[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 1st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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
094/11:01:35
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
9
094/14:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
0
000/00:00:00
000 0
0 0
0 216
9
097/20:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
9
Coasting Arc #1 (Orbit 333)
---------------------------------------
Vector Time (GMT): 2019/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 490386
38 A = 6783217
15 meter
Y = 4489460
42 meter E =
0007265
Z = 5057580
09 I = 51
77044
XDOT = -7312
827047 Wp = 127
95377
YDOT = -1332
756530 meter/sec RA = 21
85764 deg
ZDOT = 1885
897780 TA = 303
76804
MA = 303
83722
Ha = 224
033 n
mi
Hp = 216
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1608879
21 X = 415580
78
Y = 14729200
86 feet Y = 4494526
48 meter
Z = 16593110
53 Z = 5059780
07
XDOT = -23992
214721 XDOT = -7306
540861
YDOT = -4372
560793 feet/sec YDOT = -1414
498353 meter/sec
ZDOT = 6187
328673 ZDOT = 1850
390468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3702188
40 X = 1128427
02
Y = 14335921
17 feet Y = 4369588
77 meter
Z = 16602539
95 Z = 5060454
18
XDOT = -23372
214179 XDOT = -7123
850882
YDOT = -967
511073 feet/sec YDOT = -294
897375 meter/sec
ZDOT = 6026
826618 ZDOT = 1836
976753
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 19091
55147747
00016717 00000-0 10270-3 0 9007
2 25544 51
6412 22
1935 0001813 140
7302 219
3981 15
52498385 3346
Satellite: ISS
Catalog Number: 25544
Epoch time: 19091
55147747 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 22
1935 deg
Eccentricity:
0001813
Arg of perigee: 140
7302 deg
Mean anomaly: 219
3981 deg
Mean motion: 15
52498385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 334
Checksum: 297
Coasting Arc #2 (Orbit 348)
---------------------------------------
Vector Time (GMT): 2019/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 578449
09 A = 6782267
97 meter
Y = -4199481
55 meter E =
0015907
Z = -5307969
13 I = 51
73665
XDOT = 7424
004005 Wp = 90
48631
YDOT = 1766
651079 meter/sec RA = 16
88330 deg
ZDOT = -590
326133 TA = 173
88631
MA = 173
86688
Ha = 224
101 n
mi
Hp = 216
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1897798
86 X = 651148
94
Y = -13777826
59 feet Y = -4192606
99 meter
Z = -17414596
88 Z = -5304982
24
XDOT = 24356
968519 XDOT = 7406
564508
YDOT = 5796
099341 feet/sec YDOT = 1849
573916 meter/sec
ZDOT = -1936
765529 ZDOT = -554
305832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -326301
90 X = -99456
82
Y = -13921611
59 feet Y = -4243307
21 meter
Z = -17400591
61 Z = -5303700
32
XDOT = 23981
244324 XDOT = 7309
483270
YDOT = 1648
421845 feet/sec YDOT = 502
438978 meter/sec
ZDOT = -1774
007535 ZDOT = -540
717497
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 19092
51704267
00016717 00000-0 10270-3 0 9011
2 25544 51
6422 17
3916 0001821 137
4121 222
7172 15
52476843 3494
Satellite: ISS
Catalog Number: 25544
Epoch time: 19092
51704267 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 17
3916 deg
Eccentricity:
0001821
Arg of perigee: 137
4121 deg
Mean anomaly: 222
7172 deg
Mean motion: 15
52476843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 349
Checksum: 289
Coasting Arc #3 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2019/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1662299
57 A = 6782272
61 meter
Y = 3911880
83 meter E =
0003839
Z = 5281893
82 I = 51
70463
XDOT = -7330
692625 Wp = 86
87980
YDOT = -2132
