[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 8th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16491 3871 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 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
338/17:51:57
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 220
5
339/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 220
4
340/09:34:11
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 220
3
341/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
2
342/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
0
343/10:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 219
8
346/03:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 219
4
Coasting Arc #1 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2019/338/15:42:20
087
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -220001
35 A = 6795060
39 meter
Y = -5624837
41 meter E =
0012379
Z = 3791558
10 I = 51
32036
XDOT = 5883
763196 Wp = 61
85988
YDOT = 2590
532616 meter/sec RA = 235
12894 deg
ZDOT = 4179
771296 TA = 343
83427
MA = 343
87372
Ha = 228
652 n
mi
Hp = 220
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -721789
20 X = -175503
80
Y = -18454190
97 feet Y = -5627049
06 meter
Z = 12439495
07 Z = 3790597
12
XDOT = 19303
685026 XDOT = 5834
054707
YDOT = 8499
122757 feet/sec YDOT = 2656
050808 meter/sec
ZDOT = 13713
160419 ZDOT = 4208
231986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14075387
26 X = 4290178
04
Y = -11960843
02 feet Y = -3645664
95 meter
Z = 12435469
00 Z = 3790330
95
XDOT = 4205
859741 XDOT = 1281
946049
YDOT = 19357
631210 feet/sec YDOT = 5900
205993 meter/sec
ZDOT = 13842
795085 ZDOT = 4219
283942
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 19338
71075275
00016717 00000-0 10270-3 0 9005
2 25544 51
6409 235
8936 0007291 356
1520 3
9573 15
50076869 1706
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
71075275 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 235
8936 deg
Eccentricity:
0007291
Arg of perigee: 356
1520 deg
Mean anomaly: 3
9573 deg
Mean motion: 15
50076869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 170
Checksum: 315
Coasting Arc #2 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2019/338/17:51:57
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3384481
42 A = 6800718
64 meter
Y = 5847456
08 meter E =
0006478
Z = -776878
23 I = 51
34004
XDOT = -4504
620891 Wp = 97
20566
YDOT = 1827
256062 meter/sec RA = 234
65988 deg
ZDOT = -5914
348930 TA = 91
20634
MA = 91
13212
Ha = 228
631 n
mi
Hp = 220
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11103941
66 X = 3322615
58
Y = 19184567
19 feet Y = 5884957
88 meter
Z = -2548813
10 Z = -760587
49
XDOT = -14778
939930 XDOT = -4495
990242
YDOT = 5994
934586 feet/sec YDOT = 1776
930840 meter/sec
ZDOT = -19404
031921 ZDOT = -5936
209723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4021661
13 X = 1225802
31
Y = 21806943
13 feet Y = 6646756
27 meter
Z = -2474885
84 Z = -754345
21
XDOT = -14219
808708 XDOT = -4334
197694
YDOT = 425
572979 feet/sec YDOT = 129
714644 meter/sec
ZDOT = -19503
847238 ZDOT = -5944
772638
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 19338
77522233
00016717 00000-0 10270-3 0 9013
2 25544 51
6393 235
5714 0007179 358
2454 1
8671 15
50133949 1713
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
77522233 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 235
5714 deg
Eccentricity:
0007179
Arg of perigee: 358
2454 deg
Mean anomaly: 1
8671 deg
Mean motion: 15
50133949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 171
Checksum: 310
Coasting Arc #3 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2019/339/17:51:57
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3604483
00 A = 6800590
