183
03155
Ha = 223
268 n
mi
Hp = 217
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6517712
09 X = -1912207
40
Y = -15373747
39 feet Y = -4707718
08 meter
Z = -14753989
48 Z = -4506485
31
XDOT = 15734
622941 XDOT = 4836
844600
YDOT = -16616
388696 feet/sec YDOT = -5010
814955 meter/sec
ZDOT = 10365
372551 ZDOT = 3182
762375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12588395
10 X = -3836942
83
Y = -10913964
98 feet Y = -3326576
53 meter
Z = -14796302
33 Z = -4509912
95
XDOT = 5841
552735 XDOT = 1780
505274
YDOT = -20931
825101 feet/sec YDOT = -6380
020291 meter/sec
ZDOT = 10471
643940 ZDOT = 3191
757073
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 19109
51036417
00016717 00000-0 10270-3 0 9004
2 25544 51
6370 292
8820 0001448 207
3206 152
7870 15
52570009 6136
Satellite: ISS
Catalog Number: 25544
Epoch time: 19109
51036417 = yrday
fracday
Element set: 900
Inclination: 51
6370 deg
RA of node: 292
8820 deg
Eccentricity:
0001448
Arg of perigee: 207
3206 deg
Mean anomaly: 152
7870 deg
Mean motion: 15
52570009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 613
Checksum: 284
Coasting Arc #2 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2019/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1452764
89 A = 6787911
18 meter
Y = 5468509
85 meter E =
0010696
Z = 3740537
88 I = 51
27160
XDOT = -4839
134414 Wp = 89
41651
YDOT = 4185
036106 meter/sec RA = 287
13912 deg
ZDOT = -4228
286804 TA = 45
59976
MA = 45
51225
Ha = 223
145 n
mi
Hp = 217
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4766289
03 X = 1373336
73
Y = 17941305
27 feet Y = 5484311
72 meter
Z = 12272105
92 Z = 3747401
86
XDOT = -15876
425244 XDOT = -4865
034007
YDOT = 13730
433420 feet/sec YDOT = 4130
776539 meter/sec
ZDOT = -13872
332033 ZDOT = -4251
856969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12415685
83 X = 3784301
04
Y = 13773528
19 feet Y = 4198171
39 meter
Z = 12302568
68 Z = 3749822
93
XDOT = -6689
500122 XDOT = -2038
959637
YDOT = 18547
421423 feet/sec YDOT = 5653
254050 meter/sec
ZDOT = -13979
288923 ZDOT = -4260
887264
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 19110
54023024
00016717 00000-0 10270-3 0 9010
2 25544 51
6373 287
7594 0001440 215
9681 144
1374 15
52568973 6292
Satellite: ISS
Catalog Number: 25544
Epoch time: 19110
54023024 = yrday
fracday
Element set: 901
Inclination: 51
6373 deg
RA of node: 287
7594 deg
Eccentricity:
0001440
Arg of perigee: 215
9681 deg
Mean anomaly: 144
1374 deg
Mean motion: 15
52568973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 306
Coasting Arc #3 (Orbit 643)
---------------------------------------
Vector Time (GMT): 2019/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -997748
20 A = 6790481
17 meter
Y = -6098774
85 meter E =
0003579
Z = -2815820
39 I = 51
27122
XDOT = 4825
863855 Wp = 73
31329
YDOT = -3124
352582 meter/sec RA = 282
14205 deg
ZDOT = 5063
419013 TA = 254
57981
MA = 254
61935
Ha = 223
254 n
mi
Hp = 217
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3273452
09 X = -915797
89
Y = -20009103
84 feet Y = -6109474
19 meter
Z = -9238255
88 Z = -2820468
04
XDOT = 15832
886664 XDOT = 4835
846895
YDOT = -10250
500597 feet/sec YDOT = -3070
330516 meter/sec
ZDOT = 16612
267102 ZDOT = 5086
885927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12338313
74 X = -3760718
03
Y = -16076958
90 feet Y = -4900257
07 meter
Z = -9258644
78 Z = -2822034
93
XDOT = 7785
834855 XDOT = 2373
122464
YDOT = -15591
433588 feet/sec YDOT = -4752
268958 meter/sec
ZDOT = 16718
645834 ZDOT = 5095
843250
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 19111
50572992
00016717 00000-0 10270-3 0 9021
2 25544 51
6371 282
