[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 6th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
191/05:39:57
291 4
1 4
5 4
5
N/A 0
2 -0
7 228
9
000/00:09:54
582 1
9 -0
1 221
0
Coasting Arc #1 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2013/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4385191
57 A = 6791016
67 meter
Y = 2426675
30 meter E =
0014219
Z = 4569416
64 I = 51
74547
XDOT = -5583
525885 Wp = 96
82247
YDOT = -4256
133056 meter/sec RA = 17
00126 deg
ZDOT = -3091
515803 TA = 24
08807
MA = 24
02164
Ha = 229
412 n
mi
Hp = 217
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14387111
46 X = -4434198
14
Y = 7961533
12 feet Y = 2377362
65 meter
Z = 14991524
40 Z = 4547995
19
XDOT = -18318
654477 XDOT = -5520
500232
YDOT = -13963
691127 feet/sec YDOT = -4318
218729 meter/sec
ZDOT = -10142
768384 ZDOT = -3118
487461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10979458
93 X = 3346539
08
Y = 12349809
36 feet Y = 3764221
89 meter
Z = 14901492
54 Z = 4541974
93
XDOT = -8661
153011 XDOT = -2639
919438
YDOT = 20100
164511 feet/sec YDOT = 6126
530143 meter/sec
ZDOT = -10254
935926 ZDOT = -3125
704470
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 13186
54276827
00016717 00000-0 10270-3 0 9007
2 25544 51
6473 17
3580 0007971 130
8042 229
3802 15
50549659 37559
Satellite: ISS
Catalog Number: 25544
Epoch time: 13186
54276827 = yrday
fracday
Element set: 900
Inclination: 51
6473 deg
RA of node: 17
3580 deg
Eccentricity:
0007971
Arg of perigee: 130
8042 deg
Mean anomaly: 229
3802 deg
Mean motion: 15
50549659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 320
Coasting Arc #2 (Orbit 3769)
---------------------------------------
Vector Time (GMT): 2013/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4665548
55 A = 6792060
00 meter
Y = -2467942
20 meter E =
0015940
Z = -4291926
49 I = 51
71848
XDOT = 5422
772719 Wp = 121
55443
YDOT = 4040
678660 meter/sec RA = 12
04639 deg
ZDOT = 3573
040825 TA = 184
95869
MA = 184
97450
Ha = 229
282 n
mi
Hp = 217
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15306917
82 X = 4713647
71
Y = -8096923
24 feet Y = -2415499
54 meter
Z = -14081123
64 Z = -4269145
37
XDOT = 17791
249077 XDOT = 5359
829217
YDOT = 13256
819752 feet/sec YDOT = 4100
967078 meter/sec
ZDOT = 11722
574886 ZDOT = 3599
231657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11539983
38 X = -3517386
93
Y = -13014509
74 feet Y = -3966822
57 meter
Z = -13985394
59 Z = -4262748
27
XDOT = 7693
736565 XDOT = 2345
050905
YDOT = -19530
248966 feet/sec YDOT = -5952
819885 meter/sec
ZDOT = 11831
508428 ZDOT = 3606
243769
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 13187
50952255
00016717 00000-0 10270-3 0 9011
2 25544 51
6464 12
5635 0008124 133
9911 226
1911 15
50566045 37708
Satellite: ISS
Catalog Number: 25544
Epoch time: 13187
50952255 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 12
5635 deg
Eccentricity:
0008124
Arg of perigee: 133
9911 deg
Mean anomaly: 226
1911 deg
Mean motion: 15
50566045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3770
Checksum: 293
Coasting Arc #3 (Orbit 3785)
---------------------------------------
Vector Time (GMT): 2013/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4920055
81 A = 6793231
13 meter
Y = 2518215
07 meter E =
0016901
Z = 3932249
79 I = 51
69235
XDOT = -5232
895109 Wp = 103
87490
YDOT = -3877
784941 meter/sec RA = 7
09154 deg
ZDOT = -4053
440450 TA = 28
49818
MA = 28
40588
Ha = 229
262 n
mi
Hp = 218
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16141915
39 X = -4966950
96
Y = 8261860
46 feet Y = 2462933
14 meter
Z = 12901081
99 Z = 3908235
31
XDOT = -17168
291040 XDOT = -5169
453659
YDOT = -12722
391540 feet/sec YDOT = -3935
947192 meter/sec
ZDOT = -13298
689139 ZDOT = -4078
707556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12132972
18 X = 3698129
92
Y = 13572176
33 feet Y = 4136799
34 meter
Z = 12800183
71 Z = 3901496
00
XDOT = -6946
445460 XDOT = -2117
276576
YDOT = 18884
437816 feet/sec YDOT = 5755
976646 meter/sec
ZDOT = -13403
783539 ZDOT = -4085
473223
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 13188
54071510
00016717 00000-0 10270-3 0 9023
2 25544 51
6464 7
4504 0008001 138
1737 222
0027 15
50577068 37860
Satellite: ISS
Catalog Number: 25544
Epoch time: 13188
54071510 = yrday
fracday
Element set: 902
