[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 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
108/10:36:05
758 0
2 0
9 0
9
N/A -0
8 -0
1 220
9
000/00:02:11
515 -0
3 -0
0 214
8
Coasting Arc #1 (Orbit 2813)
---------------------------------------
Vector Time (GMT): 2018/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3092962
20 A = 6778511
92 meter
Y = -3467089
65 meter E =
0012284
Z = -4947078
75 I = 51
56937
XDOT = 6747
110162 Wp = 63
32671
YDOT = -2882
727536 meter/sec RA = 350
60878 deg
ZDOT = -2196
872494 TA = 185
18786
MA = 185
20060
Ha = 220
600 n
mi
Hp = 214
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10147513
79 X = -3029932
08
Y = -11374966
05 feet Y = -3501325
27 meter
Z = -16230573
33 Z = -4961949
92
XDOT = 22136
188197 XDOT = 6789
515401
YDOT = -9457
767506 feet/sec YDOT = -2807
039783 meter/sec
ZDOT = -7207
586923 ZDOT = -2163
994136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13168217
52 X = -4013672
70
Y = -7537885
14 feet Y = -2297547
39 meter
Z = -16296371
82 Z = -4967134
13
XDOT = 17407
137864 XDOT = 5305
695621
YDOT = -15136
728834 feet/sec YDOT = -4613
674949 meter/sec
ZDOT = -7060
456969 ZDOT = -2152
027284
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 18101
51984524
00016717 00000-0 10270-3 0 9006
2 25544 51
6426 351
0710 0002247 334
4062 25
6980 15
54258655 28141
Satellite: ISS
Catalog Number: 25544
Epoch time: 18101
51984524 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 351
0710 deg
Eccentricity:
0002247
Arg of perigee: 334
4062 deg
Mean anomaly: 25
6980 deg
Mean motion: 15
54258655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2814
Checksum: 291
Coasting Arc #2 (Orbit 2829)
---------------------------------------
Vector Time (GMT): 2018/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1330573
00 A = 6776956
40 meter
Y = 4006166
49 meter E =
0002152
Z = 5300310
29 I = 51
53224
XDOT = -7371
111949 Wp = 42
83480
YDOT = 2105
705392 meter/sec RA = 345
60308 deg
ZDOT = 260
335887 TA = 44
68939
MA = 44
67205
Ha = 220
556 n
mi
Hp = 214
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4365396
97 X = 1259929
89
Y = 13143590
85 feet Y = 4020651
38 meter
Z = 17389469
47 Z = 5306601
82
XDOT = -24183
438154 XDOT = -7395
375263
YDOT = 6908
482257 feet/sec YDOT = 2023
140903 meter/sec
ZDOT = 854
120363 ZDOT = 224
470381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8445638
55 X = 2574230
63
Y = 10932831
10 feet Y = 3332326
92 meter
Z = 17416908
83 Z = 5308673
81
XDOT = -19629
446033 XDOT = -5983
055151
YDOT = 14066
255653 feet/sec YDOT = 4287
394723 meter/sec
ZDOT = 693
800812 ZDOT = 211
470487
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 18102
54860269
00016717 00000-0 10270-3 0 9010
2 25544 51
6429 345
9421 0002209 334
4899 25
6144 15
54266985 28306
Satellite: ISS
Catalog Number: 25544
Epoch time: 18102
54860269 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 345
9421 deg
Eccentricity:
0002209
Arg of perigee: 334
4899 deg
Mean anomaly: 25
6144 deg
Mean motion: 15
54266985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2830
Checksum: 320
Coasting Arc #3 (Orbit 2844)
---------------------------------------
Vector Time (GMT): 2018/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 470988
25 A = 6777953
02 meter
Y = -4460164
41 meter E =
0012116
Z = -5092569
15 I = 51
50370
XDOT = 7376
823469 Wp = 93
45859
YDOT = -1162
500834 meter/sec RA = 340
59381 deg
ZDOT = 1703
179334 TA = 193
03140
MA = 193
06273
Ha = 220
648 n
mi
Hp = 214
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1545237
04 X = 545565
17
Y = -14633085
33 feet Y = -4454481
01 meter
Z = -16707904
04 Z = -5090099
66
XDOT = 24202
176737 XDOT = 7381
001418
YDOT = -3813
979114 feet/sec YDOT = -1079
984585 meter/sec
ZDOT = 5587
858708 ZDOT = 1739
023832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3637423
09 X = -1108686
56
Y = -14271482