48 meter
Y = -5642033
89 meter E =
0018418
Z = 1127879
83 I = 51
35884
XDOT = 4626
389602 Wp = 39
76287
YDOT = -1778
049008 meter/sec RA = 229
68690 deg
ZDOT = 5851
465375 TA = 332
51684
MA = 332
61412
Ha = 228
684 n
mi
Hp = 220
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11825731
63 X = -3546602
90
Y = -18510609
86 feet Y = -5682018
20 meter
Z = 3700393
15 Z = 1110510
72
XDOT = 15178
443575 XDOT = 4617
505031
YDOT = -5833
494121 feet/sec YDOT = -1726
363463 meter/sec
ZDOT = 19197
721046 ZDOT = 5873
917137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5303076
98 X = -1616377
86
Y = -21329451
64 feet Y = -6501216
86 meter
Z = 3621516
61 Z = 1103838
26
XDOT = 14568
060854 XDOT = 4440
344948
YDOT = -322
740622 feet/sec YDOT = -98
371342 meter/sec
ZDOT = 19300
233615 ZDOT = 5882
711206
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 19339
80674247
00016717 00000-0 10270-3 0 9022
2 25544 51
6387 230
4602 0006825 2
6184 357
5001 15
50088926 1872
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80674247 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 230
4602 deg
Eccentricity:
0006825
Arg of perigee: 2
6184 deg
Mean anomaly: 357
5001 deg
Mean motion: 15
50088926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 308
Coasting Arc #4 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2019/339/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -347370
86 A = 6792636
32 meter
Y = 5108812
07 meter E =
0013596
Z = -4476667
40 I = 51
33437
XDOT = -6143
416284 Wp = 42
46988
YDOT = -3235
720895 meter/sec RA = 229
49954 deg
ZDOT = -3211
838100 TA = 194
98347
MA = 195
02380
Ha = 228
709 n
mi
Hp = 220
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1139668
19 X = -382727
94
Y = 16761194
47 feet Y = 5104730
09 meter
Z = -14687229
01 Z = -4478440
40
XDOT = -20155
565236 XDOT = -6091
175469
YDOT = -10615
882203 feet/sec YDOT = -3304
128637 meter/sec
ZDOT = -10537
526574 ZDOT = -3241
554054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2239868
55 X = -682711
93
Y = 16642496
48 feet Y = 5072632
93 meter
Z = -14695627
91 Z = -4479227
39
XDOT = -18057
059039 XDOT = -5503
791595
YDOT = -11866
431551 feet/sec YDOT = -3616
888337 meter/sec
ZDOT = -10672
865705 ZDOT = -3253
089467
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 19339
80674267
00016717 00000-0 10270-3 0 9035
2 25544 51
6399 230
4607 0006813 3
0517 357
0673 15
50096483 1879
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80674267 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 230
4607 deg
Eccentricity:
0006813
Arg of perigee: 3
0517 deg
Mean anomaly: 357
0673 deg
Mean motion: 15
50096483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 318
Coasting Arc #5 (Orbit 196)
---------------------------------------
Vector Time (GMT): 2019/340/09:34:11
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 922439
61 A = 6791054
56 meter
Y = -4657780
94 meter E =
0007443
Z = 4848116
41 I = 51
34411
XDOT = 6234
559484 Wp = 61
24203
YDOT = 3750
563026 meter/sec RA = 226
44504 deg
ZDOT = 2417
770205 TA = 4
94427
MA = 4
93692
Ha = 228
733 n
mi
Hp = 220
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3026376
68 X = 950906
03
Y = -15281433
53 feet Y = -4647306
68 meter
Z = 15905893
72 Z = 4852666
19
XDOT = 20454
591484 XDOT = 6180
411930
YDOT = 12304
996803 feet/sec YDOT = 3819
979380 meter/sec
ZDOT = 7932
316946 ZDOT = 2447
924356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6995678
38 X = 2132282
77
Y = 13895039
38 feet Y = 4235208
00 meter
Z = 15926926
45 Z = 4854527
18
XDOT = -22660
921879 XDOT = -6907
048989
YDOT = 2161
918310 feet/sec YDOT = 658
952701 meter/sec
ZDOT = 8069
634763 ZDOT = 2459
624676
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 19340
45144066
