[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 11th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
132/22:41:24
349 -1
0 1
0 1
1
N/A -0
1 -0
1 222
0
000/00:02:44
698 0
0 -0
0 213
8
134/06:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
9
137/14:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
8
140/09:04:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 213
8
Coasting Arc #1 (Orbit 3249)
---------------------------------------
Vector Time (GMT): 2018/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1468635
20 A = 6780749
51 meter
Y = -4935668
08 meter E =
0011603
Z = 4402474
51 I = 51
43660
XDOT = 6847
115386 Wp = 98
39796
YDOT = 944
048990 meter/sec RA = 210
46168 deg
ZDOT = 3333
341515 TA = 317
80960
MA = 317
89883
Ha = 221
833 n
mi
Hp = 213
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4818356
95 X = -1434719
11
Y = -16193136
74 feet Y = -4951901
79 meter
Z = 14443814
02 Z = 4395422
65
XDOT = 22464
289325 XDOT = 6819
858148
YDOT = 3097
273588 feet/sec YDOT = 1020
465701 meter/sec
ZDOT = 10936
159827 ZDOT = 3366
536479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15111632
28 X = -4606025
52
Y = -7613429
75 feet Y = -2320573
39 meter
Z = 14412919
97 Z = 4393058
01
XDOT = 17135
159341 XDOT = 5222
796567
YDOT = -12970
321693 feet/sec YDOT = -3953
354052 meter/sec
ZDOT = 11084
215662 ZDOT = 3378
468934
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 18129
55434548
00016717 00000-0 10270-3 0 9006
2 25544 51
6408 211
2999 0003044 59
7407 300
4047 15
54259312 32507
Satellite: ISS
Catalog Number: 25544
Epoch time: 18129
55434548 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 211
2999 deg
Eccentricity:
0003044
Arg of perigee: 59
7407 deg
Mean anomaly: 300
4047 deg
Mean motion: 15
54259312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3250
Checksum: 297
Coasting Arc #2 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2018/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -200571
59 A = 6777917
40 meter
Y = 4436007
63 meter E =
0016600
Z = -5135603
42 I = 51
45497
XDOT = -7206
952511 Wp = 75
42352
YDOT = -2087
556668 meter/sec RA = 205
45308 deg
ZDOT = -1521
754461 TA = 179
85412
MA = 179
85364
Ha = 221
913 n
mi
Hp = 213
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -658043
28 X = -225215
04
Y = 14553830
79 feet Y = 4433626
93 meter
Z = -16849092
59 Z = -5136637
57
XDOT = -23644
857321 XDOT = -7175
681296
YDOT = -6848
939199 feet/sec YDOT = -2167
974920 meter/sec
ZDOT = -4992
632745 ZDOT = -1556
687724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10335739
77 X = 3150333
48
Y = 10258969
40 feet Y = 3126933
87 meter
Z = -16854226
86 Z = -5137168
35
XDOT = -20283
477701 XDOT = -6182
404003
YDOT = 11977
418393 feet/sec YDOT = 3650
717126 meter/sec
ZDOT = -5148
331493 ZDOT = -1569
211439
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 18130
51880989
00016717 00000-0 10270-3 0 9019
2 25544 51
6400 206
4920 0003116 61
3384 298
8082 15
54217122 32650
Satellite: ISS
Catalog Number: 25544
Epoch time: 18130
51880989 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 206
4920 deg
Eccentricity:
0003116
Arg of perigee: 61
3384 deg
Mean anomaly: 298
8082 deg
Mean motion: 15
54217122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 293
Coasting Arc #3 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2018/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1943750
29 A = 6776986
53 meter
Y = -3764560
95 meter E =
0005746
Z = 5284873
24 I = 51
48289
XDOT = 7045
611408 Wp = 68
65339
YDOT = 3006
133011 meter/sec RA = 200
44102 deg
ZDOT = -447
546086 TA = 25
63595
MA = 25
60747
Ha = 221
780 n
mi
Hp = 213
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6377133
50 X = 1960030
72
Y = -12350921
74 feet Y = -3742733
