[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 22nd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
300/09:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 215
6
303/21:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 1830)
---------------------------------------
Vector Time (GMT): 2018/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -940426
97 A = 6786442
23 meter
Y = -6035017
36 meter E =
0010399
Z = 2950665
10 I = 52
01376
XDOT = 4802
624972 Wp = 83
49006
YDOT = -3218
758498 meter/sec RA = 103
30622 deg
ZDOT = -5036
347301 TA = 63
01168
MA = 62
90553
Ha = 220
900 n
mi
Hp = 216
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3085390
32 X = -887204
89
Y = -19799925
73 feet Y = -6045236
02 meter
Z = 9680659
79 Z = 2946226
57
XDOT = 15756
643610 XDOT = 4862
725484
YDOT = -10560
231294 feet/sec YDOT = -3164
716627 meter/sec
ZDOT = -16523
449150 ZDOT = -5012
871090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12624837
10 X = 3848050
35
Y = 15573815
66 feet Y = 4746899
01 meter
Z = 9661346
71 Z = 2944778
48
XDOT = -7326
955045 XDOT = -2233
255898
YDOT = 16157
580543 feet/sec YDOT = 4924
830549 meter/sec
ZDOT = -16417
489388 ZDOT = -5004
050765
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 18295
53819223
00016717 00000-0 10270-3 0 9005
2 25544 51
6360 104
0933 0004083 317
4381 42
6455 15
53857956 18318
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
53819223 = yrday
fracday
Element set: 900
Inclination: 51
6360 deg
RA of node: 104
0933 deg
Eccentricity:
0004083
Arg of perigee: 317
4381 deg
Mean anomaly: 42
6455 deg
Mean motion: 15
53857956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1831
Checksum: 307
Coasting Arc #2 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2018/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 199529
08 A = 6789196
04 meter
Y = 6615858
64 meter E =
0010059
Z = -1485113
03 I = 52
03015
XDOT = -4794
165109 Wp = 16
35069
YDOT = 1444
266318 meter/sec RA = 98
35767 deg
ZDOT = 5808
688625 TA = 327
52543
MA = 327
58728
Ha = 221
080 n
mi
Hp = 215
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 654622
96 X = 132747
94
Y = 21705572
96 feet Y = 6617716
39 meter
Z = -4872418
08 Z = -1484306
52
XDOT = -15728
888154 XDOT = -4838
175199
YDOT = 4738
406554 feet/sec YDOT = 1390
409042 meter/sec
ZDOT = 19057
377379 ZDOT = 5785
292670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11760370
66 X = -3584560
98
Y = -18256021
38 feet Y = -5564435
32 meter
Z = -4869522
76 Z = -1484230
54
XDOT = 9823
309035 XDOT = 2994
144594
YDOT = -11366
694063 feet/sec YDOT = -3464
568351 meter/sec
ZDOT = 18951
965374 ZDOT = 5776
559046
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 18296
50289686
00016717 00000-0 10270-3 0 9018
2 25544 51
6366 99
2854 0003806 323
4376 36
6516 15
53852375 18461
Satellite: ISS
Catalog Number: 25544
Epoch time: 18296
50289686 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 99
2854 deg
Eccentricity:
0003806
Arg of perigee: 323
4376 deg
Mean anomaly: 36
6516 deg
Mean motion: 15
53852375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 343
Coasting Arc #3 (Orbit 1861)
---------------------------------------
Vector Time (GMT): 2018/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 518396
91 A = 6790011
91 meter
Y = -6765260
84 meter E =
0007948
Z = -146677
70 I = 52
03616
XDOT = 4693
312545 Wp = 129
68019
YDOT = 485
807745 meter/sec RA = 93
41531 deg
ZDOT = -6041
394250 TA = 51
89067
MA = 51
81903
Ha = 221
119 n
mi
Hp = 215
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1700777
25 X = 594721
91
Y = -22195737
67 feet Y = -6759037
02 meter
Z = -481226
06 Z = -143973
60
XDOT = 15398
007039 XDOT = 4716
877998
YDOT = 1593
857432 feet/sec YDOT = 538
422979 meter/sec
ZDOT = -19820
847276 ZDOT = -6018
537941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10303837
98 X = 3140609
82