556464 meter/sec RA = 11
90783 deg
ZDOT = -727
014719 TA = 10
06163
MA = 10
05395
Ha = 224
039 n
mi
Hp = 216
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5453738
73 X = -1731576
25
Y = 12834254
69 feet Y = 3892905
07 meter
Z = 17329047
95 Z = 5273650
31
XDOT = -24050
828821 XDOT = -7302
769514
YDOT = -6996
576324 feet/sec YDOT = -2214
377353 meter/sec
ZDOT = -2385
218893 ZDOT = -762
556358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3102683
38 X = -945697
89
Y = 13643374
67 feet Y = 4158500
60 meter
Z = 17291296
84 Z = 5270387
28
XDOT = -23918
294112 XDOT = -7290
296045
YDOT = -2210
157676 feet/sec YDOT = -673
656060 meter/sec
ZDOT = -2545
752534 ZDOT = -775
945372
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 19093
54697351
00016717 00000-0 10270-3 0 9021
2 25544 51
6420 12
2714 0001694 142
4883 217
6387 15
52505662 3652
Satellite: ISS
Catalog Number: 25544
Epoch time: 19093
54697351 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 12
2714 deg
Eccentricity:
0001694
Arg of perigee: 142
4883 deg
Mean anomaly: 217
6387 deg
Mean motion: 15
52505662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 365
Checksum: 307
Coasting Arc #4 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2019/094/11:01:35
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2631484
65 A = 6784544
34 meter
Y = 4093176
81 meter E =
0009300
Z = 4723201
97 I = 51
68032
XDOT = -7029
996261 Wp = 122
79449
YDOT = 1318
429308 meter/sec RA = 7
16867 deg
ZDOT = 2765
245126 TA = 299
79690
MA = 299
88936
Ha = 223
906 n
mi
Hp = 216
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8633479
83 X = 2562575
27
Y = 13429057
76 feet Y = 4122219
14 meter
Z = 15496069
47 Z = 4735816
94
XDOT = -23064
292196 XDOT = -7057
648886
YDOT = 4325
555472 feet/sec YDOT = 1239
660661 meter/sec
ZDOT = 9072
326529 ZDOT = 2731
028658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7811808
61 X = 2381039
26
Y = 13859850
12 feet Y = 4224482
32 meter
Z = 15552650
46 Z = 4740447
86
XDOT = -22309
275641 XDOT = -6799
867215
YDOT = 2535
024499 feet/sec YDOT = 772
675467 meter/sec
ZDOT = 8917
397525 ZDOT = 2718
022765
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 19094
51253329
00016717 00000-0 10270-3 0 9033
2 25544 51
6415 7
4703 0001795 148
8530 211
2729 15
52500393 3804
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
51253329 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 7
4703 deg
Eccentricity:
0001795
Arg of perigee: 148
8530 deg
Mean anomaly: 211
2729 deg
Mean motion: 15
52500393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 380
Checksum: 291
Coasting Arc #5 (Orbit 381)
---------------------------------------
Vector Time (GMT): 2019/094/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4921200
47 A = 6787677
03 meter
Y = 2552269
86 meter E =
0012042
Z = 3906621
52 I = 51
68745
XDOT = -5238
972757 Wp = 87
82380
YDOT = -3835
552100 meter/sec RA = 6
42150 deg
ZDOT = -4082
418691 TA = 44
94144
MA = 44
84403
Ha = 224
030 n
mi
Hp = 216
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16145670
84 X = -4968351
18
Y = 8373588
78 feet Y = 2496974
35 meter
Z = 12816999
73 Z = 3882601
30
XDOT = -17188
230831 XDOT = -5175
862973
YDOT = -12583
832348 feet/sec YDOT = -3893
785544 meter/sec
ZDOT = -13393
762110 ZDOT = -4107
714018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4643387
53 X = -1415304
52
Y = 17664076
78 feet Y = 5384010
60 meter
Z = 12708048
70 Z = 3873413
24
XDOT = -19506
552714 XDOT = -5945
597267
YDOT = 4617
067484 feet/sec YDOT = 1407
282169 meter/sec
ZDOT = -13507
729453 ZDOT = -4117
