[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 24th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17545 17 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 ET - UTC (sec) : 67 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
329/19:38:37
914 5
2 5
8 5
8
N/A -2
1 -0
4 221
6
000/00:15:15
829 -1
6 0
3 215
1
Coasting Arc #1 (Orbit 1281)
---------------------------------------
Vector Time (GMT): 2015/327/10:18:02
162
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6726414
29 A = 6785753
98 meter
Y = -701556
89 meter E =
0017663
Z = 417970
73 I = 51
72418
XDOT = 117
410396 Wp = 141
54317
YDOT = -4777
235278 meter/sec RA = 8
74961 deg
ZDOT = -6006
458519 TA = 33
95007
MA = 33
83715
Ha = 220
322 n
mi
Hp = 212
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22068288
35 X = -6720099
77
Y = -2301695
84 feet Y = -776740
79 meter
Z = 1371295
06 Z = 385309
72
XDOT = 385
204710 XDOT = 199
999667
YDOT = -15673
344088 feet/sec YDOT = -4775
460528 meter/sec
ZDOT = -19706
228738 ZDOT = -6005
687548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19263719
98 X = 5871581
85
Y = -11026469
82 feet Y = -3360868
00 meter
Z = 1230308
98 Z = 374998
18
XDOT = 7936
611334 XDOT = 2419
079135
YDOT = 11617
301856 feet/sec YDOT = 3540
953606 meter/sec
ZDOT = -19701
897891 ZDOT = -6005
138477
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 15327
46208239
00016717 00000-0 10270-3 0 9009
2 25544 51
6441 9
1474 0005687 167
8044 192
3248 15
55340621 12828
Satellite: ISS
Catalog Number: 25544
Epoch time: 15327
46208239 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 9
1474 deg
Eccentricity:
0005687
Arg of perigee: 167
8044 deg
Mean anomaly: 192
3248 deg
Mean motion: 15
55340621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1282
Checksum: 301
Coasting Arc #2 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2015/328/10:18:02
162
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6339057
78 A = 6784517
42 meter
Y = 1738514
32 meter E =
0013510
Z = 1667040
57 I = 51
68847
XDOT = -2703
863052 Wp = 87
32719
YDOT = 4344
155789 meter/sec RA = 3
77761 deg
ZDOT = 5711
906010 TA = 290
93104
MA = 291
07558
Ha = 220
191 n
mi
Hp = 212
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20797433
67 X = 6311048
10
Y = 5703787
13 feet Y = 1809245
19 meter
Z = 5469293
21 Z = 1697767
22
XDOT = -8870
941773 XDOT = -2779
986462
YDOT = 14252
479623 feet/sec YDOT = 4313
493648 meter/sec
ZDOT = 18739
849113 ZDOT = 5698
586053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20052227
54 X = -6111918
95
Y = 7842753
46 feet Y = 2390471
25 meter
Z = 5601695
45 Z = 1707396
77
XDOT = -745
362495 XDOT = -227
186488
YDOT = -15338
945527 feet/sec YDOT = -4675
310597 meter/sec
ZDOT = 18681
380852 ZDOT = 5694
084884
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 15328
49010004
00016717 00000-0 10270-3 0 9015
2 25544 51
6439 4
0130 0005577 170
8184 189
3072 15
55359725 12988
Satellite: ISS
Catalog Number: 25544
Epoch time: 15328
49010004 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 4
0130 deg
Eccentricity:
0005577
Arg of perigee: 170
8184 deg
Mean anomaly: 189
3072 deg
Mean motion: 15
55359725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1298
Checksum: 297
Coasting Arc #3 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2015/329/10:18:02
162
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5126037
28 A = 6780234
58 meter
Y = -2687706
00 meter E =
0007666
Z = -3531792
96 I = 51
64221
XDOT = 5012
607044 Wp = 129
95417
YDOT = -3665
387032 meter/sec RA = 358
79364 deg
ZDOT = -4497
195672 TA = 91
67180
MA = 91
58399
Ha = 220
003 n
mi
Hp = 212
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16817707
61 X = -5078445
20
Y = -8817933
07 feet Y = -2744762
47 meter
Z = -11587247
25 Z = -3556579
34
XDOT = 16445
561169 XDOT = 5075
067929
YDOT = -12025
548004 feet/sec YDOT = -3608
983308 meter/sec
ZDOT = -14754
578978 ZDOT = -4472
693303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18640163
