[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 24th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
358/04:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
6
361/02:52:51
333 -1
8 2
1 2
1
N/A 1
0 -0
0 221
4
000/00:05:42
666 0
6 -0
0 216
2
361/09:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 216
2
364/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 216
6
Coasting Arc #1 (Orbit 2763)
---------------------------------------
Vector Time (GMT): 2018/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5080942
81 A = 6786382
00 meter
Y = -3621731
08 meter E =
0015738
Z = 2645434
66 I = 51
74482
XDOT = 4805
647211 Wp = 118
81270
YDOT = 2912
464060 meter/sec RA = 164
04819 deg
ZDOT = -5226
547991 TA = 31
38010
MA = 31
28628
Ha = 221
839 n
mi
Hp = 214
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16669759
87 X = 5108214
19
Y = -11882319
83 feet Y = -3564760
34 meter
Z = 8679247
56 Z = 2670181
99
XDOT = 15766
559091 XDOT = 4798
110015
YDOT = 9555
328280 feet/sec YDOT = 2966
162741 meter/sec
ZDOT = -17147
467163 ZDOT = -5203
221579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11627319
28 X = 3544006
92
Y = 16790506
67 feet Y = 5117746
43 meter
Z = 8791136
97 Z = 2679538
55
XDOT = -8570
390671 XDOT = -2612
255077
YDOT = 14885
375571 feet/sec YDOT = 4537
062474 meter/sec
ZDOT = -17042
636793 ZDOT = -5194
595694
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 18355
53759505
00016717 00000-0 10270-3 0 9008
2 25544 51
6349 165
0580 0004712 172
7381 187
3841 15
54095142 27645
Satellite: ISS
Catalog Number: 25544
Epoch time: 18355
53759505 = yrday
fracday
Element set: 900
Inclination: 51
6349 deg
RA of node: 165
0580 deg
Eccentricity:
0004712
Arg of perigee: 172
7381 deg
Mean anomaly: 187
3841 deg
Mean motion: 15
54095142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2764
Checksum: 317
Coasting Arc #2 (Orbit 2778)
---------------------------------------
Vector Time (GMT): 2018/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5911154
20 A = 6788926
74 meter
Y = 3161104
98 meter E =
0006924
Z = -1069903
27 I = 51
78504
XDOT = -3089
519099 Wp = 68
99317
YDOT = -3791
800244 meter/sec RA = 159
08275 deg
ZDOT = 5899
479464 TA = 279
43457
MA = 279
51284
Ha = 221
954 n
mi
Hp = 214
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19393550
51 X = -5940866
20
Y = 10371079
35 feet Y = 3094836
38 meter
Z = -3510181
34 Z = -1098689
31
XDOT = -10136
217517 XDOT = -3075
545080
YDOT = -12440
289514 feet/sec YDOT = -3826
272164 meter/sec
ZDOT = 19355
247586 ZDOT = 5884
505000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10409009
89 X = -3172666
22
Y = -19349200
01 feet Y = -5897636
16 meter
Z = -3640251
80 Z = -1109548
75
XDOT = 11007
592948 XDOT = 3355
114331
YDOT = -9530
595670 feet/sec YDOT = -2904
925560 meter/sec
ZDOT = 19288
135542 ZDOT = 5879
023713
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 18356
50215498
00016717 00000-0 10270-3 0 9015
2 25544 51
6351 160
2493 0004919 172
9519 187
1703 15
54085107 27793
Satellite: ISS
Catalog Number: 25544
Epoch time: 18356
50215498 = yrday
fracday
Element set: 901
Inclination: 51
6351 deg
RA of node: 160
2493 deg
Eccentricity:
0004919
Arg of perigee: 172
9519 deg
Mean anomaly: 187
1703 deg
Mean motion: 15
54085107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2779
Checksum: 322
Coasting Arc #3 (Orbit 2794)
---------------------------------------
Vector Time (GMT): 2018/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6279104
62 A = 6789202
10 meter
Y = -2476195
27 meter E =
0014758
Z = -651521
51 I = 51
81673
XDOT = 1216
595584 Wp = 151
03544
YDOT = 4641
696188 meter/sec RA = 154
12430 deg
ZDOT = -5985
482080 TA = 35
98551
MA = 35
88623
Ha = 221
802 n
mi
Hp = 214
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20600736
96 X = 6309492
19
Y = -8124000
22 feet Y = -2405807
95 meter
Z = -2137537
77 Z = -620946
54
XDOT = 3991
455328 XDOT = 1193
674559
