[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
There are no maneuvers
Coasting Arc #1 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2015/105/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2803825
10 A = 6780258
17 meter
Y = 5264824
13 meter E =
0009543
Z = 3220047
36 I = 51
87140
XDOT = -5972
735011 Wp = 111
74069
YDOT = 232
771672 meter/sec RA = 36
89247 deg
ZDOT = 4805
266833 TA = 285
40831
MA = 285
51372
Ha = 218
124 n
mi
Hp = 213
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9198901
24 X = 2729102
33
Y = 17273045
05 feet Y = 5295760
88 meter
Z = 10564459
84 Z = 3233485
80
XDOT = -19595
587305 XDOT = -5998
236316
YDOT = 763
686588 feet/sec YDOT = 165
838578 meter/sec
ZDOT = 15765
311131 ZDOT = 4776
190339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10135923
98 X = 3089429
63
Y = 16704524
11 feet Y = 5091538
95 meter
Z = 10621092
23 Z = 3237308
91
XDOT = -18397
566108 XDOT = -5607
578150
YDOT = 1187
805981 feet/sec YDOT = 362
043263 meter/sec
ZDOT = 15640
567949 ZDOT = 4767
245111
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 15105
50460828
00016717 00000-0 10270-3 0 9002
2 25544 51
6444 37
1895 0005776 222
8021 137
2683 15
55719937 18282
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
50460828 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 37
1895 deg
Eccentricity:
0005776
Arg of perigee: 222
8021 deg
Mean anomaly: 137
2683 deg
Mean motion: 15
55719937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 318
Coasting Arc #2 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2015/106/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -791994
78 A = 6775282
65 meter
Y = -4833031
80 meter E =
0005998
Z = -4686826
29 I = 51
82967
XDOT = 6915
042880 Wp = 92
30275
YDOT = 1647
205720 meter/sec RA = 31
90616 deg
ZDOT = -2870
515972 TA = 149
27239
MA = 149
23726
Ha = 217
915 n
mi
Hp = 213
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2598408
06 X = -715124
75
Y = -15856403
53 feet Y = -4841459
13 meter
Z = -15376726
69 Z = -4690486
42
XDOT = 22687
148558 XDOT = 6910
053510
YDOT = 5404
218243 feet/sec YDOT = 1724
506027 meter/sec
ZDOT = -9417
703320 ZDOT = -2836
936046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3702206
83 X = -1128432
64
Y = -15621023
63 feet Y = -4761288
00 meter
Z = -15391499
81 Z = -4691329
14
XDOT = 21953
041157 XDOT = 6691
286945
YDOT = 3923
864474 feet/sec YDOT = 1195
993892 meter/sec
ZDOT = -9274
014578 ZDOT = -2826
719643
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 15106
46815121
00016717 00000-0 10270-3 0 9019
2 25544 51
6449 32
3743 0005663 227
2603 132
8075 15
55747032 18436
Satellite: ISS
Catalog Number: 25544
Epoch time: 15106
46815121 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 32
3743 deg
Eccentricity:
0005663
Arg of perigee: 227
2603 deg
Mean anomaly: 132
8075 deg
Mean motion: 15
55747032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 289
Coasting Arc #3 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2015/107/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1460103
78 A = 6772523
37 meter
Y = 3945370
22 meter E =
0004829
Z = 5309487
05 I = 51
79415
XDOT = -6974
757969 Wp = 204
85895
YDOT = -3161
982991 meter/sec RA = 26
90480 deg
ZDOT = 427
416513 TA = 241
05017
MA = 241
09860
Ha = 217
678 n
mi
Hp = 213
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4790366
73 X = -1529905
18
Y = 12944128
01 feet Y = 3928652
68 meter
Z = 17419576
93 Z = 5302224
08
XDOT = -22883
064202 XDOT = -6940
957799
YDOT = -10373
959945 feet/sec YDOT = -3239
790260 meter/sec
ZDOT = 1402
285149 ZDOT = 393
616487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3670780
