[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 11th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20989 63 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 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
352/11:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
1
000/00:00:00
000 0
0 0
0 215
8
Coasting Arc #1 (Orbit 3869)
---------------------------------------
Vector Time (GMT): 2014/344/14:07:51
014
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4318383
89 A = 6784184
18 meter
Y = -987624
58 meter E =
0020191
Z = -5155680
51 I = 51
33187
XDOT = 3240
794823 Wp = 91
20649
YDOT = -6782
715627 meter/sec RA = 304
23575 deg
ZDOT = -1420
438987 TA = 165
06632
MA = 165
00661
Ha = 226
887 n
mi
Hp = 215
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14167926
16 X = -4281974
49
Y = -3240238
11 feet Y = -1035711
60 meter
Z = -16914962
30 Z = -5176570
22
XDOT = 10632
528947 XDOT = 3323
299895
YDOT = -22253
004025 feet/sec YDOT = -6746
013543 meter/sec
ZDOT = -4660
232898 ZDOT = -1404
495768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1851786
70 X = -564424
59
Y = -14310342
05 feet Y = -4361792
26 meter
Z = -17003829
58 Z = -5182767
26
XDOT = 23528
883616 XDOT = 7171
603726
YDOT = 2389
954906 feet/sec YDOT = 728
458255 meter/sec
ZDOT = -4590
927944 ZDOT = -1399
314837
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
60733673
00016717 00000-0 10270-3 0 9008
2 25544 51
6463 304
7988 0007264 115
1509 245
0397 15
52008802 38706
Satellite: ISS
Catalog Number: 25544
Epoch time: 14344
60733673 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 304
7988 deg
Eccentricity:
0007264
Arg of perigee: 115
1509 deg
Mean anomaly: 245
0397 deg
Mean motion: 15
52008802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3870
Checksum: 308
Coasting Arc #2 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2014/345/14:07:51
014
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3855745
41 A = 6783346
74 meter
Y = 1774574
37 meter E =
0009571
Z = 5283936
33 I = 51
31281
XDOT = -3537
949429 Wp = 114
93640
YDOT = 6801
344504 meter/sec RA = 299
23716 deg
ZDOT = 293
109904 TA = 332
23264
MA = 332
28370
Ha = 226
581 n
mi
Hp = 215
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12650083
38 X = 3809947
53
Y = 5822094
40 feet Y = 1817435
44 meter
Z = 17335749
11 Z = 5302555
83
XDOT = -11607
445632 XDOT = -3615
164532
YDOT = 22314
122388 feet/sec YDOT = 6761
349107 meter/sec
ZDOT = 961
646666 ZDOT = 275
735915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -860520
65 X = -262286
69
Y = 13799793
41 feet Y = 4206177
03 meter
Z = 17414786
71 Z = 5308026
99
XDOT = -24004
168518 XDOT = -7316
470564
YDOT = -2633
321353 feet/sec YDOT = -802
636348 meter/sec
ZDOT = 886
249447 ZDOT = 270
128832
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
63756478
00016717 00000-0 10270-3 0 9011
2 25544 51
6463 299
6802 0007140 119
7601 240
4262 15
52075855 38868
Satellite: ISS
Catalog Number: 25544
Epoch time: 14345
63756478 = yrday
fracday
Element set: 901
Inclination: 51
6463 deg
RA of node: 299
6802 deg
Eccentricity:
0007140
Arg of perigee: 119
7601 deg
Mean anomaly: 240
4262 deg
Mean motion: 15
52075855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 323
Coasting Arc #3 (Orbit 3900)
---------------------------------------
Vector Time (GMT): 2014/346/14:07:51
014
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3427285