YDOT = 15228
662035 feet/sec YDOT = 4655
173764 meter/sec
ZDOT = -19637
408399 ZDOT = -5979
627273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8517928
41 X = 2596264
58
Y = 20454973
03 feet Y = 6234675
78 meter
Z = -1999445
96 Z = -609431
13
XDOT = -13653
745387 XDOT = -4161
661594
YDOT = 3792
451209 feet/sec YDOT = 1155
939128 meter/sec
ZDOT = -19611
486862 ZDOT = -5977
581195
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 18357
53101558
00016717 00000-0 10270-3 0 9021
2 25544 51
6350 155
1205 0004706 177
5110 182
6067 15
54118746 27955
Satellite: ISS
Catalog Number: 25544
Epoch time: 18357
53101558 = yrday
fracday
Element set: 902
Inclination: 51
6350 deg
RA of node: 155
1205 deg
Eccentricity:
0004706
Arg of perigee: 177
5110 deg
Mean anomaly: 182
6067 deg
Mean motion: 15
54118746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2795
Checksum: 300
Coasting Arc #4 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2018/358/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4987715
73 A = 6781255
69 meter
Y = -1201173
37 meter E =
0011684
Z = 4431388
19 I = 51
81373
XDOT = 4284
209697 Wp = 131
17031
YDOT = -5412
392878 meter/sec RA = 150
74517 deg
ZDOT = 3341
744467 TA = 285
09761
MA = 285
22685
Ha = 221
793 n
mi
Hp = 214
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16363896
75 X = -4995438
31
Y = -3940857
50 feet Y = -1256993
29 meter
Z = 14538675
16 Z = 4407140
90
XDOT = 14055
806092 XDOT = 4328
181913
YDOT = -17757
194482 feet/sec YDOT = -5364
238490 meter/sec
ZDOT = 10963
728566 ZDOT = 3362
661480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13789989
89 X = 4203188
92
Y = 9813616
26 feet Y = 2991190
24 meter
Z = 14429472
09 Z = 4398103
09
XDOT = -18895
755507 XDOT = -5759
426278
YDOT = 10227
781358 feet/sec YDOT = 3117
427758 meter/sec
ZDOT = 11058
592894 ZDOT = 3370
659114
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 18358
23835864
00016717 00000-0 10270-3 0 9034
2 25544 51
6388 151
5993 0004467 180
2339 179
8813 15
54083472 28065
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
23835864 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 151
5993 deg
Eccentricity:
0004467
Arg of perigee: 180
2339 deg
Mean anomaly: 179
8813 deg
Mean motion: 15
54083472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 343
Coasting Arc #5 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2018/359/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3742907
46 A = 6778263
61 meter
Y = 2349342
17 meter E =
0013038
Z = -5150453
99 I = 51
83404
XDOT = -5414
661245 Wp = 96
90945
YDOT = 5182
890024 meter/sec RA = 145
76339 deg
ZDOT = -1575
718588 TA = 157
94970
MA = 157
89356
Ha = 221
565 n
mi
Hp = 214
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12279880
13 X = 3741376
10
Y = 7707815
51 feet Y = 2391190
04 meter
Z = -16897814
94 Z = -5132275
93
XDOT = -17764
636630 XDOT = -5464
561450
YDOT = 17004
232361 feet/sec YDOT = 5122
060705 meter/sec
ZDOT = -5169
680406 ZDOT = -1602
141305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8809196
50 X = -2685043
09
Y = -11634409
79 feet Y = -3546168
10 meter
Z = -16816081
34 Z = -5125541
59
XDOT = 21795
972075 XDOT = 6643
412289
YDOT = -8881
649929 feet/sec YDOT = -2707
126898 meter/sec
ZDOT = -5289
367052 ZDOT = -1612
199078
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 18359
20291258
00016717 00000-0 10270-3 0 9046
2 25544 51
6403 146
7912 0004339 183
6488 176
4634 15
54111070 28217
Satellite: ISS
Catalog Number: 25544
Epoch time: 18359
20291258 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 146
7912 deg
Eccentricity:
0004339
Arg of perigee: 183
6488 deg
Mean anomaly: 176
4634 deg
Mean motion: 15
54111070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 307
Coasting Arc #6 (Orbit 2836)
---------------------------------------
Vector Time (GMT): 2018/360/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2352441
71 A = 6777373
98 meter
Y = -3473698
