[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 6th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 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
105/14:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 218
1
000/00:00:00
000 0
0 0
0 213
5
111/11:13:10
493 0
8 1
0 1
0
N/A 0
4 -0
0 216
9
000/00:02:20
986 0
3 -0
1 214
6
Coasting Arc #1 (Orbit 1687)
---------------------------------------
Vector Time (GMT): 2015/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4062888
22 A = 6776932
63 meter
Y = 2932154
10 meter E =
0012506
Z = -4575266
33 I = 51
99221
XDOT = -1424
620603 Wp = 136
49343
YDOT = 6848
990525 meter/sec RA = 81
34848 deg
ZDOT = 3120
474833 TA = 164
65801
MA = 164
62006
Ha = 219
814 n
mi
Hp = 212
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13329685
76 X = 4052023
45
Y = 9619928
15 feet Y = 2977526
71 meter
Z = -15010716
30 Z = -4555556
06
XDOT = -4673
952110 XDOT = -1516
260069
YDOT = 22470
441356 feet/sec YDOT = 6832
547452 meter/sec
ZDOT = 10237
778322 ZDOT = 3113
330849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15312437
53 X = 4667230
96
Y = 6186118
59 feet Y = 1885528
95 meter
Z = -14926698
82 Z = -4549657
80
XDOT = 1138
259045 XDOT = 346
941357
YDOT = 21838
690174 feet/sec YDOT = 6656
432765 meter/sec
ZDOT = 10205
934819 ZDOT = 3110
768933
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 15096
51051411
00016717 00000-0 10270-3 0 9006
2 25544 51
6413 82
1156 0005699 186
6175 173
4904 15
55377464 16886
Satellite: ISS
Catalog Number: 25544
Epoch time: 15096
51051411 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 82
1156 deg
Eccentricity:
0005699
Arg of perigee: 186
6175 deg
Mean anomaly: 173
4904 deg
Mean motion: 15
55377464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1688
Checksum: 316
Coasting Arc #2 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2015/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3657500
73 A = 6781455
76 meter
Y = -4777870
40 meter E =
0013640
Z = 3109483
06 I = 52
00243
XDOT = 2677
098838 Wp = 119
62530
YDOT = -5253
978030 meter/sec RA = 76
37619 deg
ZDOT = -4914
543655 TA = 24
74233
MA = 24
67697
Ha = 219
656 n
mi
Hp = 212
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11999674
32 X = -3618906
54
Y = -15675427
82 feet Y = -4818554
87 meter
Z = 10201716
07 Z = 3091809
58
XDOT = 8783
132672 XDOT = 2759
524456
YDOT = -17237
460728 feet/sec YDOT = -5223
580562 meter/sec
ZDOT = -16123
830888 ZDOT = -4901
337935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15627444
64 X = -4763245
13
Y = -12125087
44 feet Y = -3695726
65 meter
Z = 10126769
49 Z = 3086639
34
XDOT = 3365
987890 XDOT = 1025
953109
YDOT = -17782
978397 feet/sec YDOT = -5420
251816 meter/sec
ZDOT = -16066
257233 ZDOT = -4896
995205
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 15097
53849084
00016717 00000-0 10270-3 0 9011
2 25544 51
6414 76
9806 0005637 191
5036 168
5990 15
55444714 17045
Satellite: ISS
Catalog Number: 25544
Epoch time: 15097
53849084 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 76
9806 deg
Eccentricity:
0005637
Arg of perigee: 191
5036 deg
Mean anomaly: 168
5990 deg
Mean motion: 15
55444714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 330
Coasting Arc #3 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2015/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2963301
32 A = 6784853
62 meter
Y = 5993406
93 meter E =
0004824
Z = -1150969
36 I = 52
00595
XDOT = -3843
588460 Wp = 67
96825
YDOT = 3029
254454 meter/sec RA = 71
41879 deg
ZDOT = 5899
874808 TA = 279
60016