81 A = 6783613
32 meter
Y = -2630288
25 meter E =
0021193
Z = -5248483
14 I = 51
29939
XDOT = 3741
553645 Wp = 105
19700
YDOT = -6614
951051 meter/sec RA = 294
23506 deg
ZDOT = 869
348546 TA = 173
19096
MA = 173
16212
Ha = 226
716 n
mi
Hp = 215
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11244376
02 X = -3372123
18
Y = -8629554
62 feet Y = -2668305
71 meter
Z = -17219432
88 Z = -5264998
53
XDOT = 12275
438468 XDOT = 3811
022480
YDOT = -21702
595313 feet/sec YDOT = -6572
722188 meter/sec
ZDOT = 2852
193394 ZDOT = 887
692899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3753724
65 X = 1144135
27
Y = -13579484
95 feet Y = -4139027
01 meter
Z = -17289338
14 Z = -5269790
27
XDOT = 23741
517418 XDOT = 7236
414509
YDOT = 2819
796307 feet/sec YDOT = 859
473915 meter/sec
ZDOT = 2931
679870 ZDOT = 893
576024
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
60338357
00016717 00000-0 10270-3 0 9022
2 25544 51
6466 294
8801 0007230 122
5937 237
5913 15
52074719 39017
Satellite: ISS
Catalog Number: 25544
Epoch time: 14346
60338357 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 294
8801 deg
Eccentricity:
0007230
Arg of perigee: 122
5937 deg
Mean anomaly: 237
5913 deg
Mean motion: 15
52074719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3901
Checksum: 313
Coasting Arc #4 (Orbit 3916)
---------------------------------------
Vector Time (GMT): 2014/347/14:07:51
014
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3017301
35 A = 6784532
03 meter
Y = 3467901
75 meter E =
0010815
Z = 4980282
40 I = 51
29061
XDOT = -3903
738595 Wp = 94
84443
YDOT = 6291
510807 meter/sec RA = 289
23399 deg
ZDOT = -2012
981704 TA = 14
81701
MA = 14
78534
Ha = 226
459 n
mi
Hp = 215
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9899282
65 X = 2954105
60
Y = 11377630
41 feet Y = 3501289
64 meter
Z = 16339509
19 Z = 4994786
66
XDOT = -12807
541323 XDOT = -3964
023183
YDOT = 20641
439656 feet/sec YDOT = 6247
519673 meter/sec
ZDOT = -6604
270682 ZDOT = -2032
091716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6573338
79 X = -2003553
66
Y = 13499429
16 feet Y = 4114626
01 meter
Z = 16400684
76 Z = 4998928
71
XDOT = -23023
270401 XDOT = -7017
492818
YDOT = -3075
283115 feet/sec YDOT = -937
346293 meter/sec
ZDOT = -6686
948329 ZDOT = -2038
181851
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
63356448
00016717 00000-0 10270-3 0 9038
2 25544 51
6462 289
7609 0007170 126
4595 233
7223 15
52132612 39174
Satellite: ISS
Catalog Number: 25544
Epoch time: 14347
63356448 = yrday
fracday
Element set: 903
Inclination: 51
6462 deg
RA of node: 289
7609 deg
Eccentricity:
0007170
Arg of perigee: 126
4595 deg
Mean anomaly: 233
7223 deg
Mean motion: 15
52132612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3917
Checksum: 316
Coasting Arc #5 (Orbit 3931)
---------------------------------------
Vector Time (GMT): 2014/348/14:07:51
014
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2669812
26 A = 6786317
35 meter
Y = -4291950
22 meter E =
0016826
Z = -4545362
81 I = 51
28777
XDOT = 4002
915637 Wp = 118
42540
YDOT = -5748
386477 meter/sec RA = 284
23320 deg
ZDOT = 3077
583481 TA = 182
60105
MA = 182
60981
Ha = 226
508 n
mi
Hp = 215
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8759226
59 X = -2599540
29
Y = -14081201
50 feet Y = -4321412
73 meter
Z = -14912607
63 Z = -4558161
86
XDOT = 13132
925319 XDOT = 4051
947985
YDOT = -18859
