[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 13th 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 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
072/21:25:54
220 -0
5 0
7 0
7
N/A 0
4 -0
1 220
9
000/00:01:48
441 0
2 0
0 215
0
073/06:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
0
077/07:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
2
080/17:44:26
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
3
082/19:41:05
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
3
086/11:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2018/071/12:41:31
826
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5824224
43 A = 6786009
82 meter
Y = -2163489
82 meter E =
0006534
Z = -2725028
10 I = 51
89132
XDOT = -329
592028 Wp = 141
97586
YDOT = 5633
456628 meter/sec RA = 139
50038 deg
ZDOT = -5188
644690 TA = 68
71945
MA = 68
64970
Ha = 221
117 n
mi
Hp = 214
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19108347
87 X = 5861220
86
Y = -7098063
73 feet Y = -2098152
72 meter
Z = -8940380
92 Z = -2696646
40
XDOT = -1081
338675 XDOT = -367
359026
YDOT = 18482
469251 feet/sec YDOT = 5629
559287 meter/sec
ZDOT = -17023
112501 ZDOT = -5190
337925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19213048
04 X = 5856137
04
Y = -6973021
27 feet Y = -2125376
88 meter
Z = -8813491
78 Z = -2686352
29
XDOT = -1598
488668 XDOT = -487
219346
YDOT = 17073
352804 feet/sec YDOT = 5203
957935 meter/sec
ZDOT = -17031
327153 ZDOT = -5191
148516
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 18071
55561011
00016717 00000-0 10270-3 0 9008
2 25544 51
6398 140
4475 0002340 179
8036 180
3120 15
54216654 23483
Satellite: ISS
Catalog Number: 25544
Epoch time: 18071
55561011 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 140
4475 deg
Eccentricity:
0002340
Arg of perigee: 179
8036 deg
Mean anomaly: 180
3120 deg
Mean motion: 15
54216654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 285
Coasting Arc #2 (Orbit 2363)
---------------------------------------
Vector Time (GMT): 2018/072/12:41:31
826
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5358226
35 A = 6782200
48 meter
Y = 919065
81 meter E =
0011332
Z = 4049409
17 I = 51
90263
XDOT = 1893
420415 Wp = 113
70564
YDOT = -6311
888126 meter/sec RA = 134
53549 deg
ZDOT = 3924
853517 TA = 295
67641
MA = 295
79340
Ha = 221
059 n
mi
Hp = 214
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17579482
76 X = -5387774
96
Y = 3015307
79 feet Y = 858981
62 meter
Z = 13285463
16 Z = 4023309
31
XDOT = 6212
009235 XDOT = 1944
796359
YDOT = -20708
294375 feet/sec YDOT = -6290
426951 meter/sec
ZDOT = 12876
816001 ZDOT = 3934
176356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17633677
05 X = -5374744
76
Y = 3204317
53 feet Y = 976675
98 meter
Z = 13168887
94 Z = 4013877
04
XDOT = 6139
650501 XDOT = 1871
365473
YDOT = -19485
493596 feet/sec YDOT = -5939
178448 meter/sec
ZDOT = 12919
162009 ZDOT = 3937
760580
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 18072
58438288
00016717 00000-0 10270-3 0 9012
2 25544 51
6394 135
3187 0002359 185
4102 174
7025 15
54229687 23648
Satellite: ISS
Catalog Number: 25544
Epoch time: 18072
58438288 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 135
3187 deg
Eccentricity:
0002359
Arg of perigee: 185
4102 deg
Mean anomaly: 174
7025 deg
Mean motion: 15
54229687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2364
Checksum: 324
Coasting Arc #3 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2018/072/21:26:48
441
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1149860
75 A = 6779064
71 meter
Y = 4489022
60 meter E =
0012256
Z = -4959301
71 I = 51
90046
XDOT = -6110
692986 Wp = 115
63067
YDOT = 4038
