[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 26th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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
245/10:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 212
0
248/04:23:11
080 1
2 1
6 1
6
N/A 1
0 0
0 218
9
000/00:08:22
159 -0
2 -0
1 212
9
249/03:30:11
032 1
3 1
6 1
6
N/A 0
9 0
0 218
9
000/00:08:22
065 -0
2 -0
1 213
8
Coasting Arc #1 (Orbit 3867)
---------------------------------------
Vector Time (GMT): 2015/236/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4317891
55 A = 6775006
38 meter
Y = -1476149
02 meter E =
0013701
Z = -5020268
65 I = 51
98358
XDOT = 113
352144 Wp = 73
70025
YDOT = 7373
547444 meter/sec RA = 101
80482 deg
ZDOT = -2071
542970 TA = 176
22856
MA = 176
21823
Ha = 219
316 n
mi
Hp = 212
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14166310
87 X = 4358463
68
Y = -4843008
61 feet Y = -1427636
77 meter
Z = -16470697
66 Z = -4999194
77
XDOT = 371
890235 XDOT = 40
953627
YDOT = 24191
428623 feet/sec YDOT = 7374
410178 meter/sec
ZDOT = -6796
400819 ZDOT = -2071
168323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14880640
75 X = -4535619
30
Y = 2387500
05 feet Y = 727710
01 meter
Z = -16379540
64 Z = -4992483
99
XDOT = 3813
696118 XDOT = 1162
414577
YDOT = -22833
940557 feet/sec YDOT = -6959
785082 meter/sec
ZDOT = -6796
085266 ZDOT = -2071
446789
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 15236
57164737
00016717 00000-0 10270-3 0 9004
2 25544 51
6420 102
5939 0001076 60
6483 299
4778 15
55424442 38687
Satellite: ISS
Catalog Number: 25544
Epoch time: 15236
57164737 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 102
5939 deg
Eccentricity:
0001076
Arg of perigee: 60
6483 deg
Mean anomaly: 299
4778 deg
Mean motion: 15
55424442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3868
Checksum: 325
Coasting Arc #2 (Orbit 3883)
---------------------------------------
Vector Time (GMT): 2015/237/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4090018
58 A = 6773588
27 meter
Y = -865702
83 meter E =
0003611
Z = 5326612
10 I = 51
98501
XDOT = 1167
997268 Wp = 72
54790
YDOT = -7576
988065 meter/sec RA = 96
81529 deg
ZDOT = -333
360867 TA = 20
62026
MA = 20
60570
Ha = 219
463 n
mi
Hp = 212
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13418696
14 X = -4105908
50
Y = -2840232
39 feet Y = -911528
85 meter
Z = 17475761
48 Z = 5306705
23
XDOT = 3832
012033 XDOT = 1254
257495
YDOT = -24858
884729 feet/sec YDOT = -7563
444449 meter/sec
ZDOT = -1093
703633 ZDOT = -327
477366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12949124
12 X = 3946893
03
Y = 4841181
45 feet Y = 1475592
11 meter
Z = 17390046
36 Z = 5300486
13
XDOT = -7180
853363 XDOT = -2188
724105
YDOT = 23054
628642 feet/sec YDOT = 7027
050810 meter/sec
ZDOT = -1066
976934 ZDOT = -325
214570
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 15237
59961464
00016717 00000-0 10270-3 0 9010
2 25544 51
6425 97
4592 0001064 66
1330 293
9935 15
55431174 38840
Satellite: ISS
Catalog Number: 25544
Epoch time: 15237
59961464 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 97
4592 deg
Eccentricity:
0001064
Arg of perigee: 66
1330 deg
Mean anomaly: 293
9935 deg
Mean motion: 15
55431174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3884
Checksum: 324
Coasting Arc #3 (Orbit 3898)
---------------------------------------
Vector Time (GMT): 2015/238/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3641793
81 A = 6775802
95 meter
Y = 3138743
08 meter E =
0012015
Z = -4785974
72 I = 51
99444
XDOT = -2319
135048 Wp = 105
62210
YDOT = 6787
990695 meter/sec RA = 91
82605 deg
ZDOT = 2689
459599 TA = 190
82304
MA = 190
84892
Ha = 219
257 n
mi
Hp = 212
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11948142
43 X = 3629673
10
Y = 10297713
51 feet Y = 3179400
10 meter
Z = -15702016
79 Z = -4768313
38
XDOT = -7608
710787 XDOT = -2407
931834
YDOT = 22270
310679 feet/sec YDOT = 6761