535687 feet/sec YDOT = -5703
349219 meter/sec
ZDOT = 10097
058665 ZDOT = 3097
148040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9269514
95 X = 2825348
16
Y = -13692122
87 feet Y = -4173359
05 meter
Z = -14966362
83 Z = -4561747
39
XDOT = 21567
278724 XDOT = 6573
706555
YDOT = 3474
997434 feet/sec YDOT = 1059
179218 meter/sec
ZDOT = 10181
561344 ZDOT = 3103
339898
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
59933738
00016717 00000-0 10270-3 0 9048
2 25544 51
6468 284
9605 0007202 129
9813 230
1973 15
52149667 39328
Satellite: ISS
Catalog Number: 25544
Epoch time: 14348
59933738 = yrday
fracday
Element set: 904
Inclination: 51
6468 deg
RA of node: 284
9605 deg
Eccentricity:
0007202
Arg of perigee: 129
9813 deg
Mean anomaly: 230
1973 deg
Mean motion: 15
52149667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3932
Checksum: 340
Coasting Arc #6 (Orbit 3947)
---------------------------------------
Vector Time (GMT): 2014/349/14:07:51
014
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2339377
49 A = 6788534
61 meter
Y = 5035367
91 meter E =
0016577
Z = 3889280
34 I = 51
28825
XDOT = -4113
755072 Wp = 101
05241
YDOT = 5051
828395 meter/sec RA = 279
23573 deg
ZDOT = -4054
489532 TA = 31
61794
MA = 31
51846
Ha = 226
350 n
mi
Hp = 215
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7675122
99 X = 2264004
00
Y = 16520235
94 feet Y = 5061106
79 meter
Z = 12760106
09 Z = 3900461
83
XDOT = -13496
571757 XDOT = -4150
244554
YDOT = 16574
240142 feet/sec YDOT = 5005
621818 meter/sec
ZDOT = -13302
131009 ZDOT = -4074
562142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11695031
05 X = -3564645
46
Y = 13923265
52 feet Y = 4243811
33 meter
Z = 12806831
84 Z = 3903522
35
XDOT = -19698
520804 XDOT = -6004
109141
YDOT = -4196
039739 feet/sec YDOT = -1278
952912 meter/sec
ZDOT = -13388
661028 ZDOT = -4080
863881
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
62947156
00016717 00000-0 10270-3 0 9053
2 25544 51
6464 279
8406 0007238 133
6824 226
4929 15
52181563 39486
Satellite: ISS
Catalog Number: 25544
Epoch time: 14349
62947156 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 279
8406 deg
Eccentricity:
0007238
Arg of perigee: 133
6824 deg
Mean anomaly: 226
4929 deg
Mean motion: 15
52181563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3948
Checksum: 343
Coasting Arc #7 (Orbit 3962)
---------------------------------------
Vector Time (GMT): 2014/350/14:07:51
014
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2072810
95 A = 6790750
86 meter
Y = -5680238
69 meter E =
0010076
Z = -3103732
26 I = 51
29274
XDOT = 4203
439607 Wp = 114
21167
YDOT = -4176
945224 meter/sec RA = 274
24105 deg
ZDOT = 4845
560284 TA = 209
97185
MA = 210
02957
Ha = 226
262 n
mi
Hp = 215
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6800560
87 X = -1994062
10
Y = -18635953
69 feet Y = -5702977
78 meter
Z = -10182848
62 Z = -3113610
69
XDOT = 13790
812358 XDOT = 4226
296438
YDOT = -13703
888530 feet/sec YDOT = -4129
812012 meter/sec
ZDOT = 15897
507492 ZDOT = 4866
035507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13730662
21 X = 4185105
84
Y = -14289068
37 feet Y = -4355308
04 meter
Z = -10223905
55 Z = -3116246
41
XDOT = 17304
483720 XDOT = 5274
406638
YDOT = 5210
209619 feet/sec YDOT = 1588
071892 meter/sec
ZDOT = 15985
585699 ZDOT = 4872
406521
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 14350
59519925
