[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 5th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25144 4947 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
311/16:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
2
319/09:49:40
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
5
320/04:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
5
320/18:14:08
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
3
322/09:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 213
1
322/19:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2018/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3441945
89 A = 6786314
47 meter
Y = 5063483
05 meter E =
0015397
Z = 2906805
56 I = 51
86639
XDOT = -5691
882115 Wp = 66
21554
YDOT = 957
361706 meter/sec RA = 33
91052 deg
ZDOT = 5057
030704 TA = 326
82687
MA = 326
92331
Ha = 222
183 n
mi
Hp = 214
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11292473
41 X = 3370948
74
Y = 16612477
21 feet Y = 5101576
45 meter
Z = 9536763
66 Z = 2923353
05
XDOT = -18674
153921 XDOT = -5726
729527
YDOT = 3140
950478 feet/sec YDOT = 893
516517 meter/sec
ZDOT = 16591
308084 ZDOT = 5029
296188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19602369
12 X = -5974802
11
Y = -4222497
43 feet Y = -1287017
22 meter
Z = 9610507
59 Z = 2929282
71
XDOT = 11077
798457 XDOT = 3376
512970
YDOT = -13837
665004 feet/sec YDOT = -4217
720293 meter/sec
ZDOT = 16466
409670 ZDOT = 5018
961667
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
55834577
00016717 00000-0 10270-3 0 9002
2 25544 51
6428 34
2302 0004382 13
7100 346
4171 15
53914070 20497
Satellite: ISS
Catalog Number: 25544
Epoch time: 18309
55834577 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 34
2302 deg
Eccentricity:
0004382
Arg of perigee: 13
7100 deg
Mean anomaly: 346
4171 deg
Mean motion: 15
53914070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 283
Coasting Arc #2 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2018/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2171901
08 A = 6782693
24 meter
Y = -4922496
35 meter E =
0010840
Z = -4142052
18 I = 51
82493
XDOT = 6644
745401 Wp = 51
15421
YDOT = 263
254613 meter/sec RA = 28
94380 deg
ZDOT = -3797
116781 TA = 179
73979
MA = 179
73923
Ha = 222
292 n
mi
Hp = 214
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7125659
71 X = -2096574
49
Y = -16149922
40 feet Y = -4946363
01 meter
Z = -13589410
04 Z = -4152419
68
XDOT = 21800
345805 XDOT = 6659
752642
YDOT = 863
696236 feet/sec YDOT = 337
644558 meter/sec
ZDOT = -12457
732220 ZDOT = -3764
801612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16369501
61 X = 4989424
09
Y = 6510257
57 feet Y = 1984326
51 meter
Z = -13635360
23 Z = -4156057
80
XDOT = -15667
090283 XDOT = -4775
329118
YDOT = 13606
393346 feet/sec YDOT = 4147
228692 meter/sec
ZDOT = -12312
406121 ZDOT = -3752
821386
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 18310
52301547
00016717 00000-0 10270-3 0 9018
2 25544 51
6417 29
4241 0004372 16
8480 343
2817 15
53898322 20647
Satellite: ISS
Catalog Number: 25544
Epoch time: 18310
52301547 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 29
4241 deg
Eccentricity:
0004372
Arg of perigee: 16
8480 deg
Mean anomaly: 343
2817 deg
Mean motion: 15
53898322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 289
Coasting Arc #3 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2018/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 668705
48 A = 6779419
34 meter
Y = 4568858
94 meter E =
0006779
Z = 4957680
14 I = 51
78523
XDOT = -7232
235445 Wp = 83
21510
YDOT = -1324
237990 meter/sec RA = 23
96502 deg
ZDOT = 2194
097546 TA = 345
43210
MA = 345
45163
Ha = 222
297 n
mi
Hp = 214
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2193915
