[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 20th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13923 1181 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
266/16:46:57
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
4
268/13:57:43
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
3
268/17:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
271/11:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
272/00:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
275/04:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 218
3
276/07:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
4
Coasting Arc #1 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2019/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4650881
04 A = 6794411
10 meter
Y = 2999516
07 meter E =
0018248
Z = 3930244
02 I = 51
27849
XDOT = -787
264699 Wp = 74
06783
YDOT = 6491
668548 meter/sec RA = 247
52712 deg
ZDOT = -4002
274990 TA = 58
01823
MA = 57
84099
Ha = 229
854 n
mi
Hp = 218
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15258796
07 X = 4597902
77
Y = 9840931
98 feet Y = 3051229
45 meter
Z = 12894501
39 Z = 3952707
70
XDOT = -2582
889432 XDOT = -840
356856
YDOT = 21298
125157 feet/sec YDOT = 6482
567763 meter/sec
ZDOT = -13130
823457 ZDOT = -4006
228512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14854846
50 X = -4527757
21
Y = -10313506
54 feet Y = -3143556
79 meter
Z = 12996464
29 Z = 3961322
31
XDOT = 2410
133417 XDOT = 734
608665
YDOT = -20125
224194 feet/sec YDOT = -6134
168334 meter/sec
ZDOT = -13149
212671 ZDOT = -4007
880022
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19263
54091017
00016717 00000-0 10270-3 0 9005
2 25544 51
6391 248
3577 0007403 65
2740 294
9180 15
50109248 30046
Satellite: ISS
Catalog Number: 25544
Epoch time: 19263
54091017 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 248
3577 deg
Eccentricity:
0007403
Arg of perigee: 65
2740 deg
Mean anomaly: 294
9180 deg
Mean motion: 15
50109248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 295
Coasting Arc #2 (Orbit 3018)
---------------------------------------
Vector Time (GMT): 2019/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4877789
76 A = 6795284
65 meter
Y = -2966140
54 meter E =
0012727
Z = -3695445
69 I = 51
29448
XDOT = 596
771782 Wp = 83
21939
YDOT = -6309
019630 meter/sec RA = 242
54875 deg
ZDOT = 4290
471786 TA = 232
64621
MA = 232
76221
Ha = 230
020 n
mi
Hp = 218
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16003247
23 X = -4826308
41
Y = -9731432
21 feet Y = -3020399
68 meter
Z = -12124165
65 Z = -3719015
24
XDOT = 1957
912671 XDOT = 646
435799
YDOT = -20698
883301 feet/sec YDOT = -6302
068288 meter/sec
ZDOT = 14076
351003 ZDOT = 4293
491521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15781159
42 X = 4810097
39
Y = 9957583
59 feet Y = 3035071
48 meter
Z = -12231174
25 Z = -3728061
91
XDOT = -1431
008161 XDOT = -436
171287
YDOT = 19518
671403 feet/sec YDOT = 5949
291044 meter/sec
ZDOT = 14090
472662 ZDOT = 4294
776067
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19264
50795400
00016717 00000-0 10270-3 0 9010
2 25544 51
6386 243
5671 0007492 68
9882 291
2069 15
50073353 30196
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
50795400 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 243
5671 deg
Eccentricity:
0007492
Arg of perigee: 68
9882 deg
Mean anomaly: 291
2069 deg
Mean motion: 15
50073353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3019
Checksum: 320
Coasting Arc #3 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2019/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5089282
08 A = 6796100
95 meter
Y = 2950056
95 meter E =
