[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 30th 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
122/14:29:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 213
9
128/00:24:00
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
5
132/22:41:26
692 -1
1 1
1 1
1
N/A -0
1 -0
1 222
0
000/00:02:49
384 0
0 -0
0 213
9
134/06:25:00
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
9
Coasting Arc #1 (Orbit 3109)
---------------------------------------
Vector Time (GMT): 2018/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3077307
44 A = 6779056
60 meter
Y = -3607826
12 meter E =
0007487
Z = 4838544
44 I = 51
25841
XDOT = 3625
212306 Wp = 99
06225
YDOT = 6321
014239 meter/sec RA = 255
50928 deg
ZDOT = 2403
239169 TA = 327
23839
MA = 327
28480
Ha = 221
420 n
mi
Hp = 213
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10096153
02 X = 3093918
86
Y = -11836699
87 feet Y = -3573320
62 meter
Z = 15874489
64 Z = 4853533
61
XDOT = 11893
741163 XDOT = 3542
585668
YDOT = 20738
235692 feet/sec YDOT = 6361
091890 meter/sec
ZDOT = 7884
642943 ZDOT = 2420
648783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 719123
25 X = 219188
77
Y = -15471938
03 feet Y = -4715846
71 meter
Z = 15941806
24 Z = 4859062
54
XDOT = 20892
557996 XDOT = 6368
051677
YDOT = 9188
946170 feet/sec YDOT = 2800
790793 meter/sec
ZDOT = 7961
451867 ZDOT = 2426
650529
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 18120
55249557
00016717 00000-0 10270-3 0 9001
2 25544 51
6399 256
1759 0002750 30
5390 329
5923 15
54210838 31109
Satellite: ISS
Catalog Number: 25544
Epoch time: 18120
55249557 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 256
1759 deg
Eccentricity:
0002750
Arg of perigee: 30
5390 deg
Mean anomaly: 329
5923 deg
Mean motion: 15
54210838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3110
Checksum: 304
Coasting Arc #2 (Orbit 3124)
---------------------------------------
Vector Time (GMT): 2018/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3796674
71 A = 6777251
90 meter
Y = 1958016
16 meter E =
0016708
Z = -5275904
45 I = 51
26131
XDOT = -2931
505799 Wp = 78
52963
YDOT = -7054
723018 meter/sec RA = 250
48544 deg
ZDOT = -506
700205 TA = 186
59220
MA = 186
61420
Ha = 221
645 n
mi
Hp = 213
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12456281
85 X = -3792659
54
Y = 6423937
53 feet Y = 1915581
64 meter
Z = -17309397
80 Z = -5294337
96
XDOT = -9617
801179 XDOT = -2849
938754
YDOT = -23145
416727 feet/sec YDOT = -7087
049059 meter/sec
ZDOT = -1662
402247 ZDOT = -520
742693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5661784
66 X = -1725711
96
Y = 12708601
42 feet Y = 3873581
71 meter
Z = -17391860
96 Z = -5301039
22
XDOT = -20998
692747 XDOT = -6400
401549
YDOT = -11723
010851 feet/sec YDOT = -3573
173707 meter/sec
ZDOT = -1724
111569 ZDOT = -525
509206
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 18121
51699473
00016717 00000-0 10270-3 0 9015
2 25544 51
6397 251
3689 0002858 35
8559 324
2785 15
54196997 31253
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
51699473 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 251
3689 deg
Eccentricity:
0002858
Arg of perigee: 35
8559 deg
Mean anomaly: 324
2785 deg
Mean motion: 15
54196997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3125
Checksum: 352
Coasting Arc #3 (Orbit 3140)
---------------------------------------
Vector Time (GMT): 2018/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4422364
12 A = 6777887
40 meter
Y = -214407
18 meter E =
0007381
Z = 5128125
34 I = 51
27617
XDOT = 2036
649209 Wp = 48
91203
YDOT = 7253
766025 meter/sec RA = 245
45852 deg
ZDOT = -1446
939998 TA = 55
11215
MA = 55
04279
Ha = 221
577 n
mi
Hp = 213
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14509068
64 X = 4399522
82