MA = 279
65466
Ha = 219
475 n
mi
Hp = 212
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9722117
20 X = 2901652
44
Y = 19663408
55 feet Y = 6026199
71 meter
Z = -3776146
20 Z = -1136724
24
XDOT = -12610
198358 XDOT = -3905
836406
YDOT = 9938
498866 feet/sec YDOT = 2985
925359 meter/sec
ZDOT = 19356
544646 ZDOT = 5881
051714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14672957
77 X = 4472317
53
Y = 16319410
00 feet Y = 4974156
17 meter
Z = -3716133
28 Z = -1132677
42
XDOT = -8401
914683 XDOT = -2560
903595
YDOT = 11927
158991 feet/sec YDOT = 3635
398061 meter/sec
ZDOT = 19275
267613 ZDOT = 5875
101568
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 15098
50219983
00016717 00000-0 10270-3 0 9029
2 25544 51
6415 72
1671 0005732 193
2576 166
8428 15
55479452 17198
Satellite: ISS
Catalog Number: 25544
Epoch time: 15098
50219983 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 72
1671 deg
Eccentricity:
0005732
Arg of perigee: 193
2576 deg
Mean anomaly: 166
8428 deg
Mean motion: 15
55479452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1719
Checksum: 331
Coasting Arc #4 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2015/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1915677
00 A = 6784880
31 meter
Y = -6418072
51 meter E =
0013513
Z = -1031846
76 I = 51
99635
XDOT = 4840
846011 Wp = 161
79247
YDOT = -496
317076 meter/sec RA = 66
46671 deg
ZDOT = -5933
536428 TA = 29
34887
MA = 29
27304
Ha = 219
260 n
mi
Hp = 212
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6285029
53 X = -1838753
83
Y = -21056668
36 feet Y = -6439064
83 meter
Z = -3385324
00 Z = -1040965
57
XDOT = 15882
040719 XDOT = 4874
859386
YDOT = -1628
336862 feet/sec YDOT = -441
993794 meter/sec
ZDOT = -19466
983032 ZDOT = -5909
937626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12011578
26 X = -3661129
05
Y = -18394253
72 feet Y = -5606568
53 meter
Z = -3423260
86 Z = -1043409
91
XDOT = 13533
337239 XDOT = 4124
961191
YDOT = -5253
448752 feet/sec YDOT = -1601
251179 meter/sec
ZDOT = -19365
678490 ZDOT = -5902
658804
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 15099
53013434
00016717 00000-0 10270-3 0 9037
2 25544 51
6426 67
0317 0005604 198
8793 161
2153 15
55501368 17354
Satellite: ISS
Catalog Number: 25544
Epoch time: 15099
53013434 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 67
0317 deg
Eccentricity:
0005604
Arg of perigee: 198
8793 deg
Mean anomaly: 161
2153 deg
Mean motion: 15
55501368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1735
Checksum: 305
Coasting Arc #5 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2015/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 586374
63 A = 6781269
43 meter
Y = 6038824
05 meter E =
0011460
Z = 3024408
03 I = 51
97167
XDOT = -5494
867501 Wp = 109
52386
YDOT = -1967
546942 meter/sec RA = 61
50847 deg
ZDOT = 4974
917252 TA = 284
97308
MA = 285
09991
Ha = 219
067 n
mi
Hp = 212
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1923801
28 X = 504111
92
Y = 19812414
88 feet Y = 6044921
51 meter
Z = 9922598
54 Z = 3027056
37
XDOT = -18027
780516 XDOT = -5496
624015
YDOT = -6455
206504 feet/sec YDOT = -2029
003657 meter/sec
ZDOT = 16321
906996 ZDOT = 4948
219891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7753532
44 X = 2363276
69
Y = 18327906
07 feet Y = 5586345
77 meter
Z = 9932842
00 Z = 3027530
24
XDOT = -17896
804643 XDOT = -5454
946055
YDOT = -1246
464403 feet/sec YDOT = -379
922350 meter/sec
ZDOT = 16207
765285 ZDOT = 4940
126859
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 15100
55804523