00016717 00000-0 10270-3 0 9048
2 25544 51
6411 227
2706 0007169 3
5153 356
6046 15
50115085 1974
Satellite: ISS
Catalog Number: 25544
Epoch time: 19340
45144066 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 227
2706 deg
Eccentricity:
0007169
Arg of perigee: 3
5153 deg
Mean anomaly: 356
6046 deg
Mean motion: 15
50115085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 197
Checksum: 286
Coasting Arc #6 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2019/341/09:34:11
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -914930
34 A = 6790522
58 meter
Y = 4521817
91 meter E =
0016856
Z = -4997467
84 I = 51
36702
XDOT = -6464
409923 Wp = 51
55163
YDOT = -3552
661426 meter/sec RA = 221
46912 deg
ZDOT = -2025
421936 TA = 198
60386
MA = 198
66555
Ha = 228
968 n
mi
Hp = 220
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3001739
97 X = -941151
39
Y = 14835360
59 feet Y = 4511440
21 meter
Z = -16395891
85 Z = -5001975
68
XDOT = -21208
693973 XDOT = -6414
364077
YDOT = -11655
713340 feet/sec YDOT = -3624
671075 meter/sec
ZDOT = -6645
085092 ZDOT = -2056
702692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6977675
14 X = -2126795
38
Y = -13406228
63 feet Y = -4086218
49 meter
Z = -16416720
73 Z = -5003816
48
XDOT = 22839
423810 XDOT = 6961
456377
YDOT = -3553
182196 feet/sec YDOT = -1083
009933 meter/sec
ZDOT = -6787
572209 ZDOT = -2068
852009
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 19341
41848936
00016717 00000-0 10270-3 0 9053
2 25544 51
6420 222
4792 0007305 7
7325 352
3937 15
50105462 2123
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
41848936 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 222
4792 deg
Eccentricity:
0007305
Arg of perigee: 7
7325 deg
Mean anomaly: 352
3937 deg
Mean motion: 15
50105462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 212
Checksum: 290
Coasting Arc #7 (Orbit 212)
---------------------------------------
Vector Time (GMT): 2019/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 942917
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1838086
57 A = 6795589
54 meter
Y = 5454783
27 meter E =
0010015
Z = -3624779
53 I = 51
38639
XDOT = -6226
614076 Wp = 38
16077
YDOT = -807
963022 meter/sec RA = 221
18271 deg
ZDOT = -4372
105831 TA = 184
83676
MA = 184
84645
Ha = 228
940 n
mi
Hp = 220
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6030467
76 X = 1794560
38
Y = 17896270
58 feet Y = 5475094
92 meter
Z = -11892321
29 Z = -3615956
05
XDOT = -20428
523872 XDOT = -6195
878885
YDOT = -2650
797315 feet/sec YDOT = -877
421292 meter/sec
ZDOT = -14344
179237 ZDOT = -4402
278185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18555662
39 X = -5655765
90
Y = -3643980
77 feet Y = -1110685
34 meter
Z = -11852389
84 Z = -3612608
42
XDOT = 12185
938989 XDOT = 3714
274204
YDOT = -14936
196334 feet/sec YDOT = -4552
552642 meter/sec
ZDOT = -14481
771822 ZDOT = -4414
044051
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 19341
48295860
00016717 00000-0 10270-3 0 9063
2 25544 51
6431 222
1607 0007244 6
6180 353
5065 15
50093569 2136
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
48295860 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 222
1607 deg
Eccentricity:
0007244
Arg of perigee: 6
6180 deg
Mean anomaly: 353
5065 deg
Mean motion: 15
50093569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 213
Checksum: 293
Coasting Arc #8 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2019/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 942917
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1904568
54 A = 6794792
10 meter
Y = -5231647
39 meter E =
0013766
Z = 3879674
55 I = 51
40986
XDOT = 6454
038264 Wp = 66
44046
YDOT = 684
728146 meter/sec RA = 216
21081 deg
ZDOT = 4085