62 X = 593483
05
Y = 14989694
69 feet Y = 4575916
34 meter
Z = 16265354
78 Z = 4960745
80
XDOT = -23727
806579 XDOT = -7227
548000
YDOT = -4344
612829 feet/sec YDOT = -1405
087634 meter/sec
ZDOT = 7198
482763 ZDOT = 2158
976258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12194955
57 X = -3717022
46
Y = -8964345
55 feet Y = -2732332
52 meter
Z = 16278499
51 Z = 4961686
65
XDOT = 19045
531826 XDOT = 5805
078101
YDOT = -13113
296925 feet/sec YDOT = -3996
932903 meter/sec
ZDOT = 7040
694379 ZDOT = 2146
003647
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 18311
55199063
00016717 00000-0 10270-3 0 9021
2 25544 51
6421 24
2966 0004393 19
7944 340
3378 15
53938985 20807
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
55199063 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 24
2966 deg
Eccentricity:
0004393
Arg of perigee: 19
7944 deg
Mean anomaly: 340
3378 deg
Mean motion: 15
53938985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 322
Coasting Arc #4 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2018/311/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4212869
74 A = 6780315
37 meter
Y = 2306794
06 meter E =
0011680
Z = 4781831
82 I = 51
77917
XDOT = -5536
212207 Wp = 46
30042
YDOT = -4603
291238 meter/sec RA = 22
92754 deg
ZDOT = -2644
914254 TA = 69
79653
MA = 69
67097
Ha = 222
563 n
mi
Hp = 214
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13821751
10 X = -4261580
12
Y = 7568221
97 feet Y = 2259410
50 meter
Z = 15688424
59 Z = 4761248
24
XDOT = -18163
425877 XDOT = -5471
477488
YDOT = -15102
661542 feet/sec YDOT = -4664
839076 meter/sec
ZDOT = -8677
540202 ZDOT = -2671
650750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13290767
55 X = -4051025
95
Y = -8636021
73 feet Y = -2632259
42 meter
Z = 15595514
74 Z = 4753512
89
XDOT = 4020
751755 XDOT = 1225
525135
YDOT = -22145
387912 feet/sec YDOT = -6749
914236 meter/sec
ZDOT = -8797
148088 ZDOT = -2681
370737
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 18311
74492347
00016717 00000-0 10270-3 0 9034
2 25544 51
6395 23
3365 0004768 21
9042 338
2314 15
53930325 20839
Satellite: ISS
Catalog Number: 25544
Epoch time: 18311
74492347 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 23
3365 deg
Eccentricity:
0004768
Arg of perigee: 21
9042 deg
Mean anomaly: 338
2314 deg
Mean motion: 15
53930325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 297
Coasting Arc #5 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2018/312/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5395899
42 A = 6783794
63 meter
Y = -1444523
98 meter E =
0008692
Z = -3853904
70 I = 51
75992
XDOT = 4256
121694 Wp = 69
75220
YDOT = 4825
494488 meter/sec RA = 17
94919 deg
ZDOT = 4160
891836 TA = 243
94228
MA = 244
03178
Ha = 222
691 n
mi
Hp = 214
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17703082
09 X = 5430372
22
Y = -4739251
90 feet Y = -1383990
48 meter
Z = -12644044
29 Z = -3827608
84
XDOT = 13963
653853 XDOT = 4181
633353
YDOT = 15831
674829 feet/sec YDOT = 4872
672845 meter/sec
ZDOT = 13651
219936 ZDOT = 4181
386331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12871593
00 X = 3923261
55
Y = 13159169
82 feet Y = 4010914
96 meter
Z = -12525566
80 Z = -3817792
76
XDOT = -6008
559632 XDOT = -1831
408976
YDOT = 18925
032782 feet/sec YDOT = 5768
349992 meter/sec
ZDOT = 13742
707442 ZDOT = 4188
777228
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 18312
70958383
00016717 00000-0 10270-3 0 9049
2 25544 51
6398 18
5300 0004956 26
7503 333
3904 15
53907452 20983
Satellite: ISS
Catalog Number: 25544
Epoch time: 18312
70958383 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 18
5300 deg
Eccentricity:
0004956
Arg of perigee: 26
7503 deg
Mean anomaly: 333