0019526
Z = 3388842
10 I = 51
31384
XDOT = -471
028829 Wp = 83
50323
YDOT = 6119
293614 meter/sec RA = 237
57066 deg
ZDOT = -4594
541026 TA = 56
74231
MA = 56
55535
Ha = 229
903 n
mi
Hp = 218
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16697119
70 X = 5039454
25
Y = 9678664
52 feet Y = 3006690
36 meter
Z = 11118248
37 Z = 3413442
97
XDOT = -1545
370175 XDOT = -517
103686
YDOT = 20076
422617 feet/sec YDOT = 6113
768511 meter/sec
ZDOT = -15073
953496 ZDOT = -4596
941168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16650580
70 X = -5075097
00
Y = -9629736
93 feet Y = -2935143
82 meter
Z = 11229965
67 Z = 3422893
54
XDOT = 681
649155 XDOT = 207
766662
YDOT = -18865
551454 feet/sec YDOT = -5750
220083 meter/sec
ZDOT = -15085
235228 ZDOT = -4597
979697
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19265
53946506
00016717 00000-0 10270-3 0 9020
2 25544 51
6386 238
4556 0007374 72
2335 287
9619 15
50106833 30352
Satellite: ISS
Catalog Number: 25544
Epoch time: 19265
53946506 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 238
4556 deg
Eccentricity:
0007374
Arg of perigee: 72
2335 deg
Mean anomaly: 287
9619 deg
Mean motion: 15
50106833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 326
Coasting Arc #4 (Orbit 3049)
---------------------------------------
Vector Time (GMT): 2019/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5325216
89 A = 6796911
61 meter
Y = -2855470
37 meter E =
0011994
Z = -3119036
55 I = 51
33592
XDOT = 349
512160 Wp = 76
37019
YDOT = -5919
132776 meter/sec RA = 232
59504 deg
ZDOT = 4840
740693 TA = 247
65467
MA = 247
78184
Ha = 230
027 n
mi
Hp = 218
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17471184
04 X = -5277739
85
Y = -9368341
12 feet Y = -2914755
32 meter
Z = -10233059
53 Z = -3144789
10
XDOT = 1146
693438 XDOT = 392
161974
YDOT = -19419
726956 feet/sec YDOT = -5914
985692 meter/sec
ZDOT = 15881
695188 ZDOT = 4842
542233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17587348
22 X = 5360623
74
Y = 9015843
70 feet Y = 2748029
16 meter
Z = -10350040
55 Z = -3154692
36
XDOT = 9
969316 XDOT = 3
038648
YDOT = 18153
309400 feet/sec YDOT = 5533
128705 meter/sec
ZDOT = 15890
230685 ZDOT = 4843
342313
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19266
50650441
00016717 00000-0 10270-3 0 9039
2 25544 51
6392 233
6645 0007464 75
4984 284
6994 15
50084060 30504
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
50650441 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 233
6645 deg
Eccentricity:
0007464
Arg of perigee: 75
4984 deg
Mean anomaly: 284
6994 deg
Mean motion: 15
50084060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 317
Coasting Arc #5 (Orbit 3052)
---------------------------------------
Vector Time (GMT): 2019/266/16:46:57
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4400579
01 A = 6800995
47 meter
Y = -5168335
79 meter E =
0017988
Z = -301980
32 I = 51
35717
XDOT = 3482
276247 Wp = 55
87006
YDOT = -3298
605422 meter/sec RA = 231
62562 deg
ZDOT = 5975
841167 TA = 300
86793
MA = 301
04475
Ha = 229
950 n
mi
Hp = 218
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14437595
18 X = -4340991
27
Y = -16956482
25 feet Y = -5217213
00 meter
Z = -990749
07 Z = -323211
83
XDOT = 11424
790836 XDOT = 3489
876058
YDOT = -10822
196267 feet/sec YDOT = -3259
621499 meter/sec
ZDOT = 19605
778108 ZDOT = 5992
775319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20420753
61 X = 6224245
70
Y = -8874638
22 feet Y = -2704989
73 meter
Z = -1087035
92 Z = -331328
55
XDOT = 6421
480421 XDOT = 1957
267232
YDOT = 12462
465722 feet/sec YDOT = 3798
559552 meter/sec
ZDOT = 19682
999553 ZDOT = 5999
378264