15 feet Y = -4349947
76 meter
Z = -16696195
73 Z = -5089000
46
XDOT = 20204
830255 XDOT = 6158
432262
YDOT = -11863
443834 feet/sec YDOT = -3615
977681 meter/sec
ZDOT = 5747
922323 ZDOT = 1751
966724
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 18103
51305830
00016717 00000-0 10270-3 0 9027
2 25544 51
6428 341
1334 0002355 338
9093 21
1962 15
54271339 28457
Satellite: ISS
Catalog Number: 25544
Epoch time: 18103
51305830 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 341
1334 deg
Eccentricity:
0002355
Arg of perigee: 338
9093 deg
Mean anomaly: 21
1962 deg
Mean motion: 15
54271339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2845
Checksum: 288
Coasting Arc #4 (Orbit 2860)
---------------------------------------
Vector Time (GMT): 2018/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2182624
08 A = 6780989
30 meter
Y = 4756268
19 meter E =
0010142
Z = 4308181
47 I = 51
48262
XDOT = -6827
035358 Wp = 57
96910
YDOT = 43
376074 meter/sec RA = 335
58858 deg
ZDOT = -3495
301636 TA = 67
70736
MA = 67
59986
Ha = 220
709 n
mi
Hp = 214
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7160840
15 X = -2256574
82
Y = 15604554
41 feet Y = 4731447
52 meter
Z = 14134453
63 Z = 4297398
86
XDOT = -22398
409966 XDOT = -6810
034509
YDOT = 142
309953 feet/sec YDOT = -32
873822 meter/sec
ZDOT = -11467
525052 ZDOT = -3528
424022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -958221
24 X = -292065
83
Y = 17182533
45 feet Y = 5237236
20 meter
Z = 14085626
92 Z = 4293299
09
XDOT = -19429
313034 XDOT = -5922
054613
YDOT = 8468
806476 feet/sec YDOT = 2581
292214 meter/sec
ZDOT = -11615
259729 ZDOT = -3540
331166
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 18104
54180493
00016717 00000-0 10270-3 0 9038
2 25544 51
6419 336
0043 0002500 342
8005 17
3062 15
54306699 28610
Satellite: ISS
Catalog Number: 25544
Epoch time: 18104
54180493 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 336
0043 deg
Eccentricity:
0002500
Arg of perigee: 342
8005 deg
Mean anomaly: 17
3062 deg
Mean motion: 15
54306699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2861
Checksum: 282
Coasting Arc #5 (Orbit 2875)
---------------------------------------
Vector Time (GMT): 2018/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3614626
77 A = 6784982
43 meter
Y = -4848472
09 meter E =
0005202
Z = -3074696
00 I = 51
46513
XDOT = 5778
073389 Wp = 43
76433
YDOT = 1212
760789 meter/sec RA = 330
59128 deg
ZDOT = 4888
975146 TA = 280
82886
MA = 280
88741
Ha = 220
774 n
mi
Hp = 214
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11859011
71 X = 3683510
51
Y = -15907060
67 feet Y = -4807665
97 meter
Z = -10087585
30 Z = -3056969
42
XDOT = 18956
933692 XDOT = 5740
334141
YDOT = 3978
873981 feet/sec YDOT = 1277
164607 meter/sec
ZDOT = 16039
944705 ZDOT = 4916
951629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4854497
07 X = 1479650
71
Y = -19279736
53 feet Y = -5876463
69 meter
Z = -10007783
61 Z = -3050372
45
XDOT = 17518
872985 XDOT = 5339
752486
YDOT = -3964
771081 feet/sec YDOT = -1208
462225 meter/sec
ZDOT = 16164
524254 ZDOT = 4926
946993
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 18105
50625314
00016717 00000-0 10270-3 0 9042
2 25544 51
6410 331
1956 0002430 344
0386 16
0689 15
54265417 28767
Satellite: ISS
Catalog Number: 25544
Epoch time: 18105
50625314 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 331
1956 deg
Eccentricity:
0002430
Arg of perigee: 344
0386 deg
Mean anomaly: 16
0689 deg
Mean motion: 15
54265417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2876
Checksum: 293
Coasting Arc #6 (Orbit 2891)
---------------------------------------
Vector Time (GMT): 2018/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4714288
28 A = 6788024
16 meter
Y = 4649539
09 meter E =
0012440
Z = 1472160
46 I = 51
44773
XDOT = -4355
358338 Wp = 109
78461
YDOT = -2581
023805 meter/sec RA = 325
60197 deg