00016717 00000-0 10270-3 0 9061
2 25544 51
6471 275
0399 0007161 137
7203 222
4502 15
52229237 39635
Satellite: ISS
Catalog Number: 25544
Epoch time: 14350
59519925 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 275
0399 deg
Eccentricity:
0007161
Arg of perigee: 137
7203 deg
Mean anomaly: 222
4502 deg
Mean motion: 15
52229237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3963
Checksum: 310
Coasting Arc #8 (Orbit 3978)
---------------------------------------
Vector Time (GMT): 2014/351/14:07:51
014
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1793845
92 A = 6792909
12 meter
Y = 6180787
78 meter E =
0020428
Z = 2137859
74 I = 51
29834
XDOT = -4345
461778 Wp = 120
50163
YDOT = 3164
895787 meter/sec RA = 269
25057 deg
ZDOT = -5474
903332 TA = 35
67339
MA = 35
53706
Ha = 226
198 n
mi
Hp = 215
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5885321
27 X = 1714212
46
Y = 20278175
13 feet Y = 6200402
37 meter
Z = 7013975
54 Z = 2146380
95
XDOT = -14256
764364 XDOT = -4353
933872
YDOT = 10383
516360 feet/sec YDOT = 3116
254915 meter/sec
ZDOT = -17962
281273 ZDOT = -5496
033573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15352437
73 X = -4679423
02
Y = 14479269
28 feet Y = 4413281
28 meter
Z = 7049160
42 Z = 2148584
10
XDOT = -14650
259182 XDOT = -4465
398999
YDOT = -6698
738589 feet/sec YDOT = -2041
775522 meter/sec
ZDOT = -18052
962504 ZDOT = -5502
542971
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 14351
62528729
00016717 00000-0 10270-3 0 9079
2 25544 51
6470 269
9195 0007275 141
6854 218
4816 15
52228591 39794
Satellite: ISS
Catalog Number: 25544
Epoch time: 14351
62528729 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 269
9195 deg
Eccentricity:
0007275
Arg of perigee: 141
6854 deg
Mean anomaly: 218
4816 deg
Mean motion: 15
52228591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3979
Checksum: 347
Coasting Arc #9 (Orbit 3991)
---------------------------------------
Vector Time (GMT): 2014/352/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -767789
59 A = 6794687
61 meter
Y = -6746527
97 meter E =
0012442
Z = -206769
58 I = 51
30413
XDOT = 4741
441306 Wp = 77
86650
YDOT = -713
266563 meter/sec RA = 264
90512 deg
ZDOT = 5974
849980 TA = 279
89846
MA = 280
03890
Ha = 226
051 n
mi
Hp = 215
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2518994
72 X = -691286
85
Y = -22134278
11 feet Y = -6754686
12 meter
Z = -678377
87 Z = -210314
05
XDOT = 15555
909797 XDOT = 4720
040669
YDOT = -2340
113397 feet/sec YDOT = -660
364743 meter/sec
ZDOT = 19602
526181 ZDOT = 5997
831410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21858861
50 X = 6662580
99
Y = 4294504
55 feet Y = 1308964
99 meter
Z = -692244
75 Z = -210996
20
XDOT = -2123
163438 XDOT = -647
140216
YDOT = 13822
584574 feet/sec YDOT = 4213
123778 meter/sec
ZDOT = 19700
648766 ZDOT = 6004
757744
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 14352
46221492
00016717 00000-0 10270-3 0 9080
2 25544 51
6453 265
7585 0007095 144
8489 215
3132 15
52278222 39929
Satellite: ISS
Catalog Number: 25544
Epoch time: 14352
46221492 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 265
7585 deg
Eccentricity:
0007095
Arg of perigee: 144
8489 deg
Mean anomaly: 215
3132 deg
Mean motion: 15
52278222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3992
Checksum: 323
Coasting Arc #10 (Orbit 4007)
---------------------------------------