00016717 00000-0 10270-3 0 9040
2 25544 51
6428 61
8974 0005798 202
9947 157
0948 15
55564355 17517
Satellite: ISS
Catalog Number: 25544
Epoch time: 15100
55804523 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 61
8974 deg
Eccentricity:
0005798
Arg of perigee: 202
9947 deg
Mean anomaly: 157
0948 deg
Mean motion: 15
55564355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 331
Coasting Arc #6 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2015/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1005834
70 A = 6776402
72 meter
Y = -4930033
32 meter E =
0006868
Z = -4543940
17 I = 51
93986
XDOT = 5667
961385 Wp = 103
21655
YDOT = 4073
052284 meter/sec RA = 56
53250 deg
ZDOT = -3170
034294 TA = 135
12907
MA = 135
07353
Ha = 218
929 n
mi
Hp = 213
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3299982
60 X = 1082961
61
Y = -16174650
00 feet Y = -4918354
46 meter
Z = -14907940
20 Z = -4538866
36
XDOT = 18595
673836 XDOT = 5637
393208
YDOT = 13363
032427 feet/sec YDOT = 4136
264019 meter/sec
ZDOT = -10400
374981 ZDOT = -3142
574801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1928190
08 X = -587712
34
Y = -16415449
48 feet Y = -5003429
00 meter
Z = -14885260
16 Z = -4537027
30
XDOT = 20745
759300 XDOT = 6323
307435
YDOT = 6871
423356 feet/sec YDOT = 2094
409839 meter/sec
ZDOT = -10283
358473 ZDOT = -3134
367662
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 15101
52169355
00016717 00000-0 10270-3 0 9056
2 25544 51
6432 57
0826 0005609 206
8226 153
2638 15
55569962 17668
Satellite: ISS
Catalog Number: 25544
Epoch time: 15101
52169355 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 57
0826 deg
Eccentricity:
0005609
Arg of perigee: 206
8226 deg
Mean anomaly: 153
2638 deg
Mean motion: 15
55569962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1766
Checksum: 318
Coasting Arc #7 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2015/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2653370
49 A = 6773223
43 meter
Y = 3312445
62 meter E =
0006416
Z = 5279508
56 I = 51
91181
XDOT = -5238
376127 Wp = 181
14386
YDOT = -5540
399381 meter/sec RA = 51
54189 deg
ZDOT = 837
199838 TA = 260
84876
MA = 260
92135
Ha = 218
723 n
mi
Hp = 213
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8705283
75 X = -2715859
78
Y = 10867603
72 feet Y = 3282424
86 meter
Z = 17321222
32 Z = 5266466
96
XDOT = -17186
273381 XDOT = -5180
099551
YDOT = -18177
163323 feet/sec YDOT = -5598
652424 meter/sec
ZDOT = 2746
718630 ZDOT = 811
894689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4672815
50 X = -1424274
17
Y = 13191195
91 feet Y = 4020676
51 meter
Z = 17264665
19 Z = 5262269
95
XDOT = -21329
513133 XDOT = -6501
235603
YDOT = -11036
790526 feet/sec YDOT = -3364
013752 meter/sec
ZDOT = 2639
222277 ZDOT = 804
434950
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 15102
54956116
00016717 00000-0 10270-3 0 9069
2 25544 51
6436 51
9481 0005684 211
9059 148
1751 15
55620258 17829
Satellite: ISS
Catalog Number: 25544
Epoch time: 15102
54956116 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 51
9481 deg
Eccentricity:
0005684
Arg of perigee: 211
9059 deg
Mean anomaly: 148
1751 deg
Mean motion: 15
55620258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 312
Coasting Arc #8 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2015/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4206863
42 A = 6773934
66 meter
Y = -1408888
38 meter E =
0012389
Z = -5129281
54 I = 51
89373
XDOT = 4120
848132 Wp = 127
27244
YDOT = 6242
494055 meter/sec RA = 46
54318 deg