Y = -703435
64 feet Y = -165081
14 meter
Z = 16824558
20 Z = 5149552
55
XDOT = 6681
919977 XDOT = 1962
412847
YDOT = 23798
444963 feet/sec YDOT = 7276
126203 meter/sec
ZDOT = -4747
178472 ZDOT = -1437
226565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10666326
60 X = 3251096
35
Y = -9695954
68 feet Y = -2955326
99 meter
Z = 16920153
45 Z = 5157262
77
XDOT = 19605
458230 XDOT = 5975
743668
YDOT = 13322
451190 feet/sec YDOT = 4060
683123 meter/sec
ZDOT = -4704
789302 ZDOT = -1434
019779
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 18122
54578999
00016717 00000-0 10270-3 0 9029
2 25544 51
6406 246
2392 0002899 39
0323 321
1039 15
54177028 31418
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
54578999 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 246
2392 deg
Eccentricity:
0002899
Arg of perigee: 39
0323 deg
Mean anomaly: 321
1039 deg
Mean motion: 15
54177028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3141
Checksum: 311
Coasting Arc #4 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2018/122/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4604340
22 A = 6784816
24 meter
Y = -3844271
42 meter E =
0006856
Z = -3172681
07 I = 51
30152
XDOT = 1533
152126 Wp = 62
85078
YDOT = -5781
562464 meter/sec RA = 244
93005 deg
ZDOT = 4791
497278 TA = 260
34416
MA = 260
42161
Ha = 221
593 n
mi
Hp = 213
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15106103
09 X = -4545598
84
Y = -12612439
05 feet Y = -3895431
77 meter
Z = -10409058
62 Z = -3194905
21
XDOT = 5030
026660 XDOT = 1574
414207
YDOT = -18968
380786 feet/sec YDOT = -5764
187150 meter/sec
ZDOT = 15720
135427 ZDOT = 4799
044960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15707194
67 X = -4787552
94
Y = 11768135
64 feet Y = 3586927
74 meter
Z = -10507687
16 Z = -3202743
05
XDOT = -16488
057364 XDOT = -5025
559885
YDOT = -7972
009343 feet/sec YDOT = -2429
868448 meter/sec
ZDOT = 15754
542630 ZDOT = 4801
984593
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 18122
61008784
00016717 00000-0 10270-3 0 9038
2 25544 51
6412 245
9213 0002834 34
2636 325
8699 15
54184005 31423
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
61008784 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 245
9213 deg
Eccentricity:
0002834
Arg of perigee: 34
2636 deg
Mean anomaly: 325
8699 deg
Mean motion: 15
54184005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 295
Coasting Arc #5 (Orbit 3157)
---------------------------------------
Vector Time (GMT): 2018/123/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4353703
31 A = 6787992
01 meter
Y = 4944455
13 meter E =
0014918
Z = 1612269
34 I = 51
32683
XDOT = -2774
349337 Wp = 105
30565
YDOT = 4314
977200 meter/sec RA = 239
93119 deg
ZDOT = -5700
978997 TA = 56
96770
MA = 56
82447
Ha = 221
720 n
mi
Hp = 213
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14283803
51 X = 4290257
81
Y = 16221965
64 feet Y = 4992786
42 meter
Z = 5289597
56 Z = 1633264
57
XDOT = -9102
195989 XDOT = -2794
701623
YDOT = 14156
749343 feet/sec YDOT = 4283
838978 meter/sec
ZDOT = -18703
999333 ZDOT = -5714
505268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18863903
81 X = 5749717
88
Y = -10504265
75 feet Y = -3201700
20 meter
Z = 5382619
08 Z = 1640622
30
XDOT = 11175
816008 XDOT = 3406
388719
YDOT = 10387
742219 feet/sec YDOT = 3166
183828 meter/sec
ZDOT = -18764
883553 ZDOT = -5719
536507
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 18123
63887815
00016717 00000-0 10270-3 0 9042
2 25544 51
6410 240
7926 0003019 39
8810 320
2564 15
54196891 31589
Satellite: ISS
Catalog Number: 25544
Epoch time: 18123
63887815 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 240
7926 deg
Eccentricity:
0003019
Arg of perigee: 39
8810 deg
Mean anomaly: 320
2564 deg
Mean motion: 15