155937
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 19094
64127381
00016717 00000-0 10270-3 0 9046
2 25544 51
6430 6
8310 0001603 145
7994 214
3262 15
52511820 3821
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
64127381 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 6
8310 deg
Eccentricity:
0001603
Arg of perigee: 145
7994 deg
Mean anomaly: 214
3262 deg
Mean motion: 15
52511820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 281
Coasting Arc #6 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2019/095/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5639436
02 A = 6790329
81 meter
Y = -2259499
64 meter E =
0004892
Z = -3037072
67 I = 51
66276
XDOT = 4263
565462 Wp = 87
12026
YDOT = 4014
085646 meter/sec RA = 1
45270 deg
ZDOT = 4937
615413 TA = 238
12452
MA = 238
17213
Ha = 223
917 n
mi
Hp = 217
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18502086
70 X = 5679035
77
Y = -7413056
56 feet Y = -2196214
42 meter
Z = -9964149
17 Z = -3009581
80
XDOT = 13988
075662 XDOT = 4194
377579
YDOT = 13169
572330 feet/sec YDOT = 4061
377479 meter/sec
ZDOT = 16199
525634 ZDOT = 4958
157893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6597972
76 X = 2011062
10
Y = -18873658
43 feet Y = -5752691
09 meter
Z = -9839545
78 Z = -2999093
55
XDOT = 17670
439464 XDOT = 5385
949948
YDOT = -2303
938408 feet/sec YDOT = -702
240427 meter/sec
ZDOT = 16291
962474 ZDOT = 4965
790162
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 19095
60683123
00016717 00000-0 10270-3 0 9055
2 25544 51
6429 2
0297 0001542 155
0888 205
0338 15
52476222 3972
Satellite: ISS
Catalog Number: 25544
Epoch time: 19095
60683123 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 2
0297 deg
Eccentricity:
0001542
Arg of perigee: 155
0888 deg
Mean anomaly: 205
0338 deg
Mean motion: 15
52476222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 301
Coasting Arc #7 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2019/096/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6185100
66 A = 6792497
02 meter
Y = 1956306
90 meter E =
0015156
Z = 1987937
16 I = 51
63694
XDOT = -3138
055788 Wp = 115
77998
YDOT = -4228
744829 meter/sec RA = 356
48605 deg
ZDOT = -5575
364973 TA = 42
27764
MA = 42
16090
Ha = 223
936 n
mi
Hp = 217
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20292325
01 X = -6216173
35
Y = 6418329
71 feet Y = 1886967
21 meter
Z = 6522103
55 Z = 1957816
30
XDOT = -10295
458622 XDOT = -3063
453225
YDOT = -13873
834740 feet/sec YDOT = -4263
420144 meter/sec
ZDOT = -18291
879832 ZDOT = -5590
427045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8171027
62 X = -2490529
22
Y = 19696928
27 feet Y = 6003623
74 meter
Z = 6385653
42 Z = 1946347
16
XDOT = -15730
533226 XDOT = -4794
666527
YDOT = -544
594087 feet/sec YDOT = -165
992278 meter/sec
ZDOT = -18359
495984 ZDOT = -5595
974376
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 19096
63675576
00016717 00000-0 10270-3 0 9063
2 25544 51
6430 356
9081 0001562 153
0880 207
0353 15
52489865 4133
Satellite: ISS
Catalog Number: 25544
Epoch time: 19096
63675576 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 356
9081 deg
Eccentricity:
0001562
Arg of perigee: 153
0880 deg
Mean anomaly: 207
0353 deg
Mean motion: 15
52489865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 320
Coasting Arc #8 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2019/097/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6521791
60 A = 6793819
63 meter
Y = -1674772
41 meter E =
0009523
Z = -876767
61 I = 51
60630
XDOT = 1935
199444 Wp = 46
