[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 4th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2014/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6309163
54 A = 6793960
27 meter
Y = -770392
51 meter E =
0011727
Z = -2404557
80 I = 51
59565
XDOT = 2619
007160 Wp = 104
48326
YDOT = -4804
033497 meter/sec RA = 349
51058 deg
ZDOT = -5357
483221 TA = 102
35844
MA = 102
22715
Ha = 227
510 n
mi
Hp = 215
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20699355
44 X = -6288399
19
Y = -2527534
50 feet Y = -840829
55 meter
Z = -7888969
17 Z = -2435156
82
XDOT = 8592
543175 XDOT = 2698
557616
YDOT = -15761
264753 feet/sec YDOT = -4774
301209 meter/sec
ZDOT = -17577
044687 ZDOT = -5344
567107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9620350
86 X = 2932282
94
Y = -18445259
41 feet Y = -5622115
07 meter
Z = -8019278
97 Z = -2444276
23
XDOT = 10356
238474 XDOT = 3156
581487
YDOT = 12984
079600 feet/sec YDOT = 3957
547462 meter/sec
ZDOT = -17521
010059 ZDOT = -5340
403866
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 14335
52738093
00016717 00000-0 10270-3 0 9000
2 25544 51
6457 349
9031 0007310 85
0206 275
1779 15
51668181 37292
Satellite: ISS
Catalog Number: 25544
Epoch time: 14335
52738093 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 349
9031 deg
Eccentricity:
0007310
Arg of perigee: 85
0206 deg
Mean anomaly: 275
1779 deg
Mean motion: 15
51668181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 316
Coasting Arc #2 (Orbit 3744)
---------------------------------------
Vector Time (GMT): 2014/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5932422
75 A = 6792088
07 meter
Y = 952375
77 meter E =
0020200
Z = 3148274
57 I = 51
55815
XDOT = -3367
519330 Wp = 86
24777
YDOT = 4912
350499 meter/sec RA = 344
54270 deg
ZDOT = 4834
027036 TA = 310
09196
MA = 310
26887
Ha = 227
428 n
mi
Hp = 215
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19463329
24 X = 5906038
60
Y = 3124592
41 feet Y = 1018568
37 meter
Z = 10328984
81 Z = 3177029
85
XDOT = -11048
291766 XDOT = -3445
682628
YDOT = 16116
635497 feet/sec YDOT = 4874
255565 meter/sec
ZDOT = 15859
668754 ZDOT = 4817
478092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9445041
61 X = -2878848
68
Y = 17228807
82 feet Y = 5251340
62 meter
Z = 10451390
35 Z = 3185583
78
XDOT = -10194
024496 XDOT = -3107
138666
YDOT = -15216
096154 feet/sec YDOT = -4637
866108 meter/sec
ZDOT = 15788
125761 ZDOT = 4812
220732
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 14336
55782947
00016717 00000-0 10270-3 0 9012
2 25544 51
6447 344
7853 0007368 87
9112 272
2883 15
51706639 37459
Satellite: ISS
Catalog Number: 25544
Epoch time: 14336
55782947 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 344
7853 deg
Eccentricity:
0007368
Arg of perigee: 87
9112 deg
Mean anomaly: 272
2883 deg
Mean motion: 15
51706639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3745
Checksum: 345
Coasting Arc #3 (Orbit 3759)
---------------------------------------
Vector Time (GMT): 2014/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5452922
32 A = 6789884
70 meter
Y = -1244917
66 meter E =
0013623
Z = -3862545
68 I = 51
52076
XDOT = 4057
658841 Wp = 83
08955
YDOT = -5010
010582 meter/sec RA = 339
56879 deg
ZDOT = -4124
558920 TA = 143
45284
MA = 143
35981
Ha = 227
429 n
mi
Hp = 215
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17890165
10 X = -5419832
75
Y = -4084375
54 feet Y = -1305710
61 meter
Z = -12672393
98 Z = -3888955
36
XDOT = 13312
529007 XDOT = 4133
416504
YDOT = -16437
042592 feet/sec YDOT = -4964
211457 meter/sec
ZDOT = -13532
017453 ZDOT = -4104