560188 meter/sec
ZDOT = 8823
686350 ZDOT = 2677
977986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10567292
13 X = -3220910
64
Y = -11811120
66 feet Y = -3600029
58 meter
Z = -15626391
39 Z = -4762924
10
XDOT = 9705
304208 XDOT = 2958
176723
YDOT = -20279
348699 feet/sec YDOT = -6181
145483 meter/sec
ZDOT = 8772
940489 ZDOT = 2673
992261
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 15238
56331890
00016717 00000-0 10270-3 0 9023
2 25544 51
6413 92
6439 0001049 70
3830 289
7437 15
55475195 38996
Satellite: ISS
Catalog Number: 25544
Epoch time: 15238
56331890 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 92
6439 deg
Eccentricity:
0001049
Arg of perigee: 70
3830 deg
Mean anomaly: 289
7437 deg
Mean motion: 15
55475195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3899
Checksum: 333
Coasting Arc #4 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2015/239/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2961277
36 A = 6780339
54 meter
Y = -5035013
69 meter E =
0013224
Z = 3431814
45 I = 52
01047
XDOT = 3338
513076 Wp = 88
12322
YDOT = -5129
345335 meter/sec RA = 86
85098 deg
ZDOT = -4629
043562 TA = 51
88056
MA = 51
76141
Ha = 219
172 n
mi
Hp = 212
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9715476
89 X = -2921424
71
Y = -16519073
79 feet Y = -5067905
65 meter
Z = 11259233
78 Z = 3417526
43
XDOT = 10953
126889 XDOT = 3418
108303
YDOT = -16828
560812 feet/sec YDOT = -5091
567064 meter/sec
ZDOT = -15187
150793 ZDOT = -4612
632425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7799693
30 X = 2377346
52
Y = 17544200
52 feet Y = 5347472
32 meter
Z = 11198502
03 Z = 3413303
42
XDOT = -11652
779637 XDOT = -3551
767233
YDOT = 14861
889364 feet/sec YDOT = 4529
903878 meter/sec
ZDOT = -15115
428296 ZDOT = -4607
182545
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 15239
59125420
00016717 00000-0 10270-3 0 9038
2 25544 51
6416 87
5090 0000898 63
1810 296
9435 15
55519137 39156
Satellite: ISS
Catalog Number: 25544
Epoch time: 15239
59125420 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 87
5090 deg
Eccentricity:
0000898
Arg of perigee: 63
1810 deg
Mean anomaly: 296
9435 deg
Mean motion: 15
55519137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 318
Coasting Arc #5 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2015/240/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2103150
11 A = 6784312
31 meter
Y = 6261176
76 meter E =
0009004
Z = -1535541
33 I = 52
01984
XDOT = -4166
108995 Wp = 41
73810
YDOT = 2813
312842 meter/sec RA = 81
89012 deg
ZDOT = 5791
163279 TA = 301
56649
MA = 301
65436
Ha = 219
200 n
mi
Hp = 212
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6900098
78 X = 2040438
76
Y = 20541918
49 feet Y = 6284344
81 meter
Z = -5037865
27 Z = -1525477
59
XDOT = -13668
336597 XDOT = -4225
389298
YDOT = 9230
029008 feet/sec YDOT = 2766
393629 meter/sec
ZDOT = 18999
879523 ZDOT = 5770
781315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4860278
52 X = -1481412
89
Y = -21127794
88 feet Y = -6439751
88 meter
Z = -4995582
17 Z = -1522653
45
XDOT = 13096
382599 XDOT = 3991
777416
YDOT = -7463
936178 feet/sec YDOT = -2275
007747 meter/sec
ZDOT = 18911
439050 ZDOT = 5764
206622
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 15240
55493169
00016717 00000-0 10270-3 0 9045
2 25544 51
6404 82
6937 0001001 78
4367 281
6898 15
55515092 39309
Satellite: ISS
Catalog Number: 25544
Epoch time: 15240
55493169 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 82
6937 deg
Eccentricity:
0001001
Arg of perigee: 78
4367 deg
Mean anomaly: 281
6898 deg
Mean motion: 15
55515092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 318
Coasting Arc #6 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2015/241/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1018319
21 A = 6784931
63 meter
Y = -6670901
75 meter E =
0011045
Z = -660324
39 I = 52
01713
XDOT = 4776
012145 Wp = 134
17720
YDOT = -142
047106 meter/sec RA = 76