96195
YDOT = 4458
617259 meter/sec RA = 351
52024 deg
ZDOT = 5925
257211 TA = 303
55556
MA = 303
64646
Ha = 223
872 n
mi
Hp = 217
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21396954
06 X = 6544293
57
Y = -5494660
14 feet Y = -1601715
42 meter
Z = -2876534
16 Z = -845032
01
XDOT = 6349
079540 XDOT = 1856
416111
YDOT = 14628
009379 feet/sec YDOT = 4479
817943 meter/sec
ZDOT = 19439
820246 ZDOT = 5934
466125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9229087
52 X = 2813025
88
Y = -20091067
26 feet Y = -6123757
30 meter
Z = -2732826
72 Z = -832965
58
XDOT = 13812
827042 XDOT = 4210
149682
YDOT = 3717
376344 feet/sec YDOT = 1133
056310 meter/sec
ZDOT = 19480
933414 ZDOT = 5937
788505
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 19097
60230755
00016717 00000-0 10270-3 0 9078
2 25544 51
6411 352
1065 0001522 159
3241 200
7973 15
52482697 4288
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
60230755 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 352
1065 deg
Eccentricity:
0001522
Arg of perigee: 159
3241 deg
Mean anomaly: 200
7973 deg
Mean motion: 15
52482697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 300
Coasting Arc #9 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2019/097/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2049385
96 A = 6782565
19 meter
Y = -3845831
36 meter E =
0014628
Z = -5210106
00 I = 51
56070
XDOT = 7227
917285 Wp = 88
84601
YDOT = -2209
180173 meter/sec RA = 350
33538 deg
ZDOT = -1215
055522 TA = 169
47757
MA = 169
44692
Ha = 223
925 n
mi
Hp = 216
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6723707
20 X = -1980920
32
Y = -12617556
97 feet Y = -3868366
57 meter
Z = -17093523
63 Z = -5219894
73
XDOT = 23713
639385 XDOT = 7257
985913
YDOT = -7247
966446 feet/sec YDOT = -2128
184502 meter/sec
ZDOT = -3986
402630 ZDOT = -1179
871365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3550166
47 X = -1082090
74
Y = 13795207
70 feet Y = 4204779
31 meter
Z = -17137330
45 Z = -5223458
32
XDOT = -21472
340889 XDOT = -6544
769503
YDOT = -10269
211619 feet/sec YDOT = -3130
055701 meter/sec
ZDOT = -3827
040145 ZDOT = -1166
481836
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 19097
85978939
00016717 00000-0 10270-3 0 9089
2 25544 51
6408 350
8225 0002129 162
4726 197
6499 15
52495701 4326
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
85978939 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 350
8225 deg
Eccentricity:
0002129
Arg of perigee: 162
4726 deg
Mean anomaly: 197
6499 deg
Mean motion: 15
52495701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 349
Coasting Arc #10 (Orbit 447)
---------------------------------------
Vector Time (GMT): 2019/098/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 959620
22 A = 6782078
28 meter
Y = 4108525
73 meter E =
0003310
Z = 5307472
34 I = 51
52717
XDOT = -7438
023709 Wp = 120
57307
YDOT = 1863
444218 meter/sec RA = 345
34579 deg
ZDOT = -99
263633 TA = 330
36491
MA = 330
38366
Ha = 223
787 n
mi
Hp = 217
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3148360
31 X = 887825
09
Y = 13479415
11 feet Y = 4118855
69 meter
Z = 17412966
99 Z = 5311959
30
XDOT = -24402
964924 XDOT = -7457
826287
YDOT = 6113
662134 feet/sec YDOT = 1780
156305 meter/sec
ZDOT = -325
668088 ZDOT = -135
443442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6575036
22 X = 2004071
04
Y = -12152604
45 feet Y = -3704113
84 meter
Z = 17432765
91 Z = 5313507
05
XDOT = 21521
953831 XDOT = 6559
891528
YDOT = 10949
603854 feet/sec YDOT = 3337
439255 meter/sec
ZDOT = -489