ZDOT = -5759
876224 TA = 54
10292
MA = 53
98750
Ha = 220
823 n
mi
Hp = 214
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15466825
05 X = -4773081
42
Y = 15254393
32 feet Y = 4596492
04 meter
Z = 4829922
78 Z = 1449116
55
XDOT = -14289
233392 XDOT = -4298
194003
YDOT = -8467
925871 feet/sec YDOT = -2629
409220 meter/sec
ZDOT = -18897
231707 ZDOT = -5780
894371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8056160
86 X = -2455517
83
Y = 20199166
02 feet Y = 6156705
80 meter
Z = 4726448
08 Z = 1440621
37
XDOT = -14901
185538 XDOT = -4541
881352
YDOT = -1471
575952 feet/sec YDOT = -448
536350 meter/sec
ZDOT = -18990
562914 ZDOT = -5788
323576
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 18106
53499223
00016717 00000-0 10270-3 0 9055
2 25544 51
6415 326
0658 0002456 349
4935 10
6166 15
54275282 28920
Satellite: ISS
Catalog Number: 25544
Epoch time: 18106
53499223 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 326
0658 deg
Eccentricity:
0002456
Arg of perigee: 349
4935 deg
Mean anomaly: 10
6166 deg
Mean motion: 15
54275282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2892
Checksum: 319
Coasting Arc #7 (Orbit 2907)
---------------------------------------
Vector Time (GMT): 2018/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5367273
10 A = 6788831
63 meter
Y = -4136126
91 meter E =
0014173
Z = 261789
77 I = 51
42239
XDOT = 2733
624020 Wp = 39
68801
YDOT = 3937
082243 meter/sec RA = 320
61549 deg
ZDOT = 5989
512159 TA = 323
14256
MA = 323
23990
Ha = 220
834 n
mi
Hp = 214
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17609163
72 X = 5411853
83
Y = -13569970
18 feet Y = -4075857
09 meter
Z = 858890
32 Z = 287971
12
XDOT = 8968
582742 XDOT = 2660
300871
YDOT = 12916
936492 feet/sec YDOT = 3967
241852 meter/sec
ZDOT = 19650
630444 ZDOT = 6002
613109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10323661
67 X = 3146652
08
Y = -19683326
43 feet Y = -5999477
89 meter
Z = 976268
72 Z = 297566
71
XDOT = 11992
162898 XDOT = 3655
211251
YDOT = 7291
411723 feet/sec YDOT = 2222
422293 meter/sec
ZDOT = 19708
446353 ZDOT = 6007
134449
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 18107
56372568
00016717 00000-0 10270-3 0 9062
2 25544 51
6398 320
9352 0002466 352
6101 7
5015 15
54288165 29086
Satellite: ISS
Catalog Number: 25544
Epoch time: 18107
56372568 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 320
9352 deg
Eccentricity:
0002466
Arg of perigee: 352
6101 deg
Mean anomaly: 7
5015 deg
Mean motion: 15
54288165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2908
Checksum: 312
Coasting Arc #8 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2018/108/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4985398
99 A = 6780254
26 meter
Y = -286255
75 meter E =
0010546
Z = -4597021
32 I = 51
36928
XDOT = 3113
092443 Wp = 57
39504
YDOT = -6331
296472 meter/sec RA = 315
92000 deg
ZDOT = -2981
286285 TA = 182
71679
MA = 182
72252
Ha = 220
878 n
mi
Hp = 214
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16356295
90 X = -4959497
14
Y = -939159
27 feet Y = -341861
23 meter
Z = -15082090
94 Z = -4621176
20
XDOT = 10213
557885 XDOT = 3198
141149
YDOT = -20771
970052 feet/sec YDOT = -6296
008286 meter/sec
ZDOT = -9781
122982 ZDOT = -2965
956902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16277023
76 X = -4961236
84
Y = 458049
46 feet Y = 139613
48 meter
Z = -15189752
83 Z = -4629836
66
XDOT = 8490
972815 XDOT = 2588
048514
YDOT = -20391
110203 feet/sec YDOT = -6215
210390 meter/sec
ZDOT = -9711
804037 ZDOT = -2960
157870
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 18108
46386708
00016717 00000-0 10270-3 0 9074
2 25544 51
6402 316
4479 0002263 339
4819 20
6242 15
54130189 29222
Satellite: ISS
Catalog Number: 25544
Epoch time: 18108
46386708 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 316
4479 deg
Eccentricity:
0002263
Arg of perigee: 339