45 X = 5681521
82
Y = -3264266
29 feet Y = -994948
37 meter
Z = -11693776
28 Z = -3564263
01
XDOT = -5966
461950 XDOT = -1818
577602
YDOT = 18272
116026 feet/sec YDOT = 5569
340965 meter/sec
ZDOT = -14647
934710 ZDOT = -4464
690500
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 15329
45384535
00016717 00000-0 10270-3 0 9026
2 25544 51
6434 359
1991 0005588 173
8334 186
2889 15
55401185 13132
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
45384535 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 359
1991 deg
Eccentricity:
0005588
Arg of perigee: 173
8334 deg
Mean anomaly: 186
2889 deg
Mean motion: 15
55401185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1313
Checksum: 332
Coasting Arc #4 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2015/329/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 74105
60 A = 6776997
74 meter
Y = -4219941
73 meter E =
0013575
Z = -5312176
88 I = 51
60787
XDOT = 7652
692942 Wp = 125
33358
YDOT = -214
450587 meter/sec RA = 356
79392 deg
ZDOT = 269
927129 TA = 147
28522
MA = 147
20108
Ha = 221
581 n
mi
Hp = 215
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 243128
60 X = 147093
63
Y = -13844953
17 feet Y = -4218704
64 meter
Z = -17428401
85 Z = -5311639
83
XDOT = 25107
260309 XDOT = 7653
210978
YDOT = -703
578042 feet/sec YDOT = -128
870243 meter/sec
ZDOT = 885
587693 ZDOT = 307
104470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 317032
36 X = 96631
46
Y = -13847502
68 feet Y = -4220718
82 meter
Z = -17425188
40 Z = -5311197
43
XDOT = 24089
302310 XDOT = 7342
419344
YDOT = -794
745396 feet/sec YDOT = -242
238397 meter/sec
ZDOT = 1046
267448 ZDOT = 318
902318
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 15329
83934464
00016717 00000-0 10270-3 0 9031
2 25544 51
6438 357
2731 0008227 207
5877 152
4840 15
54262749 13195
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
83934464 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 357
2731 deg
Eccentricity:
0008227
Arg of perigee: 207
5877 deg
Mean anomaly: 152
4840 deg
Mean motion: 15
54262749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 330
Coasting Arc #5 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2015/330/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1908504
82 A = 6778505
48 meter
Y = 4231695
95 meter E =
0003702
Z = 4937193
23 I = 51
58110
XDOT = -7308
998493 Wp = 159
92012
YDOT = -718
474008 meter/sec RA = 351
79078 deg
ZDOT = -2212
444434 TA = 311
66593
MA = 311
69761
Ha = 221
343 n
mi
Hp = 215
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6261498
74 X = -1979666
28
Y = 13883516
89 feet Y = 4209955
55 meter
Z = 16198140
51 Z = 4927749
37
XDOT = -23979
653847 XDOT = -7289
673703
YDOT = -2357
198188 feet/sec YDOT = -800
099844 meter/sec
ZDOT = -7258
675965 ZDOT = -2247
903864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6087215
16 X = -1855383
18
Y = 14009049
49 feet Y = 4269958
29 meter
Z = 16156438
58 Z = 4924482
48
XDOT = -22953
376871 XDOT = -6996
189270
YDOT = -1436
900563 feet/sec YDOT = -437
967292 meter/sec
ZDOT = -7411
733313 ZDOT = -2259
096314
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 15330
86808059
00016717 00000-0 10270-3 0 9047
2 25544 51
6434 352
1437 0008176 211
9559 148
1099 15
54308825 13359
Satellite: ISS
Catalog Number: 25544
Epoch time: 15330
86808059 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 352
1437 deg
Eccentricity:
0008176
Arg of perigee: 211
9559 deg
Mean anomaly: 148
1099 deg
Mean motion: 15
54308825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1335
Checksum: 320
Coasting Arc #6 (Orbit 1349)
---------------------------------------
Vector Time (GMT): 2015/331/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3596390
19 A = 6781995
00 meter
Y = -4120332
03 meter E =
0008934
Z = -4018758
77 I = 51
56213
XDOT = 6352
680017 Wp = 167
31520
YDOT = 1709
300892 meter/sec RA = 346
79132 deg
ZDOT = 3925
647050 TA = 143