Vector Time (GMT): 2014/353/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 438516
02 A = 6794275
75 meter
Y = 6708262
40 meter E =
0017042
Z = -926928
26 I = 51
30773
XDOT = -4881
357816 Wp = 144
35058
YDOT = -485
915929 meter/sec RA = 259
91956 deg
ZDOT = -5894
343704 TA = 45
72811
MA = 45
58841
Ha = 225
930 n
mi
Hp = 215
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1438700
87 X = 367972
83
Y = 22008734
90 feet Y = 6712771
82 meter
Z = -3041103
23 Z = -924968
77
XDOT = -16014
953464 XDOT = -4846
928350
YDOT = -1594
212365 feet/sec YDOT = -540
309423 meter/sec
ZDOT = -19338
397978 ZDOT = -5917
973252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21506765
37 X = -6555262
08
Y = -4894546
65 feet Y = -1491857
82 meter
Z = -3033980
48 Z = -924757
25
XDOT = 5715
680472 XDOT = 1742
139408
YDOT = -13204
651039 feet/sec YDOT = -4024
777637 meter/sec
ZDOT = -19439
069683 ZDOT = -5925
028439
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 14353
49225983
00016717 00000-0 10270-3 0 9094
2 25544 51
6464 260
6376 0007140 148
9844 211
1731 15
52304375 40081
Satellite: ISS
Catalog Number: 25544
Epoch time: 14353
49225983 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 260
6376 deg
Eccentricity:
0007140
Arg of perigee: 148
9844 deg
Mean anomaly: 211
1731 deg
Mean motion: 15
52304375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4008
Checksum: 309
Coasting Arc #11 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2014/354/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -107982
03 A = 6792872
70 meter
Y = -6494098
75 meter E =
0016235
Z = 1977669
91 I = 51
30938
XDOT = 5035
726815 Wp = 93
72887
YDOT = 1617
709447 meter/sec RA = 254
93282 deg
ZDOT = 5546
483870 TA = 288
18364
MA = 288
36032
Ha = 225
806 n
mi
Hp = 215
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -354271
74 X = -44962
40
Y = -21306098
26 feet Y = -6494954
12 meter
Z = 6488418
33 Z = 1977297
75
XDOT = 16521
413434 XDOT = 4990
319779
YDOT = 5307
445691 feet/sec YDOT = 1673
767753 meter/sec
ZDOT = 18197
125557 ZDOT = 5570
836718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20624586
30 X = 6286373
91
Y = 5357888
07 feet Y = 1633084
28 meter
Z = 6488018
12 Z = 1977547
92
XDOT = -9141
137807 XDOT = -2786
218803
YDOT = 12865
805969 feet/sec YDOT = 3921
497659 meter/sec
ZDOT = 18300
684232 ZDOT = 5578
048554
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 14354
52228195
00016717 00000-0 10270-3 0 9109
2 25544 51
6459 255
5172 0007058 152
4744 207
6783 15
52343452 40243
Satellite: ISS
Catalog Number: 25544
Epoch time: 14354
52228195 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 255
5172 deg
Eccentricity:
0007058
Arg of perigee: 152
4744 deg
Mean anomaly: 207
6783 deg
Mean motion: 15
52343452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4024
Checksum: 306
Coasting Arc #12 (Orbit 4038)
---------------------------------------
Vector Time (GMT): 2014/355/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -336931
72 A = 6790586
15 meter
Y = 6080921
78 meter E =
0010694
Z = -2999406
76 I = 51
31188
XDOT = -5197
636433 Wp = 138
79154
YDOT = -2713
250299 meter/sec RA = 249
94322 deg
ZDOT = -4934
879413 TA = 75
68209
MA = 75
56338
Ha = 225
625 n
mi
Hp = 215
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1105419
01 X = -390334
80
Y = 19950530
79 feet Y = 6076855
74 meter
Z = -9840573
36 Z = -3001172
56
XDOT = -17052
612970 XDOT = -5142