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19266
69991212
00016717 00000-0 10270-3 0 9044
2 25544 51
6427 232
7070 0007314 75
6101 284
5861 15
50107432 30536
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
69991212 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 232
7070 deg
Eccentricity:
0007314
Arg of perigee: 75
6101 deg
Mean anomaly: 284
5861 deg
Mean motion: 15
50107432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3053
Checksum: 294
Coasting Arc #6 (Orbit 3068)
---------------------------------------
Vector Time (GMT): 2019/267/16:46:57
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4599258
38 A = 6801138
67 meter
Y = 5002501
99 meter E =
0017263
Z = -111333
06 I = 51
37841
XDOT = -3578
764493 Wp = 115
09317
YDOT = 3173
519829 meter/sec RA = 226
65487 deg
ZDOT = -5984
266628 TA = 66
10825
MA = 65
92747
Ha = 230
074 n
mi
Hp = 218
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15089430
38 X = 4543517
92
Y = 16412408
10 feet Y = 5053622
47 meter
Z = -365265
94 Z = -89127
23
XDOT = -11741
353324 XDOT = -3584
917555
YDOT = 10411
810462 feet/sec YDOT = 3133
464906 meter/sec
ZDOT = -19633
420697 ZDOT = -6001
665959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19923145
92 X = -6072574
88
Y = 10009483
37 feet Y = 3050890
53 meter
Z = -264513
34 Z = -80623
66
XDOT = -6096
231914 XDOT = -1858
131487
YDOT = -12566
726048 feet/sec YDOT = -3830
338099 meter/sec
ZDOT = -19712
752942 ZDOT = -6008
447097
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19267
73141889
00016717 00000-0 10270-3 0 9058
2 25544 51
6422 227
5964 0007357 80
6293 279
5689 15
50073262 30692
Satellite: ISS
Catalog Number: 25544
Epoch time: 19267
73141889 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 227
5964 deg
Eccentricity:
0007357
Arg of perigee: 80
6293 deg
Mean anomaly: 279
5689 deg
Mean motion: 15
50073262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3069
Checksum: 344
Coasting Arc #7 (Orbit 3082)
---------------------------------------
Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 841306
74 A = 6790601
23 meter
Y = -4572030
26 meter E =
0012869
Z = 4939774
77 I = 51
36288
XDOT = 6454
971885 Wp = 101
70346
YDOT = 3532
769295 meter/sec RA = 222
28162 deg
ZDOT = 2163
050155 TA = 327
09186
MA = 327
17192
Ha = 229
896 n
mi
Hp = 218
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2760192
72 X = 868375
39
Y = -15000099
28 feet Y = -4562470
52 meter
Z = 16206610
13 Z = 4943927
53
XDOT = 21177
729281 XDOT = 6404
480835
YDOT = 11590
450444 feet/sec YDOT = 3604
671164 meter/sec
ZDOT = 7096
621245 ZDOT = 2194
283011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5857045
43 X = 1785227
45
Y = 14060443
47 feet Y = 4285623
17 meter
Z = 16225745
05 Z = 4945607
09
XDOT = -23018
979578 XDOT = -7016
184975
YDOT = 1207
735838 feet/sec YDOT = 368
117883 meter/sec
ZDOT = 7238
545159 ZDOT = 2206
308564
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19268
63398427
00016717 00000-0 10270-3 0 9061
2 25544 51
6404 223
1237 0007250 83
1587 277
0388 15
50138178 30836
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
63398427 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 223
1237 deg
Eccentricity:
0007250
Arg of perigee: 83
1587 deg
Mean anomaly: 277
0388 deg
Mean motion: 15
50138178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3083
Checksum: 321
Coasting Arc #8 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1028537
46 A = 6790384
76 meter
Y = -4449350
71 meter E =
0012388
Z = 5015568
79 I = 51
36659
XDOT = 6451
244572 Wp = 101
32257
YDOT = 3672
662171 meter/sec RA = 221
63728 deg
ZDOT = 1928
653007 TA = 329
86361
MA = 329
93483
Ha = 229
994 n
mi
Hp = 218