54196891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3158
Checksum: 315
Coasting Arc #6 (Orbit 3173)
---------------------------------------
Vector Time (GMT): 2018/124/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3841616
68 A = 6789218
93 meter
Y = -5588164
30 meter E =
0015359
Z = 81940
01 I = 51
34736
XDOT = 3994
109637 Wp = 45
30509
YDOT = -2647
951942 meter/sec RA = 234
93947 deg
ZDOT = 5989
603716 TA = 315
58140
MA = 315
70448
Ha = 221
810 n
mi
Hp = 213
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12603729
26 X = -3779240
81
Y = -18333872
38 feet Y = -5630775
14 meter
Z = 268832
05 Z = 63429
76
XDOT = 13104
034241 XDOT = 3994
328210
YDOT = -8687
506372 feet/sec YDOT = -2603
286138 meter/sec
ZDOT = 19650
930828 ZDOT = 6009
006357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20432599
90 X = -6227856
45
Y = 8805171
53 feet Y = 2683816
28 meter
Z = 186959
93 Z = 56985
39
XDOT = -5359
223604 XDOT = -1633
491354
YDOT = -12923
577844 feet/sec YDOT = -3939
106527 meter/sec
ZDOT = 19737
820410 ZDOT = 6016
087661
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 18124
66766602
00016717 00000-0 10270-3 0 9057
2 25544 51
6404 235
6639 0003148 41
1742 318
9648 15
54167188 31741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18124
66766602 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 235
6639 deg
Eccentricity:
0003148
Arg of perigee: 41
1742 deg
Mean anomaly: 318
9648 deg
Mean motion: 15
54167188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3174
Checksum: 322
Coasting Arc #7 (Orbit 3188)
---------------------------------------
Vector Time (GMT): 2018/125/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2995264
36 A = 6787736
34 meter
Y = 5814393
10 meter E =
0007737
Z = -1812139
07 I = 51
36168
XDOT = -5125
622476 Wp = 118
61010
YDOT = 893
443866 meter/sec RA = 229
94895 deg
ZDOT = -5627
352192 TA = 81
37824
MA = 81
29059
Ha = 221
810 n
mi
Hp = 213
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9826982
82 X = 2938826
12
Y = 19076092
86 feet Y = 5847572
74 meter
Z = -5945338
15 Z = -1797725
76
XDOT = -16816
346706 XDOT = -5107
897285
YDOT = 2931
246280 feet/sec YDOT = 836
225012 meter/sec
ZDOT = -18462
441575 ZDOT = -5652
207839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20522536
33 X = 6255269
07
Y = -6328066
04 feet Y = -1928794
53 meter
Z = -5881754
75 Z = -1792758
85
XDOT = -537
588914 XDOT = -163
857101
YDOT = 15452
358166 feet/sec YDOT = 4709
878769 meter/sec
ZDOT = -18573
447858 ZDOT = -5661
186907
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 18125
63214960
00016717 00000-0 10270-3 0 9061
2 25544 51
6395 230
8558 0003061 46
4884 313
6522 15
54206019 31892
Satellite: ISS
Catalog Number: 25544
Epoch time: 18125
63214960 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 230
8558 deg
Eccentricity:
0003061
Arg of perigee: 46
4884 deg
Mean anomaly: 313
6522 deg
Mean motion: 15
54206019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3189
Checksum: 307
Coasting Arc #8 (Orbit 3204)
---------------------------------------
Vector Time (GMT): 2018/126/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1874542
70 A = 6784445
83 meter
Y = -5608557
48 meter E =
0015208
Z = 3309854
46 I = 51
37315
XDOT = 6038
722897 Wp = 80
90260
YDOT = 750
089067 meter/sec RA = 224
95218 deg
ZDOT = 4675
036245 TA = 317
79297
MA = 317
90995
Ha = 221
837 n
mi
Hp = 213
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6150074
48 X = -1827764
61
Y = -18400779
12 feet Y = -5629258
50 meter
Z = 10859102
57 Z = 3300861
88
XDOT = 19812
082994 XDOT = 6007
177349
YDOT = 2460
922136 feet/sec YDOT = 817
441636 meter/sec
ZDOT = 15338
045424 ZDOT = 4704
293910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19159404
45 X = -5839786
47
Y = 3191281
40 feet Y = 972702
57 meter