259760 meter/sec RA = 132
68185 deg
ZDOT = 2237
639786 TA = 176
16829
MA = 176
15890
Ha = 220
890 n
mi
Hp = 215
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3772509
02 X = 1123667
13
Y = 14727764
44 feet Y = 4501734
16 meter
Z = -16270674
90 Z = -4953780
25
XDOT = -20048
205336 XDOT = -6166
264856
YDOT = 13248
883726 feet/sec YDOT = 3969
615298 meter/sec
ZDOT = 7341
337880 ZDOT = 2207
821229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8283455
32 X = 2524797
18
Y = -12779170
24 feet Y = -3895091
09 meter
Z = -16246566
01 Z = -4951953
32
XDOT = 22391
701417 XDOT = 6824
990592
YDOT = 5347
206619 feet/sec YDOT = 1629
828577 meter/sec
ZDOT = 7207
794767 ZDOT = 2196
935845
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 18072
90587547
00016717 00000-0 10270-3 0 9022
2 25544 51
6405 133
7168 0001980 203
8504 156
2557 15
54091094 23691
Satellite: ISS
Catalog Number: 25544
Epoch time: 18072
90587547 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 133
7168 deg
Eccentricity:
0001980
Arg of perigee: 203
8504 deg
Mean anomaly: 156
2557 deg
Mean motion: 15
54091094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 317
Coasting Arc #4 (Orbit 2374)
---------------------------------------
Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -571624
66 A = 6782697
77 meter
Y = 5458562
84 meter E =
0007182
Z = -3993528
98 I = 51
92056
XDOT = -6114
755741 Wp = 127
69407
YDOT = 2290
055504 meter/sec RA = 130
73635 deg
ZDOT = 4006
061352 TA = 183
93593
MA = 183
94159
Ha = 220
949 n
mi
Hp = 215
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1875408
98 X = -613223
14
Y = 17908670
73 feet Y = 5451937
51 meter
Z = -13102129
19 Z = -3996407
32
XDOT = -20061
534583 XDOT = -6159
368343
YDOT = 7513
305458 feet/sec YDOT = 2221
427093 meter/sec
ZDOT = 13143
245905 ZDOT = 3976
249845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17974379
22 X = -5478590
79
Y = -897554
37 feet Y = -273574
57 meter
Z = -13115621
34 Z = -3997641
38
XDOT = -8570
842647 XDOT = -2612
392839
YDOT = -18439
217445 feet/sec YDOT = -5620
273477 meter/sec
ZDOT = 13009
935411 ZDOT = 3965
428313
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 18073
29169693
00016717 00000-0 10270-3 0 9034
2 25544 51
6399 131
7894 0002445 201
1374 158
9678 15
54082045 23756
Satellite: ISS
Catalog Number: 25544
Epoch time: 18073
29169693 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 131
7894 deg
Eccentricity:
0002445
Arg of perigee: 201
1374 deg
Mean anomaly: 158
9678 deg
Mean motion: 15
54082045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2375
Checksum: 334
Coasting Arc #5 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1749961
65 A = 6786450
39 meter
Y = -5986116
80 meter E =
0013342
Z = 2657482
96 I = 51
95362
XDOT = 5561
244373 Wp = 112
82091
YDOT = -706
477059 meter/sec RA = 125
77491 deg
ZDOT = -5237
658229 TA = 37
32628
MA = 37
23365
Ha = 220
943 n
mi
Hp = 215
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5741344
01 X = 1803861
51
Y = -19639490
81 feet Y = -5966245
82 meter
Z = 8718776
12 Z = 2666115
20
XDOT = 18245
552406 XDOT = 5594
172489
YDOT = -2317
838121 feet/sec YDOT = -644
103938 meter/sec
ZDOT = -17183
918075 ZDOT = -5210
563964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19974711
33 X = 6088292
01
Y = 4358638
85 feet Y = 1328513
12 meter
Z = 8758017
02 Z = 2669443
59
XDOT = 3858
589426 XDOT = 1176
098057
YDOT = 16706
012567 feet/sec YDOT = 5091
992630 meter/sec
ZDOT = -17062
911180 ZDOT = -5200
775328
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 18074
32055355
00016717 00000-0 10270-3 0 9049
2 25544 51
6398 126
6607 0002455 202
2631 157
8415 15
54079723 23913
Satellite: ISS
Catalog Number: 25544