Y = 19732881
62 feet Y = 6014582
32 meter
Z = -468293
15 Z = -142735
75
XDOT = -12579
278119 XDOT = -3834
163971
YDOT = 6118
267610 feet/sec YDOT = 1864
847967 meter/sec
ZDOT = -19718
076361 ZDOT = -6010
069675
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 18297
53191072
00016717 00000-0 10270-3 0 9024
2 25544 51
6358 94
1576 0004007 327
8320 32
2587 15
53889726 18626
Satellite: ISS
Catalog Number: 25544
Epoch time: 18297
53191072 = yrday
fracday
Element set: 902
Inclination: 51
6358 deg
RA of node: 94
1576 deg
Eccentricity:
0004007
Arg of perigee: 327
8320 deg
Mean anomaly: 32
2587 deg
Mean motion: 15
53889726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1862
Checksum: 324
Coasting Arc #4 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2018/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1185786
74 A = 6788785
04 meter
Y = 6445457
05 meter E =
0014102
Z = 1739330
73 I = 52
03489
XDOT = -4526
807290 Wp = 49
18745
YDOT = -2381
521104 meter/sec RA = 88
47224 deg
ZDOT = 5717
893866 TA = 329
80072
MA = 329
88193
Ha = 221
201 n
mi
Hp = 215
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3890376
46 X = -1266222
51
Y = 21146512
64 feet Y = 6431747
10 meter
Z = 5706465
64 Z = 1733374
74
XDOT = -14851
729954 XDOT = -4527
615351
YDOT = -7813
389448 feet/sec YDOT = -2432
147254 meter/sec
ZDOT = 18759
494310 ZDOT = 5695
901705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8204730
92 X = -2500801
99
Y = -19882304
52 feet Y = -6060126
42 meter
Z = 5678920
08 Z = 1730934
84
XDOT = 15366
472353 XDOT = 4683
700773
YDOT = -991
217748 feet/sec YDOT = -302
123169 meter/sec
ZDOT = 18660
831254 ZDOT = 5687
821366
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 18298
56092344
00016717 00000-0 10270-3 0 9031
2 25544 51
6378 89
0297 0003795 329
5665 30
5266 15
53880298 18782
Satellite: ISS
Catalog Number: 25544
Epoch time: 18298
56092344 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 89
0297 deg
Eccentricity:
0003795
Arg of perigee: 329
5665 deg
Mean anomaly: 30
5266 deg
Mean motion: 15
53880298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 357
Coasting Arc #5 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2018/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1864200
22 A = 6785784
00 meter
Y = -5691864
58 meter E =
0003904
Z = -3195261
77 I = 52
02347
XDOT = 4273
558895 Wp = 46
80190
YDOT = 4118
617466 meter/sec RA = 83
52367 deg
ZDOT = -4844
491481 TA = 169
86268
MA = 169
85481
Ha = 221
335 n
mi
Hp = 215
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6116142
45 X = 1943231
05
Y = -18674096
39 feet Y = -5670575
99 meter
Z = -10483142
30 Z = -3186013
76
XDOT = 14020
862515 XDOT = 4250
718442
YDOT = 13512
524496 feet/sec YDOT = 4166
279539 meter/sec
ZDOT = -15894
000921 ZDOT = -4823
786966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5292523
92 X = 1613161
29
Y = 18947376
33 feet Y = 5775160
30 meter
Z = -10440855
70 Z = -3182372
82
XDOT = -17881
172730 XDOT = -5450
181448
YDOT = -3710
515308 feet/sec YDOT = -1130
965066 meter/sec
ZDOT = -15801
343289 ZDOT = -4816
249435
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 18299
52562000
00016717 00000-0 10270-3 0 9040
2 25544 51
6384 84
2224 0003908 335
7442 24
3525 15
53872311 18937
Satellite: ISS
Catalog Number: 25544
Epoch time: 18299
52562000 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 84
2224 deg
Eccentricity:
0003908
Arg of perigee: 335
7442 deg
Mean anomaly: 24
3525 deg
Mean motion: 15
53872311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 301
Coasting Arc #6 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2018/300/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3387617
26 A = 6779563
60 meter
Y = -3085832
65 meter E =
0012983
Z = -5008036
92 I = 51
99692
XDOT = 2989
878832 Wp = 56
25471
YDOT = 6724
628418 meter/sec RA = 79
02503 deg
ZDOT = -2118
016452 TA = 193