57 meter
Z = 17338822
97 Z = 5294354
96
XDOT = 23115
522992 XDOT = 7013
646332
YDOT = 9862
641113 feet/sec YDOT = 3084
743164 meter/sec
ZDOT = -1468
327053 ZDOT = -413
398149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5066059
87 X = -1544135
05
Y = -12886553
19 feet Y = -3927821
41 meter
Z = 17381589
86 Z = 5297908
59
XDOT = 21797
907510 XDOT = 6644
002209
YDOT = -10355
488935 feet/sec YDOT = -3156
353028 meter/sec
ZDOT = -1316
223092 ZDOT = -401
184799
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 18131
54756759
00016717 00000-0 10270-3 0 9021
2 25544 51
6402 201
3633 0003122 64
9601 295
1875 15
54269404 32813
Satellite: ISS
Catalog Number: 25544
Epoch time: 18131
54756759 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 201
3633 deg
Eccentricity:
0003122
Arg of perigee: 64
9601 deg
Mean anomaly: 295
1875 deg
Mean motion: 15
54269404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 298
Coasting Arc #4 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2018/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3612510
57 A = 6778795
18 meter
Y = 3030061
15 meter E =
0014759
Z = -4883872
07 I = 51
51944
XDOT = -6282
225682 Wp = 99
13085
YDOT = -3684
309941 meter/sec RA = 195
43231 deg
ZDOT = 2364
848786 TA = 194
08467
MA = 194
12588
Ha = 221
948 n
mi
Hp = 213
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11852068
80 X = -3622401
39
Y = 9941145
50 feet Y = 2989608
31 meter
Z = -16023202
32 Z = -4901444
68
XDOT = -20610
976648 XDOT = -6252
047188
YDOT = -12087
631040 feet/sec YDOT = -3754
393397 meter/sec
ZDOT = 7758
690243 ZDOT = 2334
404682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -114050
41 X = -34762
57
Y = 15386783
77 feet Y = 4689891
69 meter
Z = -16102012
27 Z = -4907893
34
XDOT = -21510
232996 XDOT = -6556
319017
YDOT = 7805
017485 feet/sec YDOT = 2378
969329 meter/sec
ZDOT = 7623
184882 ZDOT = 2323
546752
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 18132
51202749
00016717 00000-0 10270-3 0 9035
2 25544 51
6397 196
5549 0003293 67
2970 292
8531 15
54247857 32968
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
51202749 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 196
5549 deg
Eccentricity:
0003293
Arg of perigee: 67
2970 deg
Mean anomaly: 292
8531 deg
Mean motion: 15
54247857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 337
Coasting Arc #5 (Orbit 3302)
---------------------------------------
Vector Time (GMT): 2018/132/22:42:46
698
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1253617
16 A = 6777554
99 meter
Y = 4039954
74 meter E =
0017157
Z = -5310322
15 I = 51
52928
XDOT = -7397
977898 Wp = 87
14067
YDOT = -1952
497484 meter/sec RA = 193
22173 deg
ZDOT = 262
616222 TA = 185
36128
MA = 185
37967
Ha = 221
982 n
mi
Hp = 213
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4112917
18 X = -1272904
66
Y = 13254444
69 feet Y = 4025828
16 meter
Z = -17422316
76 Z = -5316458
69
XDOT = -24271
581031 XDOT = -7376
870377
YDOT = -6405
831642 feet/sec YDOT = -2035
108753 meter/sec
ZDOT = 861
601779 ZDOT = 226
730005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3275034
15 X = -998230
41
Y = -13449861
33 feet Y = -4099517
73 meter
Z = -17450183
23 Z = -5318815
85
XDOT = 23191
457424 XDOT = 7068
756223
YDOT = -6550
688930 feet/sec YDOT = -1996
649986 meter/sec
ZDOT = 701
590362 ZDOT = 213
844742
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 18132
96210858
00016717 00000-0 10270-3 0 9045
2 25544 51
6413 194
3124 0002690 58
0714 302
0700 15
54066381 33038
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
96210858 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 194
3124 deg
Eccentricity:
0002690
Arg of perigee: 58
0714 deg
Mean anomaly: 302
0700 deg
Mean motion: 15