3904 deg
Mean motion: 15
53907452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 316
Coasting Arc #6 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2018/313/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6270487
43 A = 6787242
73 meter
Y = 592348
92 meter E =
0015638
Z = 2517328
09 I = 51
73868
XDOT = -2602
367103 Wp = 86
25630
YDOT = -4890
805957 meter/sec RA = 12
97688 deg
ZDOT = -5302
072626 TA = 65
53642
MA = 65
37339
Ha = 222
646 n
mi
Hp = 213
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20572465
31 X = -6288873
37
Y = 1943401
98 feet Y = 522125
09 meter
Z = 8258950
42 Z = 2486822
80
XDOT = -8537
949813 XDOT = -2521
727982
YDOT = -16045
951301 feet/sec YDOT = -4919
456366 meter/sec
ZDOT = -17395
251396 ZDOT = -5314
518662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12123548
38 X = -3695257
55
Y = -16800937
40 feet Y = -5120925
72 meter
Z = 8121667
28 Z = 2475484
19
XDOT = 8345
907263 XDOT = 2543
832534
YDOT = -14505
485801 feet/sec YDOT = -4421
272072 meter/sec
ZDOT = -17450
520884 ZDOT = -5318
918765
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 18313
73854925
00016717 00000-0 10270-3 0 9051
2 25544 51
6385 13
4016 0005032 28
0949 332
0474 15
53953895 21141
Satellite: ISS
Catalog Number: 25544
Epoch time: 18313
73854925 = yrday
fracday
Element set: 905
Inclination: 51
6385 deg
RA of node: 13
4016 deg
Eccentricity:
0005032
Arg of perigee: 28
0949 deg
Mean anomaly: 332
0474 deg
Mean motion: 15
53953895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 306
Coasting Arc #7 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2018/314/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6709377
18 A = 6789451
67 meter
Y = 162243
89 meter E =
0014806
Z = -981067
32 I = 51
71331
XDOT = 740
320908 Wp = 36
98804
YDOT = 4822
010754 meter/sec RA = 8
01144 deg
ZDOT = 5918
312116 TA = 312
39294
MA = 312
51815
Ha = 222
701 n
mi
Hp = 213
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22012392
32 X = 6711829
88
Y = 532296
23 feet Y = 237286
57 meter
Z = -3218724
80 Z = -948468
77
XDOT = 2428
874370 XDOT = 657
596111
YDOT = 15820
245256 feet/sec YDOT = 4829
826707 meter/sec
ZDOT = 19417
034502 ZDOT = 5921
707727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11030707
68 X = 3362159
70
Y = 19080733
13 feet Y = 5815807
46 meter
Z = -3072141
86 Z = -936388
84
XDOT = -10912
311486 XDOT = -3326
072541
YDOT = 9405
061323 feet/sec YDOT = 2866
662691 meter/sec
ZDOT = 19431
604315 ZDOT = 5922
752995
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 18314
70320243
00016717 00000-0 10270-3 0 9061
2 25544 51
6381 8
5951 0004896 34
5161 325
6309 15
53957995 21291
Satellite: ISS
Catalog Number: 25544
Epoch time: 18314
70320243 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 8
5951 deg
Eccentricity:
0004896
Arg of perigee: 34
5161 deg
Mean anomaly: 325
6309 deg
Mean motion: 15
53957995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 316
Coasting Arc #8 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2018/315/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6690536
42 A = 6789605
50 meter
Y = -908385
16 meter E =
0010422
Z = -698044
22 I = 51
68192
XDOT = 1245
756262 Wp = 111
34602
YDOT = -4651
898697 meter/sec RA = 3
04551 deg
ZDOT = -5961
942560 TA = 76
18551
MA = 76
06956
Ha = 222
730 n
mi
Hp = 213
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21950578
80 X = -6676490
55
Y = -2980266
27 feet Y = -983124
81 meter
Z = -2290171
32 Z = -730511
10
XDOT = 4087
126845 XDOT = 1326
643047
YDOT = -15262
134832 feet/sec YDOT = -4637
515197 meter/sec
ZDOT = -19560
179002 ZDOT = -5955
694775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9237313
83 X = -2815533
26
Y = -20116970
07 feet Y = -6131652
48 meter
Z = -2436047