480875 ZDOT = -149
193771
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 19098
88970895
00016717 00000-0 10270-3 0 9097
2 25544 51
6415 345
7002 0002048 168
5132 191
6067 15
52506676 4484
Satellite: ISS
Catalog Number: 25544
Epoch time: 19098
88970895 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 345
7002 deg
Eccentricity:
0002048
Arg of perigee: 168
5132 deg
Mean anomaly: 191
6067 deg
Mean motion: 15
52506676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 448
Checksum: 335
Coasting Arc #11 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2019/099/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 128696
29 A = 6782767
69 meter
Y = -4409112
48 meter E =
0014684
Z = -5165646
54 I = 51
49807
XDOT = 7383
651069 Wp = 108
07642
YDOT = -1441
781867 meter/sec RA = 340
35562 deg
ZDOT = 1413
439908 TA = 175
57754
MA = 175
56455
Ha = 223
825 n
mi
Hp = 216
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 422231
92 X = 203082
82
Y = -14465592
13 feet Y = -4407257
53 meter
Z = -16947659
27 Z = -5164840
59
XDOT = 24224
576999 XDOT = 7392
358925
YDOT = -4730
255470 feet/sec YDOT = -1359
163989 meter/sec
ZDOT = 4637
270041 ZDOT = 1449
328542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9728895
55 X = -2965367
36
Y = 10720146
02 feet Y = 3267500
51 meter
Z = -16943489
92 Z = -5164375
73
XDOT = -20769
819037 XDOT = -6330
640843
YDOT = -11257
322649 feet/sec YDOT = -3431
231943 meter/sec
ZDOT = 4799
707412 ZDOT = 1462
950819
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 19099
85525676
00016717 00000-0 10270-3 0 9100
2 25544 51
6420 340
8997 0002062 167
9476 192
1725 15
52515587 4634
Satellite: ISS
Catalog Number: 25544
Epoch time: 19099
85525676 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 340
8997 deg
Eccentricity:
0002062
Arg of perigee: 167
9476 deg
Mean anomaly: 192
1725 deg
Mean motion: 15
52515587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 338
Coasting Arc #12 (Orbit 478)
---------------------------------------
Vector Time (GMT): 2019/100/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1162604
49 A = 6784587
49 meter
Y = 4695450
56 meter E =
0007386
Z = 4751725
90 I = 51
47240
XDOT = -7130
432928 Wp = 77
35601
YDOT = 936
004012 meter/sec RA = 335
36441 deg
ZDOT = -2664
433196 TA = 39
03572
MA = 38
98243
Ha = 223
888 n
mi
Hp = 217
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3814319
18 X = -1238105
39
Y = 15405021
51 feet Y = 4682027
40 meter
Z = 15589651
91 Z = 4745894
92
XDOT = -23393
808820 XDOT = -7127
427189
YDOT = 3070
879303 feet/sec YDOT = 856
283299 meter/sec
ZDOT = -8741
578728 ZDOT = -2699
063187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12760326
51 X = 3889347
52
Y = -9480318
16 feet Y = -2889600
97 meter
Z = 15562731
13 Z = 4743520
45
XDOT = 19349
910388 XDOT = 5897
852686
YDOT = 11409
925237 feet/sec YDOT = 3477
745212 meter/sec
ZDOT = -8898
258672 ZDOT = -2712
189243
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 19100
88517334
00016717 00000-0 10270-3 0 9119
2 25544 51
6416 335
7778 0002050 168
8378 191
2820 15
52479989 4795
Satellite: ISS
Catalog Number: 25544
Epoch time: 19100
88517334 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 335
7778 deg
Eccentricity:
0002050
Arg of perigee: 168
8378 deg
Mean anomaly: 191
2820 deg
Mean motion: 15
52479989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 479
Checksum: 338
Coasting Arc #13 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2019/101/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2093655
65 A = 6786914
86 meter
Y = -4972852
