[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 6th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 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
133/21:39:30
000 0
0 0
0 0
0
N/A 0
0 0
0 217
9
000/00:00:00
000 0
0 0
0 213
9
136/01:09:28
999 -5
2 7
1 7
1
N/A -1
0 -0
3 218
2
000/00:24:57
999 -4
7 0
1 217
3
Coasting Arc #1 (Orbit 2155)
---------------------------------------
Vector Time (GMT): 2015/126/13:28:35
909
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -756510
93 A = 6779922
65 meter
Y = -5767769
72 meter E =
0001685
Z = -3480645
22 I = 51
30916
XDOT = 5188
076146 Wp = 285
83280
YDOT = -3401
632211 meter/sec RA = 291
16104 deg
ZDOT = 4507
848609 TA = 33
03344
MA = 33
02292
Ha = 216
411 n
mi
Hp = 214
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2481991
26 X = -675050
15
Y = -18923129
01 feet Y = -5775773
95 meter
Z = -11419439
70 Z = -3484122
57
XDOT = 17021
247198 XDOT = 5203
830563
YDOT = -11160
210665 feet/sec YDOT = -3343
527793 meter/sec
ZDOT = 14789
529556 ZDOT = 4533
089922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18209682
27 X = -5550311
16
Y = -5686575
33 feet Y = -1733268
16 meter
Z = -11433242
23 Z = -3484852
23
XDOT = -3514
823545 XDOT = -1071
318217
YDOT = -18707
895665 feet/sec YDOT = -5702
166599 meter/sec
ZDOT = 14898
337323 ZDOT = 4541
013216
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 15126
56884093
00016717 00000-0 10270-3 0 9005
2 25544 51
6440 291
8788 0006698 276
4705 83
5686 15
55590566 21562
Satellite: ISS
Catalog Number: 25544
Epoch time: 15126
56884093 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 291
8788 deg
Eccentricity:
0006698
Arg of perigee: 276
4705 deg
Mean anomaly: 83
5686 deg
Mean motion: 15
55590566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2156
Checksum: 351
Coasting Arc #2 (Orbit 2171)
---------------------------------------
Vector Time (GMT): 2015/127/13:28:35
909
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -602536
62 A = 6783980
04 meter
Y = 6570077
59 meter E =
0007704
Z = 1559587
64 I = 51
31199
XDOT = -5029
899558 Wp = 132
37908
YDOT = 899
734619 meter/sec RA = 286
15178 deg
ZDOT = -5720
562642 TA = 30
48028
MA = 30
43553
Ha = 216
662 n
mi
Hp = 214
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1976826
18 X = -683536
02
Y = 21555372
66 feet Y = 6562886
68 meter
Z = 5116757
34 Z = 1556464
09
XDOT = -16502
295137 XDOT = -5011
797987
YDOT = 2951
885233 feet/sec YDOT = 843
588421 meter/sec
ZDOT = -18768
250138 ZDOT = -5744
953298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18946187
30 X = 5774797
89
Y = 10475371
46 feet Y = 3192893
22 meter
Z = 5102128
71 Z = 1555128
83
XDOT = -3095
196179 XDOT = -943
415795
YDOT = 14811
207970 feet/sec YDOT = 4514
456189 meter/sec
ZDOT = -18872
939210 ZDOT = -5752
471871
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 15127
59669424
00016717 00000-0 10270-3 0 9019
2 25544 51
6436 286
7431 0006774 280
5282 79
5108 15
55616558 21728
Satellite: ISS
Catalog Number: 25544
Epoch time: 15127
59669424 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 286
7431 deg
Eccentricity:
0006774
Arg of perigee: 280
5282 deg
Mean anomaly: 79
5108 deg
Mean motion: 15
55616558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2172
Checksum: 331
Coasting Arc #3 (Orbit 2187)
---------------------------------------
Vector Time (GMT): 2015/128/13:28:35
909
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1797626
51 A = 6784719
41 meter
Y = -6504461
62 meter E =
0010578
Z = 631379
71 I = 51
30838
XDOT = 4494
582066 Wp = 21
22480
YDOT = 1821
399343 meter/sec RA = 281
15166 deg
ZDOT = 5945
715106 TA = 345