18036
MA = 193
21431
Ha = 221
494 n
mi
Hp = 215
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11114229
86 X = 3446199
24
Y = -10124122
86 feet Y = -3047622
43 meter
Z = -16430567
33 Z = -4991438
27
XDOT = 9809
313753 XDOT = 2924
748453
YDOT = 22062
429194 feet/sec YDOT = 6757
699141 meter/sec
ZDOT = -6948
872873 ZDOT = -2103
650466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11031124
38 X = -3362286
71
Y = 10334363
31 feet Y = 3149913
94 meter
Z = -16355511
06 Z = -4985159
77
XDOT = -9514
439731 XDOT = -2900
001230
YDOT = -21068
496273 feet/sec YDOT = -6421
677664 meter/sec
ZDOT = -6885
059973 ZDOT = -2098
566280
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 18300
42600084
00016717 00000-0 10270-3 0 9058
2 25544 51
6369 79
7374 0004057 341
1893 18
9109 15
53873080 19079
Satellite: ISS
Catalog Number: 25544
Epoch time: 18300
42600084 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 79
7374 deg
Eccentricity:
0004057
Arg of perigee: 341
1893 deg
Mean anomaly: 18
9109 deg
Mean motion: 15
53873080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 311
Coasting Arc #7 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2018/301/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3913789
05 A = 6778250
12 meter
Y = 1475450
46 meter E =
0003615
Z = 5332543
83 I = 51
98459
XDOT = -2336
098542 Wp = 21
91324
YDOT = -7298
726678 meter/sec RA = 74
05272 deg
ZDOT = 308
101844 TA = 65
18283
MA = 65
14524
Ha = 221
791 n
mi
Hp = 215
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12840515
25 X = -3955900
42
Y = 4840716
74 feet Y = 1431448
23 meter
Z = 17495222
53 Z = 5313429
24
XDOT = -7664
365296 XDOT = -2255
805157
YDOT = -23945
953668 feet/sec YDOT = -7324
401609 meter/sec
ZDOT = 1010
832822 ZDOT = 296
948524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12774041
00 X = 3893527
70
Y = -5305046
17 feet Y = -1616978
07 meter
Z = 17409036
26 Z = 5306274
25
XDOT = 8140
695937 XDOT = 2481
284122
YDOT = 22722
874576 feet/sec YDOT = 6925
932171 meter/sec
ZDOT = 961
562761 ZDOT = 293
084330
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 18301
45500718
00016717 00000-0 10270-3 0 9066
2 25544 51
6368 74
6093 0004090 344
4767 15
6259 15
53828011 19235
Satellite: ISS
Catalog Number: 25544
Epoch time: 18301
45500718 = yrday
fracday
Element set: 906
Inclination: 51
6368 deg
RA of node: 74
6093 deg
Eccentricity:
0004090
Arg of perigee: 344
4767 deg
Mean anomaly: 15
6259 deg
Mean motion: 15
53828011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 305
Coasting Arc #8 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2018/302/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4389908
48 A = 6778850
57 meter
Y = 155018
27 meter E =
0012621
Z = -5173620
58 I = 51
97880
XDOT = 1532
421280 Wp = 84
35260
YDOT = 7347
660355 meter/sec RA = 69
07950 deg
ZDOT = 1524
842442 TA = 200
26093
MA = 200
31105
Ha = 221
689 n
mi
Hp = 215
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14402586
86 X = 4412980
00
Y = 508590
12 feet Y = 204238
39 meter
Z = -16973820
80 Z = -5152239
43
XDOT = 5027
628871 XDOT = 1442
736763
YDOT = 24106
497227 feet/sec YDOT = 7364
295461 meter/sec
ZDOT = 5002
763916 ZDOT = 1532
068907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14521668
71 X = -4426204
62
Y = 265075
83 feet Y = 80795
11 meter
Z = -16877637
20 Z = -5144303
82
XDOT = -6249
489425 XDOT = -1904
844377
YDOT = -22748
314280 feet/sec YDOT = -6933
686192 meter/sec
ZDOT = 5034
343143 ZDOT = 1534
467790
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 18302
41969534
00016717 00000-0 10270-3 0 9079
2 25544 51
6386 69
8023 0004037 348
4808 11
6251 15
53881922 19389
Satellite: ISS
Catalog Number: 25544
Epoch time: 18302
41969534 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 69
8023 deg
Eccentricity:
0004037
Arg of perigee: 348
4808 deg
Mean anomaly: 11
6251 deg
Mean motion: 15