551778 TA = 340
56744
MA = 340
61987
Ha = 229
126 n
mi
Hp = 220
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6248584
46 X = -1864770
78
Y = -17164197
47 feet Y = -5252723
40 meter
Z = 12728591
06 Z = 3870518
98
XDOT = 21174
666219 XDOT = 6426
056109
YDOT = 2246
483419 feet/sec YDOT = 756
744985 meter/sec
ZDOT = 13404
041268 ZDOT = 4116
835652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18083540
22 X = 5511863
06
Y = 2773810
28 feet Y = 845457
37 meter
Z = 12687121
91 Z = 3867034
76
XDOT = -11978
164694 XDOT = -3650
944599
YDOT = 16036
577205 feet/sec YDOT = 4887
948732 meter/sec
ZDOT = 13546
727610 ZDOT = 4129
042575
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 19342
51447410
00016717 00000-0 10270-3 0 9079
2 25544 51
6434 217
0493 0007376 11
4064 348
7253 15
50083154 2297
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
51447410 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 217
0493 deg
Eccentricity:
0007376
Arg of perigee: 11
4064 deg
Mean anomaly: 348
7253 deg
Mean motion: 15
50083154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 229
Checksum: 290
Coasting Arc #9 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2019/342/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 942917
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -228170
52 A = 6791212
85 meter
Y = -4780490
07 meter E =
0008476
Z = 4810137
39 I = 51
41038
XDOT = 6894
041152 Wp = 68
55296
YDOT = 2211
729870 meter/sec RA = 213
94309 deg
ZDOT = 2524
564935 TA = 356
53175
MA = 356
53762
Ha = 228
890 n
mi
Hp = 220
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -748590
94 X = -198062
08
Y = -15684022
52 feet Y = -4782873
70 meter
Z = 15781290
67 Z = 4809101
72
XDOT = 22618
245249 XDOT = 6856
533432
YDOT = 7256
331594 feet/sec YDOT = 2288
613970 meter/sec
ZDOT = 8282
693355 ZDOT = 2557
963238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11711690
41 X = -3569723
24
Y = -10465454
91 feet Y = -3189870
66 meter
Z = 15776838
95 Z = 4808780
51
XDOT = 20303
824774 XDOT = 6188
605791
YDOT = -10003
063790 feet/sec YDOT = -3048
933843 meter/sec
ZDOT = 8434
947396 ZDOT = 2570
971966
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 19342
96575889
00016717 00000-0 10270-3 0 9081
2 25544 51
6430 214
8105 0006875 12
5126 347
6194 15
50124299 2368
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
96575889 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 214
8105 deg
Eccentricity:
0006875
Arg of perigee: 12
5126 deg
Mean anomaly: 347
6194 deg
Mean motion: 15
50124299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 323
Coasting Arc #10 (Orbit 243)
---------------------------------------
Vector Time (GMT): 2019/343/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6042368
39 A = 6797273
89 meter
Y = 894269
73 meter E =
0015974
Z = 2976036
33 I = 51
44465
XDOT = 1624
925047 Wp = 70
05052
YDOT = 5609
633506 meter/sec RA = 211
26879 deg
ZDOT = -4957
707223 TA = 75
88697
MA = 75
70950
Ha = 229
165 n
mi
Hp = 219
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19824043
29 X = 6017463
16
Y = 2933955
80 feet Y = 961700
21 meter
Z = 9763898
72 Z = 3005327
98
XDOT = 5331
118921 XDOT = 1586
157906
YDOT = 18404
309403 feet/sec YDOT = 5627
588296 meter/sec
ZDOT = -16265
443644 ZDOT = -4949
907419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13353991
50 X = -4070296
61
Y = 14854120
56 feet Y = 4527535
95 meter
Z = 9897500
72 Z = 3016758
22
XDOT = -17265
397213 XDOT = -5262
493071
YDOT = -4648
958843 feet/sec YDOT = -1417
002655 meter/sec
ZDOT = -16230
173547 ZDOT = -4946
956897
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 19343
48151853
00016717 00000-0 10270-3 0 9091
2 25544 51
6424 212
2589 0007365 15
6211 344
5166 15
50085113 2448