62973
MA = 345
65979
Ha = 216
811 n
mi
Hp = 214
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5897724
76 X = 1867160
30
Y = -21340097
17 feet Y = -6483970
62 meter
Z = 2071455
73 Z = 640280
97
XDOT = 14746
004154 XDOT = 4444
998299
YDOT = 5975
719628 feet/sec YDOT = 1871
383223 meter/sec
ZDOT = 19506
939323 ZDOT = 5967
428808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17433343
78 X = -5313683
18
Y = -13641729
50 feet Y = -4157999
15 meter
Z = 2110823
14 Z = 643378
89
XDOT = 10148
172010 XDOT = 3093
162829
YDOT = -9925
308710 feet/sec YDOT = -3025
234095 meter/sec
ZDOT = 19599
648851 ZDOT = 5973
972970
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 15128
62452820
00016717 00000-0 10270-3 0 9025
2 25544 51
6450 281
6079 0006736 285
0964 74
9444 15
55656179 21883
Satellite: ISS
Catalog Number: 25544
Epoch time: 15128
62452820 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 281
6079 deg
Eccentricity:
0006736
Arg of perigee: 285
0964 deg
Mean anomaly: 74
9444 deg
Mean motion: 15
55656179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2188
Checksum: 332
Coasting Arc #4 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2015/129/13:28:35
909
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2795444
13 A = 6781623
68 meter
Y = 5542714
60 meter E =
0002402
Z = -2727690
59 I = 51
29277
XDOT = -3661
243278 Wp = 261
95282
YDOT = -4371
203865 meter/sec RA = 276
14702 deg
ZDOT = -5126
622789 TA = 309
07872
MA = 309
10008
Ha = 217
103 n
mi
Hp = 214
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9171404
63 X = -2843966
11
Y = 18184759
19 feet Y = 5511182
91 meter
Z = -8949116
10 Z = -2741388
10
XDOT = -12011
953011 XDOT = -3587
187898
YDOT = -14341
220030 feet/sec YDOT = -4411
732039 meter/sec
ZDOT = -16819
628572 ZDOT = -5144
228823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13540717
28 X = 4127210
63
Y = 15178155
49 feet Y = 4626301
79 meter
Z = -9008850
08 Z = -2745897
51
XDOT = -16615
450190 XDOT = -5064
389218
YDOT = 4788
648390 feet/sec YDOT = 1459
580029 meter/sec
ZDOT = -16894
267294 ZDOT = -5149
372671
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 15129
58810553
00016717 00000-0 10270-3 0 9033
2 25544 51
6447 276
7937 0006815 289
1185 70
9231 15
55678645 22035
Satellite: ISS
Catalog Number: 25544
Epoch time: 15129
58810553 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 276
7937 deg
Eccentricity:
0006815
Arg of perigee: 289
1185 deg
Mean anomaly: 70
9231 deg
Mean motion: 15
55678645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 332
Coasting Arc #5 (Orbit 2218)
---------------------------------------
Vector Time (GMT): 2015/130/13:28:35
909
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3559469
18 A = 6776546
05 meter
Y = -3788577
82 meter E =
0002690
Z = 4345170
30 I = 51
27458
XDOT = 2607
239426 Wp = 98
76053
YDOT = 6359
277479 meter/sec RA = 271
12642 deg
ZDOT = 3406
682253 TA = 316
53100
MA = 316
55220
Ha = 217
110 n
mi
Hp = 214
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11678048
49 X = 3580462
06
Y = -12429717
26 feet Y = -3748656
22 meter
Z = 14255808
06 Z = 4362512
53
XDOT = 8553
935124 XDOT = 2519
386199
YDOT = 20863
771256 feet/sec YDOT = 6387
942045 meter/sec
ZDOT = 11176
779046 ZDOT = 3419
134550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7541936
58 X = -2298782
27
Y = -15226595
47 feet Y = -4641066
30 meter
Z = 14330831
59 Z = 4368037
47
XDOT = 21405
521675 XDOT = 6524
403007
YDOT = -27
257373 feet/sec YDOT = -8
308047 meter/sec
ZDOT = 11228
975597 ZDOT = 3422
591762
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 15130
61590123