Epoch time: 18074
32055355 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 126
6607 deg
Eccentricity:
0002455
Arg of perigee: 202
2631 deg
Mean anomaly: 157
8415 deg
Mean motion: 15
54079723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 306
Coasting Arc #6 (Orbit 2405)
---------------------------------------
Vector Time (GMT): 2018/075/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2685951
40 A = 6788927
17 meter
Y = 6138772
67 meter E =
0007202
Z = -1073076
09 I = 51
98043
XDOT = -4758
755822 Wp = 42
28179
YDOT = -1052
782868 meter/sec RA = 120
82395 deg
ZDOT = 5916
855208 TA = 306
13895
MA = 306
20558
Ha = 220
841 n
mi
Hp = 215
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8812176
52 X = -2749184
83
Y = 20140330
28 feet Y = 6108382
80 meter
Z = -3520590
86 Z = -1086277
77
XDOT = -15612
715953 XDOT = -4775
370258
YDOT = -3454
012034 feet/sec YDOT = -1106
090637 meter/sec
ZDOT = 19412
254619 ZDOT = 5893
698898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20806954
21 X = -6341959
64
Y = -7066424
67 feet Y = -2153846
24 meter
Z = -3580253
82 Z = -1091261
36
XDOT = 1603
204901 XDOT = 488
656854
YDOT = -14457
592832 feet/sec YDOT = -4406
674295 meter/sec
ZDOT = 19309
027708 ZDOT = 5885
391645
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 18075
28510436
00016717 00000-0 10270-3 0 9052
2 25544 51
6398 121
8531 0002351 206
7467 153
3565 15
54091542 24064
Satellite: ISS
Catalog Number: 25544
Epoch time: 18075
28510436 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 121
8531 deg
Eccentricity:
0002351
Arg of perigee: 206
7467 deg
Mean anomaly: 153
3565 deg
Mean motion: 15
54091542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2406
Checksum: 300
Coasting Arc #7 (Orbit 2421)
---------------------------------------
Vector Time (GMT): 2018/076/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3397012
60 A = 6789218
12 meter
Y = -5834466
00 meter E =
0011683
Z = -652590
53 I = 51
99747
XDOT = 3810
742185 Wp = 150
82090
YDOT = 2883
557058 meter/sec RA = 115
87785 deg
ZDOT = -5998
753538 TA = 36
19238
MA = 36
11338
Ha = 220
786 n
mi
Hp = 215
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11145054
48 X = 3465172
63
Y = -19141948
81 feet Y = -5796097
25 meter
Z = -2141045
05 Z = -635922
78
XDOT = 12502
434991 XDOT = 3807
352779
YDOT = 9460
489034 feet/sec YDOT = 2926
151583 meter/sec
ZDOT = -19680
949927 ZDOT = -5980
251085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20172234
45 X = 6148497
06
Y = 9166426
67 feet Y = 2793926
85 meter
Z = -2065937
33 Z = -629697
70
XDOT = -7464
922434 XDOT = -2275
308358
YDOT = 12052
719642 feet/sec YDOT = 3673
668947 meter/sec
ZDOT = -19598
715241 ZDOT = -5973
688405
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 18076
31395644
00016717 00000-0 10270-3 0 9060
2 25544 51
6398 116
7243 0002396 211
4561 148
6448 15
54108960 24222
Satellite: ISS
Catalog Number: 25544
Epoch time: 18076
31395644 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 116
7243 deg
Eccentricity:
0002396
Arg of perigee: 211
4561 deg
Mean anomaly: 148
6448 deg
Mean motion: 15
54108960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2422
Checksum: 316
Coasting Arc #8 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/077/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3856274
06 A = 6787196
33 meter
Y = 5090875
83 meter E =
0012164
Z = 2282824
37 I = 52
00494
XDOT = -2812
711747 Wp = 78
68574
YDOT = -4589
882559 meter/sec RA = 110
93008 deg
ZDOT = 5462
170655 TA = 306
59833
MA = 306
71018
Ha = 220
736 n
mi
Hp = 215
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12651817
78 X = -3924003
72
Y = 16702348
51 feet Y = 5047373
95 meter
Z = 7489581
25 Z = 2263926