4819 deg
Mean anomaly: 20
6242 deg
Mean motion: 15
54130189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 310
Coasting Arc #9 (Orbit 2937)
---------------------------------------
Vector Time (GMT): 2018/109/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4005664
88 A = 6777797
49 meter
Y = 1716193
21 meter E =
0002635
Z = 5188843
11 I = 51
33884
XDOT = -4217
236139 Wp = 89
50193
YDOT = 6299
402067 meter/sec RA = 310
90356 deg
ZDOT = 1171
606413 TA = 349
21531
MA = 349
22096
Ha = 220
827 n
mi
Hp = 214
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13141945
13 X = 3960971
13
Y = 5630555
15 feet Y = 1760737
46 meter
Z = 17023763
49 Z = 5208193
00
XDOT = -13836
076571 XDOT = -4293
055478
YDOT = 20667
329615 feet/sec YDOT = 6251
818108 meter/sec
ZDOT = 3843
853061 ZDOT = 1150
935985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13539682
43 X = 4126895
21
Y = 4260840
03 feet Y = 1298704
04 meter
Z = 17109781
94 Z = 5215061
54
XDOT = -11349
442953 XDOT = -3459
310212
YDOT = 20997
295037 feet/sec YDOT = 6399
975527 meter/sec
ZDOT = 3750
729482 ZDOT = 1143
222346
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 18109
49269903
00016717 00000-0 10270-3 0 9086
2 25544 51
6410 311
3188 0002257 344
3626 15
7456 15
54121727 29383
Satellite: ISS
Catalog Number: 25544
Epoch time: 18109
49269903 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 311
3188 deg
Eccentricity:
0002257
Arg of perigee: 344
3626 deg
Mean anomaly: 15
7456 deg
Mean motion: 15
54121727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2938
Checksum: 313
Coasting Arc #10 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2018/110/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2901693
04 A = 6777485
63 meter
Y = -3167023
84 meter E =
0013952
Z = -5254573
99 I = 51
31634
XDOT = 4947
275098 Wp = 86
79132
YDOT = -5795
894749 meter/sec RA = 305
88016 deg
ZDOT = 763
818325 TA = 190
53460
MA = 190
56386
Ha = 220
938 n
mi
Hp = 214
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9519990
30 X = -2840538
58
Y = -10390498
16 feet Y = -3199130
59 meter
Z = -17239415
97 Z = -5268521
08
XDOT = 16231
217513 XDOT = 5008
008406
YDOT = -19015
402719 feet/sec YDOT = -5740
231339 meter/sec
ZDOT = 2505
965634 ZDOT = 787
998253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10585189
70 X = -3226365
82
Y = -9187757
24 feet Y = -2800428
41 meter
Z = -17301127
31 Z = -5273383
60
XDOT = 13144
735610 XDOT = 4006
515414
YDOT = -20052
019985 feet/sec YDOT = -6111
855691 meter/sec
ZDOT = 2614
655184 ZDOT = 796
946900
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 18110
45722297
00016717 00000-0 10270-3 0 9095
2 25544 51
6401 306
5090 0002330 346
9185 13
1907 15
54156145 29533
Satellite: ISS
Catalog Number: 25544
Epoch time: 18110
45722297 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 306
5090 deg
Eccentricity:
0002330
Arg of perigee: 346
9185 deg
Mean anomaly: 13
1907 deg
Mean motion: 15
54156145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 292
Coasting Arc #11 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2018/111/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1736818
12 A = 6779580
39 meter
Y = 4511478
71 meter E =
0008571
Z = 4750324
22 I = 51
30484
XDOT = -5342
460107 Wp = 46
21745
YDOT = 4834
605142 meter/sec RA = 300
86030 deg
ZDOT = -2629
402049 TA = 69
88377
MA = 69
79157
Ha = 220
910 n
mi
Hp = 214
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5698222
19 X = 1663165
69
Y = 14801439
34 feet Y = 4530489
13 meter
Z = 15585053
22 Z = 4758582
32
XDOT = -17527
756256 XDOT = -5383
352562
YDOT = 15861
565428 feet/sec YDOT = 4774
633467 meter/sec
ZDOT = -8626
647142 ZDOT = -2655
453344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7571551
01 X = 2307808
75
Y = 13895893
90 feet Y = 4235468
46 meter
Z = 15621202
72 Z = 4761342
59
XDOT = -14117
793570 XDOT = -4303
103480
YDOT = 17553