937868
YDOT = -8901
739827 feet/sec YDOT = -2771
067253 meter/sec
ZDOT = -16190
549254 ZDOT = -4959
996256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19038278
37 X = -5802867
25
Y = -6051409
98 feet Y = -1844469
76 meter
Z = -9849208
49 Z = -3002038
75
XDOT = 12456
856566 XDOT = 3796
849881
YDOT = -12761
143559 feet/sec YDOT = -3889
596557 meter/sec
ZDOT = -16297
180371 ZDOT = -4967
380577
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 14355
48790672
00016717 00000-0 10270-3 0 9110
2 25544 51
6466 250
7164 0007034 156
4358 203
7117 15
52384409 40399
Satellite: ISS
Catalog Number: 25544
Epoch time: 14355
48790672 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 250
7164 deg
Eccentricity:
0007034
Arg of perigee: 156
4358 deg
Mean anomaly: 203
7117 deg
Mean motion: 15
52384409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4039
Checksum: 313
Coasting Arc #13 (Orbit 4054)
---------------------------------------
Vector Time (GMT): 2014/356/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 814024
62 A = 6788060
38 meter
Y = -5530666
19 meter E =
0015913
Z = 3845468
99 I = 51
31457
XDOT = 5340
366691 Wp = 121
12581
YDOT = 3656
937780 meter/sec RA = 244
94992 deg
ZDOT = 4108
303456 TA = 285
43038
MA = 285
60610
Ha = 225
530 n
mi
Hp = 216
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2670684
44 X = 857129
36
Y = -18145230
27 feet Y = -5521322
65 meter
Z = 12616368
08 Z = 3849527
48
XDOT = 17520
888095 XDOT = 5279
120329
YDOT = 11997
827361 feet/sec YDOT = 3716
314322 meter/sec
ZDOT = 13478
685878 ZDOT = 4134
097726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17019676
87 X = 5187597
51
Y = 6800754
16 feet Y = 2072869
87 meter
Z = 12634675
41 Z = 3851049
06
XDOT = -15279
843340 XDOT = -4657
296250
YDOT = 12868
990273 feet/sec YDOT = 3922
468235 meter/sec
ZDOT = 13588
053271 ZDOT = 4141
638637
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 14356
51788596
00016717 00000-0 10270-3 0 9128
2 25544 51
6459 245
5955 0007019 159
9345 200
2084 15
52408708 40550
Satellite: ISS
Catalog Number: 25544
Epoch time: 14356
51788596 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 245
5955 deg
Eccentricity:
0007019
Arg of perigee: 159
9345 deg
Mean anomaly: 200
2084 deg
Mean motion: 15
52408708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4055
Checksum: 332
Coasting Arc #14 (Orbit 4069)
---------------------------------------
Vector Time (GMT): 2014/357/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1424288
37 A = 6785352
43 meter
Y = 4827035
20 meter E =
0011699
Z = -4559137
56 I = 51
32048
XDOT = -5413
320815 Wp = 106
20162
YDOT = -4473
588340 meter/sec RA = 239
95214 deg
ZDOT = -3055
070819 TA = 133
11642
MA = 133
01850
Ha = 225
296 n
mi
Hp = 216
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4672862
12 X = -1456012
94
Y = 15836729
67 feet Y = 4810930
96 meter
Z = -14957800
39 Z = -4566133
06
XDOT = -17760
238893 XDOT = -5348
053366
YDOT = -14677
127101 feet/sec YDOT = -4533
758369 meter/sec
ZDOT = -10023
198224 ZDOT = -3081
209638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14445787
14 X = -4403075
92
Y = -7939611
00 feet Y = -2419993
43 meter
Z = -14988503
95 Z = -4568496
00
XDOT = 17622
790489 XDOT = 5371
426541
YDOT = -12993
254472 feet/sec YDOT = -3960
343963 meter/sec
ZDOT = -10133
909708 ZDOT = -3088
815679
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 14357
48347035