Z = 10819664
56 Z = 3297833
76
XDOT = 5823
061689 XDOT = 1774
869203
YDOT = -17663
403662 feet/sec YDOT = -5383
805436 meter/sec
ZDOT = 15468
503887 ZDOT = 4714
799985
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 18126
66092794
00016717 00000-0 10270-3 0 9075
2 25544 51
6399 225
7264 0003144 49
0916 311
0509 15
54221059 32057
Satellite: ISS
Catalog Number: 25544
Epoch time: 18126
66092794 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 225
7264 deg
Eccentricity:
0003144
Arg of perigee: 49
0916 deg
Mean anomaly: 311
0509 deg
Mean motion: 15
54221059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3205
Checksum: 306
Coasting Arc #9 (Orbit 3219)
---------------------------------------
Vector Time (GMT): 2018/127/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 477038
57 A = 6780600
50 meter
Y = 5073466
15 meter E =
0012610
Z = -4485958
89 I = 51
38356
XDOT = -6602
222653 Wp = 65
68005
YDOT = -2201
646523 meter/sec RA = 219
94727 deg
ZDOT = -3194
089859 TA = 172
06444
MA = 172
04447
Ha = 221
921 n
mi
Hp = 213
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1565087
17 X = 442060
80
Y = 16645230
16 feet Y = 5078605
31 meter
Z = -14717712
89 Z = -4483726
36
XDOT = -21660
835476 XDOT = -6561
597245
YDOT = -7223
249749 feet/sec YDOT = -2275
249860 meter/sec
ZDOT = -10479
297438 ZDOT = -3226
062782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16710484
72 X = 5093355
74
Y = 740269
75 feet Y = 225634
22 meter
Z = -14708363
56 Z = -4483109
21
XDOT = -10190
020751 XDOT = -3105
918325
YDOT = 19114
243958 feet/sec YDOT = 5826
021558 meter/sec
ZDOT = -10621
713920 ZDOT = -3237
498403
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 18127
62540659
00016717 00000-0 10270-3 0 9081
2 25544 51
6392 220
9184 0003256 53
1466 306
9985 15
54206740 32206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18127
62540659 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 220
9184 deg
Eccentricity:
0003256
Arg of perigee: 53
1466 deg
Mean anomaly: 306
9985 deg
Mean motion: 15
54206740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3220
Checksum: 311
Coasting Arc #10 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2018/128/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3245432
41 A = 6785989
57 meter
Y = -5286061
29 meter E =
0016687
Z = 2731377
95 I = 51
41284
XDOT = 5644
832172 Wp = 73
20371
YDOT = -800
834937 meter/sec RA = 217
88123 deg
ZDOT = 5136
041391 TA = 317
83193
MA = 317
96017
Ha = 222
008 n
mi
Hp = 213
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10647744
13 X = -3199348
70
Y = -17342720
76 feet Y = -5322096
36 meter
Z = 8961213
76 Z = 2715724
44
XDOT = 18519
790589 XDOT = 5628
419453
YDOT = -2627
411209 feet/sec YDOT = -737
802463 meter/sec
ZDOT = 16850
529498 ZDOT = 5163
422314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20211488
07 X = 6160461
56
Y = 2622217
55 feet Y = 799251
91 meter
Z = 8891990
53 Z = 2710278
71
XDOT = -9375
543403 XDOT = -2857
665629
YDOT = 14470
643904 feet/sec YDOT = 4410
652262 meter/sec
ZDOT = 16972
821890 ZDOT = 5173
316112
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 18128
07549648
00016717 00000-0 10270-3 0 9099
2 25544 51
6400 218
6758 0003514 50
5341 309
6122 15
54206497 32276
Satellite: ISS
Catalog Number: 25544
Epoch time: 18128
07549648 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 218
6758 deg
Eccentricity:
0003514
Arg of perigee: 50
5341 deg
Mean anomaly: 309
6122 deg
Mean motion: 15
54206497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 309
Coasting Arc #11 (Orbit 3241)
---------------------------------------
Vector Time (GMT): 2018/129/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1890686
90 A = 6782044
34 meter
Y = 5091017
31 meter E =
0010414
Z = -4073731
76 I = 51
42755
XDOT = -6597
688284 Wp = 65