00016717 00000-0 10270-3 0 9048
2 25544 51
6454 271
6581 0006897 293
2327 66
8100 15
55737217 22193
Satellite: ISS
Catalog Number: 25544
Epoch time: 15130
61590123 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 271
6581 deg
Eccentricity:
0006897
Arg of perigee: 293
2327 deg
Mean anomaly: 66
8100 deg
Mean motion: 15
55737217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2219
Checksum: 305
Coasting Arc #6 (Orbit 2233)
---------------------------------------
Vector Time (GMT): 2015/131/13:28:35
909
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4079469
14 A = 6773063
27 meter
Y = 1503425
01 meter E =
0009605
Z = -5201241
02 I = 51
26304
XDOT = -1374
698950 Wp = 56
18651
YDOT = -7463
329090 meter/sec RA = 266
09001 deg
ZDOT = -1075
253408 TA = 203
43064
MA = 203
47443
Ha = 217
441 n
mi
Hp = 214
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13384085
09 X = -4070711
75
Y = 4932496
76 feet Y = 1457854
72 meter
Z = -17064439
03 Z = -5221037
14
XDOT = -4510
167158 XDOT = -1285
916842
YDOT = -24485
987829 feet/sec YDOT = -7478
205456 meter/sec
ZDOT = -3527
734278 ZDOT = -1081
715878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 174532
31 X = 53197
45
Y = 14160526
17 feet Y = 4316128
38 meter
Z = -17149559
02 Z = -5227185
59
XDOT = -23535
383446 XDOT = -7173
584874
YDOT = -4029
290766 feet/sec YDOT = -1228
127826 meter/sec
ZDOT = -3554
072387 ZDOT = -1083
281263
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 15131
57944431
00016717 00000-0 10270-3 0 9050
2 25544 51
6452 266
8441 0006973 298
1072 61
9376 15
55736697 22347
Satellite: ISS
Catalog Number: 25544
Epoch time: 15131
57944431 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 266
8441 deg
Eccentricity:
0006973
Arg of perigee: 298
1072 deg
Mean anomaly: 61
9376 deg
Mean motion: 15
55736697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2234
Checksum: 331
Coasting Arc #7 (Orbit 2249)
---------------------------------------
Vector Time (GMT): 2015/132/13:28:35
909
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4318534
83 A = 6773261
58 meter
Y = 998706
84 meter E =
0006766
Z = 5124724
08 I = 51
26743
XDOT = -
211862 Wp = 342
15860
YDOT = 7528
096266 meter/sec RA = 261
04587 deg
ZDOT = -1461
078930 TA = 122
01141
MA = 121
94565
Ha = 217
592 n
mi
Hp = 214
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14168421
35 X = 4282151
88
Y = 3276597
23 feet Y = 1046796
12 meter
Z = 16813399
21 Z = 5145614
49
XDOT = -
695086 XDOT = -77
295377
YDOT = 24698
478563 feet/sec YDOT = 7527
662889 meter/sec
ZDOT = -4793
566043 ZDOT = -1461
267233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7610100
72 X = 2319558
70
Y = -12270035
35 feet Y = -3739906
77 meter
Z = 16902758
52 Z = 5151960
80
XDOT = 22511
112330 XDOT = 6861
387038
YDOT = 7329
219422 feet/sec YDOT = 2233
946080 meter/sec
ZDOT = -4795
730349 ZDOT = -1461
738610
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 15132
60720403
00016717 00000-0 10270-3 0 9067
2 25544 51
6454 261
7077 0006973 303
0056 57
0427 15
55777856 22509
Satellite: ISS
Catalog Number: 25544
Epoch time: 15132
60720403 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 261
7077 deg
Eccentricity:
0006973
Arg of perigee: 303
0056 deg
Mean anomaly: 57
0427 deg
Mean motion: 15
55777856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2250
Checksum: 300
Coasting Arc #8 (Orbit 2264)
---------------------------------------
Vector Time (GMT): 2015/133/13:28:35
909
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4235798
95 A = 6777125
81 meter
Y = -3305224
05 meter E =
0002259
Z = -4131047
33 I = 51
28644
XDOT = 1458
497342 Wp = 45
88627
YDOT = -6536