Satellite: ISS
Catalog Number: 25544
Epoch time: 19343
48151853 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 212
2589 deg
Eccentricity:
0007365
Arg of perigee: 15
6211 deg
Mean anomaly: 344
5166 deg
Mean motion: 15
50085113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 244
Checksum: 293
Coasting Arc #11 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2019/344/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6204973
41 A = 6797916
68 meter
Y = -685283
18 meter E =
0011540
Z = -2681975
04 I = 51
47607
XDOT = -1632
478236 Wp = 33
38023
YDOT = -5405
387356 meter/sec RA = 206
30264 deg
ZDOT = 5178
094567 TA = 296
31849
MA = 296
43698
Ha = 229
135 n
mi
Hp = 219
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20357524
30 X = -6183821
45
Y = -2248304
38 feet Y = -754552
98 meter
Z = -8799130
72 Z = -2712065
68
XDOT = -5355
899726 XDOT = -1597
064999
YDOT = -17734
210487 feet/sec YDOT = -5423
445504 meter/sec
ZDOT = 16988
499237 ZDOT = 5170
249827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12808634
08 X = 3904071
67
Y = -15905591
57 feet Y = -4848024
31 meter
Z = -8936409
75 Z = -2723817
69
XDOT = 16733
621592 XDOT = 5100
407861
YDOT = 3986
968879 feet/sec YDOT = 1215
228114 meter/sec
ZDOT = 16953
005168 ZDOT = 5167
275975
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 19344
44856133
00016717 00000-0 10270-3 0 9103
2 25544 51
6422 207
4676 0007378 17
4899 342
6504 15
50104272 2594
Satellite: ISS
Catalog Number: 25544
Epoch time: 19344
44856133 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 207
4676 deg
Eccentricity:
0007378
Arg of perigee: 17
4899 deg
Mean anomaly: 342
6504 deg
Mean motion: 15
50104272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 259
Checksum: 311
Coasting Arc #12 (Orbit 274)
---------------------------------------
Vector Time (GMT): 2019/345/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6365184
38 A = 6798728
97 meter
Y = 500032
33 meter E =
0016196
Z = 2327151
49 I = 51
50898
XDOT = 1572
821121 Wp = 80
05183
YDOT = 5213
761928 meter/sec RA = 201
33956 deg
ZDOT = -5387
417262 TA = 74
00271
MA = 73
82437
Ha = 229
317 n
mi
Hp = 219
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20883150
86 X = 6347815
64
Y = 1640526
01 feet Y = 571114
87 meter
Z = 7635011
47 Z = 2358029
49
XDOT = 5160
174282 XDOT = 1540
571858
YDOT = 17105
518136 feet/sec YDOT = 5231
170771 meter/sec
ZDOT = -17675
253485 ZDOT = -5379
854570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12294097
71 X = -3747240
98
Y = 16896182
98 feet Y = 5149956
57 meter
Z = 7775916
51 Z = 2370099
35
XDOT = -16107
569966 XDOT = -4909
587326
YDOT = -3549
966921 feet/sec YDOT = -1082
029918 meter/sec
ZDOT = -17641
028653 ZDOT = -5376
985534
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 19345
48007397
00016717 00000-0 10270-3 0 9119
2 25544 51
6421 202
3571 0007380 21
8987 338
2478 15
50089789 2755
Satellite: ISS
Catalog Number: 25544
Epoch time: 19345
48007397 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 202
3571 deg
Eccentricity:
0007380
Arg of perigee: 21
8987 deg
Mean anomaly: 338
2478 deg
Mean motion: 15
50089789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 275
Checksum: 328
Coasting Arc #13 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2019/346/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6415330
42 A = 6800913
47 meter
Y = -2219965
47 meter E =
0019223
Z = 165980
17 I = 51
53465
XDOT = 1707
331388 Wp = 39
78155
YDOT = -4457
572547 meter/sec RA = 197
97471 deg
ZDOT = 6000
245883 TA = 322
00736
MA = 322
14280
Ha = 229
251 n
mi
Hp = 219
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21047671
98 X = -6390835
57
Y = -7283351
28 feet Y = -2291569
29 meter
Z = 544554
35 Z = 134875
69
XDOT = 5601