30 meter E =
0008380
Z = -4126271
97 I = 51
45100
XDOT = 6655
590596 Wp = 121
49354
YDOT = -326
762254 meter/sec RA = 330
37622 deg
ZDOT = 3772
214205 TA = 187
54333
MA = 187
55595
Ha = 223
724 n
mi
Hp = 217
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6868948
99 X = 2169151
13
Y = -16315132
21 feet Y = -4949017
47 meter
Z = -13537637
70 Z = -4115918
34
XDOT = 21835
927152 XDOT = 6640
426477
YDOT = -1072
054638 feet/sec YDOT = -252
419557 meter/sec
ZDOT = 12376
030857 ZDOT = 3804
507896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15549116
17 X = -4739370
61
Y = 8536509
91 feet Y = 2601928
22 meter
Z = -13490241
60 Z = -4111825
64
XDOT = -17149
120823 XDOT = -5227
052027
YDOT = -11455
447995 feet/sec YDOT = -3491
620549 meter/sec
ZDOT = 12522
071170 ZDOT = 3816
727293
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 19101
85071722
00016717 00000-0 10270-3 0 9124
2 25544 51
6420 330
9774 0002017 177
7777 182
3384 15
52503303 4949
Satellite: ISS
Catalog Number: 25544
Epoch time: 19101
85071722 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 330
9774 deg
Eccentricity:
0002017
Arg of perigee: 177
7777 deg
Mean anomaly: 182
3384 deg
Mean motion: 15
52503303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 297
Coasting Arc #14 (Orbit 509)
---------------------------------------
Vector Time (GMT): 2019/102/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2908932
59 A = 6789608
32 meter
Y = 5179456
76 meter E =
0013028
Z = 3274001
53 I = 51
43171
XDOT = -6036
325121 Wp = 101
14019
YDOT = -401
647268 meter/sec RA = 325
38986 deg
ZDOT = -4714
342023 TA = 40
73696
MA = 40
63960
Ha = 223
764 n
mi
Hp = 217
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9543742
09 X = -2982537
84
Y = 16992968
38 feet Y = 5146515
52 meter
Z = 10741474
85 Z = 3259692
21
XDOT = -19804
216275 XDOT = -6008
485480
YDOT = -1317
740381 feet/sec YDOT = -468
994054 meter/sec
ZDOT = -15467
001388 ZDOT = -4743
596632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17926254
05 X = 5463922
23
Y = -7738985
03 feet Y = -2358842
64 meter
Z = 10676178
90 Z = 3254099
33
XDOT = 14342
044537 XDOT = 4371
455175
YDOT = 11640
226329 feet/sec YDOT = 3547
940985 meter/sec
ZDOT = -15599
213240 ZDOT = -4754
640196
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 19102
88063003
00016717 00000-0 10270-3 0 9132
2 25544 51
6422 325
8557 0002004 178
3271 181
7887 15
52491679 5107
Satellite: ISS
Catalog Number: 25544
Epoch time: 19102
88063003 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 325
8557 deg
Eccentricity:
0002004
Arg of perigee: 178
3271 deg
Mean anomaly: 181
7887 deg
Mean motion: 15
52491679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 510
Checksum: 303
Coasting Arc #15 (Orbit 524)
---------------------------------------
Vector Time (GMT): 2019/103/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3559538
63 A = 6791958
72 meter
Y = -5312455
11 meter E =
0004721
Z = -2287347
26 I = 51
41302
XDOT = 5290
061348 Wp = 56
25134
YDOT = 1221
772875 meter/sec RA = 320
40685 deg
ZDOT = 5405
332248 TA = 278
22580
MA = 278
27934
Ha = 223
642 n
mi
Hp = 217
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11678276
34 X = 3629790
10
Y = -17429314
67 feet Y = -5272257
11 meter
Z = -7504420
14 Z = -2269885
65
XDOT = 17355
844316 XDOT = 5249
749918
YDOT = 4008
441192 feet/sec YDOT = 1280
704764 meter/sec
ZDOT = 17734
029686 ZDOT = 5430
931398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19753612
72 X = -6020901
16
Y = 7151613
32 feet Y = 2179811
74 meter
Z = -7424869
08 Z = -2263100