77
XDOT = -9228
056914 XDOT = -2787
709617
YDOT = -15058
669814 feet/sec YDOT = -4621
195649 meter/sec
ZDOT = 17920
507399 ZDOT = 5448
568932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18087109
61 X = -5512951
01
Y = -10637628
24 feet Y = -3242349
09 meter
Z = 7404599
76 Z = 2256922
01
XDOT = 13071
285258 XDOT = 3984
127747
YDOT = -9741
512261 feet/sec YDOT = -2969
212937 meter/sec
ZDOT = 17860
360721 ZDOT = 5443
837948
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 18077
34280516
00016717 00000-0 10270-3 0 9076
2 25544 51
6406 111
5956 0002267 213
6166 146
4843 15
54120375 24384
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
34280516 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 111
5956 deg
Eccentricity:
0002267
Arg of perigee: 213
6166 deg
Mean anomaly: 146
4843 deg
Mean motion: 15
54120375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 304
Coasting Arc #9 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/077/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2749613
99 A = 6778955
27 meter
Y = 3717705
09 meter E =
0011769
Z = -4967935
26 I = 51
97826
XDOT = -4142
106222 Wp = 116
44744
YDOT = 6044
306570 meter/sec RA = 110
65858 deg
ZDOT = 2229
634305 TA = 175
24491
MA = 175
23372
Ha = 220
646 n
mi
Hp = 215
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9021043
28 X = 2731968
76
Y = 12197195
19 feet Y = 3748353
79 meter
Z = -16299000
20 Z = -4954622
05
XDOT = -13589
587342 XDOT = -4220
217795
YDOT = 19830
402131 feet/sec YDOT = 5997
550262 meter/sec
ZDOT = 7315
073180 ZDOT = 2209
322885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7437897
71 X = -2267071
22
Y = 13294629
53 feet Y = 4052203
08 meter
Z = -16240033
97 Z = -4949962
35
XDOT = -22690
875800 XDOT = -6916
178944
YDOT = -3866
617007 feet/sec YDOT = -1178
544864 meter/sec
ZDOT = 7223
662340 ZDOT = 2201
772281
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 18077
34280499
00016717 00000-0 10270-3 0 9087
2 25544 51
6407 111
5971 0002213 216
4852 143
6150 15
54130979 24387
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
34280499 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 111
5971 deg
Eccentricity:
0002213
Arg of perigee: 216
4852 deg
Mean anomaly: 143
6150 deg
Mean motion: 15
54130979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 308
Coasting Arc #10 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2018/078/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1885180
97 A = 6782350
16 meter
Y = -5074064
22 meter E =
0009018
Z = 4079332
97 I = 51
99967
XDOT = 4518
121437 Wp = 85
79134
YDOT = -4819
761689 meter/sec RA = 105
69044 deg
ZDOT = -3899
047401 TA = 44
41156
MA = 44
33928
Ha = 220
695 n
mi
Hp = 215
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6184976
95 X = -1848116
55
Y = -16647192
31 feet Y = -5094937
80 meter
Z = 13383638
34 Z = 4070266
14
XDOT = 14823
233061 XDOT = 4590
621045
YDOT = -15812
866435 feet/sec YDOT = -4768
832120 meter/sec
ZDOT = -12792
150265 ZDOT = -3876
923178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12447392
71 X = 3793965
30
Y = -12708660
31 feet Y = -3873599
66 meter
Z = 13343803
61 Z = 4067191
34
XDOT = 19699
145630 XDOT = 6004
299588
YDOT = 5939
256338 feet/sec YDOT = 1810
285332 meter/sec
ZDOT = -12692
786438 ZDOT = -3868
761306
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 18078
37165260
00016717 00000-0 10270-3 0 9090
2 25544 51
6402 106
4684 0002150 221
0144 139
0847 15
54113958 24540
Satellite: ISS
Catalog Number: 25544
Epoch time: 18078
37165260 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 106
4684 deg
Eccentricity:
0002150
Arg of perigee: 221
0144 deg
Mean anomaly: 139
0847 deg
Mean motion: 15