93888 deg
ZDOT = -5999
653520 TA = 52
92025
MA = 52
81932
Ha = 219
103 n
mi
Hp = 212
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3340942
30 X = -940440
34
Y = -21886160
61 feet Y = -6681853
88 meter
Z = -2166418
59 Z = -665081
31
XDOT = 15669
331184 XDOT = 4806
389171
YDOT = -466
033813 feet/sec YDOT = -88
469316 meter/sec
ZDOT = -19683
902625 ZDOT = -5976
379177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1519720
05 X = 463210
67
Y = 22085568
53 feet Y = 6731681
29 meter
Z = -2185727
53 Z = -666209
75
XDOT = -14169
232704 XDOT = -4318
782128
YDOT = -940
791869 feet/sec YDOT = -286
753362 meter/sec
ZDOT = -19583
466785 ZDOT = -5969
040676
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 15241
58283665
00016717 00000-0 10270-3 0 9058
2 25544 51
6404 77
5581 0001088 69
1661 290
9609 15
55576919 39461
Satellite: ISS
Catalog Number: 25544
Epoch time: 15241
58283665 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 77
5581 deg
Eccentricity:
0001088
Arg of perigee: 69
1661 deg
Mean anomaly: 290
9609 deg
Mean motion: 15
55576919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 343
Coasting Arc #7 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2015/242/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -212008
16 A = 6782017
59 meter
Y = 6204415
93 meter E =
0014531
Z = 2714303
58 I = 51
99854
XDOT = -5075
418869 Wp = 79
08468
YDOT = -2459
098389 meter/sec RA = 71
98178 deg
ZDOT = 5203
795989 TA = 311
47179
MA = 311
59647
Ha = 219
129 n
mi
Hp = 212
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -695564
82 X = -294556
58
Y = 20355695
29 feet Y = 6201583
86 meter
Z = 8905195
48 Z = 2713072
51
XDOT = -16651
636710 XDOT = -5072
821183
YDOT = -8067
908102 feet/sec YDOT = -2515
839962 meter/sec
ZDOT = 17072
821486 ZDOT = 5179
147498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2072126
45 X = 631584
14
Y = -20264727
84 feet Y = -6176689
04 meter
Z = 8898749
66 Z = 2712338
90
XDOT = 14723
589333 XDOT = 4487
750029
YDOT = 8986
176238 feet/sec YDOT = 2738
986517 meter/sec
ZDOT = 16966
934570 ZDOT = 5171
521657
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 15242
61072698
00016717 00000-0 10270-3 0 9066
2 25544 51
6397 72
4214 0001027 87
8825 272
2446 15
55570732 39628
Satellite: ISS
Catalog Number: 25544
Epoch time: 15242
61072698 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 72
4214 deg
Eccentricity:
0001027
Arg of perigee: 87
8825 deg
Mean anomaly: 272
2446 deg
Mean motion: 15
55570732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 318
Coasting Arc #8 (Orbit 3976)
---------------------------------------
Vector Time (GMT): 2015/243/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1591336
07 A = 6777066
92 meter
Y = -4956966
76 meter E =
0009811
Z = -4348686
27 I = 51
97242
XDOT = 4960
833267 Wp = 71
27341
YDOT = 4667
572623 meter/sec RA = 67
01069 deg
ZDOT = -3508
508270 TA = 163
19958
MA = 163
16706
Ha = 219
123 n
mi
Hp = 211
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5220918
86 X = 1667771
91
Y = -16263014
31 feet Y = -4938744
52 meter
Z = -14267343
40 Z = -4340769
71
XDOT = 16275
699696 XDOT = 4925
313518
YDOT = 15313
558475 feet/sec YDOT = 4722
848916 meter/sec
ZDOT = -11510
853905 ZDOT = -3484
496527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6082181
43 X = -1853848
90
Y = 15992186
96 feet Y = 4874418
59 meter
Z = -14232278
15 Z = -4337998
38
XDOT = -14433
075181 XDOT = -4399
201315
YDOT = -15631
972683 feet/sec YDOT = -4764
625274 meter/sec
ZDOT = -11408
127261 ZDOT = -3477
197189
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 15243
57435921
00016717 00000-0 10270-3 0 9075
2 25544 51
6406 67
6068 0001192 85
7308 274
3982 15
55602806 39770
Satellite: ISS
Catalog Number: 25544
Epoch time: 15243
57435921 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 67
6068 deg
Eccentricity:
0001192
Arg of perigee: 85
7308 deg
Mean anomaly: 274
3982 deg
Mean motion: 15