663226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9550873
39 X = 2911106
21
Y = -15577581
89 feet Y = -4748046
96 meter
Z = -12784735
43 Z = -3896787
36
XDOT = 10172
566905 XDOT = 3100
598393
YDOT = 17243
246653 feet/sec YDOT = 5255
741580 meter/sec
ZDOT = -13446
188109 ZDOT = -4098
398136
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 14337
52385302
00016717 00000-0 10270-3 0 9025
2 25544 51
6444 339
9864 0007347 91
6045 268
5948 15
51736139 37603
Satellite: ISS
Catalog Number: 25544
Epoch time: 14337
52385302 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 339
9864 deg
Eccentricity:
0007347
Arg of perigee: 91
6045 deg
Mean anomaly: 268
5948 deg
Mean motion: 15
51736139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 332
Coasting Arc #4 (Orbit 3775)
---------------------------------------
Vector Time (GMT): 2014/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4900345
02 A = 6787790
26 meter
Y = 1564142
21 meter E =
0016324
Z = 4417135
86 I = 51
48426
XDOT = -4640
948841 Wp = 103
14643
YDOT = 5128
716045 meter/sec RA = 334
59000 deg
ZDOT = 3318
531918 TA = 313
22288
MA = 313
35908
Ha = 227
260 n
mi
Hp = 215
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16077247
43 X = 4861032
82
Y = 5131700
15 feet Y = 1618720
98 meter
Z = 14491915
56 Z = 4440846
06
XDOT = -15226
210108 XDOT = -4714
075047
YDOT = 16826
496209 feet/sec YDOT = 5076
408878 meter/sec
ZDOT = 10887
571910 ZDOT = 3295
809135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9728060
29 X = -2965112
78
Y = 13683798
61 feet Y = 4170821
82 meter
Z = 14592681
27 Z = 4447849
25
XDOT = -10414
740505 XDOT = -3174
412906
YDOT = -18958
963644 feet/sec YDOT = -5778
692119 meter/sec
ZDOT = 10789
667267 ZDOT = 3288
690583
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 14338
55425553
00016717 00000-0 10270-3 0 9033
2 25544 51
6435 334
8678 0007310 94
7632 265
4355 15
51776960 37767
Satellite: ISS
Catalog Number: 25544
Epoch time: 14338
55425553 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 334
8678 deg
Eccentricity:
0007310
Arg of perigee: 94
7632 deg
Mean anomaly: 265
4355 deg
Mean motion: 15
51776960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3776
Checksum: 334
Coasting Arc #5 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2014/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4284569
46 A = 6785939
54 meter
Y = -1999546
11 meter E =
0018963
Z = -4884845
79 I = 51
45016
XDOT = 5107
900597 Wp = 82
19529
YDOT = -5180
889634 meter/sec RA = 329
60529 deg
ZDOT = -2364
874351 TA = 164
55087
MA = 164
49291
Ha = 227
337 n
mi
Hp = 215
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14056986
41 X = -4238162
26
Y = -6560190
66 feet Y = -2047199
10 meter
Z = -16026396
96 Z = -4905547
37
XDOT = 16758
204059 XDOT = 5176
942850
YDOT = -16997
669404 feet/sec YDOT = -5123
383563 meter/sec
ZDOT = -7758
774118 ZDOT = -2339
893204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10279510
01 X = 3133194
65
Y = -11495349
49 feet Y = -3503782
53 meter
Z = -16114247
79 Z = -4911622
73
XDOT = 10642
131023 XDOT = 3243
721536
YDOT = 20217
431590 feet/sec YDOT = 6162
273149 meter/sec
ZDOT = -7651
232018 ZDOT = -2332
095519
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 14339
52023631
00016717 00000-0 10270-3 0 9043
2 25544 51
6434 330
0684 0007368 98
2983 261
9005 15
51802111 37910
Satellite: ISS
Catalog Number: 25544
Epoch time: 14339
52023631 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 330
0684 deg
Eccentricity:
0007368
Arg of perigee: 98
2983 deg
Mean anomaly: 261
9005 deg
Mean motion: 15