127219 meter/sec RA = 256
01120 deg
ZDOT = 3736
852167 TA = 262
74510
MA = 262
77078
Ha = 217
672 n
mi
Hp = 213
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13896978
17 X = -4178457
00
Y = -10843910
93 feet Y = -3352270
95 meter
Z = -13553304
88 Z = -4151484
95
XDOT = 4785
096267 XDOT = 1513
325028
YDOT = -21443
986939 feet/sec YDOT = -6519
510748 meter/sec
ZDOT = 12260
013672 ZDOT = 3744
070593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14530519
69 X = -4428902
40
Y = 9859728
90 feet Y = 3005245
37 meter
Z = -13640316
09 Z = -4157568
35
XDOT = -18277
825837 XDOT = -5571
081315
YDOT = -9943
811595 feet/sec YDOT = -3030
873774 meter/sec
ZDOT = 12292
121214 ZDOT = 3746
638546
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 15133
57071159
00016717 00000-0 10270-3 0 9072
2 25544 51
6454 256
8932 0007024 306
3104 53
7400 15
55800664 22656
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
57071159 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 256
8932 deg
Eccentricity:
0007024
Arg of perigee: 306
3104 deg
Mean anomaly: 53
7400 deg
Mean motion: 15
55800664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2265
Checksum: 292
Coasting Arc #9 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2015/133/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2577447
45 A = 6775565
59 meter
Y = -4309743
41 meter E =
0002722
Z = 4546010
47 I = 51
28048
XDOT = 4137
080368 Wp = 62
28530
YDOT = 5694
433232 meter/sec RA = 254
34847 deg
ZDOT = 3052
723135 TA = 357
05105
MA = 357
05266
Ha = 217
900 n
mi
Hp = 213
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8456192
42 X = 2603365
35
Y = -14139578
11 feet Y = -4280775
74 meter
Z = 14914732
52 Z = 4558594
38
XDOT = 13573
098319 XDOT = 4058
267195
YDOT = 18682
523726 feet/sec YDOT = 5740
256131 meter/sec
ZDOT = 10015
495849 ZDOT = 3072
629046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4317067
86 X = -1315842
28
Y = 15848120
62 feet Y = 4830507
17 meter
Z = 14969438
97 Z = 4562685
00
XDOT = -16820
456771 XDOT = -5126
875224
YDOT = -14122
261208 feet/sec YDOT = -4304
465216 meter/sec
ZDOT = 10099
805030 ZDOT = 3078
420573
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 15133
95610951
00016717 00000-0 10270-3 0 9084
2 25544 51
6419 254
9688 0007259 310
7564 49
2959 15
55818724 22715
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
95610951 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 254
9688 deg
Eccentricity:
0007259
Arg of perigee: 310
7564 deg
Mean anomaly: 49
2959 deg
Mean motion: 15
55818724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 343
Coasting Arc #10 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2015/134/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3692935
41 A = 6772578
88 meter
Y = 2157609
11 meter E =
0011539
Z = -5260073
91 I = 51
28027
XDOT = -3162
664218 Wp = 56
09623
YDOT = -6952
741298 meter/sec RA = 249
30857 deg
ZDOT = -626
176887 TA = 207
86175
MA = 207
92359
Ha = 218
165 n
mi
Hp = 213
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12115929
83 X = -3691235
94
Y = 7078770
06 feet Y = 2116321
79 meter
Z = -17257460
32 Z = -5278009
66
XDOT = -10376
194940 XDOT = -3081
640164
YDOT = -22810
831031 feet/sec YDOT = -6987
655247 meter/sec
ZDOT = -2054
386111 ZDOT = -641
343940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9528684
88 X = 2904343
15
Y = -10170358
89 feet Y = -3099925
39 meter
Z = -17334723
61 Z = -5283623
76
XDOT = 15622
866386 XDOT = 4761
849674
YDOT = 18277
147491 feet/sec YDOT = 5570
874555 meter/sec
ZDOT = -2118
169774 ZDOT = -645
618147
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 15134