35 X = -1118853
85
Y = 13346679
76 feet Y = 4068067
99 meter
Z = 17387674
79 Z = 5299763
28
XDOT = -22786
785979 XDOT = -6945
412366
YDOT = -7923
663228 feet/sec YDOT = -2415
132552 meter/sec
ZDOT = 1257
955862 ZDOT = 383
424947
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 15107
49590291
00016717 00000-0 10270-3 0 9022
2 25544 51
6456 27
2394 0005807 231
9433 128
1197 15
55803616 18593
Satellite: ISS
Catalog Number: 25544
Epoch time: 15107
49590291 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 27
2394 deg
Eccentricity:
0005807
Arg of perigee: 231
9433 deg
Mean anomaly: 128
1197 deg
Mean motion: 15
55803616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 319
Coasting Arc #4 (Orbit 1873)
---------------------------------------
Vector Time (GMT): 2015/108/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3674431
44 A = 6773975
92 meter
Y = -2756981
99 meter E =
0009870
Z = -4986850
45 I = 51
77049
XDOT = 6038
379224 Wp = 132
02473
YDOT = 4220
356745 meter/sec RA = 21
89708 deg
ZDOT = 2112
230717 TA = 158
53550
MA = 158
49408
Ha = 217
507 n
mi
Hp = 213
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12055221
26 X = 3729212
24
Y = -9045216
50 feet Y = -2715586
28 meter
Z = -16361057
92 Z = -4968867
15
XDOT = 19810
955458 XDOT = 5980
476800
YDOT = 13846
314779 feet/sec YDOT = 4287
558300 meter/sec
ZDOT = 6929
890804 ZDOT = 2141
423444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11084962
22 X = 3378696
49
Y = -10334529
08 feet Y = -3149964
46 meter
Z = -16283416
06 Z = -4963185
22
XDOT = 20421
712048 XDOT = 6224
537832
YDOT = 10770
156453 feet/sec YDOT = 3282
743687 meter/sec
ZDOT = 7054
245836 ZDOT = 2150
134131
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 15108
45939767
00016717 00000-0 10270-3 0 9035
2 25544 51
6458 22
4238 0005747 235
4592 124
6028 15
55816483 18744
Satellite: ISS
Catalog Number: 25544
Epoch time: 15108
45939767 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 22
4238 deg
Eccentricity:
0005747
Arg of perigee: 235
4592 deg
Mean anomaly: 124
6028 deg
Mean motion: 15
55816483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1874
Checksum: 333
Coasting Arc #5 (Orbit 1889)
---------------------------------------
Vector Time (GMT): 2015/109/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5463052
67 A = 6778465
98 meter
Y = 1424339
59 meter E =
0006964
Z = 3744148
47 I = 51
75636
XDOT = -4187
614368 Wp = 105
00645
YDOT = -4797
915479 meter/sec RA = 16
90031 deg
ZDOT = -4280
028691 TA = 30
26730
MA = 30
22710
Ha = 217
403 n
mi
Hp = 213
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17923401
15 X = -5496761
96
Y = 4673030
15 feet Y = 1363059
96 meter
Z = 12283951
66 Z = 3717527
53
XDOT = -13738
892283 XDOT = -4112
860529
YDOT = -15741
192516 feet/sec YDOT = -4844
326469 meter/sec
ZDOT = -14042
088882 ZDOT = -4300
189760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17257758
42 X = -5260164
77
Y = 6932038
30 feet Y = 2112885
27 meter
Z = 12169536
04 Z = 3709274
58
XDOT = -15040
525452 XDOT = -4584
352158
YDOT = -12614
358785 feet/sec YDOT = -3844
856558 meter/sec
ZDOT = -14127
594221 ZDOT = -4306
090718
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 15109
48709876
00016717 00000-0 10270-3 0 9046
2 25544 51
6460 17
2884 0005782 239
1210 120
9376 15
55854326 18904
Satellite: ISS
Catalog Number: 25544
Epoch time: 15109
48709876 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 17
2884 deg
Eccentricity:
0005782
Arg of perigee: 239
1210 deg
Mean anomaly: 120
9376 deg
Mean motion: 15
55854326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1890
Checksum: 324
Coasting Arc #6 (Orbit 1904)
---------------------------------------