51802111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 297
Coasting Arc #6 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2014/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3634234
81 A = 6784589
47 meter
Y = 2469047
62 meter E =
0011344
Z = 5161286
83 I = 51
41909
XDOT = -5468
804202 Wp = 109
58429
YDOT = 5208
108349 meter/sec RA = 324
61669 deg
ZDOT = 1353
160244 TA = 327
34153
MA = 327
41162
Ha = 227
135 n
mi
Hp = 215
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11923342
57 X = 3581283
08
Y = 8100549
93 feet Y = 2509391
46 meter
Z = 16933355
75 Z = 5178813
24
XDOT = -17942
271004 XDOT = -5533
209322
YDOT = 17086
969648 feet/sec YDOT = 5146
592405 meter/sec
ZDOT = 4439
502114 ZDOT = 1326
437271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10987074
77 X = -3348860
39
Y = 9195110
89 feet Y = 2802669
80 meter
Z = 17007576
77 Z = 5183909
40
XDOT = -10941
046382 XDOT = -3334
830937
YDOT = -21109
282499 feet/sec YDOT = -6434
109306 meter/sec
ZDOT = 4324
529919 ZDOT = 1318
116719
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 14340
55059283
00016717 00000-0 10270-3 0 9051
2 25544 51
6430 324
9494 0007279 101
5564 258
6405 15
51840067 38078
Satellite: ISS
Catalog Number: 25544
Epoch time: 14340
55059283 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 324
9494 deg
Eccentricity:
0007279
Arg of perigee: 101
5564 deg
Mean anomaly: 258
6405 deg
Mean motion: 15
51840067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 313
Coasting Arc #7 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2014/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2975225
05 A = 6783976
76 meter
Y = -3033306
89 meter E =
0021952
Z = -5307599
21 I = 51
39239
XDOT = 5683
101660 Wp = 93
39524
YDOT = -5111
900355 meter/sec RA = 319
62408 deg
ZDOT = -266
481694 TA = 174
06238
MA = 174
03632
Ha = 227
210 n
mi
Hp = 215
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9761237
04 X = -2915301
97
Y = -9951794
25 feet Y = -3066242
23 meter
Z = -17413383
25 Z = -5321907
29
XDOT = 18645
346654 XDOT = 5741
136231
YDOT = -16771
326625 feet/sec YDOT = -5048
023713 meter/sec
ZDOT = -874
283772 ZDOT = -238
733289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12070768
51 X = 3679170
24
Y = -6819799
92 feet Y = -2078675
01 meter
Z = -17473773
21 Z = -5326006
07
XDOT = 11011
603981 XDOT = 3356
336894
YDOT = 21405
783666 feet/sec YDOT = 6524
482861 meter/sec
ZDOT = -754
961206 ZDOT = -230
112176
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 14341
51653015
00016717 00000-0 10270-3 0 9062
2 25544 51
6433 320
1501 0007334 105
0608 255
1356 15
51865625 38229
Satellite: ISS
Catalog Number: 25544
Epoch time: 14341
51653015 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 320
1501 deg
Eccentricity:
0007334
Arg of perigee: 105
0608 deg
Mean anomaly: 255
1356 deg
Mean motion: 15
51865625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 275
Coasting Arc #8 (Orbit 3837)
---------------------------------------
Vector Time (GMT): 2014/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2318789
62 A = 6784053
87 meter
Y = 3615085
92 meter E =
0009788
Z = 5242902
29 I = 51
36986
XDOT = -5812
172982 Wp = 93
16813
YDOT = 4938
940936 meter/sec RA = 314
62970 deg
ZDOT = -834
118676 TA = 4
83598
MA = 4
82653
Ha = 227
007 n
mi
Hp = 215
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7607577
51 X = 2252724
12
Y = 11860518
12 feet Y = 3640646
24 meter
Z = 17201123
00 Z = 5254006
56
XDOT = -19068
808997 XDOT = -5862
917500
YDOT = 16203
874463 feet/sec YDOT = 4873
661800 meter/sec
ZDOT = -2736
609828 ZDOT = -862
476300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13297880