91959486
00016717 00000-0 10270-3 0 9091
2 25544 51
6423 250
1528 0007241 315
7324 44
3250 15
55817709 22869
Satellite: ISS
Catalog Number: 25544
Epoch time: 15134
91959486 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 250
1528 deg
Eccentricity:
0007241
Arg of perigee: 315
7324 deg
Mean anomaly: 44
3250 deg
Mean motion: 15
55817709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2286
Checksum: 314
Coasting Arc #11 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2015/135/21:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 893564
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4563416
82 A = 6773571
45 meter
Y = 235795
16 meter E =
0008816
Z = 5002722
25 I = 51
29646
XDOT = 1756
055401 Wp = 359
85141
YDOT = 7210
567116 meter/sec RA = 244
26626 deg
ZDOT = -1933
050372 TA = 109
04046
MA = 108
94494
Ha = 218
273 n
mi
Hp = 213
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14971839
95 X = 4536139
10
Y = 773606
15 feet Y = 286673
68 meter
Z = 16413130
73 Z = 5024824
63
XDOT = 5761
336619 XDOT = 1684
684829
YDOT = 23656
716260 feet/sec YDOT = 7229
805445 meter/sec
ZDOT = -6342
028781 ZDOT = -1924
692884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14423048
81 X = -4396145
28
Y = 3689489
57 feet Y = 1124556
42 meter
Z = 16507835
96 Z = 5031588
40
XDOT = -12316
882904 XDOT = -3754
185909
YDOT = -19801
668047 feet/sec YDOT = -6035
548421 meter/sec
ZDOT = -6307
471937 ZDOT = -1922
517446
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 15135
94729339
00016717 00000-0 10270-3 0 9109
2 25544 51
6427 245
0165 0007377 319
6454 40
4151 15
55850329 23021
Satellite: ISS
Catalog Number: 25544
Epoch time: 15135
94729339 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 245
0165 deg
Eccentricity:
0007377
Arg of perigee: 319
6454 deg
Mean anomaly: 40
4151 deg
Mean motion: 15
55850329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 304
Coasting Arc #12 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2015/136/01:21:57
999
Vector Time (MET): N/A
Weight (LBS) : 892643
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2859913
69 A = 6778138
76 meter
Y = 3430300
35 meter E =
0006282
Z = -5104301
16 I = 51
29950
XDOT = -4430
205832 Wp = 64
26530
YDOT = -6050
051082 meter/sec RA = 243
52036 deg
ZDOT = -1582
507740 TA = 190
38576
MA = 190
39875
Ha = 218
181 n
mi
Hp = 217
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9382918
92 X = -2873264
28
Y = 11254266
25 feet Y = 3398244
36 meter
Z = -16746394
87 Z = -5118226
72
XDOT = -14534
796037 XDOT = -4354
536067
YDOT = -19849
248956 feet/sec YDOT = -6099
169420 meter/sec
ZDOT = -5191
954526 ZDOT = -1603
845559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8070582
93 X = -2459913
68
Y = -12146610
51 feet Y = -3702286
88 meter
Z = -16806693
95 Z = -5122680
32
XDOT = 22322
054749 XDOT = 6803
762288
YDOT = -7517
289255 feet/sec YDOT = -2291
269765 meter/sec
ZDOT = -5282
360136 ZDOT = -1610
063369
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 15136
07577879
00016717 00000-0 10270-3 0 9115
2 25544 51
6449 244
3756 0007581 269
2701 90
7583 15
54152597 23045
Satellite: ISS
Catalog Number: 25544
Epoch time: 15136
07577879 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 244
3756 deg
Eccentricity:
0007581
Arg of perigee: 269
2701 deg
Mean anomaly: 90
7583 deg
Mean motion: 15
54152597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 334
Coasting Arc #13 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2015/137/01:21:57
999
Vector Time (MET): N/A
Weight (LBS) : 892643
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3813604
69 A = 6777200
27 meter
Y = -1875232