Vector Time (GMT): 2015/110/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6533533
45 A = 6782883
62 meter
Y = -81550
71 meter E =
0003302
Z = -1812127
17 I = 51
74075
XDOT = 1631
229622 Wp = 349
25855
YDOT = 4907
670841 meter/sec RA = 11
91797 deg
ZDOT = 5661
965216 TA = 350
84323
MA = 350
84925
Ha = 217
026 n
mi
Hp = 213
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21435477
19 X = 6542762
58
Y = -267554
82 feet Y = -8436
96 meter
Z = -5945299
11 Z = -1780365
52
XDOT = 5351
803222 XDOT = 1548
725422
YDOT = 16101
282286 feet/sec YDOT = 4925
451303 meter/sec
ZDOT = 18576
001366 ZDOT = 5669
688907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21208353
60 X = 6464306
18
Y = -3370136
85 feet Y = -1027217
71 meter
Z = -5809110
46 Z = -1770616
87
XDOT = 7261
464179 XDOT = 2213
294282
YDOT = 13630
395244 feet/sec YDOT = 4154
544470 meter/sec
ZDOT = 18608
151374 ZDOT = 5671
764539
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 15110
45054436
00016717 00000-0 10270-3 0 9051
2 25544 51
6459 12
4728 0005826 243
5342 116
5215 15
55888116 19054
Satellite: ISS
Catalog Number: 25544
Epoch time: 15110
45054436 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 12
4728 deg
Eccentricity:
0005826
Arg of perigee: 243
5342 deg
Mean anomaly: 116
5215 deg
Mean motion: 15
55888116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1905
Checksum: 299
Coasting Arc #7 (Orbit 1920)
---------------------------------------
Vector Time (GMT): 2015/111/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6654167
82 A = 6784026
22 meter
Y = -1191630
95 meter E =
0010770
Z = -479218
22 I = 51
71436
XDOT = 1256
538054 Wp = 169
55061
YDOT = -4616
900381 meter/sec RA = 6
94517 deg
ZDOT = -5998
593623 TA = 15
61803
MA = 15
58483
Ha = 216
834 n
mi
Hp = 213
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21831259
24 X = -6638020
26
Y = -3909550
37 feet Y = -1265951
93 meter
Z = -1572238
26 Z = -511504
15
XDOT = 4122
500176 XDOT = 1337
211346
YDOT = -15147
310961 feet/sec YDOT = -4602
398070 meter/sec
ZDOT = -19680
425271 ZDOT = -5992
293407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22165841
39 X = -6756148
46
Y = -332175
81 feet Y = -101247
19 meter
Z = -1710418
64 Z = -521335
60
XDOT = 1719
265987 XDOT = 524
032273
YDOT = -14019
962876 feet/sec YDOT = -4273
284684 meter/sec
ZDOT = -19652
502934 ZDOT = -5990
082894
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 15111
47819479
00016717 00000-0 10270-3 0 9061
2 25544 51
6465 7
3362 0005884 246
5285 113
5251 15
55915286 19215
Satellite: ISS
Catalog Number: 25544
Epoch time: 15111
47819479 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 7
3362 deg
Eccentricity:
0005884
Arg of perigee: 246
5285 deg
Mean anomaly: 113
5251 deg
Mean motion: 15
55915286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1921
Checksum: 320
Coasting Arc #8 (Orbit 1936)
---------------------------------------
Vector Time (GMT): 2015/112/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5779954
09 A = 6780872
62 meter
Y = 2315918
72 meter E =
0007763
Z = 2676983
75 I = 51
67249
XDOT = -4004
777755 Wp = 83
57601
YDOT = 3973
484012 meter/sec RA = 1
96623 deg
ZDOT = 5197
193798 TA = 306
65436
MA = 306
72570
Ha = 216
549 n
mi
Hp = 213
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18963103
96 X = 5740623
39
Y = 7598158
54 feet Y = 2380334
09 meter
Z = 8782755
07 Z = 2704966
45
XDOT = -13139
034628 XDOT = -4074
158913
YDOT = 13036
364868 feet/sec YDOT = 3928
312133 meter/sec
ZDOT = 17051
160753 ZDOT = 5177
570507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19959935
52 X = 6083788
35
Y = 4101080
07 feet Y = 1250009
20 meter