57469
MA = 143
51387
Ha = 221
160 n
mi
Hp = 215
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11799180
43 X = 3661719
33
Y = -13518149
69 feet Y = -4079749
23 meter
Z = -13184904
11 Z = -4001129
62
XDOT = 20842
126040 XDOT = 6314
024485
YDOT = 5607
942560 feet/sec YDOT = 1780
124310 meter/sec
ZDOT = 12879
419456 ZDOT = 3956
413774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11373403
66 X = 3466613
44
Y = -13951072
80 feet Y = -4252286
99 meter
Z = -13107859
59 Z = -3995275
60
XDOT = 19935
820388 XDOT = 6076
438054
YDOT = 4005
549190 feet/sec YDOT = 1220
891393 meter/sec
ZDOT = 13011
989866 ZDOT = 3966
054511
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 15331
83250143
00016717 00000-0 10270-3 0 9051
2 25544 51
6441 347
3337 0008144 215
1818 144
8798 15
54326632 13503
Satellite: ISS
Catalog Number: 25544
Epoch time: 15331
83250143 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 347
3337 deg
Eccentricity:
0008144
Arg of perigee: 215
1818 deg
Mean anomaly: 144
8798 deg
Mean motion: 15
54326632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1350
Checksum: 298
Coasting Arc #7 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2015/332/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4932542
28 A = 6785857
86 meter
Y = 3826948
29 meter E =
0012562
Z = 2638013
93 I = 51
54411
XDOT = -4918
071121 Wp = 138
53868
YDOT = -2741
640664 meter/sec RA = 341
80164 deg
ZDOT = -5213
502639 TA = 11
65654
MA = 11
62748
Ha = 221
075 n
mi
Hp = 215
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16182881
48 X = -4987784
14
Y = 12555604
61 feet Y = 3771480
27 meter
Z = 8654901
34 Z = 2613918
50
XDOT = -16135
403939 XDOT = -4861
722448
YDOT = -8994
884068 feet/sec YDOT = -2796
322324 meter/sec
ZDOT = -17104
667450 ZDOT = -5237
257216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15532234
14 X = -4734224
97
Y = 13419526
13 feet Y = 4090271
56 meter
Z = 8549982
36 Z = 2606034
62
XDOT = -15511
875782 XDOT = -4728
019738
YDOT = -6980
500232 feet/sec YDOT = -2127
656471 meter/sec
ZDOT = -17206
721916 ZDOT = -5244
608840
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 15332
86119652
00016717 00000-0 10270-3 0 9065
2 25544 51
6440 342
2039 0008136 218
1852 141
8725 15
54331386 13663
Satellite: ISS
Catalog Number: 25544
Epoch time: 15332
86119652 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 342
2039 deg
Eccentricity:
0008136
Arg of perigee: 218
1852 deg
Mean anomaly: 141
8725 deg
Mean motion: 15
54331386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 302
Coasting Arc #8 (Orbit 1380)
---------------------------------------
Vector Time (GMT): 2015/333/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5837558
42 A = 6788176
04 meter
Y = -3327331
51 meter E =
0001920
Z = -957201
90 I = 51
52331
XDOT = 3114
962214 Wp = 22
39398
YDOT = 3768
748032 meter/sec RA = 336
81844 deg
ZDOT = 5901
894055 TA = 327
22749
MA = 327
23939
Ha = 220
715 n
mi
Hp = 215
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19152094
54 X = 5878981
34
Y = -10916441
95 feet Y = -3261820
40 meter
Z = -3140426
19 Z = -928743
63
XDOT = 10219
692303 XDOT = 3043
918305
YDOT = 12364
658899 feet/sec YDOT = 3803
183988 meter/sec
ZDOT = 19363
169472 ZDOT = 5916
853697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18342643
08 X = 5590837
61
Y = -12258885
38 feet Y = -3736508
26 meter
Z = -3016766
62 Z = -919510
46
XDOT = 10059
566634 XDOT = 3066
155910
YDOT = 10275
849542 feet/sec YDOT = 3132
078940 meter/sec
ZDOT = 19427
008611 ZDOT = 5921
352225
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 15333
82557634
00016717 00000-0 10270-3 0 9079
2 25544 51
6447 337
3938 0008139 222
7716 137
2804 15
54399864 13815
Satellite: ISS
Catalog Number: 25544
Epoch time: 15333
82557634 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 337
3938 deg
Eccentricity:
0008139
Arg of perigee: 222
7716 deg
Mean anomaly: 137
2804 deg
Mean motion: 15
54399864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1381