80 meter E =
0005385
Z = 5283872
55 I = 51
31164
XDOT = 3761
553224 Wp = 281
75162
YDOT = 6669
524126 meter/sec RA = 238
49698 deg
ZDOT = -347
106348 TA = 171
57882
MA = 171
56978
Ha = 218
231 n
mi
Hp = 217
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12511826
41 X = 3808622
93
Y = -6152338
58 feet Y = -1832614
63 meter
Z = 17335539
87 Z = 5302386
53
XDOT = 12341
053886 XDOT = 3688
379595
YDOT = 21881
640834 feet/sec YDOT = 6711
179149 meter/sec
ZDOT = -1138
800355 ZDOT = -329
010554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2515044
30 X = 766585
50
Y = 13612567
60 feet Y = 4149110
60 meter
Z = 17415239
53 Z = 5308165
01
XDOT = -23435
843669 XDOT = -7143
245150
YDOT = 5692
397119 feet/sec YDOT = 1735
042642 meter/sec
ZDOT = -1062
392141 ZDOT = -323
817125
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 15137
10459928
00016717 00000-0 10270-3 0 9125
2 25544 51
6448 239
2467 0007764 273
3142 86
7123 15
54191838 23208
Satellite: ISS
Catalog Number: 25544
Epoch time: 15137
10459928 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 239
2467 deg
Eccentricity:
0007764
Arg of perigee: 273
3142 deg
Mean anomaly: 86
7123 deg
Mean motion: 15
54191838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 317
Coasting Arc #14 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2015/138/01:21:57
999
Vector Time (MET): N/A
Weight (LBS) : 892643
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672529
98 A = 6778817
99 meter
Y = 288372
69 meter E =
0004808
Z = -4907177
94 I = 51
33489
XDOT = -2781
140045 Wp = 120
53001
YDOT = -6778
794883 meter/sec RA = 233
47552 deg
ZDOT = 2249
045392 TA = 171
54835
MA = 171
54025
Ha = 218
626 n
mi
Hp = 217
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15329822
76 X = -4651569
64
Y = 946104
63 feet Y = 236238
89 meter
Z = -16099665
16 Z = -4929825
72
XDOT = -9124
475214 XDOT = -2716
056483
YDOT = -22240
140692 feet/sec YDOT = -6809
531635 meter/sec
ZDOT = 7378
757848 ZDOT = 2235
692574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3009495
23 X = 917294
15
Y = -14956732
37 feet Y = -4558812
03 meter
Z = -16196817
39 Z = -4936789
94
XDOT = 22760
685702 XDOT = 6937
457002
YDOT = -3352
718623 feet/sec YDOT = -1021
908636 meter/sec
ZDOT = 7322
693737 ZDOT = 2231
957051
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 15138
06910481
00016717 00000-0 10270-3 0 9138
2 25544 51
6453 234
4383 0007716 277
6774 82
3502 15
54190560 23353
Satellite: ISS
Catalog Number: 25544
Epoch time: 15138
06910481 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 234
4383 deg
Eccentricity:
0007716
Arg of perigee: 277
6774 deg
Mean anomaly: 82
3502 deg
Mean motion: 15
54190560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 305
Coasting Arc #15 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2015/139/01:21:57
999
Vector Time (MET): N/A
Weight (LBS) : 892643
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5341958
78 A = 6782152
56 meter
Y = 1208235
03 meter E =
0004872
Z = 4000406
87 I = 51
36557
XDOT = 1492
432085 Wp = 38
36001
YDOT = 6414
421849 meter/sec RA = 228
46302 deg
ZDOT = -3923
933857 TA = 92
60730
MA = 92
55152
Ha = 219
165 n
mi
Hp = 217
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17526111
49 X = 5308618
17
Y = 3964025
69 feet Y = 1267785
58 meter
Z = 13124694
46 Z = 4026276
63
XDOT = 4896
430726 XDOT = 1439
654901
YDOT = 21044
691107 feet/sec YDOT = 6430
816403 meter/sec
ZDOT = -12873
798744 ZDOT = -3916
811492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8050686
72 X = -2453849
31
Y = 15973290
09 feet Y = 4868658
82 meter
Z = 13235412
17 Z = 4034153
63
XDOT = -20458