480932 XDOT = 1727
904184
YDOT = -14624
581847 feet/sec YDOT = -4438
365843 meter/sec
ZDOT = 19685
846074 ZDOT = 6008
588846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5971854
88 X = 1820221
37
Y = 21459800
25 feet Y = 6540947
12 meter
Z = 402695
14 Z = 122741
48
XDOT = -13574
875906 XDOT = -4137
622176
YDOT = 3376
648618 feet/sec YDOT = 1029
202499 meter/sec
ZDOT = 19724
178771 ZDOT = 6011
929689
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 19346
18923389
00016717 00000-0 10270-3 0 9126
2 25544 51
6386 198
8419 0007193 26
7763 333
3757 15
50151916 2863
Satellite: ISS
Catalog Number: 25544
Epoch time: 19346
18923389 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 198
8419 deg
Eccentricity:
0007193
Arg of perigee: 26
7763 deg
Mean anomaly: 333
3757 deg
Mean motion: 15
50151916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 286
Checksum: 343
Coasting Arc #14 (Orbit 300)
---------------------------------------
Vector Time (GMT): 2019/347/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6486577
91 A = 6800921
68 meter
Y = 1961995
89 meter E =
0010972
Z = -567988
50 I = 51
56570
XDOT = -1853
057470 Wp = 98
77089
YDOT = 4429
037084 meter/sec RA = 193
01535 deg
ZDOT = -5963
697976 TA = 87
34984
MA = 87
22425
Ha = 229
525 n
mi
Hp = 219
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21281423
58 X = 6466915
19
Y = 6436994
38 feet Y = 2034423
53 meter
Z = -1863479
33 Z = -536526
37
XDOT = -6079
584874 XDOT = -1873
478012
YDOT = 14530
961562 feet/sec YDOT = 4408
201664 meter/sec
ZDOT = -19565
938242 ZDOT = -5972
748383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7169498
62 X = -2185263
18
Y = -21058169
83 feet Y = -6418530
16 meter
Z = -1719946
09 Z = -524239
57
XDOT = 13739
172620 XDOT = 4187
699815
YDOT = -3105
367072 feet/sec YDOT = -946
515884 meter/sec
ZDOT = -19607
504425 ZDOT = -5976
367349
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 19347
15627572
00016717 00000-0 10270-3 0 9130
2 25544 51
6378 194
0494 0007548 28
7026 331
4538 15
50106923 3015
Satellite: ISS
Catalog Number: 25544
Epoch time: 19347
15627572 = yrday
fracday
Element set: 913
Inclination: 51
6378 deg
RA of node: 194
0494 deg
Eccentricity:
0007548
Arg of perigee: 28
7026 deg
Mean anomaly: 331
4538 deg
Mean motion: 15
50106923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 309
Coasting Arc #15 (Orbit 316)
---------------------------------------
Vector Time (GMT): 2019/348/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6520122
15 A = 6800620
58 meter
Y = -1657254
51 meter E =
0020326
Z = 916836
54 I = 51
59721
XDOT = 1975
212571 Wp = 47
32682
YDOT = -4458
253021 meter/sec RA = 188
05956 deg
ZDOT = 5918
163902 TA = 322
59547
MA = 322
73678
Ha = 229
435 n
mi
Hp = 219
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21391476
86 X = -6505559
14
Y = -5437186
72 feet Y = -1730085
84 meter
Z = 3007993
88 Z = 885199
29
XDOT = 6480
356205 XDOT = 1996
172070
YDOT = -14626
814373 feet/sec YDOT = -4436
048554 meter/sec
ZDOT = 19416
548235 ZDOT = 5927
808951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8403554
84 X = 2561403
52
Y = 20430033
72 feet Y = 6227074
28 meter
Z = 2863616
07 Z = 872830
18
XDOT = -14036
840601 XDOT = -4278
429015
YDOT = 3012
240967 feet/sec YDOT = 918
131047 meter/sec
ZDOT = 19460
836689 ZDOT = 5931
663023
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 19348
18778279
00016717 00000-0 10270-3 0 9146
2 25544 51
6372 188
9391 0007269 33
0077 327
1526 15
50144799 3171
Satellite: ISS
Catalog Number: 25544
Epoch time: 19348
18778279 = yrday
fracday
Element set: 914
Inclination: 51
6372 deg
RA of node: 188
9391 deg
Eccentricity:
0007269
Arg of perigee: 33
0077 deg
Mean anomaly: 327
1526 deg
Mean motion: 15