00016717 00000-0 10270-3 0 9135
2 25544 51
6462 240
7943 0006927 164
0028 196
1343 15
52463584 40701
Satellite: ISS
Catalog Number: 25544
Epoch time: 14357
48347035 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 240
7943 deg
Eccentricity:
0006927
Arg of perigee: 164
0028 deg
Mean anomaly: 196
1343 deg
Mean motion: 15
52463584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4070
Checksum: 310
Coasting Arc #15 (Orbit 4085)
---------------------------------------
Vector Time (GMT): 2014/358/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2069497
82 A = 6783354
02 meter
Y = -4054654
38 meter E =
0011741
Z = 5026546
27 I = 51
32997
XDOT = 5410
100233 Wp = 148
54505
YDOT = 5099
965812 meter/sec RA = 234
95111 deg
ZDOT = 1874
641649 TA = 283
14088
MA = 283
27186
Ha = 225
174 n
mi
Hp = 216
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6789691
02 X = 2090267
08
Y = -13302671
85 feet Y = -4031396
20 meter
Z = 16491293
55 Z = 5036649
58
XDOT = 17749
672679 XDOT = 5343
562845
YDOT = 16732
171298 feet/sec YDOT = 5160
092875 meter/sec
ZDOT = 6150
399110 ZDOT = 1900
761624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11671849
14 X = 3557579
62
Y = 9240220
38 feet Y = 2816419
17 meter
Z = 16535114
46 Z = 5039902
89
XDOT = -19298
570495 XDOT = -5882
204287
YDOT = 13104
109920 feet/sec YDOT = 3994
132704 meter/sec
ZDOT = 6260
941613 ZDOT = 1908
335004
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 14358
51340692
00016717 00000-0 10270-3 0 9143
2 25544 51
6456 235
6728 0006955 168
0416 192
0902 15
52483560 40863
Satellite: ISS
Catalog Number: 25544
Epoch time: 14358
51340692 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 235
6728 deg
Eccentricity:
0006955
Arg of perigee: 168
0416 deg
Mean anomaly: 192
0902 deg
Mean motion: 15
52483560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4086
Checksum: 320
Coasting Arc #16 (Orbit 4100)
---------------------------------------
Vector Time (GMT): 2014/359/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2822198
43 A = 6782131
09 meter
Y = 3206840
36 meter E =
0016539
Z = -5280731
60 I = 51
34514
XDOT = -5250
407494 Wp = 110
04269
YDOT = -5541
614753 meter/sec RA = 229
94721 deg
ZDOT = -566
280067 TA = 154
56231
MA = 154
48082
Ha = 224
970 n
mi
Hp = 216
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9259181
19 X = -2832196
59
Y = 10521129
80 feet Y = 3175225
14 meter
Z = -17325234
89 Z = -5294465
32
XDOT = -17225
746373 XDOT = -5185
298874
YDOT = -18181
150766 feet/sec YDOT = -5599
964139 meter/sec
ZDOT = -1857
874234 ZDOT = -591
627650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8638390
87 X = -2632981
54
Y = -10943096
90 feet Y = -3335455
94 meter
Z = -17384395
48 Z = -5298763
74
XDOT = 20262
587365 XDOT = 6176
036629
YDOT = -12909
766894 feet/sec YDOT = -3934
896949 meter/sec
ZDOT = -1965
066139 ZDOT = -598
952159
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 14359
47895234
00016717 00000-0 10270-3 0 9157
2 25544 51
6456 230
8708 0006836 172
2280 187
8979 15
52530086 41012
Satellite: ISS
Catalog Number: 25544
Epoch time: 14359
47895234 = yrday
fracday
Element set: 915
Inclination: 51
6456 deg
RA of node: 230
8708 deg
Eccentricity:
0006836
Arg of perigee: 172
2280 deg
Mean anomaly: 187
8979 deg
Mean motion: 15
52530086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4101
Checksum: 333
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