96 Z = -742507
42
XDOT = 13680
124137 XDOT = 4169
701837
YDOT = -3944
667270 feet/sec YDOT = -1202
334584 meter/sec
ZDOT = -19531
402463 ZDOT = -5953
171471
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 18315
73215996
00016717 00000-0 10270-3 0 9074
2 25544 51
6392 3
4660 0005082 35
9434 324
2059 15
53951233 21454
Satellite: ISS
Catalog Number: 25544
Epoch time: 18315
73215996 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 3
4660 deg
Eccentricity:
0005082
Arg of perigee: 35
9434 deg
Mean anomaly: 324
2059 deg
Mean motion: 15
53951233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 302
Coasting Arc #9 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2018/316/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6188363
17 A = 6787488
34 meter
Y = 1585531
98 meter E =
0018127
Z = 2264797
44 I = 51
64172
XDOT = -3131
600518 Wp = 63
61059
YDOT = 4413
707653 meter/sec RA = 358
07631 deg
ZDOT = 5441
077443 TA = 321
61159
MA = 321
74045
Ha = 222
613 n
mi
Hp = 213
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20303028
78 X = 6159172
00
Y = 5201876
56 feet Y = 1654571
21 meter
Z = 7430437
80 Z = 2294788
04
XDOT = -10274
279916 XDOT = -3207
153402
YDOT = 14480
668154 feet/sec YDOT = 4378
265194 meter/sec
ZDOT = 17851
303948 ZDOT = 5425
681685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6801236
84 X = 2073016
99
Y = 19773637
31 feet Y = 6027004
65 meter
Z = 7565074
22 Z = 2305834
62
XDOT = -16369
278247 XDOT = -4989
356010
YDOT = -1204
422058 feet/sec YDOT = -367
107843 meter/sec
ZDOT = 17781
424264 ZDOT = 5419
778116
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 18316
76111145
00016717 00000-0 10270-3 0 9080
2 25544 51
6388 358
3388 0004892 39
7186 320
4324 15
53987749 21614
Satellite: ISS
Catalog Number: 25544
Epoch time: 18316
76111145 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 358
3388 deg
Eccentricity:
0004892
Arg of perigee: 39
7186 deg
Mean anomaly: 320
4324 deg
Mean motion: 15
53987749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 338
Coasting Arc #10 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2018/317/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5251299
47 A = 6784072
56 meter
Y = -2280166
42 meter E =
0010157
Z = -3652027
28 I = 51
59695
XDOT = 4799
460652 Wp = 61
29761
YDOT = -4067
388941 meter/sec RA = 353
09593 deg
ZDOT = -4366
173588 TA = 162
03811
MA = 162
00220
Ha = 222
817 n
mi
Hp = 213
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17228672
80 X = -5207671
85
Y = -7480860
96 feet Y = -2338645
99 meter
Z = -11981716
80 Z = -3677430
78
XDOT = 15746
261982 XDOT = 4865
795491
YDOT = -13344
451906 feet/sec YDOT = -4013
346936 meter/sec
ZDOT = -14324
716495 ZDOT = -4342
698211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3506279
08 X = -1068713
86
Y = -18378084
30 feet Y = -5601640
09 meter
Z = -12095619
43 Z = -3686744
80
XDOT = 18618
576748 XDOT = 5674
942193
YDOT = 5796
298446 feet/sec YDOT = 1766
711766 meter/sec
ZDOT = -14218
558931 ZDOT = -4333
816762
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 18317
72575365
00016717 00000-0 10270-3 0 9096
2 25544 51
6388 353
5307 0005100 42
0878 318
0666 15
53958120 21769
Satellite: ISS
Catalog Number: 25544
Epoch time: 18317
72575365 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 353
5307 deg
Eccentricity:
0005100
Arg of perigee: 42
0878 deg
Mean anomaly: 318
0666 deg
Mean motion: 15
53958120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2176
Checksum: 319
Coasting Arc #11 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2018/318/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3953331
41 A = 6780407
84 meter
Y = 2939596
81 meter E =
0010651
Z = 4649515
71 I = 51
55333
XDOT = -6109
884769 Wp = 89
91986
YDOT = 3633