9572 0001424 208
0804 152
0271 15
52573533 6444
Satellite: ISS
Catalog Number: 25544
Epoch time: 19111
50572992 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 282
9572 deg
Eccentricity:
0001424
Arg of perigee: 208
0804 deg
Mean anomaly: 152
0271 deg
Mean motion: 15
52573533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 644
Checksum: 289
Coasting Arc #4 (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 = 568636
81 A = 6792539
86 meter
Y = 6539558
13 meter E =
0013594
Z = 1718514
95 I = 51
27241
XDOT = -4811
655968 Wp = 121
07167
YDOT = 1911
825580 meter/sec RA = 277
14975 deg
ZDOT = -5656
630905 TA = 39
98431
MA = 39
88429
Ha = 223
083 n
mi
Hp = 217
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1865606
32 X = 487119
63
Y = 21455243
20 feet Y = 6545461
21 meter
Z = 5638172
41 Z = 1721079
30
XDOT = -15786
272861 XDOT = -4805
199757
YDOT = 6272
393635 feet/sec YDOT = 1858
054441 meter/sec
ZDOT = -18558
500344 ZDOT = -5679
988766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12116391
99 X = 3693076
28
Y = 17801054
33 feet Y = 5425761
36 meter
Z = 5649110
16 Z = 1721848
78
XDOT = -9274
377179 XDOT = -2826
830164
YDOT = 12263
161791 feet/sec YDOT = 3737
811714 meter/sec
ZDOT = -18664
264143 ZDOT = -5688
867711
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
53559226
00016717 00000-0 10270-3 0 9031
2 25544 51
6371 277
8351 0001420 222
0970 138
0073 15
52594629 6609
Satellite: ISS
Catalog Number: 25544
Epoch time: 19112
53559226 = yrday
fracday
Element set: 903
Inclination: 51
6371 deg
RA of node: 277
8351 deg
Eccentricity:
0001420
Arg of perigee: 222
0970 deg
Mean anomaly: 138
0073 deg
Mean motion: 15
52594629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 294
Coasting Arc #5 (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 = -195668
06 A = 6793675
52 meter
Y = -6763257
67 meter E =
0009485
Z = -561703
21 I = 51
27488
XDOT = 4795
249140 Wp = 41
94610
YDOT = -627
165848 meter/sec RA = 272
15980 deg
ZDOT = 5946
351320 TA = 311
96644
MA = 312
04722
Ha = 223
171 n
mi
Hp = 217
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -641955
59 X = -117296
38
Y = -22189165
58 feet Y = -6765007
55 meter
Z = -1842858
30 Z = -562463
53
XDOT = 15732
444684 XDOT = 4773
021492
YDOT = -2057
630736 feet/sec YDOT = -573
666458 meter/sec
ZDOT = 19509
026639 ZDOT = 5969
591105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11757687
62 X = -3583743
19
Y = -18828641
24 feet Y = -5738969
85 meter
Z = -1845630
97 Z = -562548
32
XDOT = 11049
957609 XDOT = 3368
027079
YDOT = -8801
888838 feet/sec YDOT = -2682
815718 meter/sec
ZDOT = 19614
132571 ZDOT = 5978
387608
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
50108790
00016717 00000-0 10270-3 0 9046
2 25544 51
6389 273
0330 0001396 215
3510 144
7549 15
52587374 6757
Satellite: ISS
Catalog Number: 25544
Epoch time: 19113
50108790 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 273
0330 deg
Eccentricity:
0001396
Arg of perigee: 215
3510 deg
Mean anomaly: 144
7549 deg
Mean motion: 15
52587374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 675
Checksum: 307
Coasting Arc #6 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2019/114/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4042791
69 A = 6782567
98 meter
Y = 1852251
80 meter E =
0012820
Z = -5132792
71 I = 51
23632
XDOT = -1509
681752 Wp = 81
97765
YDOT = -7360
896910 meter/sec RA = 267
43902 deg
ZDOT = -1468
620910 TA = 173
78906
MA = 173
77315
Ha = 223
158 n
mi
Hp = 217
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13263752
26 X = -4038271
17
Y = 6076941
61 feet Y = 1807067
91 meter
Z = -16839871
09 Z = -5152420
19
XDOT = -4953