Inclination: 51
6464 deg
RA of node: 7
4504 deg
Eccentricity:
0008001
Arg of perigee: 138
1737 deg
Mean anomaly: 222
0027 deg
Mean motion: 15
50577068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3786
Checksum: 287
Coasting Arc #4 (Orbit 3800)
---------------------------------------
Vector Time (GMT): 2013/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5161080
46 A = 6794348
01 meter
Y = -2629766
50 meter E =
0012298
Z = -3566576
87 I = 51
66572
XDOT = 4976
744464 Wp = 123
05477
YDOT = 3718
300265 meter/sec RA = 2
13462 deg
ZDOT = 4464
701546 TA = 195
00020
MA = 195
03671
Ha = 229
144 n
mi
Hp = 218
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16932678
67 X = 5207428
73
Y = -8627842
85 feet Y = -2571792
42 meter
Z = -11701367
67 Z = -3541392
90
XDOT = 16327
901785 XDOT = 4913
107726
YDOT = 12199
147850 feet/sec YDOT = 3773
596968 meter/sec
ZDOT = 14647
970953 ZDOT = 4488
723718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12929841
84 X = -3941015
79
Y = -14015687
25 feet Y = -4271981
47 meter
Z = -11595558
86 Z = -3534326
34
XDOT = 6300
389904 XDOT = 1920
358843
YDOT = -18000
863541 feet/sec YDOT = -5486
663207 meter/sec
ZDOT = 14747
882408 ZDOT = 4495
154558
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 13189
50744890
00016717 00000-0 10270-3 0 9039
2 25544 51
6465 2
6561 0008175 141
1174 219
0566 15
50598223 38010
Satellite: ISS
Catalog Number: 25544
Epoch time: 13189
50744890 = yrday
fracday
Element set: 903
Inclination: 51
6465 deg
RA of node: 2
6561 deg
Eccentricity:
0008175
Arg of perigee: 141
1174 deg
Mean anomaly: 219
0566 deg
Mean motion: 15
50598223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3801
Checksum: 303
Coasting Arc #5 (Orbit 3816)
---------------------------------------
Vector Time (GMT): 2013/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5366020
85 A = 6795555
69 meter
Y = 2737510
99 meter E =
0019210
Z = 3120642
67 I = 51
63895
XDOT = -4690
547291 Wp = 113
70241
YDOT = -3626
449362 meter/sec RA = 357
17732 deg
ZDOT = -4868
116176 TA = 30
37980
MA = 30
26861
Ha = 229
089 n
mi
Hp = 218
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17605055
29 X = -5411392
48
Y = 8981335
28 feet Y = 2677250
71 meter
Z = 10238328
98 Z = 3094465
54
XDOT = -15388
934682 XDOT = -4625
999308
YDOT = -11897
799743 feet/sec YDOT = -3678
540546 meter/sec
ZDOT = -15971
509764 ZDOT = -4890
745732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13698778
44 X = 4175387
67
Y = 14324305
80 feet Y = 4366048
41 meter
Z = 10128349
72 Z = 3087120
99
XDOT = -5935
851723 XDOT = -1809
247605
YDOT = 17074
152147 feet/sec YDOT = 5204
201574 meter/sec
ZDOT = -16065
609649 ZDOT = -4896
797821
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 13190
53861945
00016717 00000-0 10270-3 0 9046
2 25544 51
6463 357
5427 0008055 145
2998 214
8680 15
50607662 38172
Satellite: ISS
Catalog Number: 25544
Epoch time: 13190
53861945 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 357
5427 deg
Eccentricity:
0008055
Arg of perigee: 145
2998 deg
Mean anomaly: 214
8680 deg
Mean motion: 15
50607662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3817
Checksum: 332
Coasting Arc #6 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2013/191/05:44:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4429034
90 A = 6796078
31 meter
Y = -3517076
81 meter E =
0009109
Z = -3779487
61 I = 51
61499
XDOT = 5767
348173 Wp = 131
34555
YDOT = 2717
108712 meter/sec RA = 353
51060 deg
ZDOT = 4230
842091 TA = 183
51445
MA = 183
52086
Ha = 228
882 n
mi
Hp = 220
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14530954
39 X = 4486393
87
Y = -11538965
92 feet Y = -3467227
44 meter
Z = -12399893
74 Z = -3757833
14
XDOT = 18921
745976 XDOT = 5715
984274
YDOT = 8914
398661 feet/sec YDOT = 2781
315208 meter/sec
ZDOT = 13880
715522 ZDOT = 4258
734436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11451204
57 X = 3490327
15
Y = -14677165
01 feet Y = -4473599
90 meter
Z = -12308715
44 Z = -3751696
47
XDOT = 19342
925938 XDOT = 5895
723826
YDOT = 3355
294959 feet/sec YDOT = 1022
693904 meter/sec
ZDOT = 13996
984255 ZDOT = 4266
280801
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 13191
24754309
00016717 00000-0 10270-3 0 9051
2 25544 51
6513 354
0304 0004972 167
4484 192
6791 15
49778675 38283
Satellite: ISS