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3374466
75 X = 1053852
20
Y = -14597607
31 feet Y = -4437707
01 meter
Z = 16455278
17 Z = 5020626
79
XDOT = 21165
500565 XDOT = 6400
328044
YDOT = 12049
416573 feet/sec YDOT = 3744
519972 meter/sec
ZDOT = 6327
601729 ZDOT = 1959
866700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13740605
41 X = 4188136
53
Y = 5908243
63 feet Y = 1800832
66 meter
Z = 16478524
35 Z = 5022654
22
XDOT = -15319
615204 XDOT = -4669
418714
YDOT = 17525
704091 feet/sec YDOT = 5341
834607 meter/sec
ZDOT = 6469
434321 ZDOT = 1971
883581
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19268
76292307
00016717 00000-0 10270-3 0 9076
2 25544 51
6420 222
4854 0007370 83
3018 276
8971 15
50100696 30856
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
76292307 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 222
4854 deg
Eccentricity:
0007370
Arg of perigee: 83
3018 deg
Mean anomaly: 276
8971 deg
Mean motion: 15
50100696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 316
Coasting Arc #9 (Orbit 3099)
---------------------------------------
Vector Time (GMT): 2019/269/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1076582
42 A = 6789829
07 meter
Y = 4320196
29 meter E =
0020743
Z = -5144813
89 I = 51
39109
XDOT = -6654
014039 Wp = 81
22707
YDOT = -3451
589948 meter/sec RA = 216
66195 deg
ZDOT = -1508
109916 TA = 174
16499
MA = 174
14078
Ha = 229
931 n
mi
Hp = 218
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3532094
57 X = -1099821
52
Y = 14173872
33 feet Y = 4308026
77 meter
Z = -16879310
67 Z = -5150100
35
XDOT = -21830
754720 XDOT = -6607
597283
YDOT = -11324
114002 feet/sec YDOT = -3525
740432 meter/sec
ZDOT = -4947
867178 ZDOT = -1540
319466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13396458
81 X = -4083240
64
Y = -5752329
97 feet Y = -1753310
18 meter
Z = -16903581
54 Z = -5152211
65
XDOT = 14408
297562 XDOT = 4391
649097
YDOT = -18605
879323 feet/sec YDOT = -5671
072018 meter/sec
ZDOT = -5094
265888 ZDOT = -1552
732243
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 19269
72995607
00016717 00000-0 10270-3 0 9087
2 25544 51
6424 217
6935 0007197 85
8295 274
3678 15
50129536 31006
Satellite: ISS
Catalog Number: 25544
Epoch time: 19269
72995607 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 217
6935 deg
Eccentricity:
0007197
Arg of perigee: 85
8295 deg
Mean anomaly: 274
3678 deg
Mean motion: 15
50129536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3100
Checksum: 347
Coasting Arc #10 (Orbit 3115)
---------------------------------------
Vector Time (GMT): 2019/270/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1127268
12 A = 6789498
20 meter
Y = -4191063
78 meter E =
0010715
Z = 5212491
59 I = 51
41798
XDOT = 6875
605983 Wp = 101
59318
YDOT = 3217
195704 meter/sec RA = 211
68852 deg
ZDOT = 1095
796039 TA = 337
85269
MA = 337
89895
Ha = 229
947 n
mi
Hp = 218
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3698386
21 X = 1148730
62
Y = -13750209
26 feet Y = -4178337
28 meter
Z = 17101350
36 Z = 5218020
04
XDOT = 22557
762412 XDOT = 6833
796588
YDOT = 10555
104015 feet/sec YDOT = 3293
849934 meter/sec
ZDOT = 3595
131362 ZDOT = 1129
093264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13049712
37 X = 3977552
33
Y = 5619904
49 feet Y = 1712946
89 meter
Z = 17126709
54 Z = 5220221
07
XDOT = -13429
911341 XDOT = -4093
436977
YDOT = 19727
220066 feet/sec YDOT = 6012
856676 meter/sec
ZDOT = 3746
511658 ZDOT = 1141
936753
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 19270
76145623
00016717 00000-0 10270-3 0 9099
2 25544 51
6430 212
5822 0007261 89
5602 270
6381 15
50110248 31164
Satellite: ISS
Catalog Number: 25544