Z = 8902259
71 Z = 2713408
76
XDOT = -10407
213366 XDOT = -3172
118634
YDOT = 13738
096463 feet/sec YDOT = 4187
371802 meter/sec
ZDOT = 16966
246251 ZDOT = 5171
311857
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 15112
50581885
00016717 00000-0 10270-3 0 9074
2 25544 51
6462 2
1992 0005837 251
5570 108
4949 15
55963786 19377
Satellite: ISS
Catalog Number: 25544
Epoch time: 15112
50581885 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 2
1992 deg
Eccentricity:
0005837
Arg of perigee: 251
5570 deg
Mean anomaly: 108
4949 deg
Mean motion: 15
55963786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1937
Checksum: 335
Coasting Arc #9 (Orbit 1951)
---------------------------------------
Vector Time (GMT): 2015/113/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4007780
15 A = 6775555
27 meter
Y = -3264365
74 meter E =
0003273
Z = -4384039
60 I = 51
62430
XDOT = 6175
183490 Wp = 57
55136
YDOT = -3020
345113 meter/sec RA = 356
96892 deg
ZDOT = -3396
376051 TA = 178
04512
MA = 178
04384
Ha = 216
205 n
mi
Hp = 213
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13148885
00 X = -3949683
13
Y = -10709861
36 feet Y = -3308858
58 meter
Z = -14383332
02 Z = -4403367
65
XDOT = 20259
788352 XDOT = 6224
997243
YDOT = -9909
268744 feet/sec YDOT = -2951
011702 meter/sec
ZDOT = -11142
966048 ZDOT = -3366
256864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14898948
62 X = -4541199
54
Y = -7952607
18 feet Y = -2423954
67 meter
Z = -14465542
37 Z = -4409097
32
XDOT = 17421
213875 XDOT = 5309
985989
YDOT = -12606
109909 feet/sec YDOT = -3842
342300 meter/sec
ZDOT = -11013
246089 ZDOT = -3356
837408
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 15113
46919207
00016717 00000-0 10270-3 0 9084
2 25544 51
6468 357
3834 0005910 255
7961 104
2537 15
56027520 19527
Satellite: ISS
Catalog Number: 25544
Epoch time: 15113
46919207 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 357
3834 deg
Eccentricity:
0005910
Arg of perigee: 255
7961 deg
Mean anomaly: 104
2537 deg
Mean motion: 15
56027520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1952
Checksum: 315
Coasting Arc #10 (Orbit 1967)
---------------------------------------
Vector Time (GMT): 2015/114/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1633072
70 A = 6771975
09 meter
Y = 3968044
71 meter E =
0004150
Z = 5241983
90 I = 51
58077
XDOT = -7396
004254 Wp = 225
65568
YDOT = 1798
857946 meter/sec RA = 351
95137 deg
ZDOT = 940
062201 TA = 215
32996
MA = 215
35747
Ha = 215
969 n
mi
Hp = 213
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5357850
05 X = 1563115
92
Y = 13018519
40 feet Y = 3985915
75 meter
Z = 17198109
91 Z = 5249747
11
XDOT = -24265
105821 XDOT = -7420
136327
YDOT = 5901
764915 feet/sec YDOT = 1716
016082 meter/sec
ZDOT = 3084
193574 ZDOT = 904
074931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7892916
95 X = 2405761
09
Y = 11609117
74 feet Y = 3538459
09 meter
Z = 17230601
74 Z = 5251887
41
XDOT = -21631
234165 XDOT = -6593
200173
YDOT = 10347
135988 feet/sec YDOT = 3153
807049 meter/sec
ZDOT = 2929
564405 ZDOT = 892
931231
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 15114
49676578
00016717 00000-0 10270-3 0 9090
2 25544 51
6466 352
2459 0006022 259
2842 100
7634 15
56066645 19681
Satellite: ISS
Catalog Number: 25544
Epoch time: 15114
49676578 = yrday
fracday
Element set: 909
Inclination: 51
6466 deg
RA of node: 352
2459 deg
Eccentricity:
0006022
Arg of perigee: 259
2842 deg
Mean anomaly: 100
7634 deg
Mean motion: 15
56066645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1968
Checksum: 335
Coasting Arc #11 (Orbit 1982)
---------------------------------------