54066381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3303
Checksum: 277
Coasting Arc #6 (Orbit 3318)
---------------------------------------
Vector Time (GMT): 2018/133/22:42:46
698
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2954048
66 A = 6778894
99 meter
Y = -3548839
44 meter E =
0008819
Z = 4958204
75 I = 51
56585
XDOT = 6853
277386 Wp = 58
02530
YDOT = 2705
185931 meter/sec RA = 188
21777 deg
ZDOT = -2139
507276 TA = 52
86981
MA = 52
78927
Ha = 221
849 n
mi
Hp = 213
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9691760
71 X = 2969428
35
Y = -11643174
00 feet Y = -3515719
40 meter
Z = 16267075
94 Z = 4972592
03
XDOT = 22484
505861 XDOT = 6832
910723
YDOT = 8875
281927 feet/sec YDOT = 2781
710190 meter/sec
ZDOT = -7019
380827 ZDOT = -2106
265110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2100273
72 X = -640163
43
Y = 14932340
19 feet Y = 4551377
29 meter
Z = 16331734
53 Z = 4977912
68
XDOT = -22761
723278 XDOT = -6937
773255
YDOT = 4340
023995 feet/sec YDOT = 1322
839314 meter/sec
ZDOT = -6871
246046 ZDOT = -2094
355795
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 18133
99099149
00016717 00000-0 10270-3 0 9058
2 25544 51
6407 189
1843 0002681 59
1480 300
9936 15
54096516 33191
Satellite: ISS
Catalog Number: 25544
Epoch time: 18133
99099149 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 189
1843 deg
Eccentricity:
0002681
Arg of perigee: 59
1480 deg
Mean anomaly: 300
9936 deg
Mean motion: 15
54096516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3319
Checksum: 333
Coasting Arc #7 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2018/134/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2526415
48 A = 6778729
44 meter
Y = -3741632
35 meter E =
0007972
Z = 5051480
58 I = 51
57251
XDOT = 7086
969359 Wp = 62
10447
YDOT = 2291
970152 meter/sec RA = 186
61342 deg
ZDOT = -1840
894989 TA = 45
76312
MA = 45
69770
Ha = 222
044 n
mi
Hp = 213
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8288764
68 X = 2543529
70
Y = -12275696
69 feet Y = -3713284
74 meter
Z = 16573099
03 Z = 5063794
72
XDOT = 23251
211808 XDOT = 7069
755493
YDOT = 7519
587114 feet/sec YDOT = 2371
125347 meter/sec
ZDOT = -6039
681722 ZDOT = -1806
509920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13510944
31 X = 4118135
83
Y = -5916967
89 feet Y = -1803491
81 meter
Z = 16628524
75 Z = 5068374
34
XDOT = 15114
912958 XDOT = 4607
025470
YDOT = 17917
176899 feet/sec YDOT = 5461
155519 meter/sec
ZDOT = -5886
389740 ZDOT = -1794
171593
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 18134
31252031
00016717 00000-0 10270-3 0 9067
2 25544 51
6381 187
5764 0002669 74
5163 285
6284 15
54020161 33245
Satellite: ISS
Catalog Number: 25544
Epoch time: 18134
31252031 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 187
5764 deg
Eccentricity:
0002669
Arg of perigee: 74
5163 deg
Mean anomaly: 285
6284 deg
Mean motion: 15
54020161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 296
Coasting Arc #8 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2018/135/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4090554
98 A = 6781630
16 meter
Y = 3293275
04 meter E =
0010729
Z = -4301546
76 I = 51
61555
XDOT = -6108
038357 Wp = 103
40135
YDOT = -2974
694476 meter/sec RA = 181
61803 deg
ZDOT = 3536
005081 TA = 202
65967
MA = 202
70707
Ha = 221
996 n
mi
Hp = 213
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13420455
97 X = -4106182
14
Y = 10804708
12 feet Y = 3247444
53 meter
Z = -14112686
23 Z = -4321455
46
XDOT = -20039
495922 XDOT = -6091
496981
YDOT = -9759
496312 feet/sec YDOT = -3042
906500 meter/sec
ZDOT = 11601
066540 ZDOT = 3506
373667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17015076
18 X = -5186195
22
Y = 2192926
77 feet Y = 668404
08 meter
Z = -14201990