Epoch time: 19270
76145623 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 212
5822 deg
Eccentricity:
0007261
Arg of perigee: 89
5602 deg
Mean anomaly: 270
6381 deg
Mean motion: 15
50110248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3116
Checksum: 287
Coasting Arc #11 (Orbit 3126)
---------------------------------------
Vector Time (GMT): 2019/271/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6258852
08 A = 6800621
36 meter
Y = -2487533
94 meter E =
0015437
Z = -918055
41 I = 51
47437
XDOT = 1041
055269 Wp = 61
94998
YDOT = -4767
576094 meter/sec RA = 207
90529 deg
ZDOT = 5903
840655 TA = 288
10871
MA = 288
27679
Ha = 229
992 n
mi
Hp = 218
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20534291
60 X = -6226111
16
Y = -8161200
58 feet Y = -2557341
88 meter
Z = -3011992
83 Z = -948378
89
XDOT = 3415
535659 XDOT = 1065
612592
YDOT = -15641
653853 feet/sec YDOT = -4755
796261 meter/sec
ZDOT = 19369
555954 ZDOT = 5908
957954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19690051
04 X = 6001527
56
Y = 9985716
44 feet Y = 3043646
37 meter
Z = -3149886
46 Z = -960085
39
XDOT = -3959
728657 XDOT = -1206
925295
YDOT = 13842
905026 feet/sec YDOT = 4219
317452 meter/sec
ZDOT = 19393
067029 ZDOT = 5911
006830
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 19271
47061214
00016717 00000-0 10270-3 0 9103
2 25544 51
6403 209
0676 0007397 92
2761 267
9236 15
50116790 31277
Satellite: ISS
Catalog Number: 25544
Epoch time: 19271
47061214 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 209
0676 deg
Eccentricity:
0007397
Arg of perigee: 92
2761 deg
Mean anomaly: 267
9236 deg
Mean motion: 15
50116790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3127
Checksum: 304
Coasting Arc #12 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/272/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 261172
46 A = 6790370
52 meter
Y = 4559596
71 meter E =
0019719
Z = -5042666
22 I = 51
45930
XDOT = -7206
526293 Wp = 84
17125
YDOT = -1697
766489 meter/sec RA = 205
13351 deg
ZDOT = -1912
886082 TA = 167
20190
MA = 167
15177
Ha = 229
979 n
mi
Hp = 218
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 856865
03 X = 234660
99
Y = 14959306
79 feet Y = 4562368
48 meter
Z = -16544180
50 Z = -5041462
47
XDOT = -23643
458967 XDOT = -7177
713957
YDOT = -5570
100028 feet/sec YDOT = -1778
194083 meter/sec
ZDOT = -6275
872971 ZDOT = -1947
822780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5508864
68 X = 1679101
95
Y = 13940654
29 feet Y = 4249111
43 meter
Z = -16538910
30 Z = -5041059
86
XDOT = -23155
184088 XDOT = -7057
700110
YDOT = 1533
583286 feet/sec YDOT = 467
436186 meter/sec
ZDOT = -6434
807751 ZDOT = -1961
329403
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 19272
05082929
00016717 00000-0 10270-3 0 9115
2 25544 51
6430 206
1903 0007253 98
6253 261
5719 15
50105827 31360
Satellite: ISS
Catalog Number: 25544
Epoch time: 19272
05082929 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 206
1903 deg
Eccentricity:
0007253
Arg of perigee: 98
6253 deg
Mean anomaly: 261
5719 deg
Mean motion: 15
50105827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 299
Coasting Arc #13 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2019/273/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -198536
79 A = 6789753
00 meter
Y = -4426703
16 meter E =
0011871
Z = 5135905
36 I = 51
48892
XDOT = 7381
770852 Wp = 111
77597
YDOT = 1430
132008 meter/sec RA = 200
16556 deg
ZDOT = 1510
875108 TA = 323
60178
MA = 323
68244
Ha = 229
907 n
mi
Hp = 218
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -651367
42 X = -173969
07
Y = -14523304
35 feet Y = -4428785
41 meter
Z = 16850083
20 Z = 5135001
09