980129 feet/sec YDOT = 5350
453143 meter/sec
ZDOT = -8743
530165 ZDOT = -2665
027994
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 18111
48604546
00016717 00000-0 10270-3 0 9107
2 25544 51
6399 301
3808 0002375 348
6146 11
4953 15
54171792 29698
Satellite: ISS
Catalog Number: 25544
Epoch time: 18111
48604546 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 301
3808 deg
Eccentricity:
0002375
Arg of perigee: 348
6146 deg
Mean anomaly: 11
4953 deg
Mean motion: 15
54171792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 319
Coasting Arc #12 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2018/112/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -638292
87 A = 6783210
91 meter
Y = -5606781
51 meter E =
0005522
Z = -3768022
55 I = 51
30001
XDOT = 5407
323982 Wp = 80
09264
YDOT = -3436
779771 meter/sec RA = 295
84615 deg
ZDOT = 4204
118393 TA = 234
54626
MA = 234
59781
Ha = 220
985 n
mi
Hp = 214
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2094136
71 X = -557245
72
Y = -18394952
46 feet Y = -5613466
16 meter
Z = -12362278
71 Z = -3770926
35
XDOT = 17740
564244 XDOT = 5424
931630
YDOT = -11275
524183 feet/sec YDOT = -3376
212925 meter/sec
ZDOT = 13793
039347 ZDOT = 4230
428158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4823285
11 X = -1470137
30
Y = -17866049
55 feet Y = -5445571
90 meter
Z = -12374401
55 Z = -3771717
59
XDOT = 14397
922091 XDOT = 4388
486653
YDOT = -13507
856706 feet/sec YDOT = -4117
194724 meter/sec
ZDOT = 13910
861497 ZDOT = 4240
030584
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 18112
45056466
00016717 00000-0 10270-3 0 9118
2 25544 51
6390 296
5719 0002283 350
9319 9
1792 15
54158723 29842
Satellite: ISS
Catalog Number: 25544
Epoch time: 18112
45056466 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 296
5719 deg
Eccentricity:
0002283
Arg of perigee: 350
9319 deg
Mean anomaly: 9
1792 deg
Mean motion: 15
54158723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 324
Coasting Arc #13 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2018/113/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -394139
35 A = 6786756
93 meter
Y = 6346415
01 meter E =
0013050
Z = 2358580
69 I = 51
29927
XDOT = -5228
200355 Wp = 96
12534
YDOT = 1674
474637 meter/sec RA = 290
84174 deg
ZDOT = -5355
085554 TA = 57
41165
MA = 57
28572
Ha = 221
015 n
mi
Hp = 214
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1293108
09 X = -476534
16
Y = 20821571
55 feet Y = 6341546
80 meter
Z = 7738125
62 Z = 2356465
90
XDOT = -17152
888305 XDOT = -5220
523986
YDOT = 5493
683193 feet/sec YDOT = 1616
052162 meter/sec
ZDOT = -17569
178328 ZDOT = -5380
463761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2237843
89 X = 682094
82
Y = 20745170
25 feet Y = 6323127
89 meter
Z = 7727776
14 Z = 2355426
17
XDOT = -14332
859953 XDOT = -4368
655714
YDOT = 8162
714783 feet/sec YDOT = 2487
995466 meter/sec
ZDOT = -17682
584860 ZDOT = -5389
651865
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 18113
47937818
00016717 00000-0 10270-3 0 9121
2 25544 51
6394 291
4425 0002557 354
5835 5
5289 15
54204974 30002
Satellite: ISS
Catalog Number: 25544
Epoch time: 18113
47937818 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 291
4425 deg
Eccentricity:
0002557
Arg of perigee: 354
5835 deg
Mean anomaly: 5
5289 deg
Mean motion: 15
54204974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 317
Coasting Arc #14 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2018/114/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1270994
28 A = 6789016
37 meter
Y = -6622379
62 meter E =
0012331
Z = -730521
32 I = 51
29341
XDOT = 4857
487041 Wp = 33
11387
YDOT = 284
657489 meter/sec RA = 285
84457 deg
ZDOT = 5928
384495 TA = 318
95295
MA = 319
04568
Ha = 221
117 n
mi
Hp = 214
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4169928
75 X = 1348501
57
Y = -21726967
26 feet Y = -6607733
14 meter