54113958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 294
Coasting Arc #11 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2018/079/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1061138
08 A = 6786140
46 meter
Y = 6095061
81 meter E =
0002561
Z = -2789289
94 I = 52
01969
XDOT = -4698
368297 Wp = 68
91425
YDOT = 3175
029201 meter/sec RA = 100
73316 deg
ZDOT = 5155
248770 TA = 259
65704
MA = 259
68590
Ha = 220
536 n
mi
Hp = 215
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3481424
16 X = 1006451
53
Y = 19996921
95 feet Y = 6106622
06 meter
Z = -9151213
71 Z = -2784268
88
XDOT = -15414
594149 XDOT = -4758
564715
YDOT = 10416
762469 feet/sec YDOT = 3122
152891 meter/sec
ZDOT = 16913
545833 ZDOT = 5132
279039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16434154
14 X = -5009130
18
Y = 11929427
83 feet Y = 3636089
60 meter
Z = -9129580
68 Z = -2782696
19
XDOT = -15288
661135 XDOT = -4659
983914
YDOT = -8208
564069 feet/sec YDOT = -2501
970328 meter/sec
ZDOT = 16810
604298 ZDOT = 5123
872190
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 18079
33619486
00016717 00000-0 10270-3 0 9103
2 25544 51
6399 101
6604 0002260 228
5363 131
5596 15
54095447 24697
Satellite: ISS
Catalog Number: 25544
Epoch time: 18079
33619486 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 101
6604 deg
Eccentricity:
0002260
Arg of perigee: 228
5363 deg
Mean anomaly: 131
5596 deg
Mean motion: 15
54095447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 324
Coasting Arc #12 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2018/080/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -254345
24 A = 6788774
21 meter
Y = -6672169
39 meter E =
0013201
Z = 1186184
49 I = 52
03408
XDOT = 4749
233006 Wp = 130
73632
YDOT = -1235
280200 meter/sec RA = 95
78532 deg
ZDOT = -5895
629146 TA = 36
44509
MA = 36
35530
Ha = 220
533 n
mi
Hp = 215
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -834466
01 X = -185478
21
Y = -21890319
51 feet Y = -6674628
46 meter
Z = 3891681
40 Z = 1185116
96
XDOT = 15581
473116 XDOT = 4791
331290
YDOT = -4052
756562 feet/sec YDOT = -1181
936268 meter/sec
ZDOT = -19342
615309 ZDOT = -5872
456511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19129126
13 X = 5830557
64
Y = -10676574
64 feet Y = -3254219
95 meter
Z = 3887787
70 Z = 1184997
69
XDOT = 9947
871027 XDOT = 3032
111089
YDOT = 10776
701934 feet/sec YDOT = 3284
738749 meter/sec
ZDOT = -19239
010112 ZDOT = -5864
050282
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 18080
36503781
00016717 00000-0 10270-3 0 9119
2 25544 51
6402 96
5317 0002092 230
3897 129
7071 15
54115616 24857
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
36503781 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 96
5317 deg
Eccentricity:
0002092
Arg of perigee: 230
3897 deg
Mean anomaly: 129
7071 deg
Mean motion: 15
54115616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 300
Coasting Arc #13 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2018/080/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3597618
96 A = 6779477
04 meter
Y = 3090369
80 meter E =
0010480
Z = -4854322
62 I = 52
00368
XDOT = -2429
724838 Wp = 115
07891
YDOT = 6808
102458 meter/sec RA = 93
75150 deg
ZDOT = 2533
428601 TA = 179
73701
MA = 179
73646
Ha = 220
487 n
mi
Hp = 215
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11803211
81 X = 3586374
10
Y = 10139008
53 feet Y = 3130537
49 meter
Z = -15926255
31 Z = -4836874
16
XDOT = -7971
538183 XDOT = -2517
980440
YDOT = 22336
294154 feet/sec YDOT = 6780
438392 meter/sec
ZDOT = 8311
773625 ZDOT = 2521
410730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11246080
45 X = 3427805
32
Y = -10867522
79 feet Y = -3312420