ZDOT = 1660
563639 TA = 158
74080
MA = 158
68928
Ha = 218
546 n
mi
Hp = 213
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13802045
36 X = 4247221
46
Y = -4622337
20 feet Y = -1361619
25 meter
Z = -16828351
52 Z = -5108747
24
XDOT = 13519
842954 XDOT = 4042
670400
YDOT = 20480
623541 feet/sec YDOT = 6288
139090 meter/sec
ZDOT = 5448
043436 ZDOT = 1680
391556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11404913
70 X = 3476217
70
Y = -9206287
35 feet Y = -2806076
39 meter
Z = -16740014
60 Z = -5102356
45
XDOT = 19137
901885 XDOT = 5833
232495
YDOT = 13622
248919 feet/sec YDOT = 4152
061471 meter/sec
ZDOT = 5531
908790 ZDOT = 1686
125799
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 15103
51316743
00016717 00000-0 10270-3 0 9074
2 25544 51
6436 47
1328 0005643 215
3519 144
7261 15
55628725 17971
Satellite: ISS
Catalog Number: 25544
Epoch time: 15103
51316743 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 47
1328 deg
Eccentricity:
0005643
Arg of perigee: 215
3519 deg
Mean anomaly: 144
7261 deg
Mean motion: 15
55628725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1797
Checksum: 309
Coasting Arc #9 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2015/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5383291
74 A = 6777888
71 meter
Y = -493293
30 meter E =
0007243
Z = 4081109
20 I = 51
88546
XDOT = -2379
079832 Wp = 106
81890
YDOT = -6177
632105 meter/sec RA = 41
55324 deg
ZDOT = -3881
259219 TA = 23
20206
MA = 23
16938
Ha = 218
474 n
mi
Hp = 213
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17661718
32 X = -5397200
07
Y = -1618416
35 feet Y = -553570
16 meter
Z = 13389465
88 Z = 4054924
42
XDOT = -7805
380025 XDOT = -2290
969510
YDOT = -20267
821866 feet/sec YDOT = -6203
744251 meter/sec
ZDOT = -12733
790088 ZDOT = -3892
601747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17103547
68 X = -5213161
33
Y = 5001647
42 feet Y = 1524502
13 meter
Z = 13277256
57 Z = 4046907
80
XDOT = -14252
956274 XDOT = -4344
301072
YDOT = -14778
411101 feet/sec YDOT = -4504
459704 meter/sec
ZDOT = -12781
267327 ZDOT = -3895
730281
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 15104
54099153
00016717 00000-0 10270-3 0 9082
2 25544 51
6442 41
9976 0005656 219
1244 140
9501 15
55668778 18136
Satellite: ISS
Catalog Number: 25544
Epoch time: 15104
54099153 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 41
9976 deg
Eccentricity:
0005656
Arg of perigee: 219
1244 deg
Mean anomaly: 140
9501 deg
Mean motion: 15
55668778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 322
Coasting Arc #10 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2015/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904230
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5989701
74 A = 6782565
56 meter
Y = 2171334
50 meter E =
0000233
Z = -2326355
74 I = 51
87700
XDOT = 145
874841 Wp = 62
97783
YDOT = 5412
001599 meter/sec RA = 36
57729 deg
ZDOT = 5427
470159 TA = 271
17362
MA = 271
17630
Ha = 218
129 n
mi
Hp = 213
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19651252
43 X = 5976276
82
Y = 7123800
87 feet Y = 2238239
95 meter
Z = -7632400
73 Z = -2297291
63
XDOT = 478
591999 XDOT = 58
980956
YDOT = 17755
910759 feet/sec YDOT = 5413
147604 meter/sec
ZDOT = 17806
660626 ZDOT = 5427
967148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20925791
30 X = 6378181
19
Y = -955234
43 feet Y = -291155
45 meter
Z = -7508168
06 Z = -2288489
62
XDOT = 7061
693143 XDOT = 2152
404070
YDOT = 14740
781457 feet/sec YDOT = 4492
990188 meter/sec
ZDOT = 17807
763343 ZDOT = 5427