28 X = -4053193
91
Y = 4484141
64 feet Y = 1366766
37 meter
Z = 17247742
23 Z = 5257111
83
XDOT = -10917
205746 XDOT = -3327
564311
YDOT = -21370
204143 feet/sec YDOT = -6513
638223 meter/sec
ZDOT = -2858
491851 ZDOT = -871
268316
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 14342
54684020
00016717 00000-0 10270-3 0 9077
2 25544 51
6433 315
0310 0007242 108
5799 251
6139 15
51911222 38389
Satellite: ISS
Catalog Number: 25544
Epoch time: 14342
54684020 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 315
0310 deg
Eccentricity:
0007242
Arg of perigee: 108
5799 deg
Mean anomaly: 251
6139 deg
Mean motion: 15
51911222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3838
Checksum: 290
Coasting Arc #9 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2014/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1708605
47 A = 6785026
32 meter
Y = -4242803
35 meter E =
0020093
Z = -5030005
84 I = 51
35223
XDOT = 5800
843458 Wp = 106
85168
YDOT = -4604
226941 meter/sec RA = 309
63431 deg
ZDOT = 1913
878353 TA = 181
82951
MA = 181
83687
Ha = 227
040 n
mi
Hp = 215
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5605660
98 X = -1636600
29
Y = -13919958
49 feet Y = -4261507
04 meter
Z = -16502643
82 Z = -5038131
48
XDOT = 19031
638641 XDOT = 5842
600851
YDOT = -15105
731433 feet/sec YDOT = -4539
124834 meter/sec
ZDOT = 6279
128454 ZDOT = 1942
159090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14789495
53 X = 4507838
24
Y = -2311434
62 feet Y = -704525
27 meter
Z = -16536445
33 Z = -5040308
54
XDOT = 10399
644555 XDOT = 3169
811660
YDOT = 20765
507607 feet/sec YDOT = 6329
326719 meter/sec
ZDOT = 6400
611584 ZDOT = 1950
906411
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 14343
51273386
00016717 00000-0 10270-3 0 9085
2 25544 51
6437 310
2318 0007256 111
8706 248
3218 15
51931676 38531
Satellite: ISS
Catalog Number: 25544
Epoch time: 14343
51273386 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 310
2318 deg
Eccentricity:
0007256
Arg of perigee: 111
8706 deg
Mean anomaly: 248
3218 deg
Mean motion: 15
51931676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 310
Coasting Arc #10 (Orbit 3868)
---------------------------------------
Vector Time (GMT): 2014/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1126469
16 A = 6786536
31 meter
Y = 4847253
66 meter E =
0014139
Z = 4602307
99 I = 51
33879
XDOT = -5739
252608 Wp = 88
09953
YDOT = 4147
650547 meter/sec RA = 304
63952 deg
ZDOT = -2955
310501 TA = 31
49699
MA = 31
41241
Ha = 226
846 n
mi
Hp = 215
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3695764
95 X = 1049825
81
Y = 15903063
20 feet Y = 4859421
70 meter
Z = 15099435
68 Z = 4607594
41
XDOT = -18829
568923 XDOT = -5770
850118
YDOT = 13607
777386 feet/sec YDOT = 4083
294046 meter/sec
ZDOT = -9695
900593 ZDOT = -2983
267398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16304065
76 X = -4969479
24
Y = 302035
14 feet Y = 92060
31 meter
Z = 15121020
79 Z = 4608887
14
XDOT = -9498
514235 XDOT = -2895
147139
YDOT = -19947
362256 feet/sec YDOT = -6079
956016 meter/sec
ZDOT = -9815
907461 ZDOT = -2991
888594
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 14344
54299699
00016717 00000-0 10270-3 0 9095
2 25544 51
6440 305
1127 0007178 115
5924 244
5970 15
51992160 38697
Satellite: ISS
Catalog Number: 25544
Epoch time: 14344
54299699 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 305
1127 deg
Eccentricity:
0007178
Arg of perigee: 115
5924 deg
Mean anomaly: 244
5970 deg
Mean motion: 15
51992160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3869
Checksum: 336