95 meter
Z = -15848770
75 Z = -4830705
32
XDOT = 20659
629204 XDOT = 6297
054981
YDOT = 9337
017662 feet/sec YDOT = 2845
922983 meter/sec
ZDOT = 8257
227483 ZDOT = 2516
802937
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 18080
75085406
00016717 00000-0 10270-3 0 9122
2 25544 51
6395 94
6095 0001758 240
2793 119
8185 15
54120383 24913
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
75085406 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 94
6095 deg
Eccentricity:
0001758
Arg of perigee: 240
2793 deg
Mean anomaly: 119
8185 deg
Mean motion: 15
54120383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 319
Coasting Arc #14 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2018/081/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3129608
83 A = 6783039
53 meter
Y = -4591365
49 meter E =
0009612
Z = 3882786
70 I = 52
01671
XDOT = 3121
629951 Wp = 84
77487
YDOT = -5645
513522 meter/sec RA = 88
78737 deg
ZDOT = -4150
025046 TA = 48
61339
MA = 48
53079
Ha = 220
549 n
mi
Hp = 215
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10267745
50 X = -3096894
95
Y = -15063535
06 feet Y = -4626179
70 meter
Z = 12738801
52 Z = 3867663
90
XDOT = 10241
568081 XDOT = 3204
686340
YDOT = -18522
025992 feet/sec YDOT = -5610
141244 meter/sec
ZDOT = -13615
567735 ZDOT = -4134
659000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15842029
17 X = -4828650
49
Y = 9114090
87 feet Y = 2777974
90 meter
Z = 12671906
31 Z = 3862397
04
XDOT = -16973
083310 XDOT = -5173
395793
YDOT = -10624
034208 feet/sec YDOT = -3238
205627 meter/sec
ZDOT = -13546
210417 ZDOT = -4128
884935
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 18081
77969418
00016717 00000-0 10270-3 0 9130
2 25544 51
6396 89
4818 0001779 244
3342 115
7627 15
54114599 25073
Satellite: ISS
Catalog Number: 25544
Epoch time: 18081
77969418 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 89
4818 deg
Eccentricity:
0001779
Arg of perigee: 244
3342 deg
Mean anomaly: 115
7627 deg
Mean motion: 15
54114599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 347
Coasting Arc #15 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2018/082/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904719
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2605461
69 A = 6786653
44 meter
Y = 5732202
78 meter E =
0003583
Z = -2529780
59 I = 52
02792
XDOT = -3742
721762 Wp = 39
91964
YDOT = 4048
139349 meter/sec RA = 83
83209 deg
ZDOT = 5324
781893 TA = 291
85634
MA = 291
89444
Ha = 220
402 n
mi
Hp = 215
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8548102
66 X = 2553457
36
Y = 18806439
58 feet Y = 5761047
91 meter
Z = -8299805
08 Z = -2517250
81
XDOT = -12279
270874 XDOT = -3813
576017
YDOT = 13281
297077 feet/sec YDOT = 4005
889827 meter/sec
ZDOT = 17469
756867 ZDOT = 5306
428672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19308936
50 X = 5885363
85
Y = -7404707
49 feet Y = -2256954
84 meter
Z = -8244651
07 Z = -2512969
65
XDOT = 11938
093222 XDOT = 3638
730814
YDOT = 11796
021002 feet/sec YDOT = 3595
427202 meter/sec
ZDOT = 17387
264975 ZDOT = 5299
638364
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 18082
74422980
00016717 00000-0 10270-3 0 9147
2 25544 51
6403 84
6734 0001859 248
7294 111
3660 15
54126851 25229
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
74422980 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 84
6734 deg
Eccentricity:
0001859
Arg of perigee: 248
7294 deg
Mean anomaly: 111
3660 deg
Mean motion: 15
54126851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 310
Coasting Arc #16 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2018/082/19:41:05
000
Vector Time (MET): N/A
Weight (LBS) : 919827