12 Z = -4328766
59
XDOT = -11831
391143 XDOT = -3606
208020
YDOT = -17629
405116 feet/sec YDOT = -5373
442679 meter/sec
ZDOT = 11469
066971 ZDOT = 3495
771613
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 18135
27709561
00016717 00000-0 10270-3 0 9079
2 25544 51
6383 182
7692 0002485 76
0921 284
0508 15
54048929 33399
Satellite: ISS
Catalog Number: 25544
Epoch time: 18135
27709561 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 182
7692 deg
Eccentricity:
0002485
Arg of perigee: 76
0921 deg
Mean anomaly: 284
0508 deg
Mean motion: 15
54048929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3339
Checksum: 332
Coasting Arc #9 (Orbit 3354)
---------------------------------------
Vector Time (GMT): 2018/136/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5371224
12 A = 6785448
35 meter
Y = -2757624
09 meter E =
0015456
Z = 3082040
08 I = 51
66162
XDOT = 4674
357269 Wp = 93
12969
YDOT = 3606
210106 meter/sec RA = 176
63299 deg
ZDOT = -4899
238836 TA = 51
44466
MA = 51
30625
Ha = 221
990 n
mi
Hp = 213
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17622126
37 X = 5386690
18
Y = -9047323
12 feet Y = -2697473
15 meter
Z = 10111680
05 Z = 3108169
50
XDOT = 15335
817811 XDOT = 4657
482647
YDOT = 11831
397985 feet/sec YDOT = 3658
388062 meter/sec
ZDOT = -16073
618227 ZDOT = -4876
572623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19713202
78 X = 6008584
21
Y = 1184174
21 feet Y = 360936
30 meter
Z = 10228725
93 Z = 3117715
66
XDOT = 7323
928670 XDOT = 2232
333459
YDOT = 16618
457957 feet/sec YDOT = 5065
305985 meter/sec
ZDOT = -15972
789511 ZDOT = -4868
506243
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 18136
30597480
00016717 00000-0 10270-3 0 9080
2 25544 51
6387 177
6399 0002562 80
8761 279
2681 15
54045926 33551
Satellite: ISS
Catalog Number: 25544
Epoch time: 18136
30597480 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 177
6399 deg
Eccentricity:
0002562
Arg of perigee: 80
8761 deg
Mean anomaly: 279
2681 deg
Mean motion: 15
54045926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3355
Checksum: 345
Coasting Arc #10 (Orbit 3369)
---------------------------------------
Vector Time (GMT): 2018/137/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6227727
83 A = 6788421
08 meter
Y = 2178444
90 meter E =
0010014
Z = -1585780
46 I = 51
70456
XDOT = -2909
857034 Wp = 48
58482
YDOT = -4158
404965 meter/sec RA = 171
66066 deg
ZDOT = 5745
106488 TA = 294
09155
MA = 294
19628
Ha = 222
038 n
mi
Hp = 213
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20432177
91 X = -6243921
92
Y = 7147128
92 feet Y = 2108711
78 meter
Z = -5202691
79 Z = -1616072
22
XDOT = -9546
775046 XDOT = -2891
047515
YDOT = -13643
060909 feet/sec YDOT = -4190
840434 meter/sec
ZDOT = 18848
774568 ZDOT = 5731
016411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21257607
93 X = -6479318
90
Y = -3903861
84 feet Y = -1189897
09 meter
Z = -5338287
71 Z = -1627110
09
XDOT = -1922
134838 XDOT = -585
866699
YDOT = -15091
488808 feet/sec YDOT = -4599
885789 meter/sec
ZDOT = 18786
314122 ZDOT = 5726
068544
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 18137
27054602
00016717 00000-0 10270-3 0 9092
2 25544 51
6388 172
8323 0002648 80
2152 279
9300 15
54053037 33703
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
27054602 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 172
8323 deg
Eccentricity:
0002648
Arg of perigee: 80
2152 deg
Mean anomaly: 279
9300 deg
Mean motion: 15
54053037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3370
Checksum: 299
Coasting Arc #11 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2018/137/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -986910
23 A = 6777578
40 meter
Y = -4088230
87 meter E =
0005122
Z = 5310452