50144799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 317
Checksum: 341
Coasting Arc #16 (Orbit 331)
---------------------------------------
Vector Time (GMT): 2019/349/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6526224
16 A = 6800351
90 meter
Y = 1394426
82 meter E =
0009874
Z = -1312258
74 I = 51
63032
XDOT = -2123
287755 Wp = 95
83886
YDOT = 4498
289265 meter/sec RA = 183
10437 deg
ZDOT = -5818
499899 TA = 98
40752
MA = 98
29558
Ha = 229
635 n
mi
Hp = 219
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21411496
58 X = 6516520
43
Y = 4574891
14 feet Y = 1467353
61 meter
Z = -4305310
83 Z = -1280580
26
XDOT = -6966
167175 XDOT = -2145
168198
YDOT = 14758
166881 feet/sec YDOT = 4474
423695 meter/sec
ZDOT = -19089
566598 ZDOT = -5828
866466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9454619
72 X = -2881768
09
Y = -19779186
99 feet Y = -6028696
19 meter
Z = -4160702
36 Z = -1268182
08
XDOT = 14421
447648 XDOT = 4395
657243
YDOT = -2895
606750 feet/sec YDOT = -882
580937 meter/sec
ZDOT = -19137
157477 ZDOT = -5833
005599
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 19349
15482288
00016717 00000-0 10270-3 0 9157
2 25544 51
6382 184
1466 0007525 35
1988 324
9658 15
50109208 3326
Satellite: ISS
Catalog Number: 25544
Epoch time: 19349
15482288 = yrday
fracday
Element set: 915
Inclination: 51
6382 deg
RA of node: 184
1466 deg
Eccentricity:
0007525
Arg of perigee: 35
1988 deg
Mean anomaly: 324
9658 deg
Mean motion: 15
50109208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 332
Checksum: 327
Coasting Arc #17 (Orbit 347)
---------------------------------------
Vector Time (GMT): 2019/350/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6492511
38 A = 6799867
81 meter
Y = -1097340
59 meter E =
0020848
Z = 1651603
97 I = 51
66303
XDOT = 2240
915946 Wp = 55
28939
YDOT = -4595
148937 meter/sec RA = 178
15246 deg
ZDOT = 5716
373709 TA = 322
78024
MA = 322
92456
Ha = 229
622 n
mi
Hp = 218
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21300890
34 X = -6487780
57
Y = -3600198
78 feet Y = -1169918
20 meter
Z = 5418648
20 Z = 1620077
35
XDOT = 7352
086438 XDOT = 2264
366925
YDOT = -15075
947957 feet/sec YDOT = -4569
959061 meter/sec
ZDOT = 18754
506919 ZDOT = 5727
315516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10491200
97 X = 3197718
06
Y = 18925206
63 feet Y = 5768402
98 meter
Z = 5274690
99 Z = 1607725
81
XDOT = -14910
207717 XDOT = -4544
631312
YDOT = 2987
091065 feet/sec YDOT = 910
465356 meter/sec
ZDOT = 18804
735279 ZDOT = 5731
683313
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 19350
18632690
00016717 00000-0 10270-3 0 9167
2 25544 51
6388 179
0360 0007390 39
1567 321
0117 15
50139012 3486
Satellite: ISS
Catalog Number: 25544
Epoch time: 19350
18632690 = yrday
fracday
Element set: 916
Inclination: 51
6388 deg
RA of node: 179
0360 deg
Eccentricity:
0007390
Arg of perigee: 39
1567 deg
Mean anomaly: 321
0117 deg
Mean motion: 15
50139012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 348
Checksum: 297
Coasting Arc #18 (Orbit 362)
---------------------------------------
Vector Time (GMT): 2019/351/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6435125
45 A = 6799349
42 meter
Y = 850332
87 meter E =
0009424
Z = -2033294
74 I = 51
69482
XDOT = -2369
548906 Wp = 87
19236
YDOT = 4701
441028 meter/sec RA = 173
20180 deg
ZDOT = -5555
006676 TA = 115
19889
MA = 115
10114
Ha = 229
770 n
mi
Hp = 218
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21112616
30 X = 6435015
04
Y = 2789806
00 feet Y = 922294
59 meter
Z = -6670914
51 Z = -2002035
74
XDOT = -7774
110583 XDOT = -2394
962770
YDOT = 15424
675289 feet/sec YDOT = 4674
801557 meter/sec
ZDOT = -18225
087521 ZDOT = -5566
578183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11325469