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3444378
15 A = 6779469
80 meter
Y = 3244131
97 meter E =
0006171
Z = 4852985
78 I = 52
00497
XDOT = -2749
621686 Wp = 132
94688
YDOT = -6700
959673 meter/sec RA = 83
47155 deg
ZDOT = 2521
829223 TA = 292
36028
MA = 292
42567
Ha = 220
524 n
mi
Hp = 215
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11300453
25 X = -3503972
20
Y = 10643477
60 feet Y = 3205281
66 meter
Z = 15921869
35 Z = 4836109
22
XDOT = -9021
068525 XDOT = -2686
735110
YDOT = -21984
775829 feet/sec YDOT = -6731
356055 meter/sec
ZDOT = 8273
717922 ZDOT = 2508
625657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14531967
92 X = 4429343
82
Y = 5675690
40 feet Y = 1729950
43 meter
Z = 15846079
31 Z = 4829884
97
XDOT = -15477
854001 XDOT = -4717
649899
YDOT = 16635
502446 feet/sec YDOT = 5070
501145 meter/sec
ZDOT = 8215
689421 ZDOT = 2504
142136
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 18082
87283398
00016717 00000-0 10270-3 0 9150
2 25544 51
6417 84
0330 0001832 249
4809 110
6147 15
54114160 25245
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
87283398 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 84
0330 deg
Eccentricity:
0001832
Arg of perigee: 249
4809 deg
Mean anomaly: 110
6147 deg
Mean motion: 15
54114160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 299
Coasting Arc #17 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2018/083/19:41:05
000
Vector Time (MET): N/A
Weight (LBS) : 919827
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3927402
05 A = 6777423
82 meter
Y = -1535958
80 meter E =
0012795
Z = -5316704
34 I = 51
99371
XDOT = 2010
490614 Wp = 86
14995
YDOT = 7362
614793 meter/sec RA = 78
49795 deg
ZDOT = -642
369869 TA = 177
74275
MA = 177
73697
Ha = 220
295 n
mi
Hp = 215
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12885177
34 X = 3970111
34
Y = -5039234
90 feet Y = -1491801
39 meter
Z = -17443255
71 Z = -5297522
62
XDOT = 6596
097815 XDOT = 1931
130716
YDOT = 24155
560343 feet/sec YDOT = 7384
653716 meter/sec
ZDOT = -2107
512694 ZDOT = -632
796799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10332433
42 X = -3149325
71
Y = -9362173
09 feet Y = -2853590
36 meter
Z = -17357401
53 Z = -5290535
99
XDOT = 17948
340461 XDOT = 5470
654173
YDOT = -15981
480819 feet/sec YDOT = -4871
155354 meter/sec
ZDOT = -2065
797307 ZDOT = -629
655019
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 18083
83736537
00016717 00000-0 10270-3 0 9166
2 25544 51
6418 79
2247 0001896 257
6245 102
4696 15
54150114 25397
Satellite: ISS
Catalog Number: 25544
Epoch time: 18083
83736537 = yrday
fracday
Element set: 916
Inclination: 51
6418 deg
RA of node: 79
2247 deg
Eccentricity:
0001896
Arg of perigee: 257
6245 deg
Mean anomaly: 102
4696 deg
Mean motion: 15
54150114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 327
Coasting Arc #18 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2018/084/19:41:05
000
Vector Time (MET): N/A
Weight (LBS) : 919827
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4322299
01 A = 6777818
05 meter
Y = -243756
11 meter E =
0002637
Z = 5214136
27 I = 51
98696
XDOT = -1149
969326 Wp = 36
57777
YDOT = -7470
577930 meter/sec RA = 73
52221 deg
ZDOT = -1300
119795 TA = 65
86081
MA = 65
83324
Ha = 220
400 n
mi
Hp = 215
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14180771
03 X = -4344579
38
Y = -799724
78 feet Y = -292215
28 meter
Z = 17106746
31 Z = 5193086
09
XDOT = -3772
865243 XDOT = -1060
030571
YDOT = -24509
770110 feet/sec YDOT = -7482
934880 meter/sec
ZDOT = -4265
484891 ZDOT = -1305
486997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5917488
91 X = 1803650
62
Y = 13035441
07 feet Y = 3973202
44 meter
Z = 17012795