024120 XDOT = -1420
124105
YDOT = -24149
924245 feet/sec YDOT = -7377
278433 meter/sec
ZDOT = -4818
310072 ZDOT = -1475
737147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11517410
93 X = -3510506
85
Y = 8786554
75 feet Y = 2678141
89 meter
Z = -16928771
45 Z = -5159889
54
XDOT = -9406
853170 XDOT = -2867
208846
YDOT = -21665
543364 feet/sec YDOT = -6603
657617 meter/sec
ZDOT = -4849
768075 ZDOT = -1478
209309
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
46657975
00016717 00000-0 10270-3 0 9057
2 25544 51
6376 268
2324 0001169 221
1919 138
9145 15
52588534 6901
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
46657975 = yrday
fracday
Element set: 905
Inclination: 51
6376 deg
RA of node: 268
2324 deg
Eccentricity:
0001169
Arg of perigee: 221
1919 deg
Mean anomaly: 138
9145 deg
Mean motion: 15
52588534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 332
Coasting Arc #7 (Orbit 705)
---------------------------------------
Vector Time (GMT): 2019/115/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4188697
99 A = 6781975
31 meter
Y = -702305
31 meter E =
0001928
Z = 5286057
44 I = 51
23544
XDOT = 1110
864657 Wp = 124
70974
YDOT = 7585
636149 meter/sec RA = 262
42758 deg
ZDOT = 126
459978 TA = 324
07176
MA = 324
08473
Ha = 223
056 n
mi
Hp = 217
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13742447
48 X = 4170563
20
Y = -2304151
29 feet Y = -655565
90 meter
Z = 17342708
12 Z = 5306360
60
XDOT = 3644
569085 XDOT = 1025
343080
YDOT = 24887
257708 feet/sec YDOT = 7597
580431 meter/sec
ZDOT = 414
894941 ZDOT = 131
648663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12709208
16 X = 3873766
65
Y = -5426395
76 feet Y = -1653965
43 meter
Z = 17434556
44 Z = 5314052
80
XDOT = 8966
479294 XDOT = 2732
982889
YDOT = 22418
223149 feet/sec YDOT = 6833
074416 meter/sec
ZDOT = 437
636224 ZDOT = 133
391521
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
49643781
00016717 00000-0 10270-3 0 9062
2 25544 51
6365 263
1101 0001176 225
5118 134
5938 15
52542489 7062
Satellite: ISS
Catalog Number: 25544
Epoch time: 19115
49643781 = yrday
fracday
Element set: 906
Inclination: 51
6365 deg
RA of node: 263
1101 deg
Eccentricity:
0001176
Arg of perigee: 225
5118 deg
Mean anomaly: 134
5938 deg
Mean motion: 15
52542489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 706
Checksum: 308
Coasting Arc #8 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2019/116/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4082949
18 A = 6781973
22 meter
Y = -1182590
18 meter E =
0001856
Z = 5283292
87 I = 51
24115
XDOT = 1836
678062 Wp = 128
14393
YDOT = 7440
216816 meter/sec RA = 257
60290 deg
ZDOT = 244
809107 TA = 319
50255
MA = 319
51636
Ha = 222
981 n
mi
Hp = 217
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13395502
55 X = 4070206
41
Y = -3879889
05 feet Y = -1137003
14 meter
Z = 17333638
01 Z = 5303095
39
XDOT = 6025
846659 XDOT = 1752
153786
YDOT = 24410
160157 feet/sec YDOT = 7460
283226 meter/sec
ZDOT = 803
179485 ZDOT = 253
525877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13137181
55 X = 4004212
94
Y = -4334985
80 feet Y = -1321303
67 meter
Z = 17423271
60 Z = 5310613
18
XDOT = 6543
609033 XDOT = 1994
492033
YDOT = 23229
771977 feet/sec YDOT = 7080
434499 meter/sec
ZDOT = 841
903052 ZDOT = 256
612050
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
46192531
00016717 00000-0 10270-3 0 9073
2 25544 51
6369 258
3087 0001174 237
8725 122
2313 15
52548688 7218
Satellite: ISS
Catalog Number: 25544
Epoch time: 19116
46192531 = yrday
fracday
Element set: 907
Inclination: 51
6369 deg
RA of node: 258
3087 deg
Eccentricity:
0001174
Arg of perigee: 237
8725 deg