72124
YDOT = -619
245964 meter/sec RA = 212
88334 deg
ZDOT = -3839
556051 TA = 164
41043
MA = 164
37833
Ha = 221
903 n
mi
Hp = 213
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6203041
02 X = 1853405
41
Y = 16702812
70 feet Y = 5111951
90 meter
Z = -13365261
67 Z = -4064637
85
XDOT = -21645
958936 XDOT = -6571
622690
YDOT = -2031
646863 feet/sec YDOT = -692
880044 meter/sec
ZDOT = -12596
968672 ZDOT = -3871
542249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17025394
85 X = -5189340
35
Y = -5353953
42 feet Y = -1631885
00 meter
Z = -13325276
83 Z = -4061544
38
XDOT = 14513
057541 XDOT = 4423
579938
YDOT = -14473
013195 feet/sec YDOT = -4411
374422 meter/sec
ZDOT = -12739
659606 ZDOT = -3883
048248
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
03996929
00016717 00000-0 10270-3 0 9106
2 25544 51
6410 213
8678 0003345 51
8038 308
3416 15
54232740 32423
Satellite: ISS
Catalog Number: 25544
Epoch time: 18129
03996929 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 213
8678 deg
Eccentricity:
0003345
Arg of perigee: 51
8038 deg
Mean anomaly: 308
3416 deg
Mean motion: 15
54232740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3242
Checksum: 303
Coasting Arc #12 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2018/130/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -303822
73 A = 6778646
59 meter
Y = -4619334
43 meter E =
0008411
Z = 4945082
07 I = 51
44489
XDOT = 7134
269045 Wp = 100
83684
YDOT = 1836
105207 meter/sec RA = 207
87580 deg
ZDOT = 2148
819105 TA = 328
15542
MA = 328
20624
Ha = 221
972 n
mi
Hp = 213
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -996793
73 X = -276166
29
Y = -15155296
69 feet Y = -4622577
39 meter
Z = 16224022
55 Z = 4943673
33
XDOT = 23406
394505 XDOT = 7102
769065
YDOT = 6023
967215 feet/sec YDOT = 1915
709373 meter/sec
ZDOT = 7049
931446 ZDOT = 2183
398702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12750884
39 X = 3886469
56
Y = 8263049
88 feet Y = 2518577
60 meter
Z = 16218276
03 Z = 4943330
53
XDOT = -18296
077976 XDOT = -5576
644567
YDOT = 14063
261983 feet/sec YDOT = 4286
482252 meter/sec
ZDOT = 7204
072047 ZDOT = 2195
801160
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
06873809
00016717 00000-0 10270-3 0 9113
2 25544 51
6415 208
7382 0003451 56
7141 303
4342 15
54229887 32589
Satellite: ISS
Catalog Number: 25544
Epoch time: 18130
06873809 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 208
7382 deg
Eccentricity:
0003451
Arg of perigee: 56
7141 deg
Mean anomaly: 303
4342 deg
Mean motion: 15
54229887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 306
Coasting Arc #13 (Orbit 3272)
---------------------------------------
Vector Time (GMT): 2018/131/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1420624
20 A = 6777031
86 meter
Y = 3987928
07 meter E =
0017924
Z = -5307595
01 I = 51
46880
XDOT = -7114
968623 Wp = 82
93084
YDOT = -2817
690558 meter/sec RA = 202
86389 deg
ZDOT = -211
179127 TA = 185
03927
MA = 185
05734
Ha = 221
962 n
mi
Hp = 213
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4660840
56 X = -1439330
94
Y = 13083753
52 feet Y = 3971937
09 meter
Z = -17413369
45 Z = -5314541
41
XDOT = -23343
072911 XDOT = -7081
905830
YDOT = -9244
391596 feet/sec YDOT = -2897
070172 meter/sec
ZDOT = -692
844905 ZDOT = -245
661259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7886998
23 X = -2403957
06
Y = -11384470
80 feet Y = -3469986
70 meter
Z = -17444843
37 Z = -5317188
26
XDOT = 20396
014687 XDOT = 6216
705277
YDOT = -12825
263406 feet/sec YDOT = -3909
140286 meter/sec
ZDOT = -846
454097 ZDOT = -257
999209
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
03320633
00016717 00000-0 10270-3 0 9124
2 25544 51
6409 203
9301 0003457 58
2489 301
9001 15
54248810 32737
Satellite: ISS
Catalog Number: 25544