63 I = 51
67597
XDOT = 7518
435220 Wp = 88
60991
YDOT = -1513
705650 meter/sec RA = 169
98596 deg
ZDOT = 231
856446 TA = 359
18221
MA = 359
18305
Ha = 222
131 n
mi
Hp = 213
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3237894
45 X = -966916
93
Y = -13412830
95 feet Y = -4099155
99 meter
Z = 17422744
85 Z = 5305706
59
XDOT = 24666
782218 XDOT = 7533
676850
YDOT = -4966
225887 feet/sec YDOT = -1429
544138 meter/sec
ZDOT = 760
683877 ZDOT = 268
415810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13209053
09 X = -4026119
38
Y = 4078053
62 feet Y = 1242990
74 meter
Z = 17402023
67 Z = 5304136
81
XDOT = -6003
687532 XDOT = -1829
923960
YDOT = -23391
135633 feet/sec YDOT = -7129
618141 meter/sec
ZDOT = 924
213792 ZDOT = 281
700364
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 18137
65637351
00016717 00000-0 10270-3 0 9104
2 25544 51
6355 170
9123 0002759 74
7809 285
3648 15
54057260 33768
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
65637351 = yrday
fracday
Element set: 910
Inclination: 51
6355 deg
RA of node: 170
9123 deg
Eccentricity:
0002759
Arg of perigee: 74
7809 deg
Mean anomaly: 285
3648 deg
Mean motion: 15
54057260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 326
Coasting Arc #12 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2018/138/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -771338
57 A = 6778473
33 meter
Y = 4391446
91 meter E =
0016099
Z = -5120029
90 I = 51
71148
XDOT = -7445
495574 Wp = 98
54996
YDOT = 633
573510 meter/sec RA = 164
99134 deg
ZDOT = 1667
238029 TA = 187
54554
MA = 187
56979
Ha = 222
139 n
mi
Hp = 213
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2530638
34 X = -795516
95
Y = 14407634
23 feet Y = 4382686
69 meter
Z = -16797998
37 Z = -5123835
04
XDOT = -24427
478916 XDOT = -7460
125643
YDOT = 2078
653248 feet/sec YDOT = 550
230854 meter/sec
ZDOT = 5469
941041 ZDOT = 1631
034571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14542538
82 X = 4432565
83
Y = 1381825
16 feet Y = 421180
31 meter
Z = -16815526
39 Z = -5125372
44
XDOT = 3925
977691 XDOT = 1196
638000
YDOT = 23191
032891 feet/sec YDOT = 7068
626825 meter/sec
ZDOT = 5308
076834 ZDOT = 1617
901819
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 18138
62094367
00016717 00000-0 10270-3 0 9117
2 25544 51
6358 166
1045 0002800 77
7133 282
4333 15
54043505 33914
Satellite: ISS
Catalog Number: 25544
Epoch time: 18138
62094367 = yrday
fracday
Element set: 911
Inclination: 51
6358 deg
RA of node: 166
1045 deg
Eccentricity:
0002800
Arg of perigee: 77
7133 deg
Mean anomaly: 282
4333 deg
Mean motion: 15
54043505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 295
Coasting Arc #13 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2018/139/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2432173
29 A = 6781259
39 meter
Y = -4560685
62 meter E =
0012100
Z = 4381926
19 I = 51
75324
XDOT = 6861
044342 Wp = 72
77495
YDOT = 367
415839 meter/sec RA = 160
00358 deg
ZDOT = -3414
521596 TA = 51
79748
MA = 51
68858
Ha = 222
017 n
mi
Hp = 213
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7979571
15 X = 2461706
16
Y = -14962879
33 feet Y = -4533322
75 meter
Z = 14376398
25 Z = 4393812
12
XDOT = 22509
987998 XDOT = 6873
011898
YDOT = 1205
432543 feet/sec YDOT = 444
208060 meter/sec
ZDOT = -11202
498673 ZDOT = -3381
163739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15602366
50 X = -4755601
31
Y = -6525442
03 feet Y = -1988954
73 meter
Z = 14430069
51 Z = 4398285
19
XDOT = -1280
183893 XDOT = -390
200050
YDOT = -21463
650997 feet/sec YDOT = -6542
120824 meter/sec
ZDOT = -11053
445151 ZDOT = -3369
090082
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 18139
64981495
00016717 00000-0 10270-3 0 9128
2 25544 51
6363 160
9755 0002736 79