10 Z = 5185499
95
XDOT = -19032
200100 XDOT = -5801
014591
YDOT = 14246
933178 feet/sec YDOT = 4342
465233 meter/sec
ZDOT = -4288
394917 ZDOT = -1307
102771
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 18084
86619704
00016717 00000-0 10270-3 0 9177
2 25544 51
6412 74
0961 0001955 261
0603 99
0329 15
54161145 25558
Satellite: ISS
Catalog Number: 25544
Epoch time: 18084
86619704 = yrday
fracday
Element set: 917
Inclination: 51
6412 deg
RA of node: 74
0961 deg
Eccentricity:
0001955
Arg of perigee: 261
0603 deg
Mean anomaly: 99
0329 deg
Mean motion: 15
54161145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 309
Coasting Arc #19 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2018/085/19:41:05
000
Vector Time (MET): N/A
Weight (LBS) : 919827
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4612199
22 A = 6780494
02 meter
Y = 1936486
72 meter E =
0008134
Z = -4585551
23 I = 51
98490
XDOT = 144
739332 Wp = 116
01426
YDOT = 7002
695194 meter/sec RA = 68
54966 deg
ZDOT = 3103
624057 TA = 184
92636
MA = 184
93437
Ha = 220
259 n
mi
Hp = 215
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15131887
21 X = 4612476
10
Y = 6353302
90 feet Y = 1988064
70 meter
Z = -15044459
42 Z = -4563146
46
XDOT = 474
866574 XDOT = 51
346904
YDOT = 22974
721764 feet/sec YDOT = 7003
791822 meter/sec
ZDOT = 10182
493624 ZDOT = 3104
099765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1713427
42 X = -522252
68
Y = -16413236
72 feet Y = -5002754
55 meter
Z = -14944699
87 Z = -4555144
52
XDOT = 18780
401530 XDOT = 5724
266386
YDOT = -11230
623420 feet/sec YDOT = -3423
094018 meter/sec
ZDOT = 10183
619977 ZDOT = 3103
967369
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 18085
83072669
00016717 00000-0 10270-3 0 9189
2 25544 51
6407 69
2876 0001985 265
2291 94
8635 15
54145539 25704
Satellite: ISS
Catalog Number: 25544
Epoch time: 18085
83072669 = yrday
fracday
Element set: 918
Inclination: 51
6407 deg
RA of node: 69
2876 deg
Eccentricity:
0001985
Arg of perigee: 265
2291 deg
Mean anomaly: 94
8635 deg
Mean motion: 15
54145539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 347
Coasting Arc #20 (Orbit 2579)
---------------------------------------
Vector Time (GMT): 2018/086/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919827
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4734616
37 A = 6781308
91 meter
Y = 2076869
70 meter E =
0007308
Z = -4395757
71 I = 51
97673
XDOT = 185
384688 Wp = 116
26869
YDOT = 6845
395783 meter/sec RA = 65
35391 deg
ZDOT = 3435
195624 TA = 188
41909
MA = 188
43136
Ha = 220
418 n
mi
Hp = 215
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15533518
28 X = 4732392
43
Y = 6813876
96 feet Y = 2129802
60 meter
Z = -14421777
27 Z = -4372764
41
XDOT = 608
217480 XDOT = 92
137630
YDOT = 22458
647581 feet/sec YDOT = 6846
947817 meter/sec
ZDOT = 11270
326852 ZDOT = 3435
869050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14364193
38 X = 4378206
14
Y = 9183200
42 feet Y = 2799039
49 meter
Z = -14319411
56 Z = -4364556
64
XDOT = -2331
293982 XDOT = -710
578406
YDOT = 21217
079734 feet/sec YDOT = 6466
965903 meter/sec
ZDOT = 11272
353076 ZDOT = 3435
813218
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 18086
47374489
00016717 00000-0 10270-3 0 9196
2 25544 51
6382 66
0812 0001701 264
0732 96
0227 15
54112533 25804
Satellite: ISS
Catalog Number: 25544
Epoch time: 18086
47374489 = yrday
fracday
Element set: 919
Inclination: 51
6382 deg
RA of node: 66
0812 deg
Eccentricity:
0001701
Arg of perigee: 264
0732 deg
Mean anomaly: 96
0227 deg
Mean motion: 15
54112533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2580
Checksum: 304
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