Z = -2396723
48 Z = -724158
80
XDOT = 15936
637275 XDOT = 4825
145888
YDOT = 933
915647 feet/sec YDOT = 338
796608 meter/sec
ZDOT = 19450
080364 ZDOT = 5951
901964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 26297
33 X = 8015
43
Y = -22126644
05 feet Y = -6744201
11 meter
Z = -2367409
35 Z = -721586
37
XDOT = 14088
236649 XDOT = 4294
094531
YDOT = -2055
034203 feet/sec YDOT = -626
374425 meter/sec
ZDOT = 19554
907298 ZDOT = 5960
335744
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 18114
44388981
00016717 00000-0 10270-3 0 9131
2 25544 51
6372 286
6337 0002287
2560 359
8593 15
54159719 30151
Satellite: ISS
Catalog Number: 25544
Epoch time: 18114
44388981 = yrday
fracday
Element set: 913
Inclination: 51
6372 deg
RA of node: 286
6337 deg
Eccentricity:
0002287
Arg of perigee:
2560 deg
Mean anomaly: 359
8593 deg
Mean motion: 15
54159719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 326
Coasting Arc #15 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2018/115/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2050128
49 A = 6788697
50 meter
Y = 6389427
85 meter E =
0008061
Z = -1011392
30 I = 51
28454
XDOT = -4348
050968 Wp = 129
68015
YDOT = -2318
830646 meter/sec RA = 280
85014 deg
ZDOT = -5871
822566 TA = 61
33171
MA = 61
25069
Ha = 221
147 n
mi
Hp = 214
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6726143
34 X = -2116511
62
Y = 20962689
78 feet Y = 6366130
68 meter
Z = -3318216
22 Z = -1021512
69
XDOT = -14265
259082 XDOT = -4293
275688
YDOT = -7607
712094 feet/sec YDOT = -2367
147557 meter/sec
ZDOT = -19264
509731 ZDOT = -5892
810819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2267326
09 X = -691080
99
Y = 21891255
33 feet Y = 6672454
63 meter
Z = -3364238
15 Z = -1025419
79
XDOT = -13800
315447 XDOT = -4206
336148
YDOT = -4386
139607 feet/sec YDOT = -1336
895352 meter/sec
ZDOT = -19357
774740 ZDOT = -5900
249741
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 18115
47269698
00016717 00000-0 10270-3 0 9149
2 25544 51
6370 281
5045 0002417 4
1236 355
9936 15
54191078 30317
Satellite: ISS
Catalog Number: 25544
Epoch time: 18115
47269698 = yrday
fracday
Element set: 914
Inclination: 51
6370 deg
RA of node: 281
5045 deg
Eccentricity:
0002417
Arg of perigee: 4
1236 deg
Mean anomaly: 355
9936 deg
Mean motion: 15
54191078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 310
Coasting Arc #16 (Orbit 3045)
---------------------------------------
Vector Time (GMT): 2018/116/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2685716
60 A = 6786213
53 meter
Y = -5648535
47 meter E =
0014510
Z = 2613526
97 I = 51
27076
XDOT = 3762
008049 Wp = 69
12051
YDOT = 4203
498575 meter/sec RA = 275
84985 deg
ZDOT = 5200
624492 TA = 320
49854
MA = 320
60422
Ha = 221
109 n
mi
Hp = 214
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8811406
17 X = 2735985
23
Y = -18531940
50 feet Y = -5618220
72 meter
Z = 8574563
54 Z = 2626695
76
XDOT = 12342
546091 XDOT = 3689
461703
YDOT = 13791
005822 feet/sec YDOT = 4245
162602 meter/sec
ZDOT = 17062
416311 ZDOT = 5218
722713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4428821
00 X = 1349904
64
Y = -20010880
99 feet Y = -6099316
53 meter
Z = 8634061
85 Z = 2631662
05
XDOT = 13523
443623 XDOT = 4121
945616
YDOT = 10415
273711 feet/sec YDOT = 3174
575427 meter/sec
ZDOT = 17142
540130 ZDOT = 5225
046232
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 18116
50149958
00016717 00000-0 10270-3 0 9151
2 25544 51
6367 276
3741 0002202 8
1942 351
9246 15
54190719 30465
Satellite: ISS
Catalog Number: 25544
Epoch time: 18116
50149958 = yrday
fracday
Element set: 915
Inclination: 51
6367 deg
RA of node: 276
3741 deg
Eccentricity:
0002202
Arg of perigee: 8
1942 deg
Mean anomaly: 351
9246 deg
Mean motion: 15
54190719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3046
Checksum: 310
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