3337 280
8123 15
54078621 34076
Satellite: ISS
Catalog Number: 25544
Epoch time: 18139
64981495 = yrday
fracday
Element set: 912
Inclination: 51
6363 deg
RA of node: 160
9755 deg
Eccentricity:
0002736
Arg of perigee: 79
3337 deg
Mean anomaly: 280
8123 deg
Mean motion: 15
54078621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 328
Coasting Arc #14 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1529499
37 A = 6780150
99 meter
Y = -4681675
25 meter E =
0010509
Z = 4653008
63 I = 51
77654
XDOT = 7068
145085 Wp = 69
33849
YDOT = -604
971473 meter/sec RA = 156
17076 deg
ZDOT = -2923
131641 TA = 49
71685
MA = 49
62503
Ha = 221
914 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5018042
56 X = 1559135
56
Y = -15359826
92 feet Y = -4664406
10 meter
Z = 15265776
35 Z = 4660509
93
XDOT = 23189
452380 XDOT = 7088
583788
YDOT = -1984
814545 feet/sec YDOT = -525
816033 meter/sec
ZDOT = -9590
326906 ZDOT = -2888
747375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1253916
50 X = 382193
75
Y = -16077644
25 feet Y = -4900465
97 meter
Z = 15299869
62 Z = 4663400
26
XDOT = 21000
500781 XDOT = 6400
952638
YDOT = -7370
072262 feet/sec YDOT = -2246
398025 meter/sec
ZDOT = -9436
550540 ZDOT = -2876
260605
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 18140
42146572
00016717 00000-0 10270-3 0 9136
2 25544 51
6393 157
1282 0002505 84
5686 275
5753 15
54107960 34193
Satellite: ISS
Catalog Number: 25544
Epoch time: 18140
42146572 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 157
1282 deg
Eccentricity:
0002505
Arg of perigee: 84
5686 deg
Mean anomaly: 275
5753 deg
Mean motion: 15
54107960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 313
Coasting Arc #15 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2996296
42 A = 6783787
34 meter
Y = 4897594
37 meter E =
0008262
Z = -3621201
80 I = 51
81751
XDOT = -6229
693773 Wp = 96
46041
YDOT = -545
458367 meter/sec RA = 151
19420 deg
ZDOT = 4424
681510 TA = 220
79948
MA = 220
86137
Ha = 222
049 n
mi
Hp = 213
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9830368
83 X = -3033250
06
Y = 16068222
99 feet Y = 4863881
39 meter
Z = -11880583
34 Z = -3635846
14
XDOT = -20438
627864 XDOT = -6244
624094
YDOT = -1789
561572 feet/sec YDOT = -615
206930 meter/sec
ZDOT = 14516
671621 ZDOT = 4394
383479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5487665
28 X = -1672640
38
Y = 17975968
09 feet Y = 5479075
07 meter
Z = -11946644
00 Z = -3641337
09
XDOT = -19030
160492 XDOT = -5800
392918
YDOT = 3731
344757 feet/sec YDOT = 1137
313882 meter/sec
ZDOT = 14381
280322 ZDOT = 4383
414242
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 18141
38603188
00016717 00000-0 10270-3 0 9144
2 25544 51
6384 152
3209 0002800 90
3681 269
7792 15
54102507 34344
Satellite: ISS
Catalog Number: 25544
Epoch time: 18141
38603188 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 152
3209 deg
Eccentricity:
0002800
Arg of perigee: 90
3681 deg
Mean anomaly: 269
7792 deg
Mean motion: 15
54102507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 302
Coasting Arc #16 (Orbit 3449)
---------------------------------------
Vector Time (GMT): 2018/142/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4189882
31 A = 6787307
65 meter
Y = -4863371
22 meter E =
0016404
Z = 2182267
63 I = 51
85836
XDOT = 5018
781643 Wp = 106
10003
YDOT = 1841
536239 meter/sec RA = 146
22877 deg
ZDOT = -5502
068330 TA = 49
74272
MA = 49
59938
Ha = 221
972 n
mi
Hp = 213
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13746333
05 X = 4233354
14
Y = -15955942
32 feet Y = -4816274
14 meter
Z = 7159670
70 Z = 2202725
95
XDOT = 16465
819038 XDOT = 5024
542268
YDOT = 6041
785561 feet/sec YDOT = 1897
692256 meter/sec
ZDOT = -18051
405281 ZDOT = -5477