55602806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3977
Checksum: 329
Coasting Arc #9 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2015/244/13:14:49
181
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2960944
90 A = 6773569
81 meter
Y = 3135614
19 meter E =
0004976
Z = 5219769
61 I = 51
94699
XDOT = -4375
059110 Wp = 116
23664
YDOT = -6183
761359 meter/sec RA = 62
02189 deg
ZDOT = 1229
876256 TA = 322
00278
MA = 322
03787
Ha = 219
222 n
mi
Hp = 211
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9714386
14 X = -3021143
61
Y = 10287448
14 feet Y = 3102166
94 meter
Z = 17125228
38 Z = 5205239
42
XDOT = -14353
868472 XDOT = -4311
559884
YDOT = -20287
930967 feet/sec YDOT = -6232
330969 meter/sec
ZDOT = 4035
027085 ZDOT = 1208
778073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10133180
08 X = 3088593
29
Y = -9984105
39 feet Y = -3043155
32 meter
Z = 17061964
58 Z = 5200486
80
XDOT = 13024
854182 XDOT = 3969
975555
YDOT = 19978
421749 feet/sec YDOT = 6089
422949 meter/sec
ZDOT = 3945
162281 ZDOT = 1202
485463
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 15244
60221811
00016717 00000-0 10270-3 0 9082
2 25544 51
6403 62
4699 0001118 87
7960 272
3322 15
55590807 39935
Satellite: ISS
Catalog Number: 25544
Epoch time: 15244
60221811 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 62
4699 deg
Eccentricity:
0001118
Arg of perigee: 87
7960 deg
Mean anomaly: 272
3322 deg
Mean motion: 15
55590807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 311
Coasting Arc #10 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2015/245/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3541161
63 A = 6773058
95 meter
Y = 2211346
44 meter E =
0003364
Z = 5330462
28 I = 51
93234
XDOT = -4099
114109 Wp = 83
20695
YDOT = -6487
409431 meter/sec RA = 57
52916 deg
ZDOT = -31
434092 TA = 7
09353
MA = 7
08877
Ha = 219
162 n
mi
Hp = 212
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11617984
35 X = -3591519
60
Y = 7255073
64 feet Y = 2171465
80 meter
Z = 17488393
31 Z = 5313137
50
XDOT = -13448
537104 XDOT = -4026
112976
YDOT = -21284
151675 feet/sec YDOT = -6532
840252 meter/sec
ZDOT = -103
130224 ZDOT = -51
168809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13748718
63 X = 4190609
44
Y = 1099640
25 feet Y = 335170
35 meter
Z = 17413244
43 Z = 5307556
90
XDOT = -1689
889034 XDOT = -515
078177
YDOT = 24111
581864 feet/sec YDOT = 7349
210152 meter/sec
ZDOT = -187
043431 ZDOT = -57
010838
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 15245
50157905
00016717 00000-0 10270-3 0 9095
2 25544 51
6414 57
9787 0000975 74
1995 285
9266 15
55601619 40070
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
50157905 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 57
9787 deg
Eccentricity:
0000975
Arg of perigee: 74
1995 deg
Mean anomaly: 285
9266 deg
Mean motion: 15
55601619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 339
Coasting Arc #11 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2015/246/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4723307
68 A = 6774957
66 meter
Y = -106613
19 meter E =
0012536
Z = -4867526
79 I = 51
92084
XDOT = 2705
455592 Wp = 105
40021
YDOT = 6724
476322 meter/sec RA = 52
53321 deg
ZDOT = 2480
077159 TA = 188
87320
MA = 188
89538
Ha = 218
958 n
mi
Hp = 212
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15496416
28 X = 4747793
42
Y = -349780
82 feet Y = -53657
55 meter
Z = -15969576
07 Z = -4844522
41
XDOT = 8876
166642 XDOT = 2618
012514
YDOT = 22061
930190 feet/sec YDOT = 6754
241788 meter/sec
ZDOT = 8136
736086 ZDOT = 2493
006784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12928318
54 X = -3940551
49
Y = -8733843
10 feet Y = -2662075
38 meter
Z = -15870324
14 Z = -4837274
80
XDOT = 4923
136150 XDOT = 1500
571899
YDOT = -22159
447611 feet/sec YDOT = -6754
199632 meter/sec
ZDOT = 8191
235266 ZDOT = 2496
688509
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 15246
46516646