204676 XDOT = -6235
660785
YDOT = 348
734609 feet/sec YDOT = 106
294309 meter/sec
ZDOT = -12844
377015 ZDOT = -3914
966114
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 15139
09789320
00016717 00000-0 10270-3 0 9149
2 25544 51
6449 229
3096 0007717 282
3801 77
6488 15
54224042 23518
Satellite: ISS
Catalog Number: 25544
Epoch time: 15139
09789320 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 229
3096 deg
Eccentricity:
0007717
Arg of perigee: 282
3801 deg
Mean anomaly: 77
6488 deg
Mean motion: 15
54224042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 321
Coasting Arc #16 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2015/140/01:21:57
999
Vector Time (MET): N/A
Weight (LBS) : 892643
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5718365
88 A = 6785926
27 meter
Y = -2492158
75 meter E =
0006017
Z = -2661394
97 I = 51
39999
XDOT = 50
690647 Wp = 325
11969
YDOT = -5652
079740 meter/sec RA = 223
46140 deg
ZDOT = 5182
781482 TA = 4
73896
MA = 4
73327
Ha = 219
269 n
mi
Hp = 217
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18761042
91 X = -5677144
73
Y = -8176373
85 feet Y = -2555874
54 meter
Z = -8731610
78 Z = -2689074
16
XDOT = 166
307898 XDOT = 88
713429
YDOT = -18543
568700 feet/sec YDOT = -5651
300742 meter/sec
ZDOT = 17003
876254 ZDOT = 5183
119589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12162574
92 X = 3707152
84
Y = -16395799
62 feet Y = -4997439
72 meter
Z = -8849879
86 Z = -2697443
38
XDOT = 16861
348425 XDOT = 5139
339000
YDOT = 3326
816605 feet/sec YDOT = 1014
013701 meter/sec
ZDOT = 17006
308102 ZDOT = 5183
522710
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 15140
06236677
00016717 00000-0 10270-3 0 9151
2 25544 51
6449 224
5005 0007829 286
1817 73
8474 15
54236871 23660
Satellite: ISS
Catalog Number: 25544
Epoch time: 15140
06236677 = yrday
fracday
Element set: 915
Inclination: 51
6449 deg
RA of node: 224
5005 deg
Eccentricity:
0007829
Arg of perigee: 286
1817 deg
Mean anomaly: 73
8474 deg
Mean motion: 15
54236871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 325
Coasting Arc #17 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2015/141/01:21:57
999
Vector Time (MET): N/A
Weight (LBS) : 892643
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5718620
45 A = 6788577
92 meter
Y = 3505730
85 meter E =
0006421
Z = 1019601
23 I = 51
43177
XDOT = -1762
640338 Wp = 141
30844
YDOT = 4590
517264 meter/sec RA = 218
47160 deg
ZDOT = -5882
472479 TA = 27
61002
MA = 27
57594
Ha = 219
569 n
mi
Hp = 217
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18761878
11 X = 5674040
62
Y = 11501741
62 feet Y = 3569430
84 meter
Z = 3345148
40 Z = 1047273
50
XDOT = -5782
940740 XDOT = -1785
266465
YDOT = 15060
752180 feet/sec YDOT = 4570
680296 meter/sec
ZDOT = -19299
450389 ZDOT = -5891
089667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15138594
52 X = -4614243
61
Y = 15947323
93 feet Y = 4860744
33 meter
Z = 3463230
28 Z = 1055592
59
XDOT = -12394
751435 XDOT = -3777
920237
YDOT = -7556
340027 feet/sec YDOT = -2303
172440 meter/sec
ZDOT = -19337
203506 ZDOT = -5893
979629
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 15141
09112396
00016717 00000-0 10270-3 0 9167
2 25544 51
6444 219
3715 0007715 289
2511 70
7807 15
54224059 23823
Satellite: ISS
Catalog Number: 25544
Epoch time: 15141
09112396 = yrday
fracday
Element set: 916
Inclination: 51
6444 deg
RA of node: 219
3715 deg
Eccentricity:
0007715
Arg of perigee: 289
2511 deg
Mean anomaly: 70
7807 deg
Mean motion: 15
54224059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 304
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