53881922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 322
Coasting Arc #9 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2018/303/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4758763
06 A = 6781636
05 meter
Y = -1729695
15 meter E =
0010744
Z = 4508614
18 I = 51
97385
XDOT = -554
510247 Wp = 47
19703
YDOT = -6931
897882 meter/sec RA = 64
10917 deg
ZDOT = -3232
668804 TA = 75
21549
MA = 75
09647
Ha = 221
885 n
mi
Hp = 215
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15612739
69 X = -4760968
27
Y = -5674852
85 feet Y = -1782923
37 meter
Z = 14792041
27 Z = 4485491
98
XDOT = -1819
259339 XDOT = -461
251761
YDOT = -22742
447118 feet/sec YDOT = -6937
577290 meter/sec
ZDOT = -10605
868778 ZDOT = -3235
136103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16070991
83 X = 4898438
31
Y = 4554706
44 feet Y = 1388274
52 meter
Z = 14688224
92 Z = 4476970
95
XDOT = 3676
078931 XDOT = 1120
468858
YDOT = 21391
995568 feet/sec YDOT = 6520
280249 meter/sec
ZDOT = -10616
073793 ZDOT = -3235
779292
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 18303
44869488
00016717 00000-0 10270-3 0 9081
2 25544 51
6375 64
6739 0004002 352
6965 7
4128 15
53850990 19542
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
44869488 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 64
6739 deg
Eccentricity:
0004002
Arg of perigee: 352
6965 deg
Mean anomaly: 7
4128 deg
Mean motion: 15
53850990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 337
Coasting Arc #10 (Orbit 1960)
---------------------------------------
Vector Time (GMT): 2018/303/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4836496
40 A = 6785068
80 meter
Y = 3248057
96 meter E =
0006286
Z = -3477364
59 I = 51
97837
XDOT = -796
639044 Wp = 45
96692
YDOT = 6088
185218 meter/sec RA = 61
70412 deg
ZDOT = 4588
092125 TA = 273
44684
MA = 273
51874
Ha = 222
010 n
mi
Hp = 215
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15867770
34 X = 4816707
70
Y = 10656358
15 feet Y = 3302032
44 meter
Z = -11408676
46 Z = -3453918
23
XDOT = -2613
645159 XDOT = -886
946475
YDOT = 19974
360953 feet/sec YDOT = 6078
771632 meter/sec
ZDOT = 15052
795686 ZDOT = 4584
003029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15804713
00 X = 4817276
52
Y = 10860096
01 feet Y = 3310157
26 meter
Z = -11303599
64 Z = -3445337
17
XDOT = -2179
022619 XDOT = -664
166094
YDOT = 18786
335881 feet/sec YDOT = 5726
075177 meter/sec
ZDOT = 15033
603674 ZDOT = 4582
242400
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 18303
89887997
00016717 00000-0 10270-3 0 9096
2 25544 51
6376 62
4353 0004496 354
8711 5
2395 15
53862310 19610
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
89887997 = yrday
fracday
Element set: 909
Inclination: 51
6376 deg
RA of node: 62
4353 deg
Eccentricity:
0004496
Arg of perigee: 354
8711 deg
Mean anomaly: 5
2395 deg
Mean motion: 15
53862310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1961
Checksum: 340
Coasting Arc #11 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2018/304/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4781303
04 A = 6788251
79 meter
Y = -4348522
89 meter E =
0012757
Z = 2064148
67 I = 51
97293
XDOT = 2013
493993 Wp = 91
92790
YDOT = -4870
779201 meter/sec RA = 56
74990 deg
ZDOT = -5568
052826 TA = 65
35215
MA = 65
21933
Ha = 221
961 n
mi
Hp = 214
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15686689
77 X = -4742347
95
Y = -14266807
39 feet Y = -4401772
93 meter
Z = 6772141
30 Z = 2041017
10
XDOT = 6605
951420 XDOT = 2094
857737
YDOT = -15980
246724 feet/sec YDOT = -4847
807984 meter/sec
ZDOT = -18267
889849 ZDOT = -5558
074232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15792835
19 X = -4813656
17
Y = -14198297
77 feet Y = -4327641
16 meter
Z = 6668629
85 Z = 2032598
38
XDOT = 5623
002970 XDOT = 1713
891305
YDOT = -14858
831757 feet/sec YDOT = -4528
971920 meter/sec