Coasting Arc #11 (Orbit 3883)
---------------------------------------
Vector Time (GMT): 2014/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -630156
44 A = 6788616
59 meter
Y = -5430251
90 meter E =
0014200
Z = -4040509
40 I = 51
32890
XDOT = 5576
405063 Wp = 113
27506
YDOT = -3526
937405 meter/sec RA = 299
64635 deg
ZDOT = 3875
738257 TA = 197
14591
MA = 197
19393
Ha = 226
842 n
mi
Hp = 215
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2067442
37 X = -549759
80
Y = -17815787
08 feet Y = -5436848
96 meter
Z = -13256264
43 Z = -4043375
65
XDOT = 18295
292203 XDOT = 5596
602594
YDOT = -11571
316944 feet/sec YDOT = -3464
465722 meter/sec
ZDOT = 12715
676695 ZDOT = 3902
876450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17875319
83 X = 5448397
49
Y = 1361423
07 feet Y = 414961
75 meter
Z = -13267426
36 Z = -4043911
55
XDOT = 8083
526038 XDOT = 2463
858736
YDOT = 18743
739624 feet/sec YDOT = 5713
091837 meter/sec
ZDOT = 12832
065876 ZDOT = 3911
213679
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 14345
50884689
00016717 00000-0 10270-3 0 9103
2 25544 51
6441 300
3135 0007172 118
8999 241
2873 15
52003208 38846
Satellite: ISS
Catalog Number: 25544
Epoch time: 14345
50884689 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 300
3135 deg
Eccentricity:
0007172
Arg of perigee: 118
8999 deg
Mean anomaly: 241
2873 deg
Mean motion: 15
52003208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3884
Checksum: 313
Coasting Arc #12 (Orbit 3899)
---------------------------------------
Vector Time (GMT): 2014/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 167579
92 A = 6790776
06 meter
Y = 5931459
10 meter E =
0019182
Z = 3281233
22 I = 51
32239
XDOT = -5403
540971 Wp = 102
86877
YDOT = 2760
963801 meter/sec RA = 294
65530 deg
ZDOT = -4695
961421 TA = 38
82489
MA = 38
68724
Ha = 226
681 n
mi
Hp = 215
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 549802
88 X = 85301
35
Y = 19460167
66 feet Y = 5932872
89 meter
Z = 10765200
86 Z = 3281847
73
XDOT = -17728
152792 XDOT = -5411
201670
YDOT = 9058
280187 feet/sec YDOT = 2700
495285 meter/sec
ZDOT = -15406
697577 ZDOT = -4722
229507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19262994
57 X = -5871360
75
Y = -2811706
68 feet Y = -857008
20 meter
Z = 10766675
61 Z = 3281682
73
XDOT = -6154
403895 XDOT = -1875
862307
YDOT = -17502
061404 feet/sec YDOT = -5334
628316 meter/sec
ZDOT = -15519
223414 ZDOT = -4730
259297
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 14346
53906335
00016717 00000-0 10270-3 0 9111
2 25544 51
6445 295
1939 0007156 122
6266 237
5577 15
52064549 39008
Satellite: ISS
Catalog Number: 25544
Epoch time: 14346
53906335 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 295
1939 deg
Eccentricity:
0007156
Arg of perigee: 122
6266 deg
Mean anomaly: 237
5577 deg
Mean motion: 15
52064549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3900
Checksum: 323
Coasting Arc #13 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2014/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 196296
01 A = 6792776
61 meter
Y = -6341924
93 meter E =
0009806
Z = -2434877
81 I = 51
31675
XDOT = 5186
105304 Wp = 92
80176
YDOT = -1872
134364 meter/sec RA = 289
66689 deg
ZDOT = 5312
424724 TA = 239
87783
MA = 239
97506
Ha = 226
629 n
mi
Hp = 215
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 644015
77 X = 279026
16
Y = -20806840
33 feet Y = -6339267
16 meter
Z = -7988444
26 Z = -2433723
53
XDOT = 17014
781181 XDOT = 5180
848452
YDOT = -6142
173111 feet/sec YDOT = -1814
169562 meter/sec
ZDOT = 17429
214973 ZDOT = 5337