474098 meter/sec RA = 348
10500 deg
ZDOT = 2892
102403 TA = 331
28882
MA = 331
34741
Ha = 222
612 n
mi
Hp = 213
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12970247
41 X = 3897581
02
Y = 9644346
48 feet Y = 2983493
81 meter
Z = 15254316
62 Z = 4668584
56
XDOT = -20045
553705 XDOT = -6164
109677
YDOT = 11920
846778 feet/sec YDOT = 3564
845826 meter/sec
ZDOT = 9488
524943 ZDOT = 2862
290751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -419593
22 X = -127892
01
Y = 16076518
52 feet Y = 4900122
84 meter
Z = 15339635
14 Z = 4675520
79
XDOT = -20186
705994 XDOT = -6152
907987
YDOT = -9469
860027 feet/sec YDOT = -2886
413336 meter/sec
ZDOT = 9353
946366 ZDOT = 2851
082852
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 18318
75469763
00016717 00000-0 10270-3 0 9106
2 25544 51
6398 348
4034 0004879 44
7534 315
4012 15
54001204 21927
Satellite: ISS
Catalog Number: 25544
Epoch time: 18318
75469763 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 348
4034 deg
Eccentricity:
0004879
Arg of perigee: 44
7534 deg
Mean anomaly: 315
4012 deg
Mean motion: 15
54001204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 307
Coasting Arc #12 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2018/319/09:49:40
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3759286
94 A = 6779808
43 meter
Y = 2929969
93 meter E =
0009776
Z = 4813361
88 I = 51
52974
XDOT = -6182
474714 Wp = 91
71178
YDOT = 3784
173237 meter/sec RA = 344
56837 deg
ZDOT = 2520
378919 TA = 333
46201
MA = 333
51203
Ha = 222
670 n
mi
Hp = 213
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12333618
58 X = 3702862
74
Y = 9612762
23 feet Y = 2971693
26 meter
Z = 15791869
67 Z = 4831486
45
XDOT = -20283
709691 XDOT = -6236
573723
YDOT = 12415
266527 feet/sec YDOT = 3714
733953 meter/sec
ZDOT = 8268
959707 ZDOT = 2490
214936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14859141
51 X = -4529066
33
Y = -4600229
66 feet Y = -1402150
00 meter
Z = 15872942
18 Z = 4838072
78
XDOT = 14211
496691 XDOT = 4331
664191
YDOT = -17789
384339 feet/sec YDOT = -5422
204346 meter/sec
ZDOT = 8132
782558 ZDOT = 2478
872124
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 18319
46209470
00016717 00000-0 10270-3 0 9113
2 25544 51
6413 344
8766 0004820 48
8972 311
2596 15
53980971 22034
Satellite: ISS
Catalog Number: 25544
Epoch time: 18319
46209470 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 344
8766 deg
Eccentricity:
0004820
Arg of perigee: 48
8972 deg
Mean anomaly: 311
2596 deg
Mean motion: 15
53980971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 321
Coasting Arc #13 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2018/320/04:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5906650
72 A = 6789198
97 meter
Y = 3106434
96 meter E =
0016156
Z = 1217506
99 I = 51
53437
XDOT = -3210
046833 Wp = 105
78297
YDOT = -3790
224096 meter/sec RA = 340
59268 deg
ZDOT = -5842
360368 TA = 60
96617
MA = 60
80440
Ha = 222
841 n
mi
Hp = 213
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19378775
32 X = -5946862
83
Y = 10191715
73 feet Y = 3040157
82 meter
Z = 3994445
51 Z = 1188716
55
XDOT = -10531
649716 XDOT = -3139
045444
YDOT = -12435
118425 feet/sec YDOT = -3825
723971 meter/sec
ZDOT = -19167
848977 ZDOT = -5857
781478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19665766
58 X = 5994125
65
Y = 9679177
00 feet Y = 2950213
15 meter
Z = 3864551
05 Z = 1177915
16
XDOT = -3217
132303 XDOT = -980
581926
YDOT = 14298
602710 feet/sec YDOT = 4358
214106 meter/sec
ZDOT = -19236
640797 ZDOT = -5863
328115
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 18320
23380042
00016717 00000-0 10270-3 0 9126
2 25544 51
6400 341
0276 0004784 54
8617 305
2984 15
53971765 22155