Checksum: 338
Coasting Arc #9 (Orbit 1396)
---------------------------------------
Vector Time (GMT): 2015/334/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6219222
49 A = 6788263
92 meter
Y = 2559714
59 meter E =
0013531
Z = -852908
31 I = 51
49468
XDOT = -1139
605556 Wp = 177
94198
YDOT = -4738
254031 meter/sec RA = 331
83811 deg
ZDOT = -5926
665817 TA = 11
30968
MA = 11
27930
Ha = 220
575 n
mi
Hp = 215
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20404273
26 X = -6243240
49
Y = 8398013
75 feet Y = 2490032
89 meter
Z = -2798255
59 Z = -883178
40
XDOT = -3738
863373 XDOT = -1057
746924
YDOT = -15545
452857 feet/sec YDOT = -4750
539868 meter/sec
ZDOT = -19444
441657 ZDOT = -5932
003220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19561637
50 X = -5962387
11
Y = 10171094
29 feet Y = 3100149
54 meter
Z = -2929576
09 Z = -892934
79
XDOT = -4236
076396 XDOT = -1291
156085
YDOT = -13739
408859 feet/sec YDOT = -4187
771820 meter/sec
ZDOT = -19466
506788 ZDOT = -5933
391269
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 15334
85422888
00016717 00000-0 10270-3 0 9086
2 25544 51
6448 332
2639 0008262 226
1154 133
9317 15
54379719 13975
Satellite: ISS
Catalog Number: 25544
Epoch time: 15334
85422888 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 332
2639 deg
Eccentricity:
0008262
Arg of perigee: 226
1154 deg
Mean anomaly: 133
9317 deg
Mean motion: 15
54379719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1397
Checksum: 335
Coasting Arc #10 (Orbit 1412)
---------------------------------------
Vector Time (GMT): 2015/335/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6090656
90 A = 6785565
03 meter
Y = -1542079
54 meter E =
0007298
Z = 2560036
07 I = 51
45841
XDOT = -813
463022 Wp = 105
11352
YDOT = 5526
347884 meter/sec RA = 326
85093 deg
ZDOT = 5249
820049 TA = 283
73127
MA = 283
81250
Ha = 220
264 n
mi
Hp = 216
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19982470
15 X = 6095012
41
Y = -5059316
07 feet Y = -1473945
52 meter
Z = 8399068
49 Z = 2589633
93
XDOT = -2668
841935 XDOT = -900
701277
YDOT = 18131
062610 feet/sec YDOT = 5516
763251 meter/sec
ZDOT = 17223
819060 ZDOT = 5245
656681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19281766
80 X = 5877082
52
Y = -7137181
33 feet Y = -2175412
87 meter
Z = 8527265
44 Z = 2599110
51
XDOT = -1366
727922 XDOT = -416
578671
YDOT = 16918
824518 feet/sec YDOT = 5156
857713 meter/sec
ZDOT = 17204
677611 ZDOT = 5243
985736
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 15335
88285853
00016717 00000-0 10270-3 0 9090
2 25544 51
6446 327
1330 0008025 231
1638 128
8799 15
54438688 14131
Satellite: ISS
Catalog Number: 25544
Epoch time: 15335
88285853 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 327
1330 deg
Eccentricity:
0008025
Arg of perigee: 231
1638 deg
Mean anomaly: 128
8799 deg
Mean motion: 15
54438688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1413
Checksum: 335
Coasting Arc #11 (Orbit 1427)
---------------------------------------
Vector Time (GMT): 2015/336/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5478873
88 A = 6781472
10 meter
Y = 259982
75 meter E =
0002551
Z = -3985871
25 I = 51
41849
XDOT = 2586
620753 Wp = 180
25320
YDOT = -6040
602043 meter/sec RA = 321
85256 deg
ZDOT = -3951
997591 TA = 48
51112
MA = 48
48923
Ha = 219
948 n
mi
Hp = 216
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17975308
01 X = -5462011
92
Y = 852961
78 feet Y = 198808
73 meter
Z = -13077005
42 Z = -4012445
71
XDOT = 8486
288561 XDOT = 2673
173406
YDOT = -19818
248171 feet/sec YDOT = -6011
192708 meter/sec
ZDOT = -12965
871362 ZDOT = -3939
222142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17651179
19 X = -5380079
42
Y = 3042663
18 feet Y = 927403
74 meter
Z = -13191868
20 Z = -4020881
43
XDOT = 6291
886327 XDOT = 1917
766953
YDOT = -19434
718315 feet/sec YDOT = -5923
702143 meter/sec
ZDOT = -12909
424465 ZDOT = -3934
792577