674680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9014974
15 X = 2747764
12
Y = -18998874
90 feet Y = -5790857
07 meter
Z = 7251733
98 Z = 2210328
52
XDOT = 16204
621555 XDOT = 4939
168650
YDOT = 803
704292 feet/sec YDOT = 244
969068 meter/sec
ZDOT = -17942
554776 ZDOT = -5468
890696
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 18142
41489746
00016717 00000-0 10270-3 0 9152
2 25544 51
6391 147
1920 0002655 89
3872 270
7585 15
54112562 34504
Satellite: ISS
Catalog Number: 25544
Epoch time: 18142
41489746 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 147
1920 deg
Eccentricity:
0002655
Arg of perigee: 89
3872 deg
Mean anomaly: 270
7585 deg
Mean motion: 15
54112562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3450
Checksum: 320
Coasting Arc #17 (Orbit 3464)
---------------------------------------
Vector Time (GMT): 2018/143/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4988665
74 A = 6789389
45 meter
Y = 4563994
39 meter E =
0012798
Z = -560462
59 I = 51
89166
XDOT = -3566
032418 Wp = 50
67414
YDOT = -3173
157056 meter/sec RA = 141
27314 deg
ZDOT = 6000
544348 TA = 303
29949
MA = 303
42200
Ha = 222
111 n
mi
Hp = 213
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16367013
57 X = -5036608
36
Y = 14973734
89 feet Y = 4507939
66 meter
Z = -1838788
04 Z = -584812
14
XDOT = -11699
581425 XDOT = -3559
431883
YDOT = -10410
620264 feet/sec YDOT = -3212
998265 meter/sec
ZDOT = 19686
825290 ZDOT = 5983
237603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11511288
97 X = -3508640
88
Y = 18951718
66 feet Y = 5776483
85 meter
Z = -1948229
27 Z = -593820
28
XDOT = -12887
685920 XDOT = -3928
166669
YDOT = -5843
692370 feet/sec YDOT = -1781
157434 meter/sec
ZDOT = 19609
818157 ZDOT = 5977
072574
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 18143
37945812
00016717 00000-0 10270-3 0 9160
2 25544 51
6393 142
3843 0002771 89
8678 270
2792 15
54055308 34650
Satellite: ISS
Catalog Number: 25544
Epoch time: 18143
37945812 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 142
3843 deg
Eccentricity:
0002771
Arg of perigee: 89
8678 deg
Mean anomaly: 270
2792 deg
Mean motion: 15
54055308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3465
Checksum: 334
Coasting Arc #18 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2018/144/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907497
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5419913
95 A = 6788872
46 meter
Y = -3911575
06 meter E =
0011532
Z = -1166446
70 I = 51
91550
XDOT = 1982
171800 Wp = 132
04357
YDOT = 4489
648379 meter/sec RA = 136
32147 deg
ZDOT = -5890
209010 TA = 60
57239
MA = 60
45735
Ha = 222
115 n
mi
Hp = 213
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17781869
93 X = 5468917
47
Y = -12833251
52 feet Y = -3850691
80 meter
Z = -3826924
85 Z = -1139999
56
XDOT = 6503
188319 XDOT = 1960
431766
YDOT = 14729
817516 feet/sec YDOT = 4511
693087 meter/sec
ZDOT = -19324
832711 ZDOT = -5880
632838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13204763
19 X = 4024811
82
Y = -17533291
79 feet Y = -5344147
34 meter
Z = -3708167
28 Z = -1130249
39
XDOT = 9418
476297 XDOT = 2870
751575
YDOT = 11139
358195 feet/sec YDOT = 3395
276378 meter/sec
ZDOT = -19282
557012 ZDOT = -5877
323377
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 18144
40832007
00016717 00000-0 10270-3 0 9177
2 25544 51
6394 137
2556 0002833 96
0806 264
0670 15
54098178 34813
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
40832007 = yrday
fracday
Element set: 917
Inclination: 51
6394 deg
RA of node: 137
2556 deg
Eccentricity:
0002833
Arg of perigee: 96
0806 deg
Mean anomaly: 264
0670 deg
Mean motion: 15
54098178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 314
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