Mean anomaly: 122
2313 deg
Mean motion: 15
52548688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 315
Coasting Arc #9 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2019/117/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4363532
84 A = 6782214
73 meter
Y = 42227
06 meter E =
0013451
Z = -5203848
83 I = 51
25150
XDOT = -1398
707860 Wp = 101
80423
YDOT = -7444
477696 meter/sec RA = 252
59180 deg
ZDOT = 1112
185322 TA = 178
93229
MA = 178
92941
Ha = 223
086 n
mi
Hp = 217
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14316052
61 X = -4338403
27
Y = 138540
22 feet Y = -6428
47 meter
Z = -17072994
85 Z = -5224984
24
XDOT = -4588
936548 XDOT = -1320
760027
YDOT = -24424
139424 feet/sec YDOT = -7459
683202 meter/sec
ZDOT = 3648
901974 ZDOT = 1105
580168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14175208
67 X = -4320603
60
Y = 871698
28 feet Y = 265693
64 meter
Z = -17168555
85 Z = -5232975
82
XDOT = -5806
749548 XDOT = -1769
897262
YDOT = -23118
937115 feet/sec YDOT = -7046
652033 meter/sec
ZDOT = 3619
704691 ZDOT = 1103
285990
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
42740939
00016717 00000-0 10270-3 0 9082
2 25544 51
6377 253
5066 0001093 235
3398 124
7651 15
52600220 7369
Satellite: ISS
Catalog Number: 25544
Epoch time: 19117
42740939 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 253
5066 deg
Eccentricity:
0001093
Arg of perigee: 235
3398 deg
Mean anomaly: 124
7651 deg
Mean motion: 15
52600220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 305
Coasting Arc #10 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2019/118/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 944647
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4633604
63 A = 6783840
91 meter
Y = 1057744
25 meter E =
0005827
Z = 4837319
79 I = 51
26629
XDOT = 881
176505 Wp = 60
11668
YDOT = 7223
059435 meter/sec RA = 247
58314 deg
ZDOT = -2418
435171 TA = 53
75870
MA = 53
70486
Ha = 222
980 n
mi
Hp = 217
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15202114
94 X = 4597935
19
Y = 3470289
53 feet Y = 1109361
03 meter
Z = 15870471
75 Z = 4859741
52
XDOT = 2890
999031 XDOT = 812
088152
YDOT = 23697
701560 feet/sec YDOT = 7232
527063 meter/sec
ZDOT = -7934
498594 ZDOT = -2414
322562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15298699
11 X = 4663043
49
Y = 2423177
64 feet Y = 738584
55 meter
Z = 15971759
36 Z = 4868192
25
XDOT = 4746
326352 XDOT = 1446
680272
YDOT = 22322
452645 feet/sec YDOT = 6803
883566 meter/sec
ZDOT = -7916
531590 ZDOT = -2412
958829
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
45725882
00016717 00000-0 10270-3 0 9097
2 25544 51
6364 248
3841 0001112 237
0549 123
0496 15
52563040 7522
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
45725882 = yrday
fracday
Element set: 909
Inclination: 51
6364 deg
RA of node: 248
3841 deg
Eccentricity:
0001112
Arg of perigee: 237
0549 deg
Mean anomaly: 123
0496 deg
Mean motion: 15
52563040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 303
Coasting Arc #11 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2019/118/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2171345
00 A = 6793613
51 meter
Y = -6405653
32 meter E =
0011799
Z = 573205
35 I = 51
30201
XDOT = 4719
485913 Wp = 50
88089
YDOT = -1060
840276 meter/sec RA = 247
38186 deg
ZDOT = 5947
482395 TA = 315
33068
MA = 315
42568
Ha = 223
032 n
mi
Hp = 217
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7123835
30 X = -2102338
10
Y = -21015922
95 feet Y = -6429548
97 meter
Z = 1880594
97 Z = 562825
37
XDOT = 15483
877666 XDOT = 4702
108130
YDOT = -3480
447099 feet/sec YDOT = -1008
160823 meter/sec
ZDOT = 19512