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 15336
84717825
00016717 00000-0 10270-3 0 9108
2 25544 51
6442 322
3234 0008215 235
0416 124
9966 15
54470891 14286
Satellite: ISS
Catalog Number: 25544
Epoch time: 15336
84717825 = yrday
fracday
Element set: 910
Inclination: 51
6442 deg
RA of node: 322
3234 deg
Eccentricity:
0008215
Arg of perigee: 235
0416 deg
Mean anomaly: 124
9966 deg
Mean motion: 15
54470891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1428
Checksum: 308
Coasting Arc #12 (Orbit 1443)
---------------------------------------
Vector Time (GMT): 2015/337/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4500461
71 A = 6777826
10 meter
Y = 1181022
90 meter E =
0007787
Z = 4932331
23 I = 51
38192
XDOT = -4014
651942 Wp = 190
64277
YDOT = 6154
706643 meter/sec RA = 316
84007 deg
ZDOT = 2182
460422 TA = 237
94912
MA = 238
02478
Ha = 219
795 n
mi
Hp = 216
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14765294
33 X = 4462961
17
Y = 3874747
04 feet Y = 1231140
27 meter
Z = 16182189
06 Z = 4954102
67
XDOT = -13171
430255 XDOT = -4093
778641
YDOT = 20192
607096 feet/sec YDOT = 6109
369692 meter/sec
ZDOT = 7160
303221 ZDOT = 2162
765813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15059470
90 X = 4590126
73
Y = 1787446
67 feet Y = 544813
75 meter
Z = 16276000
58 Z = 4960924
98
XDOT = -10132
239692 XDOT = -3088
306658
YDOT = 20745
300881 feet/sec YDOT = 6323
167709 meter/sec
ZDOT = 7073
950980 ZDOT = 2156
140259
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 15337
87576647
00016717 00000-0 10270-3 0 9118
2 25544 51
6442 317
1926 0008007 238
1837 121
8537 15
54496031 14448
Satellite: ISS
Catalog Number: 25544
Epoch time: 15337
87576647 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 317
1926 deg
Eccentricity:
0008007
Arg of perigee: 238
1837 deg
Mean anomaly: 121
8537 deg
Mean motion: 15
54496031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1444
Checksum: 320
Coasting Arc #13 (Orbit 1458)
---------------------------------------
Vector Time (GMT): 2015/338/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3254218
05 A = 6776081
84 meter
Y = -2712770
28 meter E =
0008508
Z = -5294953
24 I = 51
35282
XDOT = 5029
444739 Wp = 114
64106
YDOT = -5781
152838 meter/sec RA = 311
81656 deg
ZDOT = -132
823308 TA = 154
10870
MA = 154
06610
Ha = 219
502 n
mi
Hp = 216
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10676568
41 X = -3197920
20
Y = -8900164
96 feet Y = -2748846
22 meter
Z = -17371893
83 Z = -5310625
04
XDOT = 16500
802948 XDOT = 5094
362416
YDOT = -18967
036869 feet/sec YDOT = -5724
547287 meter/sec
ZDOT = -435
772007 ZDOT = -108
233448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11830877
22 X = -3606051
38
Y = -7134073
24 feet Y = -2174465
52 meter
Z = -17439039
19 Z = -5315419
14
XDOT = 12803
043897 XDOT = 3902
367780
YDOT = -20458
572698 feet/sec YDOT = -6235
772958 meter/sec
ZDOT = -328
359540 ZDOT = -100
083988
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 15338
84004561
00016717 00000-0 10270-3 0 9128
2 25544 51
6430 312
3815 0008105 242
1854 117
8478 15
54565527 14594
Satellite: ISS
Catalog Number: 25544
Epoch time: 15338
84004561 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 312
3815 deg
Eccentricity:
0008105
Arg of perigee: 242
1854 deg
Mean anomaly: 117
8478 deg
Mean motion: 15
54565527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1459
Checksum: 306
Coasting Arc #14 (Orbit 1474)
---------------------------------------
Vector Time (GMT): 2015/339/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1897459
99 A = 6777278
17 meter
Y = 4154724
47 meter E =
0002625
Z = 5009172
67 I = 51
33672
XDOT = -5585
438264 Wp = 267
12322
YDOT = 4882
943073 meter/sec RA = 306
79222 deg
ZDOT = -1935
287672 TA = 201
73145
MA = 201
74259
Ha = 219
295 n
mi
Hp = 216
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6225262
42 X = 1826526
86
Y = 13630985
81 feet Y = 4175546
41 meter
Z = 16434293