10
XDOT = -11028
681759 XDOT = -3361
542200
YDOT = -11967
491455 feet/sec YDOT = -3647
691396 meter/sec
ZDOT = 17849
618859 ZDOT = 5440
563828
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 19103
84616998
00016717 00000-0 10270-3 0 9147
2 25544 51
6425 321
0548 0001712 186
1264 173
9867 15
52478504 5251
Satellite: ISS
Catalog Number: 25544
Epoch time: 19103
84616998 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 321
0548 deg
Eccentricity:
0001712
Arg of perigee: 186
1264 deg
Mean anomaly: 173
9867 deg
Mean motion: 15
52478504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 525
Checksum: 322
Coasting Arc #16 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2019/104/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4068633
41 A = 6793544
53 meter
Y = 5305954
10 meter E =
0014611
Z = 1157444
81 I = 51
39236
XDOT = -4473
886211 Wp = 128
94783
YDOT = -2146
259727 meter/sec RA = 315
42643 deg
ZDOT = -5846
869860 TA = 38
44433
MA = 38
34033
Ha = 223
618 n
mi
Hp = 217
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13348534
81 X = -4133285
92
Y = 17407985
90 feet Y = 5260094
35 meter
Z = 3797391
10 Z = 1137523
72
XDOT = -14678
104368 XDOT = -4421
152851
YDOT = -7041
534537 feet/sec YDOT = -2195
995245 meter/sec
ZDOT = -19182
643897 ZDOT = -5868
474091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20960163
23 X = 6388657
75
Y = -6524813
87 feet Y = -1988763
27 meter
Z = 3706736
44 Z = 1129813
27
XDOT = 7359
292806 XDOT = 2243
112447
YDOT = 12609
953058 feet/sec YDOT = 3843
513692 meter/sec
ZDOT = -19280
067825 ZDOT = -5876
564673
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 19104
87608017
00016717 00000-0 10270-3 0 9155
2 25544 51
6413 315
9341 0001896 185
6813 174
4318 15
52495188 5410
Satellite: ISS
Catalog Number: 25544
Epoch time: 19104
87608017 = yrday
fracday
Element set: 915
Inclination: 51
6413 deg
RA of node: 315
9341 deg
Eccentricity:
0001896
Arg of perigee: 185
6813 deg
Mean anomaly: 174
4318 deg
Mean motion: 15
52495188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 319
Coasting Arc #17 (Orbit 556)
---------------------------------------
Vector Time (GMT): 2019/105/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4402588
12 A = 6794104
16 meter
Y = -5168526
30 meter E =
0010776
Z = -3073
43 I = 51
37153
XDOT = 3640
177374 Wp = 50
41232
YDOT = 3105
528728 meter/sec RA = 310
44532 deg
ZDOT = 5987
826570 TA = 309
55448
MA = 309
64964
Ha = 223
549 n
mi
Hp = 217
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14444186
74 X = 4460071
77
Y = -16957107
30 feet Y = -5118972
07 meter
Z = -10083
44 Z = 18452
59
XDOT = 11942
839153 XDOT = 3576
094428
YDOT = 10188
742546 feet/sec YDOT = 3145
877799 meter/sec
ZDOT = 19645
100295 ZDOT = 6005
353323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21476607
11 X = -6546069
85
Y = 5909801
96 feet Y = 1801307
64 meter
Z = 87794
97 Z = 26759
91
XDOT = -3612
552101 XDOT = -1101
105880
YDOT = -13499
965181 feet/sec YDOT = -4114
789387 meter/sec
ZDOT = 19723
986770 ZDOT = 6011
871167
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 19105
90598819
00016717 00000-0 10270-3 0 9169
2 25544 51
6415 310
8125 0001686 192
9782 167
1326 15
52487172 5578
Satellite: ISS
Catalog Number: 25544
Epoch time: 19105
90598819 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 310
8125 deg
Eccentricity:
0001686
Arg of perigee: 192
9782 deg
Mean anomaly: 167
1326 deg
Mean motion: 15
52487172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 557
Checksum: 331
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