737518 ZDOT = 5970
365743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13967544
14 X = -4257307
46
Y = -17248131
44 feet Y = -5257230
46 meter
Z = 1834218
27 Z = 559069
73
XDOT = 11942
674966 XDOT = 3640
127330
YDOT = -7558
212350 feet/sec YDOT = -2303
743124 meter/sec
ZDOT = 19616
296579 ZDOT = 5979
047197
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
52162300
00016717 00000-0 10270-3 0 9107
2 25544 51
6385 248
0639 0001229 234
3169 125
7869 15
52611019 7538
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
52162300 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 248
0639 deg
Eccentricity:
0001229
Arg of perigee: 234
3169 deg
Mean anomaly: 125
7869 deg
Mean motion: 15
52611019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 299
Coasting Arc #12 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2019/118/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4517027
70 A = 6788926
36 meter
Y = 3770720
76 meter E =
0011407
Z = 3375650
51 I = 51
28628
XDOT = -1509
411098 Wp = 94
03671
YDOT = 5942
667991 meter/sec RA = 247
23142 deg
ZDOT = -4605
688120 TA = 46
33931
MA = 46
24480
Ha = 222
983 n
mi
Hp = 217
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14819644
68 X = 4458129
63
Y = 12371131
12 feet Y = 3820904
02 meter
Z = 11074968
86 Z = 3397449
52
XDOT = -4952
136148 XDOT = -1553
379588
YDOT = 19496
942229 feet/sec YDOT = 5925
542838 meter/sec
ZDOT = -15110
525327 ZDOT = -4613
127107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18887488
60 X = 5756906
52
Y = 3707280
82 feet Y = 1129979
19 meter
Z = 11173206
00 Z = 3405593
19
XDOT = 5443
463256 XDOT = 1659
167600
YDOT = 18035
583531 feet/sec YDOT = 5497
245860 meter/sec
ZDOT = -15144
676459 ZDOT = -4616
097385
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
52162396
00016717 00000-0 10270-3 0 9113
2 25544 51
6383 248
0639 0001276 234
6466 125
4567 15
52579220 7530
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
52162396 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 248
0639 deg
Eccentricity:
0001276
Arg of perigee: 234
6466 deg
Mean anomaly: 125
4567 deg
Mean motion: 15
52579220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 317
Coasting Arc #13 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2019/119/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4511714
64 A = 6791330
27 meter
Y = -4483194
05 meter E =
0004366
Z = -2377566
28 I = 51
30956
XDOT = 2189
074137 Wp = 41
88858
YDOT = -5033
562501 meter/sec RA = 242
23836 deg
ZDOT = 5346
264706 TA = 291
45780
MA = 291
50436
Ha = 222
970 n
mi
Hp = 217
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14802213
39 X = -4449698
02
Y = -14708641
89 feet Y = -4533300
48 meter
Z = -7800414
30 Z = -2399331
90
XDOT = 7182
001761 XDOT = 2219
228873
YDOT = -16514
312667 feet/sec YDOT = -5008
914059 meter/sec
ZDOT = 17540
238536 ZDOT = 5356
971765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20116744
43 X = -6131583
70
Y = -5406211
70 feet Y = -1647813
33 meter
Z = -7898455
51 Z = -2407449
24
XDOT = -2495
270084 XDOT = -760
558322
YDOT = -16370
484477 feet/sec YDOT = -4989
723668 meter/sec
ZDOT = 17589
078530 ZDOT = 5361
151136
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
48710387
00016717 00000-0 10270-3 0 9129
2 25544 51
6395 243
2621 0001273 245
0702 115
0318 15
52596445 7680
Satellite: ISS
Catalog Number: 25544
Epoch time: 19119
48710387 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 243
2621 deg
Eccentricity:
0001273
Arg of perigee: 245
0702 deg
Mean anomaly: 115
0318 deg
Mean motion: 15
52596445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 303
Coasting Arc #14 (Orbit 783)
---------------------------------------