XDOT = 24218
408306 XDOT = 7357
890979
YDOT = 4692
034147 feet/sec YDOT = 1512
546825 meter/sec
ZDOT = 4956
939330 ZDOT = 1546
675306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5414490
67 X = -1650336
76
Y = -13496885
33 feet Y = -4113850
65 meter
Z = 16846166
61 Z = 5134711
58
XDOT = 23419
585601 XDOT = 7138
289691
YDOT = -2975
612177 feet/sec YDOT = -906
966592 meter/sec
ZDOT = 5119
832395 ZDOT = 1560
524914
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 19273
08232414
00016717 00000-0 10270-3 0 9126
2 25544 51
6434 201
0795 0007259 102
4002 257
7961 15
50152295 31524
Satellite: ISS
Catalog Number: 25544
Epoch time: 19273
08232414 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 201
0795 deg
Eccentricity:
0007259
Arg of perigee: 102
4002 deg
Mean anomaly: 257
7961 deg
Mean motion: 15
50152295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 284
Coasting Arc #14 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2019/274/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 87441
67 A = 6789497
39 meter
Y = 4339345
18 meter E =
0020946
Z = -5239276
01 I = 51
51934
XDOT = -7482
895905 Wp = 89
75343
YDOT = -1145
588149 meter/sec RA = 195
19963 deg
ZDOT = -1077
356935 TA = 169
89859
MA = 169
85643
Ha = 229
914 n
mi
Hp = 218
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 286882
11 X = 64361
28
Y = 14236696
80 feet Y = 4340193
50 meter
Z = -17189225
76 Z = -5238907
69
XDOT = -24550
183415 XDOT = -7464
296170
YDOT = -3758
491304 feet/sec YDOT = -1229
163270 meter/sec
ZDOT = -3534
635615 ZDOT = -1113
661370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5207909
45 X = 1587370
80
Y = 13254978
37 feet Y = 4040117
41 meter
Z = -17187744
09 Z = -5238824
40
XDOT = -23380
051221 XDOT = -7126
239612
YDOT = 4404
019100 feet/sec YDOT = 1342
345022 meter/sec
ZDOT = -3699
854462 ZDOT = -1127
715640
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 19274
04934909
00016717 00000-0 10270-3 0 9132
2 25544 51
6434 196
2886 0007174 105
1822 255
0122 15
50113500 31678
Satellite: ISS
Catalog Number: 25544
Epoch time: 19274
04934909 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 196
2886 deg
Eccentricity:
0007174
Arg of perigee: 105
1822 deg
Mean anomaly: 255
0122 deg
Mean motion: 15
50113500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 294
Coasting Arc #15 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2019/275/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 14604
34 A = 6789081
21 meter
Y = -4257575
24 meter E =
0010263
Z = 5280208
15 I = 51
55091
XDOT = 7594
698180 Wp = 111
26503
YDOT = 843
405373 meter/sec RA = 190
23564 deg
ZDOT = 654
382856 TA = 332
45309
MA = 332
50744
Ha = 229
850 n
mi
Hp = 218
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 47914
49 X = 36563
92
Y = -13968422
70 feet Y = -4257288
79 meter
Z = 17323517
54 Z = 5280332
70
XDOT = 24916
988778 XDOT = 7581
523836
YDOT = 2767
077995 feet/sec YDOT = 928
261026 meter/sec
ZDOT = 2146
925379 ZDOT = 691
243646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5027717
46 X = -1532448
28
Y = -13031303
61 feet Y = -3971941
34 meter
Z = 17324276
95 Z = 5280439
61
XDOT = 23309
746029 XDOT = 7104
810590
YDOT = -5895
694609 feet/sec YDOT = -1797
007717 meter/sec
ZDOT = 2314
711327 ZDOT = 705
524013
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 19275
08083759
00016717 00000-0 10270-3 0 9146
2 25544 51
6433 191
1779 0007221 108
3644 251
8292 15
50161593 31837
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
08083759 = yrday
fracday
Element set: 914
Inclination: 51
6433 deg
RA of node: 191
1779 deg
Eccentricity:
0007221
Arg of perigee: 108
3644 deg
Mean anomaly: 251
8292 deg
Mean motion: 15