70 X = -3452003
17
Y = -18087116
08 feet Y = -5512952
98 meter
Z = -6528143
15 Z = -1989778
03
XDOT = 15444
311521 XDOT = 4707
426152
YDOT = -3099
963272 feet/sec YDOT = -944
868805 meter/sec
ZDOT = -18278
202936 ZDOT = -5571
196255
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 19351
15336372
00016717 00000-0 10270-3 0 9174
2 25544 51
6391 174
2439 0007637 41
5115 318
6615 15
50113436 3638
Satellite: ISS
Catalog Number: 25544
Epoch time: 19351
15336372 = yrday
fracday
Element set: 917
Inclination: 51
6391 deg
RA of node: 174
2439 deg
Eccentricity:
0007637
Arg of perigee: 41
5115 deg
Mean anomaly: 318
6615 deg
Mean motion: 15
50113436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 363
Checksum: 296
Coasting Arc #19 (Orbit 378)
---------------------------------------
Vector Time (GMT): 2019/352/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6339565
65 A = 6798730
58 meter
Y = -579484
03 meter E =
0020724
Z = 2354705
91 I = 51
72605
XDOT = 2459
655760 Wp = 63
63212
YDOT = -4861
554168 meter/sec RA = 168
25418 deg
ZDOT = 5397
925754 TA = 322
59301
MA = 322
73709
Ha = 229
796 n
mi
Hp = 218
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20799099
89 X = -6344052
29
Y = -1901194
32 feet Y = -650402
82 meter
Z = 7725413
10 Z = 2323899
94
XDOT = 8069
736744 XDOT = 2487
616329
YDOT = -15949
980867 feet/sec YDOT = -4833
892677 meter/sec
ZDOT = 17709
730165 ZDOT = 5409
941259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12110995
71 X = 3691431
49
Y = 17079097
25 feet Y = 5205708
84 meter
Z = 7584676
89 Z = 2311809
52
XDOT = -16041
431731 XDOT = -4889
428392
YDOT = 3444
708382 feet/sec YDOT = 1049
947115 meter/sec
ZDOT = 17764
887972 ZDOT = 5414
737854
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 19352
18486742
00016717 00000-0 10270-3 0 9186
2 25544 51
6393 169
1337 0007468 45
6720 314
5041 15
50128732 3799
Satellite: ISS
Catalog Number: 25544
Epoch time: 19352
18486742 = yrday
fracday
Element set: 918
Inclination: 51
6393 deg
RA of node: 169
1337 deg
Eccentricity:
0007468
Arg of perigee: 45
6720 deg
Mean anomaly: 314
5041 deg
Mean motion: 15
50128732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 379
Checksum: 319
Coasting Arc #20 (Orbit 393)
---------------------------------------
Vector Time (GMT): 2019/353/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6226893
87 A = 6797985
39 meter
Y = 366003
50 meter E =
0009927
Z = -2714237
62 I = 51
75718
XDOT = -2546
695583 Wp = 77
44832
YDOT = 5024
888876 meter/sec RA = 163
30732 deg
ZDOT = -5178
855125 TA = 133
08409
MA = 133
00096
Ha = 229
830 n
mi
Hp = 218
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20429441
85 X = 6235522
53
Y = 1200798
89 feet Y = 435685
47 meter
Z = -8904979
08 Z = -2683968
84
XDOT = -8355
300470 XDOT = -2577
540175
YDOT = 16485
855891 feet/sec YDOT = 4996
237819 meter/sec
ZDOT = -16990
994503 ZDOT = -5191
300541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12687505
68 X = -3867151
73
Y = -16133052
62 feet Y = -4917354
44 meter
Z = -8766668
55 Z = -2672080
58
XDOT = 16627
147859 XDOT = 5067
954668
YDOT = -3837
353764 feet/sec YDOT = -1169
625427 meter/sec
ZDOT = -17048
132358 ZDOT = -5196
270743
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 19353
15190194
00016717 00000-0 10270-3 0 9198
2 25544 51
6403 164
3418 0007589 47
9997 312
1798 15
50122533 3946
Satellite: ISS
Catalog Number: 25544
Epoch time: 19353
15190194 = yrday
fracday
Element set: 919
Inclination: 51
6403 deg
RA of node: 164
3418 deg
Eccentricity:
0007589
Arg of perigee: 47
9997 deg
Mean anomaly: 312
1798 deg
Mean motion: 15
50122533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 394
Checksum: 328
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