Epoch time: 18131
03320633 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 203
9301 deg
Eccentricity:
0003457
Arg of perigee: 58
2489 deg
Mean anomaly: 301
9001 deg
Mean motion: 15
54248810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3273
Checksum: 275
Coasting Arc #14 (Orbit 3288)
---------------------------------------
Vector Time (GMT): 2018/132/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3122523
72 A = 6777882
83 meter
Y = -3230498
05 meter E =
0008481
Z = 5069781
18 I = 51
50313
XDOT = 6557
837863 Wp = 57
61756
YDOT = 3577
070040 meter/sec RA = 197
85317 deg
ZDOT = -1753
100820 TA = 49
39297
MA = 49
31921
Ha = 221
775 n
mi
Hp = 213
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10244500
39 X = 3133789
28
Y = -10598746
88 feet Y = -3195516
87 meter
Z = 16633140
36 Z = 5084976
89
XDOT = 21515
216087 XDOT = 6525
866458
YDOT = 11735
794096 feet/sec YDOT = 3650
225545 meter/sec
ZDOT = -5751
643109 ZDOT = -1721
322294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2832851
71 X = 863453
20
Y = 14386944
71 feet Y = 4385140
75 meter
Z = 16701357
88 Z = 5090573
88
XDOT = -20952
804094 XDOT = -6386
414688
YDOT = 10663
401494 feet/sec YDOT = 3250
204775 meter/sec
ZDOT = -5610
174943 ZDOT = -1709
981323
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
06196985
00016717 00000-0 10270-3 0 9130
2 25544 51
6412 198
8014 0003291 60
5731 299
5749 15
54277172 32897
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
06196985 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 198
8014 deg
Eccentricity:
0003291
Arg of perigee: 60
5731 deg
Mean anomaly: 299
5749 deg
Mean motion: 15
54277172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 331
Coasting Arc #15 (Orbit 3302)
---------------------------------------
Vector Time (GMT): 2018/132/22:42:51
384
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1268951
86 A = 6777608
67 meter
Y = 4035898
04 meter E =
0017117
Z = -5309798
89 I = 51
52944
XDOT = -7394
644764 Wp = 87
26478
YDOT = -1963
165062 meter/sec RA = 193
22204 deg
ZDOT = 276
593533 TA = 185
37091
MA = 185
38929
Ha = 221
997 n
mi
Hp = 213
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4163227
90 X = -1288195
40
Y = 13241135
31 feet Y = 4021600
23 meter
Z = -17420600
03 Z = -5316009
81
XDOT = -24260
645550 XDOT = -7373
486098
YDOT = -6440
830256 feet/sec YDOT = -2045
738771 meter/sec
ZDOT = 907
459098 ZDOT = 240
723631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3229514
46 X = -984356
01
Y = -13462804
87 feet Y = -4103462
93 meter
Z = -17448798
16 Z = -5318393
68
XDOT = 23196
786382 XDOT = 7070
380489
YDOT = -6526
717392 feet/sec YDOT = -1989
343461 meter/sec
ZDOT = 747
521763 ZDOT = 227
844633
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
96213901
00016717 00000-0 10270-3 0 9148
2 25544 51
6414 194
3126 0002656 57
8967 302
2443 15
54048630 33033
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
96213901 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 194
3126 deg
Eccentricity:
0002656
Arg of perigee: 57
8967 deg
Mean anomaly: 302
2443 deg
Mean motion: 15
54048630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3303
Checksum: 295
Coasting Arc #16 (Orbit 3318)
---------------------------------------
Vector Time (GMT): 2018/133/22:42:51
384
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2961389
65 A = 6778957
47 meter
Y = -3545957
16 meter E =
0008803
Z = 4955994
01 I = 51
56603
XDOT = 6849
181335 Wp = 57
98568
YDOT = 2710
060535 meter/sec RA = 188
21831 deg
ZDOT = -2146
253909 TA = 52
97835
MA = 52
89785
Ha = 221
865 n
mi
Hp = 213
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9715845
31 X = 2976747
30
Y = -11633717
73 feet Y = -3512755
15 meter
Z = 16259822
85 Z = 4970416
90
XDOT = 22471
067371 XDOT = 6828
793239
YDOT = 8891