Vector Time (GMT): 2019/120/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4396599
01 A = 6793094
35 meter
Y = 5022193
15 meter E =
0013019
Z = 1225766
57 I = 51
33257
XDOT = -2956
163648 Wp = 125
92874
YDOT = 4017
992758 meter/sec RA = 237
25041 deg
ZDOT = -5823
246278 TA = 40
69570
MA = 40
59849
Ha = 222
944 n
mi
Hp = 217
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14424537
43 X = 4334158
52
Y = 16477011
64 feet Y = 5071009
89 meter
Z = 4021543
88 Z = 1246971
99
XDOT = -9698
699633 XDOT = -2972
587985
YDOT = 13182
390938 feet/sec YDOT = 3984
842908 meter/sec
ZDOT = -19105
138707 ZDOT = -5837
646289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20811380
31 X = 6343308
72
Y = 6757852
92 feet Y = 2059793
57 meter
Z = 4117023
34 Z = 1254868
72
XDOT = -960
252042 XDOT = -292
684822
YDOT = 14706
583020 feet/sec YDOT = 4482
566504 meter/sec
ZDOT = -19170
587207 ZDOT = -5843
194981
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
51694608
00016717 00000-0 10270-3 0 9133
2 25544 51
6401 238
1398 0001269 248
1773 111
9244 15
52606112 7843
Satellite: ISS
Catalog Number: 25544
Epoch time: 19120
51694608 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 238
1398 deg
Eccentricity:
0001269
Arg of perigee: 248
1773 deg
Mean anomaly: 111
9244 deg
Mean motion: 15
52606112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 784
Checksum: 300
Coasting Arc #15 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2019/121/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4178055
01 A = 6793750
67 meter
Y = -5349995
43 meter E =
0011049
Z = -37695
43 I = 51
35432
XDOT = 3756
283832 Wp = 42
24702
YDOT = -2968
361955 meter/sec RA = 232
26651 deg
ZDOT = 5987
179413 TA = 317
34560
MA = 317
43134
Ha = 222
976 n
mi
Hp = 217
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13707529
57 X = -4117736
21
Y = -17552478
44 feet Y = -5396380
10 meter
Z = -123672
66 Z = -57844
44
XDOT = 12323
765853 XDOT = 3760
115031
YDOT = -9738
720325 feet/sec YDOT = -2926
335003 meter/sec
ZDOT = 19642
977078 ZDOT = 6005
435593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20905086
57 X = -6371870
39
Y = -7676754
82 feet Y = -2339874
87 meter
Z = -214363
87 Z = -65338
11
XDOT = 4657
896580 XDOT = 1419
726878
YDOT = -13180
467774 feet/sec YDOT = -4017
406578 meter/sec
ZDOT = 19725
777044 ZDOT = 6012
416843
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
48242032
00016717 00000-0 10270-3 0 9141
2 25544 51
6407 233
3384 0001108 257
1732 102
9296 15
52607561 7990
Satellite: ISS
Catalog Number: 25544
Epoch time: 19121
48242032 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 233
3384 deg
Eccentricity:
0001108
Arg of perigee: 257
1732 deg
Mean anomaly: 102
9296 deg
Mean motion: 15
52607561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 295
Coasting Arc #16 (Orbit 814)
---------------------------------------
Vector Time (GMT): 2019/122/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3793352
35 A = 6793146
27 meter
Y = 5504060
94 meter E =
0008842
Z = -1184712
36 I = 51
37338
XDOT = -4585
584206 Wp = 149
27570
YDOT = 1909
599734 meter/sec RA = 227
28439 deg
ZDOT = -5837
630263 TA = 43
63184
MA = 43
56195
Ha = 222
957 n
mi
Hp = 217
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12445381
72 X = 3737277
20
Y = 18057942
71 feet Y = 5546167
31 meter
Z = -3886851
58 Z = -1166421
71
XDOT = -15044
567606 XDOT = -4578
240719
YDOT = 6265
090992 feet/sec YDOT = 1858
361485 meter/sec
ZDOT = -19152
330259 ZDOT = -5859
887819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20270094
01 X = 6178324
66
Y = 8410292
85 feet Y = 2563457
26 meter
Z = -3804562
94 Z = -1159630