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
23380042 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 341
0276 deg
Eccentricity:
0004784
Arg of perigee: 54
8617 deg
Mean anomaly: 305
2984 deg
Mean motion: 15
53971765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 295
Coasting Arc #14 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4154175
19 A = 6779892
70 meter
Y = 2411528
10 meter E =
0010345
Z = 4776009
24 I = 51
48668
XDOT = -5624
695400 Wp = 92
18964
YDOT = 4527
234975 meter/sec RA = 337
83039 deg
ZDOT = 2601
185675 TA = 332
11413
MA = 332
16954
Ha = 222
726 n
mi
Hp = 213
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13629183
68 X = 4103700
41
Y = 7911837
59 feet Y = 2457700
70 meter
Z = 15669321
65 Z = 4796066
48
XDOT = -18453
725066 XDOT = -5687
537524
YDOT = 14853
133120 feet/sec YDOT = 4463
984323 meter/sec
ZDOT = 8534
073738 ZDOT = 2573
709902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7377836
24 X = 2248764
49
Y = 13823748
67 feet Y = 4213478
59 meter
Z = 15759155
05 Z = 4803390
46
XDOT = -22539
652465 XDOT = -6870
086071
YDOT = 2422
683463 feet/sec YDOT = 738
433920 meter/sec
ZDOT = 8409
893288 ZDOT = 2563
335474
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 18320
81257648
00016717 00000-0 10270-3 0 9136
2 25544 51
6403 338
1482 0005015 52
1111 308
0495 15
54000681 22241
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
81257648 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 338
1482 deg
Eccentricity:
0005015
Arg of perigee: 52
1111 deg
Mean anomaly: 308
0495 deg
Mean motion: 15
54000681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 271
Coasting Arc #15 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2018/321/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2718119
32 A = 6777952
37 meter
Y = -3319561
11 meter E =
0019240
Z = -5263926
79 I = 51
45036
XDOT = 6459
965329 Wp = 76
27021
YDOT = -4027
744384 meter/sec RA = 332
82231 deg
ZDOT = -793
697963 TA = 186
09858
MA = 186
12204
Ha = 222
934 n
mi
Hp = 213
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8917714
32 X = -2655227
27
Y = -10890948
53 feet Y = -3349605
36 meter
Z = -17270101
01 Z = -5276977
92
XDOT = 21194
111972 XDOT = 6508
379998
YDOT = -13214
384461 feet/sec YDOT = -3955
233859 meter/sec
ZDOT = -2603
995943 ZDOT = -762
199611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2033551
07 X = -619826
37
Y = -13856020
90 feet Y = -4223315
17 meter
Z = -17328304
37 Z = -5281667
17
XDOT = 23973
488730 XDOT = 7307
119365
YDOT = -431
411315 feet/sec YDOT = -131
494169 meter/sec
ZDOT = -2461
815468 ZDOT = -750
361355
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 18321
77720320
00016717 00000-0 10270-3 0 9145
2 25544 51
6410 333
3405 0005148 55
1355 305
0281 15
53989743 22391
Satellite: ISS
Catalog Number: 25544
Epoch time: 18321
77720320 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 333
3405 deg
Eccentricity:
0005148
Arg of perigee: 55
1355 deg
Mean anomaly: 305
0281 deg
Mean motion: 15
53989743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 290
Coasting Arc #16 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2018/322/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 917504
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4615360
76 A = 6780307
23 meter
Y = -1641781
11 meter E =
0015943
Z = -4703377
92 I = 51
43939
XDOT = 4730
165210 Wp = 67
10432
YDOT = -5338
623161 meter/sec RA = 329
64038 deg
ZDOT = -2779
590458 TA = 175
23495
MA = 175
21975
Ha = 222
967 n
mi
Hp = 213
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15142259
73 X = -4573811
96
Y = -5386420
95 feet Y = -1693160
98 meter
Z = -15431029
92 Z = -4725697
21
XDOT = 15518
914730 XDOT = 4803
013649
YDOT = -17515
167851 feet/sec YDOT = -5285