00016717 00000-0 10270-3 0 9104
2 25544 51
6410 53
1628 0000994 79
7787 280
3479 15
55661794 40221
Satellite: ISS
Catalog Number: 25544
Epoch time: 15246
46516646 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 53
1628 deg
Eccentricity:
0000994
Arg of perigee: 79
7787 deg
Mean anomaly: 280
3479 deg
Mean motion: 15
55661794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 329
Coasting Arc #12 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2015/247/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5467412
91 A = 6779603
87 meter
Y = -1876587
69 meter E =
0013053
Z = 3531802
07 I = 51
91681
XDOT = -820
620817 Wp = 87
29819
YDOT = -6146
240846 meter/sec RA = 47
54987 deg
ZDOT = -4521
142383 TA = 51
21997
MA = 51
10344
Ha = 218
947 n
mi
Hp = 211
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17937706
39 X = -5463178
25
Y = -6156783
77 feet Y = -1937703
98 meter
Z = 11587277
14 Z = 3505252
89
XDOT = -2692
325516 XDOT = -729
869081
YDOT = -20164
832173 feet/sec YDOT = -6154
910457 meter/sec
ZDOT = -14833
144300 ZDOT = -4524
907944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11398042
70 X = 3474123
42
Y = 15244163
79 feet Y = 4646421
12 meter
Z = 11473115
58 Z = 3497005
63
XDOT = -8121
081056 XDOT = -2475
305506
YDOT = 17284
554411 feet/sec YDOT = 5268
332185 meter/sec
ZDOT = -14848
211582 ZDOT = -4525
734890
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 15247
49297679
00016717 00000-0 10270-3 0 9111
2 25544 51
6413 48
0271 0000836 76
0403 284
0844 15
55687307 40383
Satellite: ISS
Catalog Number: 25544
Epoch time: 15247
49297679 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 48
0271 deg
Eccentricity:
0000836
Arg of perigee: 76
0403 deg
Mean anomaly: 284
0844 deg
Mean motion: 15
55687307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 318
Coasting Arc #13 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2015/248/04:27:22
159
Vector Time (MET): N/A
Weight (LBS) : 941127
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3841363
14 A = 6774179
43 meter
Y = -1991210
38 meter E =
0013755
Z = -5224424
50 I = 51
88331
XDOT = 4730
852806 Wp = 98
31992
YDOT = 5897
652420 meter/sec RA = 43
92287 deg
ZDOT = 1231
481818 TA = 183
46591
MA = 183
47545
Ha = 218
907 n
mi
Hp = 212
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12602897
45 X = 3888722
08
Y = -6532842
45 feet Y = -1947989
25 meter
Z = -17140500
31 Z = -5205648
79
XDOT = 15521
170622 XDOT = 4658
570158
YDOT = 19349
253346 feet/sec YDOT = 5950
151849 meter/sec
ZDOT = 4040
294678 ZDOT = 1254
287390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3173202
46 X = 967192
11
Y = -13936452
92 feet Y = -4247830
85 meter
Z = -17059128
69 Z = -5199622
43
XDOT = 23766
132086 XDOT = 7243
917060
YDOT = 350
063575 feet/sec YDOT = 106
699378 meter/sec
ZDOT = 4137
531261 ZDOT = 1261
119528
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 15248
19958964
00016717 00000-0 10270-3 0 9121
2 25544 51
6447 44
4997 0000392 317
2406 42
8717 15
55400774 40497
Satellite: ISS
Catalog Number: 25544
Epoch time: 15248
19958964 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 44
4997 deg
Eccentricity:
0000392
Arg of perigee: 317
2406 deg
Mean anomaly: 42
8717 deg
Mean motion: 15
55400774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4049
Checksum: 332
Coasting Arc #14 (Orbit 4063)
---------------------------------------
Vector Time (GMT): 2015/249/03:34:22
065
Vector Time (MET): N/A
Weight (LBS) : 940947
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3411493
94 A = 6774768
98 meter
Y = -2562789
11 meter E =
0012853
Z = -5273453
92 I = 51
85949
XDOT = 5420
588405 Wp = 96
96654
YDOT = 5335
409232 meter/sec RA = 39
13062 deg
ZDOT = 914
168924 TA = 181
75825
MA = 181
76278
Ha = 218
874 n
mi
Hp = 213
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11192565
42 X = 3465514
46
Y = -8408100
76 feet Y = -2524337
81 meter
Z = -17301358
01 Z = -5256750
27
XDOT = 17784
082693 XDOT = 5356