605256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20460631
04 X = 6236400
34
Y = 3847065
28 feet Y = 1172585
50 meter
Z = -7982309
72 Z = -2433008
00
XDOT = 3782
093677 XDOT = 1152
782153
YDOT = 16148
899243 feet/sec YDOT = 4922
184489 meter/sec
ZDOT = 17536
929484 ZDOT = 5345
256107
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 14347
50486919
00016717 00000-0 10270-3 0 9121
2 25544 51
6442 290
3945 0007126 126
3290 233
8520 15
52081997 39153
Satellite: ISS
Catalog Number: 25544
Epoch time: 14347
50486919 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 290
3945 deg
Eccentricity:
0007126
Arg of perigee: 126
3290 deg
Mean anomaly: 233
8520 deg
Mean motion: 15
52081997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 318
Coasting Arc #14 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2014/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -543930
37 A = 6794314
23 meter
Y = 6607970
22 meter E =
0020928
Z = 1434196
30 I = 51
31330
XDOT = -4992
623042 Wp = 122
72993
YDOT = 850
551689 meter/sec RA = 284
68037 deg
ZDOT = -5762
060777 TA = 41
55519
MA = 41
39629
Ha = 226
517 n
mi
Hp = 215
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1784548
45 X = -624748
69
Y = 21679692
31 feet Y = 6601435
71 meter
Z = 4705368
43 Z = 1431357
86
XDOT = -16379
996856 XDOT = -4973
772749
YDOT = 2790
523913 feet/sec YDOT = 794
826521 meter/sec
ZDOT = -18904
398876 ZDOT = -5786
268475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21237327
60 X = -6473137
45
Y = -4721767
62 feet Y = -1439194
77 meter
Z = 4692013
53 Z = 1430125
72
XDOT = -914
522090 XDOT = -278
746333
YDOT = -14939
138747 feet/sec YDOT = -4553
449490 meter/sec
ZDOT = -19007
769281 ZDOT = -5793
568077
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 14348
53503940
00016717 00000-0 10270-3 0 9130
2 25544 51
6451 285
2742 0007180 130
3203 229
8577 15
52120450 39313
Satellite: ISS
Catalog Number: 25544
Epoch time: 14348
53503940 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 285
2742 deg
Eccentricity:
0007180
Arg of perigee: 130
3203 deg
Mean anomaly: 229
8577 deg
Mean motion: 15
52120450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 287
Coasting Arc #15 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2014/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 808923
64 A = 6794979
09 meter
Y = -6731926
97 meter E =
0013085
Z = -419942
84 I = 51
30840
XDOT = 4806
813147 Wp = 74
94786
YDOT = 215
670069 meter/sec RA = 279
69524 deg
ZDOT = 5961
316285 TA = 280
50959
MA = 280
65700
Ha = 226
403 n
mi
Hp = 215
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2653948
96 X = 886181
46
Y = -22086374
56 feet Y = -6722449
07 meter
Z = -1377765
23 Z = -415825
74
XDOT = 15770
384341 XDOT = 4775
085933
YDOT = 707
578966 feet/sec YDOT = 269
245392 meter/sec
ZDOT = 19558
124293 ZDOT = 5984
590153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21619007
39 X = 6589473
45
Y = 5246085
27 feet Y = 1599006
79 meter
Z = -1358945
15 Z = -414206
48
XDOT = -2165
214234 XDOT = -659
957299
YDOT = 13877
477257 feet/sec YDOT = 4229
855068 meter/sec
ZDOT = 19657
312269 ZDOT = 5991
548780
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 14349
50080141
00016717 00000-0 10270-3 0 9142
2 25544 51
6446 280
4744 0007097 134
0315 226
1422 15
52159678 39467
Satellite: ISS
Catalog Number: 25544
Epoch time: 14349
50080141 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 280
4744 deg
Eccentricity:
0007097
Arg of perigee: 134
0315 deg
Mean anomaly: 226
1422 deg
Mean motion: 15
52159678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 303
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