53 Z = 5018218
06
XDOT = -18324
928687 XDOT = -5630
224398
YDOT = 16020
154439 feet/sec YDOT = 4820
232642 meter/sec
ZDOT = -6349
369001 ZDOT = -1962
529626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8396749
32 X = 2559329
19
Y = 12361000
25 feet Y = 3767632
88 meter
Z = 16472520
87 Z = 5020824
36
XDOT = -14319
129815 XDOT = -4364
470768
YDOT = 18341
943431 feet/sec YDOT = 5590
624358 meter/sec
ZDOT = -6468
045220 ZDOT = -1971
460183
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 15339
86858953
00016717 00000-0 10270-3 0 9134
2 25544 51
6432 307
2508 0008189 245
8776 114
1521 15
54594262 14758
Satellite: ISS
Catalog Number: 25544
Epoch time: 15339
86858953 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 307
2508 deg
Eccentricity:
0008189
Arg of perigee: 245
8776 deg
Mean anomaly: 114
1521 deg
Mean motion: 15
54594262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1475
Checksum: 336
Coasting Arc #15 (Orbit 1489)
---------------------------------------
Vector Time (GMT): 2015/340/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -534749
54 A = 6780750
57 meter
Y = -5374021
41 meter E =
0005382
Z = -4103608
23 I = 51
32877
XDOT = 5700
711952 Wp = 186
00196
YDOT = -3458
328257 meter/sec RA = 301
77162 deg
ZDOT = 3780
394480 TA = 123
20114
MA = 123
14953
Ha = 219
153 n
mi
Hp = 216
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1754427
61 X = -454682
12
Y = -17631303
85 feet Y = -5379553
53 meter
Z = -13463281
59 Z = -4106011
66
XDOT = 18703
123202 XDOT = 5720
596153
YDOT = -11346
221316 feet/sec YDOT = -3394
468067 meter/sec
ZDOT = 12402
869028 ZDOT = 3808
135988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5001212
74 X = -1524369
64
Y = -16990540
89 feet Y = -5178716
86 meter
Z = -13472573
41 Z = -4106440
38
XDOT = 14878
171931 XDOT = 4534
866805
YDOT = -14324
646970 feet/sec YDOT = -4366
152397 meter/sec
ZDOT = 12523
406655 ZDOT = 3817
134348
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 15340
83282993
00016717 00000-0 10270-3 0 9149
2 25544 51
6418 302
4388 0008171 249
0176 111
0103 15
54620242 14903
Satellite: ISS
Catalog Number: 25544
Epoch time: 15340
83282993 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 302
4388 deg
Eccentricity:
0008171
Arg of perigee: 249
0176 deg
Mean anomaly: 111
0103 deg
Mean motion: 15
54620242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1490
Checksum: 286
Coasting Arc #16 (Orbit 1505)
---------------------------------------
Vector Time (GMT): 2015/341/19:46:15
829
Vector Time (MET): N/A
Weight (LBS) : 906045
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -718366
51 A = 6784669
49 meter
Y = 6186432
25 meter E =
0007399
Z = 2679247
36 I = 51
32701
XDOT = -5439
294259 Wp = 133
33578
YDOT = 1606
571715 meter/sec RA = 296
76363 deg
ZDOT = -5163
983964 TA = 16
25531
MA = 16
23158
Ha = 218
770 n
mi
Hp = 217
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2356845
50 X = -800506
28
Y = 20296693
73 feet Y = 6177939
61 meter
Z = 8790181
61 Z = 2675558
38
XDOT = -17845
453605 XDOT = -5431
770017
YDOT = 5270
904578 feet/sec YDOT = 1545
788233 meter/sec
ZDOT = -16942
204606 ZDOT = -5190
389033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1853684
11 X = 565002
92
Y = 20356231
67 feet Y = 6204579
41 meter
Z = 8772997
04 Z = 2674009
50
XDOT = -14771
735883 XDOT = -4502
425097
YDOT = 8701
778137 feet/sec YDOT = 2652
301976 meter/sec
ZDOT = -17056
590978 ZDOT = -5198
848930
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 15341
86132993
00016717 00000-0 10270-3 0 9158
2 25544 51
6423 297
3078 0008209 254
0474 105
9775 15
54687696 15067
Satellite: ISS
Catalog Number: 25544
Epoch time: 15341
86132993 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 297
3078 deg
Eccentricity:
0008209
Arg of perigee: 254
0474 deg
Mean anomaly: 105
9775 deg
Mean motion: 15
54687696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1506
Checksum: 339
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