806267
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
50455567
00016717 00000-0 10270-3 0 9095
2 25544 51
6442 37
1825 0005663 223
5115 136
5592 15
55690292 18283
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
50455567 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 37
1825 deg
Eccentricity:
0005663
Arg of perigee: 223
5115 deg
Mean anomaly: 136
5592 deg
Mean motion: 15
55690292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 312
Coasting Arc #11 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2015/105/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -113138
18 A = 6774827
00 meter
Y = -4765515
32 meter E =
0007073
Z = -4819980
21 I = 51
85098
XDOT = 6793
818430 Wp = 93
57601
YDOT = 2441
957313 meter/sec RA = 36
05683 deg
ZDOT = -2577
517269 TA = 151
13036
MA = 151
09121
Ha = 218
074 n
mi
Hp = 213
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -371188
25 X = -36426
86
Y = -15634892
77 feet Y = -4766352
11 meter
Z = -15813583
37 Z = -4820342
97
XDOT = 22289
430546 XDOT = 6778
527635
YDOT = 8011
670974 feet/sec YDOT = 2517
844453 meter/sec
ZDOT = -8456
421485 ZDOT = -2544
551446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14067441
36 X = -4287756
13
Y = -6831852
03 feet Y = -2082348
50 meter
Z = -15814232
93 Z = -4820178
20
XDOT = 16753
338682 XDOT = 5106
417630
YDOT = -15276
144428 feet/sec YDOT = -4656
168822 meter/sec
ZDOT = -8315
508356 ZDOT = -2534
566947
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
63302854
00016717 00000-0 10270-3 0 9101
2 25544 51
6464 36
5410 0005659 224
2057 135
8645 15
55725351 18307
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
63302854 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 36
5410 deg
Eccentricity:
0005659
Arg of perigee: 224
2057 deg
Mean anomaly: 135
8645 deg
Mean motion: 15
55725351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 292
Coasting Arc #12 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2015/106/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2048526
26 A = 6772604
28 meter
Y = 3653489
20 meter E =
0004427
Z = 5323644
35 I = 51
81793
XDOT = -6615
592634 Wp = 204
39036
YDOT = -3879
895916 meter/sec RA = 31
05523 deg
ZDOT = 113
113366 TA = 244
51175
MA = 244
55755
Ha = 217
917 n
mi
Hp = 213
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6720886
68 X = -2115088
72
Y = 11986513
12 feet Y = 3630209
67 meter
Z = 17466024
77 Z = 5313530
82
XDOT = -21704
700242 XDOT = -6572
264496
YDOT = -12729
317311 feet/sec YDOT = -3953
633524 meter/sec
ZDOT = 371
106843 ZDOT = 81
081476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7797875
00 X = 2376792
30
Y = 11383207
66 feet Y = 3469601
70 meter
Z = 17421956
40 Z = 5310212
31
XDOT = -20104
634129 XDOT = -6127
892483
YDOT = 13393
825168 feet/sec YDOT = 4082
437911 meter/sec
ZDOT = 234
485348 ZDOT = 71
471134
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
66080537
00016717 00000-0 10270-3 0 9117
2 25544 51
6467 31
4052 0005757 227
9243 132
1421 15
55759121 18463
Satellite: ISS
Catalog Number: 25544
Epoch time: 15106
66080537 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 31
4052 deg
Eccentricity:
0005757
Arg of perigee: 227
9243 deg
Mean anomaly: 132
1421 deg
Mean motion: 15
55759121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 294
Coasting Arc #13 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2015/107/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4108883
10 A = 6774485
53 meter
Y = -2275474
93 meter E =
0009742
Z = -4890343
03 I = 51
79674
XDOT = 5494
533202 Wp = 136
10391