ZDOT = -18222
348667 ZDOT = -5554
171874
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 18304
92787550
00016717 00000-0 10270-3 0 9107
2 25544 51
6379 57
3069 0004573 357
1719 2
9407 15
53897522 19778
Satellite: ISS
Catalog Number: 25544
Epoch time: 18304
92787550 = yrday
fracday
Element set: 910
Inclination: 51
6379 deg
RA of node: 57
3069 deg
Eccentricity:
0004573
Arg of perigee: 357
1719 deg
Mean anomaly: 2
9407 deg
Mean motion: 15
53897522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 339
Coasting Arc #12 (Orbit 1991)
---------------------------------------
Vector Time (GMT): 2018/305/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4476987
04 A = 6789875
68 meter
Y = 5070338
22 meter E =
0014823
Z = -489432
93 I = 51
96016
XDOT = -3268
915360 Wp = 30
34673
YDOT = 3458
317851 meter/sec RA = 51
80173 deg
ZDOT = 6016
737805 TA = 324
39562
MA = 324
49442
Ha = 222
043 n
mi
Hp = 214
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14688277
70 X = 4422333
80
Y = 16634967
92 feet Y = 5120097
40 meter
Z = -1605751
09 Z = -467817
89
XDOT = -10724
787925 XDOT = -3336
570749
YDOT = 11346
187175 feet/sec YDOT = 3421
384415 meter/sec
ZDOT = 19739
953429 ZDOT = 6000
693970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15053153
45 X = 4588201
17
Y = 16314750
52 feet Y = 4972735
96 meter
Z = -1509166
22 Z = -459993
87
XDOT = -9419
579053 XDOT = -2871
087695
YDOT = 10480
880110 feet/sec YDOT = 3194
572258 meter/sec
ZDOT = 19667
303853 ZDOT = 5994
594214
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 18305
89255547
00016717 00000-0 10270-3 0 9111
2 25544 51
6385 52
5000 0004463 1
7489 358
3679 15
53910043 19921
Satellite: ISS
Catalog Number: 25544
Epoch time: 18305
89255547 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 52
5000 deg
Eccentricity:
0004463
Arg of perigee: 1
7489 deg
Mean anomaly: 358
3679 deg
Mean motion: 15
53910043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1992
Checksum: 316
Coasting Arc #13 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2018/306/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3862650
95 A = 6789379
29 meter
Y = -5458922
77 meter E =
0006551
Z = -1168477
25 I = 51
93763
XDOT = 4506
432662 Wp = 112
52855
YDOT = -1934
435236 meter/sec RA = 46
85340 deg
ZDOT = -5888
356190 TA = 80
09906
MA = 80
02512
Ha = 222
138 n
mi
Hp = 214
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12672739
34 X = -3795644
75
Y = -17909851
60 feet Y = -5501743
01 meter
Z = -3833586
79 Z = -1187077
95
XDOT = 14784
884061 XDOT = 4556
332031
YDOT = -6346
572296 feet/sec YDOT = -1883
762407 meter/sec
ZDOT = -19318
753903 ZDOT = -5866
343942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13330767
49 X = -4063217
93
Y = -17407147
68 feet Y = -5305698
61 meter
Z = -3916547
26 Z = -1193763
61
XDOT = 13386
886238 XDOT = 4080
322925
YDOT = -5948
411463 feet/sec YDOT = -1813
075814 meter/sec
ZDOT = -19219
453210 ZDOT = -5858
089338
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 18306
92154419
00016717 00000-0 10270-3 0 9123
2 25544 51
6390 47
3716 0004720 4
7149 355
4047 15
53901614 20085
Satellite: ISS
Catalog Number: 25544
Epoch time: 18306
92154419 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 47
3716 deg
Eccentricity:
0004720
Arg of perigee: 4
7149 deg
Mean anomaly: 355
4047 deg
Mean motion: 15
53901614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 292
Coasting Arc #14 (Orbit 2023)
---------------------------------------
Vector Time (GMT): 2018/307/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2956789
47 A = 6786834
99 meter
Y = 5477613
82 meter E =
0015600
Z = 2681833
64 I = 51
90614
XDOT = -5607
505425 Wp = 62
04268
YDOT = 464
364668 meter/sec RA = 41
90048 deg
ZDOT = 5218
008829 TA = 328
14044
MA = 328
23470
Ha = 222
109 n
mi
Hp = 214
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9700752
85 X = 2882290