Vector Time (GMT): 2015/115/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 970591
53 A = 6772650
14 meter
Y = -4372066
87 meter E =
0007819
Z = -5087452
39 I = 51
55230
XDOT = 7464
392315 Wp = 117
74292
YDOT = -337
583531 meter/sec RA = 346
92555 deg
ZDOT = 1712
634184 TA = 168
84046
MA = 168
82311
Ha = 215
796 n
mi
Hp = 213
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3184355
40 X = 1044121
96
Y = -14344051
43 feet Y = -4360802
11 meter
Z = -16691116
78 Z = -5082558
69
XDOT = 24489
476099 XDOT = 7459
293100
YDOT = -1107
557516 feet/sec YDOT = -254
140277 meter/sec
ZDOT = 5618
878558 ZDOT = 1748
882581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -83276
12 X = -25382
56
Y = -14717803
07 feet Y = -4485986
38 meter
Z = -16669272
56 Z = -5080794
28
XDOT = 22476
313195 XDOT = 6850
780262
YDOT = -6672
894368 feet/sec YDOT = -2033
898203 meter/sec
ZDOT = 5774
331509 ZDOT = 1760
016244
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 15115
46009364
00016717 00000-0 10270-3 0 9103
2 25544 51
6470 347
4296 0006079 263
8527 96
1934 15
56097285 19836
Satellite: ISS
Catalog Number: 25544
Epoch time: 15115
46009364 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 347
4296 deg
Eccentricity:
0006079
Arg of perigee: 263
8527 deg
Mean anomaly: 96
1934 deg
Mean motion: 15
56097285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1983
Checksum: 333
Coasting Arc #12 (Orbit 1998)
---------------------------------------
Vector Time (GMT): 2015/116/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3368085
72 A = 6777008
28 meter
Y = 4378627
41 meter E =
0005211
Z = 3922787
38 I = 51
53655
XDOT = -6391
183231 Wp = 71
28487
YDOT = -1289
796291 meter/sec RA = 341
90845 deg
ZDOT = -4041
724103 TA = 61
03155
MA = 60
97931
Ha = 215
671 n
mi
Hp = 213
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11050150
01 X = -3435853
78
Y = 14365575
48 feet Y = 4340584
52 meter
Z = 12870037
33 Z = 3906261
00
XDOT = -20968
448919 XDOT = -6356
652131
YDOT = -4231
615129 feet/sec YDOT = -1361
073777 meter/sec
ZDOT = -13260
249681 ZDOT = -4072
687460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7259231
06 X = -2212613
63
Y = 16661923
76 feet Y = 5078554
36 meter
Z = 12798331
76 Z = 3900931
52
XDOT = -20068
587645 XDOT = -6116
905514
YDOT = 1559
061842 feet/sec YDOT = 475
202049 meter/sec
ZDOT = -13392
719964 ZDOT = -4082
101045
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 15116
48761851
00016717 00000-0 10270-3 0 9113
2 25544 51
6470 342
2924 0006097 268
6822 91
3633 15
56143513 19994
Satellite: ISS
Catalog Number: 25544
Epoch time: 15116
48761851 = yrday
fracday
Element set: 911
Inclination: 51
6470 deg
RA of node: 342
2924 deg
Eccentricity:
0006097
Arg of perigee: 268
6822 deg
Mean anomaly: 91
3633 deg
Mean motion: 15
56143513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1999
Checksum: 321
Coasting Arc #13 (Orbit 2013)
---------------------------------------
Vector Time (GMT): 2015/117/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5169004
20 A = 6781802
08 meter
Y = -3912689
12 meter E =
0005885
Z = -1977643
04 I = 51
52313
XDOT = 4366
917747 Wp = 341
43905
YDOT = 2952
856377 meter/sec RA = 336
90730 deg
ZDOT = 5572
683746 TA = 356
67794
MA = 356
68184
Ha = 215
572 n
mi
Hp = 213
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16958675
21 X = 5221979
36
Y = -12836906
57 feet Y = -3854589
84 meter
Z = -6488330
17 Z = -1952403
99
XDOT = 14327
157964 XDOT = 4306
503473
YDOT = 9687
849006 feet/sec YDOT = 3001
352605 meter/sec
ZDOT = 18283
083157 ZDOT = 5593
750612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13035100
65 X = 3973098
68
Y = -16848470
27 feet Y = -5135413