083028
YDOT = 17504
623463 feet/sec YDOT = 5395
665201 meter/sec
ZDOT = 2999
241875 ZDOT = 940
343966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3808015
09 X = 1160683
00
Y = -13563691
49 feet Y = -4134213
17 meter
Z = -17228811
98 Z = -5251341
89
XDOT = 23769
687377 XDOT = 7245
000712
YDOT = 2723
199562 feet/sec YDOT = 830
031227 meter/sec
ZDOT = 3111
112712 ZDOT = 948
267155
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 15249
16332588
00016717 00000-0 10270-3 0 9138
2 25544 51
6443 39
6860 0001568 277
2017 82
8957 15
55119231 40649
Satellite: ISS
Catalog Number: 25544
Epoch time: 15249
16332588 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 39
6860 deg
Eccentricity:
0001568
Arg of perigee: 277
2017 deg
Mean anomaly: 82
8957 deg
Mean motion: 15
55119231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4064
Checksum: 321
Coasting Arc #15 (Orbit 4079)
---------------------------------------
Vector Time (GMT): 2015/250/03:34:22
065
Vector Time (MET): N/A
Weight (LBS) : 940947
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4899085
33 A = 6777626
62 meter
Y = 1014999
12 meter E =
0007555
Z = 4568558
48 I = 51
84367
XDOT = -4080
483383 Wp = 59
53564
YDOT = -5709
213433 meter/sec RA = 34
13890 deg
ZDOT = -3099
734446 TA = 61
42275
MA = 61
34674
Ha = 218
973 n
mi
Hp = 213
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16073114
59 X = -4932263
36
Y = 3330049
61 feet Y = 960029
10 meter
Z = 14988708
91 Z = 4544679
21
XDOT = -13387
412673 XDOT = -4001
281074
YDOT = -18731
015199 feet/sec YDOT = -5754
401430 meter/sec
ZDOT = -10169
732433 ZDOT = -3119
363756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10545861
34 X = -3214378
54
Y = 12700471
59 feet Y = 3871103
74 meter
Z = 14885512
02 Z = 4537104
06
XDOT = -21177
773951 XDOT = -6454
985500
YDOT = -5538
483411 feet/sec YDOT = -1688
129744 meter/sec
ZDOT = -10253
289713 ZDOT = -3125
202704
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 15250
19149470
00016717 00000-0 10270-3 0 9140
2 25544 51
6440 34
5530 0001583 283
9548 76
1430 15
55145409 40800
Satellite: ISS
Catalog Number: 25544
Epoch time: 15250
19149470 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 34
5530 deg
Eccentricity:
0001583
Arg of perigee: 283
9548 deg
Mean anomaly: 76
1430 deg
Mean motion: 15
55145409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4080
Checksum: 294
Coasting Arc #16 (Orbit 4094)
---------------------------------------
Vector Time (GMT): 2015/251/03:34:22
065
Vector Time (MET): N/A
Weight (LBS) : 940947
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5962754
38 A = 6782023
70 meter
Y = 445302
62 meter E =
0003252
Z = -3201258
99 I = 51
83252
XDOT = 2171
080983 Wp = 62
64421
YDOT = 5550
585195 meter/sec RA = 29
15699 deg
ZDOT = 4821
224098 TA = 260
46119
MA = 260
49794
Ha = 218
837 n
mi
Hp = 213
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19562842
44 X = 5972882
09
Y = 1460966
60 feet Y = 512038
46 meter
Z = -10502818
21 Z = -3172268
82
XDOT = 7122
969104 XDOT = 2085
432175
YDOT = 18210
581348 feet/sec YDOT = 5574
385104 meter/sec
ZDOT = 15817
664365 ZDOT = 4831
562252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16047769
76 X = 4891360
22
Y = -11398133
54 feet Y = -3474151
10 meter
Z = -10377863
73 Z = -3163172
86
XDOT = 16194
468637 XDOT = 4936
074041
YDOT = 8375
011461 feet/sec YDOT = 2552
703493 meter/sec
ZDOT = 15861
172321 ZDOT = 4834
485324
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 15251
15538702
00016717 00000-0 10270-3 0 9158
2 25544 51
6447 29
7398 0001626 288
6520 71
4456 15
55180456 40958
Satellite: ISS
Catalog Number: 25544
Epoch time: 15251
15538702 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 29
7398 deg
Eccentricity:
0001626
Arg of perigee: 288
6520 deg
Mean anomaly: 71
4456 deg
Mean motion: 15
55180456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4095
Checksum: 320
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