82 meter E =
0004131
Z = 5321110
44 I = 51
85791
XDOT = 6099
682541 Wp = 154
83883
YDOT = -4638
755713 meter/sec RA = 140
77911 deg
ZDOT = -335
153536 TA = 298
32511
MA = 298
36678
Ha = 221
492 n
mi
Hp = 214
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7717984
63 X = -2339269
72
Y = -11396649
68 feet Y = -3499932
34 meter
Z = 17457711
43 Z = 5309714
93
XDOT = 20012
081828 XDOT = 6152
729042
YDOT = -15219
014808 feet/sec YDOT = -4570
248187 meter/sec
ZDOT = -1099
585093 ZDOT = -305
395498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3463014
95 X = 1055526
96
Y = 13387974
45 feet Y = 4080654
61 meter
Z = 17406673
05 Z = 5305553
95
XDOT = -23041
418028 XDOT = -7023
024215
YDOT = 7199
367339 feet/sec YDOT = 2194
367165 meter/sec
ZDOT = -964
892584 ZDOT = -294
099259
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 18360
23176867
00016717 00000-0 10270-3 0 9050
2 25544 51
6400 141
6632 0004367 189
1441 170
9633 15
54128413 28372
Satellite: ISS
Catalog Number: 25544
Epoch time: 18360
23176867 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 141
6632 deg
Eccentricity:
0004367
Arg of perigee: 189
1441 deg
Mean anomaly: 170
9633 deg
Mean motion: 15
54128413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2837
Checksum: 306
Coasting Arc #7 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2018/361/02:55:42
666
Vector Time (MET): N/A
Weight (LBS) : 949509
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -375295
87 A = 6782358
38 meter
Y = 5153350
74 meter E =
0009017
Z = -4402610
89 I = 51
89362
XDOT = -6404
921815 Wp = 138
63684
YDOT = 2450
469405 meter/sec RA = 136
09788 deg
ZDOT = 3411
702876 TA = 165
85253
MA = 165
82725
Ha = 221
385 n
mi
Hp = 216
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1231285
65 X = -411508
97
Y = 16907318
69 feet Y = 5148951
77 meter
Z = -14444261
44 Z = -4404521
48
XDOT = -21013
523014 XDOT = -6448
419615
YDOT = 8039
597785 feet/sec YDOT = 2378
601647 meter/sec
ZDOT = 11193
250907 ZDOT = 3380
485018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12032337
85 X = 3667456
58
Y = -11930293
06 feet Y = -3636353
32 meter
Z = -14453412
45 Z = -4405400
12
XDOT = 20264
904015 XDOT = 6176
742744
YDOT = 7038
299246 feet/sec YDOT = 2145
273610 meter/sec
ZDOT = 11052
182360 ZDOT = 3368
705183
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 18361
13201934
00016717 00000-0 10270-3 0 9065
2 25544 51
6395 137
1751 0004321 214
3673 145
7200 15
53702326 28511
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
13201934 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 137
1751 deg
Eccentricity:
0004321
Arg of perigee: 214
3673 deg
Mean anomaly: 145
7200 deg
Mean motion: 15
53702326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 280
Coasting Arc #8 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2018/361/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 949509
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -944279
39 A = 6783788
02 meter
Y = 5402082
54 meter E =
0007174
Z = -4001204
22 I = 51
90130
XDOT = -6265
269608 Wp = 145
75827
YDOT = 1864
326878 meter/sec RA = 134
80941 deg
ZDOT = 3993
351998 TA = 165
73967
MA = 165
71941
Ha = 221
436 n
mi
Hp = 216
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3098029
48 X = -985181
37
Y = 17723367
91 feet Y = 5391294
53 meter
Z = -13127310
44 Z = -4005890
10
XDOT = -20555
346484 XDOT = -6305
048686
YDOT = 6116
558000 feet/sec YDOT = 1794
041579 meter/sec
ZDOT = 13101
548550 ZDOT = 3962
821473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12094302
71 X = -3686343
47
Y = -13299371
70 feet Y = -4053648
49 meter
Z = -13149007
20 Z = -4007817
39
XDOT = 6944
974882 XDOT = 2116
828344
YDOT = -19140
194735 feet/sec YDOT = -5833
931355 meter/sec
ZDOT = 12963
636783 ZDOT = 3951
316491
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 18361
38929841
00016717 00000-0 10270-3 0 9077
2 25544 51
6363 135
8898 0004576 213
9125 146