50161593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 317
Coasting Arc #16 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2019/275/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3953517
96 A = 6791850
34 meter
Y = -3037687
89 meter E =
0014697
Z = 4600062
19 I = 51
56296
XDOT = 6156
556496 Wp = 84
84295
YDOT = 3451
009143 meter/sec RA = 189
53816 deg
ZDOT = -3002
774483 TA = 35
19275
MA = 35
09578
Ha = 229
814 n
mi
Hp = 218
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12970859
45 X = 3964847
49
Y = -9966167
62 feet Y = -2993413
23 meter
Z = 15092067
55 Z = 4619294
94
XDOT = 20198
676167 XDOT = 6132
094810
YDOT = 11322
208473 feet/sec YDOT = 3519
719140 meter/sec
ZDOT = -9851
622321 ZDOT = -2972
927346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4881235
31 X = -1487800
52
Y = -15526953
06 feet Y = -4732615
29 meter
Z = 15179771
59 Z = 4626794
38
XDOT = 16517
131067 XDOT = 5034
421549
YDOT = -14721
672651 feet/sec YDOT = -4487
165824 meter/sec
ZDOT = -9715
884288 ZDOT = -2961
401531
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 19275
20977433
00016717 00000-0 10270-3 0 9152
2 25544 51
6416 190
5409 0007357 106
3245 253
8715 15
50153444 31856
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
20977433 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 190
5409 deg
Eccentricity:
0007357
Arg of perigee: 106
3245 deg
Mean anomaly: 253
8715 deg
Mean motion: 15
50153444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 312
Coasting Arc #17 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2019/276/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4078089
07 A = 6792676
18 meter
Y = 3185666
66 meter E =
0016565
Z = -4417000
54 I = 51
59887
XDOT = -6101
353279 Wp = 110
53301
YDOT = -3159
532076 meter/sec RA = 184
57819 deg
ZDOT = 3359
031810 TA = 193
53066
MA = 193
57513
Ha = 229
948 n
mi
Hp = 218
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13379557
33 X = -4091953
35
Y = 10451662
28 feet Y = 3139984
88 meter
Z = -14491471
58 Z = -4436844
49
XDOT = -20017
563251 XDOT = -6081
885580
YDOT = -10365
918883 feet/sec YDOT = -3227
652716 meter/sec
ZDOT = 11020
445570 ZDOT = 3329
440675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5469270
88 X = 1667033
77
Y = 15990794
39 feet Y = 4873994
13 meter
Z = -14581979
22 Z = -4444587
27
XDOT = -15261
515426 XDOT = -4651
709902
YDOT = 15133
022876 feet/sec YDOT = 4612
545373 meter/sec
ZDOT = 10885
841698 ZDOT = 3318
004550
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 19276
17679487
00016717 00000-0 10270-3 0 9168
2 25544 51
6419 185
7494 0007407 109
4806 250
7146 15
50128232 32001
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
17679487 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 185
7494 deg
Eccentricity:
0007407
Arg of perigee: 109
4806 deg
Mean anomaly: 250
7146 deg
Mean motion: 15
50128232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 323
Coasting Arc #18 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/276/07:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3762547
74 A = 6793177
52 meter
Y = -3667667
35 meter E =
0017123
Z = 4295106
74 I = 51
60251
XDOT = 6374
195602 Wp = 108
86150
YDOT = -2376
554838 meter/sec RA = 183
89012 deg
ZDOT = 3537
486998 TA = 304
99535
MA = 305
15597
Ha = 229
909 n
mi
Hp = 218
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12344316
72 X = -3742118
74
Y = -12033029
36 feet Y = -3709628
41 meter
Z = 14091557
53 Z = 4276879
18
XDOT = 20912
715229 XDOT = 6383
113767
YDOT = -7797
095925 feet/sec YDOT = -2305
224077 meter/sec
ZDOT = 11605
928471 ZDOT = 3568
472687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2920963
76 X = -890309