319854 meter/sec
ZDOT = -9119
391267 ZDOT = -2756
435598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15974326
28 X = 4868974
65
Y = -151577
50 feet Y = -46200
82 meter
Z = -15531135
46 Z = -4733890
09
XDOT = -8563
748599 XDOT = -2610
230573
YDOT = 20661
047840 feet/sec YDOT = 6297
487382 meter/sec
ZDOT = -9014
543319 ZDOT = -2747
632804
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 18322
42028382
00016717 00000-0 10270-3 0 9158
2 25544 51
6409 330
1342 0005055 60
1772 299
9882 15
53974762 22494
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
42028382 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 330
1342 deg
Eccentricity:
0005055
Arg of perigee: 60
1772 deg
Mean anomaly: 299
9882 deg
Mean motion: 15
53974762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 316
Coasting Arc #17 (Orbit 2255)
---------------------------------------
Vector Time (GMT): 2018/322/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6123894
50 A = 6788844
39 meter
Y = -2523988
54 meter E =
0019063
Z = 1445714
20 I = 51
45726
XDOT = 690
326007 Wp = 60
17821
YDOT = 5008
394391 meter/sec RA = 327
58716 deg
ZDOT = 5771
826694 TA = 315
64335
MA = 315
79592
Ha = 222
961 n
mi
Hp = 213
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20091517
39 X = 6144640
65
Y = -8280802
30 feet Y = -2455390
89 meter
Z = 4743156
81 Z = 1475512
91
XDOT = 2264
849103 XDOT = 606
232416
YDOT = 16431
740129 feet/sec YDOT = 5015
643920 meter/sec
ZDOT = 18936
439284 ZDOT = 5774
975851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21331901
63 X = 6501963
62
Y = -3987299
08 feet Y = -1215328
76 meter
Z = 4877469
98 Z = 1486652
85
XDOT = -1570
230904 XDOT = -478
606380
YDOT = 14966
709447 feet/sec YDOT = 4561
853039 meter/sec
ZDOT = 18949
890649 ZDOT = 5775
926670
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 18322
87044054
00016717 00000-0 10270-3 0 9162
2 25544 51
6420 327
8922 0005192 58
0045 302
1612 15
53975255 22569
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
87044054 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 327
8922 deg
Eccentricity:
0005192
Arg of perigee: 58
0045 deg
Mean anomaly: 302
1612 deg
Mean motion: 15
53975255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2256
Checksum: 295
Coasting Arc #18 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2018/323/19:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5907342
75 A = 6785917
67 meter
Y = 1524070
67 meter E =
0008719
Z = -2980076
83 I = 51
41958
XDOT = 1011
166065 Wp = 84
08150
YDOT = -5751
172416 meter/sec RA = 322
59935 deg
ZDOT = -4957
327108 TA = 130
07512
MA = 129
99864
Ha = 222
951 n
mi
Hp = 213
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19381045
78 X = -5909470
33
Y = 5000231
85 feet Y = 1457998
77 meter
Z = -9777154
96 Z = -3008778
46
XDOT = 3317
473967 XDOT = 1099
482747
YDOT = -18868
675907 feet/sec YDOT = -5739
371029 meter/sec
ZDOT = -16264
196548 ZDOT = -4952
200613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19911469
66 X = -6069015
95
Y = 1271580
35 feet Y = 387577
69 meter
Z = -9906385
44 Z = -3019466
28
XDOT = 7011
599969 XDOT = 2137
135670
YDOT = -16434
813347 feet/sec YDOT = -5009
331108 meter/sec
ZDOT = -16240
347971 ZDOT = -4950
058062
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 18323
83505785
00016717 00000-0 10270-3 0 9173
2 25544 51
6414 323
0853 0005011 61
9895 298
1764 15
53972715 22716
Satellite: ISS
Catalog Number: 25544
Epoch time: 18323
83505785 = yrday
fracday
Element set: 917
Inclination: 51
6414 deg
RA of node: 323
0853 deg
Eccentricity:
0005011
Arg of perigee: 61
9895 deg
Mean anomaly: 298
1764 deg
Mean motion: 15
53972715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 323
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