36
Y = 17971173
95 feet Y = 5510262
28 meter
Z = 8798666
80 Z = 2696015
71
XDOT = -18397
327510 XDOT = -5637
628073
YDOT = 1523
506128 feet/sec YDOT = 401
489483 meter/sec
ZDOT = 17119
451540 ZDOT = 5190
695877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10631396
53 X = 3240449
66
Y = 17404807
65 feet Y = 5304985
37 meter
Z = 8861733
18 Z = 2701056
27
XDOT = -17127
533190 XDOT = -5220
472116
YDOT = 1781
733323 feet/sec YDOT = 543
072317 meter/sec
ZDOT = 16996
504456 ZDOT = 5180
534558
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 18307
95052976
00016717 00000-0 10270-3 0 9133
2 25544 51
6392 42
2445 0004547 7
6236 352
4985 15
53922909 20242
Satellite: ISS
Catalog Number: 25544
Epoch time: 18307
95052976 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 42
2445 deg
Eccentricity:
0004547
Arg of perigee: 7
6236 deg
Mean anomaly: 352
4985 deg
Mean motion: 15
53922909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2024
Checksum: 319
Coasting Arc #15 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2018/308/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1757426
79 A = 6783235
12 meter
Y = -5220350
14 meter E =
0009998
Z = -3970355
68 I = 51
86984
XDOT = 6450
797569 Wp = 47
60249
YDOT = 892
905815 meter/sec RA = 36
93668 deg
ZDOT = -4029
288294 TA = 180
41591
MA = 180
41675
Ha = 222
261 n
mi
Hp = 214
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5765835
92 X = -1679634
46
Y = -17127133
00 feet Y = -5239568
15 meter
Z = -13026101
33 Z = -3978703
62
XDOT = 21164
034018 XDOT = 6459
905973
YDOT = 2929
481019 feet/sec YDOT = 965
093838 meter/sec
ZDOT = -13219
449783 ZDOT = -3997
929830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6915188
02 X = -2107749
31
Y = -16667409
39 feet Y = -5080226
38 meter
Z = -13062943
91 Z = -3981585
30
XDOT = 20193
314366 XDOT = 6154
922219
YDOT = 1872
346250 feet/sec YDOT = 570
691137 meter/sec
ZDOT = -13078
496092 ZDOT = -3986
325609
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 18308
91520137
00016717 00000-0 10270-3 0 9140
2 25544 51
6403 37
4369 0004756 11
1127 349
0130 15
53918014 20399
Satellite: ISS
Catalog Number: 25544
Epoch time: 18308
91520137 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 37
4369 deg
Eccentricity:
0004756
Arg of perigee: 11
1127 deg
Mean anomaly: 349
0130 deg
Mean motion: 15
53918014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 283
Coasting Arc #16 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2018/309/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 339148
53 A = 6779820
41 meter
Y = 4711480
79 meter E =
0007174
Z = 4856885
82 I = 51
83169
XDOT = -6966
301351 Wp = 81
21124
YDOT = -2052
904322 meter/sec RA = 31
96287 deg
ZDOT = 2475
845579 TA = 344
54645
MA = 344
56835
Ha = 222
273 n
mi
Hp = 214
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1112692
04 X = 262845
46
Y = 15457614
13 feet Y = 4714846
95 meter
Z = 15934664
76 Z = 4858347
80
XDOT = -22855
319393 XDOT = -6954
854099
YDOT = -6735
250399 feet/sec YDOT = -2130
742234 meter/sec
ZDOT = 8122
852950 ZDOT = 2442
032759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2396934
28 X = 730585
57
Y = 15304958
42 feet Y = 4664951
33 meter
Z = 15940590
11 Z = 4858691
87
XDOT = -22306
926636 XDOT = -6799
151239
YDOT = -4815
536728 feet/sec YDOT = -1467
775595 meter/sec
ZDOT = 7971
030596 ZDOT = 2429
570126
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 18309
94417804
00016717 00000-0 10270-3 0 9151
2 25544 51
6405 32
3099 0004711 13
5375 346
5903 15
53949011 20556
Satellite: ISS
Catalog Number: 25544
Epoch time: 18309
94417804 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 32
3099 deg
Eccentricity:
0004711
Arg of perigee: 13
5375 deg
Mean anomaly: 346
5903 deg
Mean motion: 15
53949011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 301
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