75
Y = 17057891
14 feet Y = 5199245
22 meter
Z = 14008721
04 Z = 4269858
17
XDOT = -16944
022185 XDOT = -5164
537962
YDOT = -12594
765667 feet/sec YDOT = -3838
884575 meter/sec
ZDOT = 11747
138025 ZDOT = 3580
527670
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 19276
37019755
00016717 00000-0 10270-3 0 9177
2 25544 51
6389 184
7918 0007213 110
9159 249
2764 15
50162800 32031
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
37019755 = yrday
fracday
Element set: 917
Inclination: 51
6389 deg
RA of node: 184
7918 deg
Eccentricity:
0007213
Arg of perigee: 110
9159 deg
Mean anomaly: 249
2764 deg
Mean motion: 15
50162800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 322
Coasting Arc #19 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2019/277/07:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3641171
88 A = 6792403
41 meter
Y = 3524250
74 meter E =
0015680
Z = -4536842
40 I = 51
63358
XDOT = -6457
363809 Wp = 88
80652
YDOT = 2619
763020 meter/sec RA = 178
93163 deg
ZDOT = -3156
634264 TA = 149
48563
MA = 149
39431
Ha = 229
906 n
mi
Hp = 218
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11946101
98 X = 3623529
81
Y = 11562502
41 feet Y = 3564870
10 meter
Z = -14884653
53 Z = -4519197
69
XDOT = -21185
576801 XDOT = -6470
845465
YDOT = 8595
023033 feet/sec YDOT = 2547
476743 meter/sec
ZDOT = -10356
411626 ZDOT = -3188
034933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2470238
21 X = 752928
61
Y = -16513019
46 feet Y = -5033168
33 meter
Z = -14804453
28 Z = -4512397
36
XDOT = 18015
125485 XDOT = 5491
010248
YDOT = 12081
083213 feet/sec YDOT = 3682
314163 meter/sec
ZDOT = -10499
544996 ZDOT = -3200
261315
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 19277
33721548
00016717 00000-0 10270-3 0 9185
2 25544 51
6394 179
9990 0007306 113
2381 246
9540 15
50131979 32184
Satellite: ISS
Catalog Number: 25544
Epoch time: 19277
33721548 = yrday
fracday
Element set: 918
Inclination: 51
6394 deg
RA of node: 179
9990 deg
Eccentricity:
0007306
Arg of perigee: 113
2381 deg
Mean anomaly: 246
9540 deg
Mean motion: 15
50131979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 333
Coasting Arc #20 (Orbit 3233)
---------------------------------------
Vector Time (GMT): 2019/278/07:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3532257
03 A = 6791547
84 meter
Y = -3372975
71 meter E =
0015138
Z = 4710733
35 I = 51
66506
XDOT = 6521
340827 Wp = 117
20361
YDOT = -2909
075096 meter/sec RA = 173
97716 deg
ZDOT = 2793
278993 TA = 305
05249
MA = 305
19440
Ha = 229
815 n
mi
Hp = 218
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11588769
78 X = -3517159
25
Y = -11066193
29 feet Y = -3412391
35 meter
Z = 15455161
92 Z = 4693611
59
XDOT = 21395
475153 XDOT = 6539
817945
YDOT = -9544
209634 feet/sec YDOT = -2836
045467 meter/sec
ZDOT = 9164
301158 ZDOT = 2825
002474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1995086
65 X = -608102
41
Y = 15974346
89 feet Y = 4868980
93 meter
Z = 15377324
85 Z = 4687008
61
XDOT = -19156
510259 XDOT = -5838
904327
YDOT = -11396
955686 feet/sec YDOT = -3473
792093 meter/sec
ZDOT = 9308
941456 ZDOT = 2837
365356
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 19278
36869477
00016717 00000-0 10270-3 0 9194
2 25544 51
6399 174
8887 0007119 117
5065 242
6809 15
50178534 32343
Satellite: ISS
Catalog Number: 25544
Epoch time: 19278
36869477 = yrday
fracday
Element set: 919
Inclination: 51
6399 deg
RA of node: 174
8887 deg
Eccentricity:
0007119
Arg of perigee: 117
5065 deg
Mean anomaly: 242
6809 deg
Mean motion: 15
50178534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3234
Checksum: 361
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