274720 feet/sec YDOT = 2786
538869 meter/sec
ZDOT = -7041
515451 ZDOT = -2113
031693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2120689
57 X = -646386
18
Y = 14937592
79 feet Y = 4552978
28 meter
Z = 16324640
12 Z = 4975750
31
XDOT = -22756
921568 XDOT = -6936
309694
YDOT = 4329
084158 feet/sec YDOT = 1319
504851 meter/sec
ZDOT = -6893
470322 ZDOT = -2101
129754
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
99103384
00016717 00000-0 10270-3 0 9156
2 25544 51
6407 189
1846 0002648 58
9340 301
2072 15
54078299 33192
Satellite: ISS
Catalog Number: 25544
Epoch time: 18133
99103384 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 189
1846 deg
Eccentricity:
0002648
Arg of perigee: 58
9340 deg
Mean anomaly: 301
2072 deg
Mean motion: 15
54078299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3319
Checksum: 322
Coasting Arc #17 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2018/134/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2498458
46 A = 6778752
38 meter
Y = -3750648
72 meter E =
0007877
Z = 5058769
59 I = 51
57256
XDOT = 7099
580966 Wp = 62
02181
YDOT = 2273
116704 meter/sec RA = 186
61451 deg
ZDOT = -1815
286056 TA = 45
58914
MA = 45
52469
Ha = 222
061 n
mi
Hp = 213
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8197042
19 X = 2515640
18
Y = -12305277
94 feet Y = -3722613
36 meter
Z = 16597013
10 Z = 5070948
09
XDOT = 23292
588470 XDOT = 7082
452589
YDOT = 7457
731967 feet/sec YDOT = 2352
413407 meter/sec
ZDOT = -5955
662913 ZDOT = -1780
839516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13449571
22 X = 4099429
31
Y = -5991465
98 feet Y = -1826198
83 meter
Z = 16651834
11 Z = 5075479
04
XDOT = 15177
229508 XDOT = 4626
019554
YDOT = 17891
625918 feet/sec YDOT = 5453
367580 meter/sec
ZDOT = -5802
094234 ZDOT = -1768
478323
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
31256645
00016717 00000-0 10270-3 0 9163
2 25544 51
6382 187
5767 0002635 74
4620 285
6823 15
54001839 33249
Satellite: ISS
Catalog Number: 25544
Epoch time: 18134
31256645 = yrday
fracday
Element set: 916
Inclination: 51
6382 deg
RA of node: 187
5767 deg
Eccentricity:
0002635
Arg of perigee: 74
4620 deg
Mean anomaly: 285
6823 deg
Mean motion: 15
54001839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 316
Coasting Arc #18 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2018/135/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4060143
25 A = 6781620
44 meter
Y = 3307987
76 meter E =
0010791
Z = -4319119
26 I = 51
61548
XDOT = -6133
819657 Wp = 103
58205
YDOT = -2953
843084 meter/sec RA = 181
61919 deg
ZDOT = 3508
606811 TA = 202
15684
MA = 202
20351
Ha = 222
013 n
mi
Hp = 213
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13320679
96 X = -4075851
84
Y = 10852978
22 feet Y = 3262496
88 meter
Z = -14170338
77 Z = -4338880
42
XDOT = -20124
080238 XDOT = -6117
376441
YDOT = -9691
086233 feet/sec YDOT = -3022
343960 meter/sec
ZDOT = 11511
177203 ZDOT = 3478
849920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16955203
29 X = -5167945
96
Y = 2286606
23 feet Y = 696957
58 meter
Z = -14258985
40 Z = -4346138
75
XDOT = -11931
958327 XDOT = -3636
860898
YDOT = -17619
681286 feet/sec YDOT = -5370
478856 meter/sec
ZDOT = 11378
614779 ZDOT = 3468
201785
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
27715332
00016717 00000-0 10270-3 0 9173
2 25544 51
6384 182
7696 0002450 76
0787 284
0638 15
54030476 33398
Satellite: ISS
Catalog Number: 25544
Epoch time: 18135
27715332 = yrday
fracday
Element set: 917
Inclination: 51
6384 deg
RA of node: 182
7696 deg
Eccentricity:
0002450
Arg of perigee: 76
0787 deg
Mean anomaly: 284
0638 deg
Mean motion: 15
54030476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3339
Checksum: 325
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list