YDOT = 4778
658064 meter/sec RA = 26
05044 deg
ZDOT = 2389
017751 TA = 157
28927
MA = 157
24615
Ha = 217
680 n
mi
Hp = 213
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13480587
59 X = 4157778
41
Y = -7465468
94 feet Y = -2229253
86 meter
Z = -16044432
51 Z = -4870263
58
XDOT = 18026
683735 XDOT = 5429
083626
YDOT = 15678
012021 feet/sec YDOT = 4839
735834 meter/sec
ZDOT = 7837
984746 ZDOT = 2415
550012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1047595
43 X = -319307
09
Y = -15463875
69 feet Y = -4713389
31 meter
Z = -15957893
82 Z = -4863966
04
XDOT = 20666
588302 XDOT = 6299
176115
YDOT = -9618
506244 feet/sec YDOT = -2931
720703 meter/sec
ZDOT = 7950
836296 ZDOT = 2423
414903
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
62432657
00016717 00000-0 10270-3 0 9129
2 25544 51
6467 26
5900 0005787 232
5180 127
5448 15
55783683 18619
Satellite: ISS
Catalog Number: 25544
Epoch time: 15107
62432657 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 26
5900 deg
Eccentricity:
0005787
Arg of perigee: 232
5180 deg
Mean anomaly: 127
5448 deg
Mean motion: 15
55783683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 322
Coasting Arc #14 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2015/108/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5701618
40 A = 6779079
22 meter
Y = 814123
60 meter E =
0007806
Z = 3566736
37 I = 51
78391
XDOT = -3535
052819 Wp = 109
44126
YDOT = -5135
330449 meter/sec RA = 21
05741 deg
ZDOT = -4473
386305 TA = 28
48260
MA = 28
43996
Ha = 217
517 n
mi
Hp = 213
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18706097
10 X = -5727624
54
Y = 2671009
18 feet Y = 750219
30 meter
Z = 11701890
98 Z = 3538975
29
XDOT = -11597
942318 XDOT = -3455
635179
YDOT = -16848
197010 feet/sec YDOT = -5174
418086 meter/sec
ZDOT = -14676
464256 ZDOT = -4490
365828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5178040
26 X = -1578266
67
Y = 18248713
43 feet Y = 5562207
85 meter
Z = 11582701
26 Z = 3530407
34
XDOT = -18737
498969 XDOT = -5711
189686
YDOT = 4055
599564 feet/sec YDOT = 1236
146747 meter/sec
ZDOT = -14748
272687 ZDOT = -4495
273515
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
65206072
00016717 00000-0 10270-3 0 9134
2 25544 51
6470 21
4545 0005733 237
1690 122
8912 15
55832866 18779
Satellite: ISS
Catalog Number: 25544
Epoch time: 15108
65206072 = yrday
fracday
Element set: 913
Inclination: 51
6470 deg
RA of node: 21
4545 deg
Eccentricity:
0005733
Arg of perigee: 237
1690 deg
Mean anomaly: 122
8912 deg
Mean motion: 15
55832866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1877
Checksum: 307
Coasting Arc #15 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2015/109/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6564255
71 A = 6783340
99 meter
Y = 581763
53 meter E =
0003602
Z = -1598027
29 I = 51
76771
XDOT = 956
198635 Wp = 356
81988
YDOT = 4986
950033 meter/sec RA = 16
07843 deg
ZDOT = 5746
194837 TA = 345
72167
MA = 345
73185
Ha = 217
217 n
mi
Hp = 213
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21536272
01 X = 6565025
18
Y = 1908673
01 feet Y = 655173
52 meter
Z = -5242871
69 Z = -1566136
98
XDOT = 3137
134629 XDOT = 872
448910
YDOT = 16361
384623 feet/sec YDOT = 4997
175010 meter/sec
ZDOT = 18852
345265 ZDOT = 5750
636172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10168685
42 X = 3099415
32
Y = -19117158
12 feet Y = -5826909
80 meter
Z = -5106256
00 Z = -1556386
83
XDOT = 14850
181067 XDOT = 4526
335189
YDOT = 2861
270802 feet/sec YDOT = 872
115341 meter/sec
ZDOT = 18870
413622 ZDOT = 5751