79
XDOT = -8522
996288 XDOT = -2597
809269
YDOT = 11872
793029 feet/sec YDOT = 3618
827315 meter/sec
ZDOT = -19253
145140 ZDOT = -5868
358639
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
51225733
00016717 00000-0 10270-3 0 9156
2 25544 51
6404 228
2167 0001197 257
3270 102
7748 15
52620042 8154
Satellite: ISS
Catalog Number: 25544
Epoch time: 19122
51225733 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 228
2167 deg
Eccentricity:
0001197
Arg of perigee: 257
3270 deg
Mean anomaly: 102
7748 deg
Mean motion: 15
52620042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 815
Checksum: 284
Coasting Arc #17 (Orbit 830)
---------------------------------------
Vector Time (GMT): 2019/123/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3269241
14 A = 6791454
30 meter
Y = -5476038
87 meter E =
0012716
Z = 2316680
11 I = 51
39249
XDOT = 5377
761459 Wp = 71
64669
YDOT = -922
742687 meter/sec RA = 222
30122 deg
ZDOT = 5387
400983 TA = 314
26035
MA = 314
36464
Ha = 222
950 n
mi
Hp = 217
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10725856
77 X = -3219016
88
Y = -17966006
78 feet Y = -5512316
98 meter
Z = 7600656
52 Z = 2300921
09
XDOT = 17643
574342 XDOT = 5361
510685
YDOT = -3027
371021 feet/sec YDOT = -862
695640 meter/sec
ZDOT = 17675
200077 ZDOT = 5413
485120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18952621
68 X = -5776759
09
Y = -8927013
47 feet Y = -2720953
70 meter
Z = 7529803
77 Z = 2295084
19
XDOT = 12223
761818 XDOT = 3725
802602
YDOT = -10886
404394 feet/sec YDOT = -3318
176059 meter/sec
ZDOT = 17793
252054 ZDOT = 5423
383226
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
54209071
00016717 00000-0 10270-3 0 9168
2 25544 51
6417 223
0949 0001139 264
9413 95
1609 15
52632802 8314
Satellite: ISS
Catalog Number: 25544
Epoch time: 19123
54209071 = yrday
fracday
Element set: 916
Inclination: 51
6417 deg
RA of node: 223
0949 deg
Eccentricity:
0001139
Arg of perigee: 264
9413 deg
Mean anomaly: 95
1609 deg
Mean motion: 15
52632802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 831
Checksum: 296
Coasting Arc #18 (Orbit 844)
---------------------------------------
Vector Time (GMT): 2019/124/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 964789
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2559307
43 A = 6788995
99 meter
Y = 5318982
33 meter E =
0003554
Z = -3356705
06 I = 51
40935
XDOT = -6096
324369 Wp = 94
56601
YDOT = 8
379593 meter/sec RA = 217
31605 deg
ZDOT = -4639
373511 TA = 124
66475
MA = 124
63124
Ha = 222
948 n
mi
Hp = 217
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8396677
92 X = 2515944
17
Y = 17450729
44 feet Y = 5347359
89 meter
Z = -11012811
88 Z = -3344377
90
XDOT = -20001
064204 XDOT = -6073
429030
YDOT = 27
492103 feet/sec YDOT = -59
665686 meter/sec
ZDOT = -15221
041703 ZDOT = -4668
932151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16915495
01 X = 5155842
88
Y = 9492853
97 feet Y = 2893421
89 meter
Z = -10957460
27 Z = -3339833
89
XDOT = -15630
989725 XDOT = -4764
325668
YDOT = 10146
642013 feet/sec YDOT = 3092
696485 meter/sec
ZDOT = -15354
750605 ZDOT = -4680
127984
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
50755699
00016717 00000-0 10270-3 0 9178
2 25544 51
6415 218
2937 0001175 271
4179 88
6839 15
52620805 8454
Satellite: ISS
Catalog Number: 25544
Epoch time: 19124
50755699 = yrday
fracday
Element set: 917
Inclination: 51
6415 deg
RA of node: 218
2937 deg
Eccentricity:
0001175
Arg of perigee: 271
4179 deg
Mean anomaly: 88
6839 deg
Mean motion: 15
52620805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 845
Checksum: 336
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