1735 15
53696572 28559
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
38929841 = yrday
fracday
Element set: 907
Inclination: 51
6363 deg
RA of node: 135
8898 deg
Eccentricity:
0004576
Arg of perigee: 213
9125 deg
Mean anomaly: 146
1735 deg
Mean motion: 15
53696572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 350
Coasting Arc #9 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2018/362/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 949509
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2030202
85 A = 6787219
48 meter
Y = -5838124
06 meter E =
0011792
Z = 2786686
64 I = 51
93590
XDOT = 5664
488627 Wp = 119
86691
YDOT = -493
325204 meter/sec RA = 129
84908 deg
ZDOT = -5149
758653 TA = 28
66470
MA = 28
59993
Ha = 221
224 n
mi
Hp = 216
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6660770
52 X = 2081799
42
Y = -19153950
32 feet Y = -5815132
57 meter
Z = 9142672
70 Z = 2796673
54
XDOT = 18584
280273 XDOT = 5694
598629
YDOT = -1618
521011 feet/sec YDOT = -429
812319 meter/sec
ZDOT = -16895
533640 ZDOT = -5122
169772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11298048
15 X = 3443645
08
Y = 16815371
64 feet Y = 5125325
28 meter
Z = 9188336
37 Z = 2800604
93
XDOT = -8757
353383 XDOT = -2669
241311
YDOT = 15066
877325 feet/sec YDOT = 4592
384209 meter/sec
ZDOT = -16771
020599 ZDOT = -5111
807079
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 18362
41841671
00016717 00000-0 10270-3 0 9087
2 25544 51
6366 130
7626 0004545 220
3844 139
6971 15
53710633 28713
Satellite: ISS
Catalog Number: 25544
Epoch time: 18362
41841671 = yrday
fracday
Element set: 908
Inclination: 51
6366 deg
RA of node: 130
7626 deg
Eccentricity:
0004545
Arg of perigee: 220
3844 deg
Mean anomaly: 139
6971 deg
Mean motion: 15
53710633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 314
Coasting Arc #10 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2018/363/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 949509
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2895244
19 A = 6789787
75 meter
Y = 5990318
60 meter E =
0004203
Z = -1345430
99 I = 51
96444
XDOT = -4850
741974 Wp = 35
88566
YDOT = -1035
016486 meter/sec RA = 124
89752 deg
ZDOT = 5842
635195 TA = 309
53906
MA = 309
57620
Ha = 221
255 n
mi
Hp = 216
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9498832
66 X = -2955479
10
Y = 19653276
23 feet Y = 5957605
23 meter
Z = -4414143
66 Z = -1359640
96
XDOT = -15914
507789 XDOT = -4867
187798
YDOT = -3395
723379 feet/sec YDOT = -1089
353099 meter/sec
ZDOT = 19168
750639 ZDOT = 5819
032189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10298380
83 X = -3138946
48
Y = -19231397
89 feet Y = -5861730
08 meter
Z = -4478888
28 Z = -1365165
15
XDOT = 10793
154684 XDOT = 3289
753548
YDOT = -10209
803095 feet/sec YDOT = -3111
947983 meter/sec
ZDOT = 19062
371140 ZDOT = 5810
210724
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 18363
38321643
00016717 00000-0 10270-3 0 9097
2 25544 51
6363 125
9557 0004494 219
5746 140
5079 15
53697527 28865
Satellite: ISS
Catalog Number: 25544
Epoch time: 18363
38321643 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node: 125
9557 deg
Eccentricity:
0004494
Arg of perigee: 219
5746 deg
Mean anomaly: 140
5079 deg
Mean motion: 15
53697527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 346
Coasting Arc #11 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2018/364/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 949509
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3542928
46 A = 6790448
27 meter
Y = -5779127
36 meter E =
0012472
Z = -235848
29 I = 51
98497
XDOT = 3922
087158 Wp = 157
17744
YDOT = 2646
039252 meter/sec RA = 119
95212 deg
ZDOT = -6037
251638 TA = 25
35212
MA = 25
29098
Ha = 221
027 n
mi
Hp = 216
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11623781
02 X = 3608434
58
Y = -18960391
62 feet Y = -5739141
59 meter
Z = -773780
49 Z = -218479
28