74 meter
Z = -6379378
04 Z = -1944434
43
XDOT = 15026
817849 XDOT = 4580
174080
YDOT = 4670
341665 feet/sec YDOT = 1423
520140 meter/sec
ZDOT = 18372
801208 ZDOT = 5600
029808
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 15117
45090002
00016717 00000-0 10270-3 0 9125
2 25544 51
6471 337
4754 0006238 272
4158 87
6281 15
56166504 20145
Satellite: ISS
Catalog Number: 25544
Epoch time: 15117
45090002 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 337
4754 deg
Eccentricity:
0006238
Arg of perigee: 272
4158 deg
Mean anomaly: 87
6281 deg
Mean motion: 15
56166504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2014
Checksum: 294
Coasting Arc #14 (Orbit 2029)
---------------------------------------
Vector Time (GMT): 2015/118/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6108094
20 A = 6783356
84 meter
Y = 2913268
19 meter E =
0007942
Z = -383338
16 I = 51
49934
XDOT = -1754
335120 Wp = 170
60538
YDOT = -4462
844371 meter/sec RA = 331
91852 deg
ZDOT = -5988
130783 TA = 13
53875
MA = 13
51746
Ha = 215
565 n
mi
Hp = 213
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20039679
13 X = -6138354
96
Y = 9557966
49 feet Y = 2844794
26 meter
Z = -1257671
12 Z = -413084
00
XDOT = -5755
692650 XDOT = -1675
211820
YDOT = -14641
877856 feet/sec YDOT = -4482
020448 meter/sec
ZDOT = -19646
098368 ZDOT = -5996
460616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16569681
72 X = -5050438
99
Y = 14766536
05 feet Y = 4500840
19 meter
Z = -1385734
59 Z = -422371
90
XDOT = -8415
657349 XDOT = -2565
092360
YDOT = -11283
168707 feet/sec YDOT = -3439
109822 meter/sec
ZDOT = -19680
926261 ZDOT = -5998
746324
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 15118
47837703
00016717 00000-0 10270-3 0 9136
2 25544 51
6469 332
3382 0006299 274
5770 85
4664 15
56159057 20307
Satellite: ISS
Catalog Number: 25544
Epoch time: 15118
47837703 = yrday
fracday
Element set: 913
Inclination: 51
6469 deg
RA of node: 332
3382 deg
Eccentricity:
0006299
Arg of perigee: 274
5770 deg
Mean anomaly: 85
4664 deg
Mean motion: 15
56159057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2030
Checksum: 327
Coasting Arc #15 (Orbit 2045)
---------------------------------------
Vector Time (GMT): 2015/119/10:43:46
723
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6065507
95 A = 6780118
66 meter
Y = -1415300
35 meter E =
0007979
Z = 2667022
23 I = 51
46107
XDOT = -983
686585 Wp = 60
19261
YDOT = 5569
521127 meter/sec RA = 326
92306 deg
ZDOT = 5184
955583 TA = 330
02237
MA = 330
06803
Ha = 215
613 n
mi
Hp = 213
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19899960
46 X = 6067927
84
Y = -4643373
86 feet Y = -1347458
18 meter
Z = 8750072
94 Z = 2696493
57
XDOT = -3227
318193 XDOT = -1071
080024
YDOT = 18272
707110 feet/sec YDOT = 5558
032583 meter/sec
ZDOT = 17011
009132 ZDOT = 5179
964350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17586507
53 X = 5360367
50
Y = -10298195
13 feet Y = -3138889
88 meter
Z = 8876657
78 Z = 2705605
29
XDOT = 1461
763992 XDOT = 445
545665
YDOT = 17161
419325 feet/sec YDOT = 5230
800610 meter/sec
ZDOT = 16988
531147 ZDOT = 5178
104294
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 15119
50582727
00016717 00000-0 10270-3 0 9145
2 25544 51
6462 327
1994 0006420 281
1558 78
8874 15
56229102 20460
Satellite: ISS
Catalog Number: 25544
Epoch time: 15119
50582727 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 327
1994 deg
Eccentricity:
0006420
Arg of perigee: 281
1558 deg
Mean anomaly: 78
8874 deg
Mean motion: 15
56229102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2046
Checksum: 319
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