702072
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
61554185
00016717 00000-0 10270-3 0 9143
2 25544 51
6463 16
6388 0005860 241
1522 118
9044 15
55834771 18928
Satellite: ISS
Catalog Number: 25544
Epoch time: 15109
61554185 = yrday
fracday
Element set: 914
Inclination: 51
6463 deg
RA of node: 16
6388 deg
Eccentricity:
0005860
Arg of perigee: 241
1522 deg
Mean anomaly: 118
9044 deg
Mean motion: 15
55834771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 315
Coasting Arc #16 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2015/110/14:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 927378
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6491159
85 A = 6784157
08 meter
Y = -1823843
36 meter E =
0010816
Z = -683494
28 I = 51
73939
XDOT = 1872
913076 Wp = 172
23909
YDOT = -4434
575488 meter/sec RA = 11
10856 deg
ZDOT = -5975
298386 TA = 15
14055
MA = 15
10821
Ha = 217
108 n
mi
Hp = 214
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21296456
20 X = -6466962
54
Y = -5983738
04 feet Y = -1896296
48 meter
Z = -2242435
31 Z = -714968
80
XDOT = 6144
727939 XDOT = 1951
388650
YDOT = -14549
132177 feet/sec YDOT = -4413
192856 meter/sec
ZDOT = -19603
997330 ZDOT = -5966
009144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13510673
50 X = -4118053
28
Y = 17498119
14 feet Y = 5333426
71 meter
Z = -2377017
45 Z = -724514
92
XDOT = -9873
284471 XDOT = -3009
377107
YDOT = -10271
907717 feet/sec YDOT = -3130
877472 meter/sec
ZDOT = -19563
299528 ZDOT = -5962
893696
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
64323462
00016717 00000-0 10270-3 0 9151
2 25544 51
6459 11
5030 0006008 243
4331 116
6207 15
55833082 19087
Satellite: ISS
Catalog Number: 25544
Epoch time: 15110
64323462 = yrday
fracday
Element set: 915
Inclination: 51
6459 deg
RA of node: 11
5030 deg
Eccentricity:
0006008
Arg of perigee: 243
4331 deg
Mean anomaly: 116
6207 deg
Mean motion: 15
55833082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 272
Coasting Arc #17 (Orbit 1920)
---------------------------------------
Vector Time (GMT): 2015/111/11:14:20
986
Vector Time (MET): N/A
Weight (LBS) : 927275
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4177292
69 A = 6776558
41 meter
Y = -3011009
60 meter E =
0005544
Z = -4410179
05 I = 51
68611
XDOT = 5996
999909 Wp = 154
46366
YDOT = 3390
790666 meter/sec RA = 6
80377 deg
ZDOT = 3361
973781 TA = 149
53582
MA = 149
50360
Ha = 216
893 n
mi
Hp = 214
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13705028
50 X = 4232075
40
Y = -9878640
40 feet Y = -2963990
21 meter
Z = -14469091
37 Z = -4389753
08
XDOT = 19675
196551 XDOT = 5942
306089
YDOT = 11124
641294 feet/sec YDOT = 3457
547332 meter/sec
ZDOT = 11030
097707 ZDOT = 3390
973568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10313790
20 X = 3143643
25
Y = -13475334
04 feet Y = -4107281
82 meter
Z = -14380926
67 Z = -4383306
45
XDOT = 21015
184542 XDOT = 6405
428248
YDOT = 4169
660107 feet/sec YDOT = 1270
912401 meter/sec
ZDOT = 11153
755128 ZDOT = 3399
664563
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
47821919
00016717 00000-0 10270-3 0 9164
2 25544 51
6461 7
3290 0006299 252
6045 107
4420 15
55717333 19217
Satellite: ISS
Catalog Number: 25544
Epoch time: 15111
47821919 = yrday
fracday
Element set: 916
Inclination: 51
6461 deg
RA of node: 7
3290 deg
Eccentricity:
0006299
Arg of perigee: 252
6045 deg
Mean anomaly: 107
4420 deg
Mean motion: 15
55717333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1921
Checksum: 295
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