XDOT = 12867
740020 XDOT = 3921
532523
YDOT = 8681
231142 feet/sec YDOT = 2689
895985 meter/sec
ZDOT = -19807
256030 ZDOT = -6018
200811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8818883
96 X = 2687995
83
Y = 20419403
16 feet Y = 6223834
08 meter
Z = -694789
07 Z = -211771
71
XDOT = -13089
153632 XDOT = -3989
574027
YDOT = 4996
625229 feet/sec YDOT = 1522
971370 meter/sec
ZDOT = -19721
583058 ZDOT = -6011
138516
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 18364
41233237
00016717 00000-0 10270-3 0 9105
2 25544 51
6361 120
8286 0004402 226
4913 133
5874 15
53737827 29020
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
41233237 = yrday
fracday
Element set: 910
Inclination: 51
6361 deg
RA of node: 120
8286 deg
Eccentricity:
0004402
Arg of perigee: 226
4913 deg
Mean anomaly: 133
5874 deg
Mean motion: 15
53737827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 299
Coasting Arc #12 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2018/364/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949509
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4930548
07 A = 6783979
45 meter
Y = -2416660
40 meter E =
0003465
Z = -3985491
70 I = 51
96876
XDOT = -51
650536 Wp = 115
48768
YDOT = 6523
035140 meter/sec RA = 119
29746 deg
ZDOT = -4023
405200 TA = 112
73573
MA = 112
69910
Ha = 221
252 n
mi
Hp = 216
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16176338
82 X = 4976564
71
Y = -7928675
85 feet Y = -2361266
06 meter
Z = -13075760
15 Z = -3961429
30
XDOT = -169
457139 XDOT = -105
045632
YDOT = 21401
033925 feet/sec YDOT = 6522
159221 meter/sec
ZDOT = -13200
148294 ZDOT = -4023
785424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11692531
39 X = 3563883
57
Y = 13807853
73 feet Y = 4208633
82 meter
Z = -12966928
21 Z = -3952319
72
XDOT = -19753
373834 XDOT = -6020
828344
YDOT = 4341
667551 feet/sec YDOT = 1323
340270 meter/sec
ZDOT = -13202
567824 ZDOT = -4024
142673
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 18364
54097306
00016717 00000-0 10270-3 0 9115
2 25544 51
6398 120
1885 0004741 223
9921 136
0855 15
53691857 29046
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
54097306 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 120
1885 deg
Eccentricity:
0004741
Arg of perigee: 223
9921 deg
Mean anomaly: 136
0855 deg
Mean motion: 15
53691857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 325
Coasting Arc #13 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2018/365/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949509
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4628485
81 A = 6780656
73 meter
Y = 1039724
39 meter E =
0007229
Z = 4845116
67 I = 51
97426
XDOT = 1057
713244 Wp = 156
66113
YDOT = -7156
824868 meter/sec RA = 114
33271 deg
ZDOT = 2538
466901 TA = 268
44347
MA = 268
52628
Ha = 221
036 n
mi
Hp = 216
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15185320
89 X = -4663303
24
Y = 3411169
26 feet Y = 987770
43 meter
Z = 15896052
07 Z = 4822548
67
XDOT = 3470
187808 XDOT = 1125
333767
YDOT = -23480
396548 feet/sec YDOT = -7144
618866 meter/sec
ZDOT = 8328
303481 ZDOT = 2543
768636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7314376
29 X = -2229421
89
Y = -13854991
15 feet Y = -4223001
30 meter
Z = 15794101
34 Z = 4814042
09
XDOT = 22540
763581 XDOT = 6870
424740
YDOT = -2348
531144 feet/sec YDOT = -715
832293 meter/sec
ZDOT = 8353
015419 ZDOT = 2545
999100
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 18365
57008637
00016717 00000-0 10270-3 0 9129
2 25544 51
6406 115
0612 0004621 228
7280 131
3474 15
53732303 29200
Satellite: ISS
Catalog Number: 25544
Epoch time: 18365
57008637 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 115
0612 deg
Eccentricity:
0004621
Arg of perigee: 228
7280 deg
Mean anomaly: 131
3474 deg
Mean motion: 15
53732303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 283
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