Catalog Number: 25544
Epoch time: 13191
24754309 = yrday
fracday
Element set: 905
Inclination: 51
6513 deg
RA of node: 354
0304 deg
Eccentricity:
0004972
Arg of perigee: 167
4484 deg
Mean anomaly: 192
6791 deg
Mean motion: 15
49778675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 338
Coasting Arc #7 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2013/192/05:44:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4370862
57 A = 6796674
43 meter
Y = 3773118
97 meter E =
0013630
Z = 3569933
92 I = 51
58665
XDOT = -5747
484756 Wp = 108
25934
YDOT = -2437
507828 meter/sec RA = 348
55562 deg
ZDOT = -4450
915145 TA = 29
58556
MA = 29
50851
Ha = 228
855 n
mi
Hp = 221
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14340100
30 X = -4430071
05
Y = 12378999
24 feet Y = 3723909
86 meter
Z = 11712381
64 Z = 3548557
51
XDOT = -18856
577283 XDOT = -5698
179848
YDOT = -7997
072926 feet/sec YDOT = -2501
503768 meter/sec
ZDOT = -14602
739976 ZDOT = -4478
715929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10794967
95 X = -3290306
23
Y = 15634835
00 feet Y = 4765497
71 meter
Z = 11622331
25 Z = 3542486
56
XDOT = -19041
788050 XDOT = -5803
936998
YDOT = -2181
900353 feet/sec YDOT = -665
043228 meter/sec
ZDOT = -14718
669579 ZDOT = -4486
250488
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 13192
27926499
00016717 00000-0 10270-3 0 9067
2 25544 51
6513 348
9215 0004921 170
6606 189
4637 15
49788707 38440
Satellite: ISS
Catalog Number: 25544
Epoch time: 13192
27926499 = yrday
fracday
Element set: 906
Inclination: 51
6513 deg
RA of node: 348
9215 deg
Eccentricity:
0004921
Arg of perigee: 170
6606 deg
Mean anomaly: 189
4637 deg
Mean motion: 15
49788707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 351
Coasting Arc #8 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2013/193/05:44:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4294825
12 A = 6797204
06 meter
Y = -4054917
55 meter E =
0006762
Z = -3372797
70 I = 51
55927
XDOT = 5687
115962 Wp = 131
32250
YDOT = 2165
382774 meter/sec RA = 343
59805 deg
ZDOT = 4640
204536 TA = 189
39864
MA = 189
41130
Ha = 228
602 n
mi
Hp = 221
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14090633
59 X = 4356232
79
Y = -13303535
26 feet Y = -4006546
51 meter
Z = -11065609
24 Z = -3351785
25
XDOT = 18658
516936 XDOT = 5639
938968
YDOT = 7104
274193 feet/sec YDOT = 2228
715590 meter/sec
ZDOT = 15223
768164 ZDOT = 4667
717206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10030241
17 X = 3057217
51
Y = -16639606
12 feet Y = -5071751
94 meter
Z = -10977043
47 Z = -3345802
85
XDOT = 18580
638130 XDOT = 5663
378502
YDOT = 1085
268296 feet/sec YDOT = 330
789777 meter/sec
ZDOT = 15338
533669 ZDOT = 4675
185062
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 13193
24649314
00016717 00000-0 10270-3 0 9074
2 25544 51
6518 344
1313 0004797 176
1710 183
9478 15
49807179 38593
Satellite: ISS
Catalog Number: 25544
Epoch time: 13193
24649314 = yrday
fracday
Element set: 907
Inclination: 51
6518 deg
RA of node: 344
1313 deg
Eccentricity:
0004797
Arg of perigee: 176
1710 deg
Mean anomaly: 183
9478 deg
Mean motion: 15
49807179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 341
Coasting Arc #9 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2013/194/05:44:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4197065
18 A = 6797781
72 meter
Y = 4317509
30 meter E =
0014271
Z = 3136743
71 I = 51
53217
XDOT = -5619
226037 Wp = 114
04412
YDOT = -1934
754373 meter/sec RA = 338
63944 deg
ZDOT = -4843
900340 TA = 29
79309
MA = 29
71191
Ha = 228
546 n
mi
Hp = 221
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13769898
88 X = -4260269
84
Y = 14165056
75 feet Y = 4270221
48 meter
Z = 10291153
91 Z = 3116201
72
XDOT = -18435
780962 XDOT = -5573
643482
YDOT = -6347
619334 feet/sec YDOT = -1997
336960 meter/sec
ZDOT = -15892
061483 ZDOT = -4871
087112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9183360
35 X = -2799088
23
Y = 17541391
53 feet Y = 5346616
14 meter
Z = 10204522
16 Z = 3110338
35
XDOT = -18108
630254 XDOT = -5519
510501
YDOT = -146
671814 feet/sec YDOT = -44
705569 meter/sec
ZDOT = -16005
496975 ZDOT = -4878
475478
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 13194
27819397
00016717 00000-0 10270-3 0 9089
2 25544 51
6518 339
0225 0004744 179
0039 181
1122 15
49826046 38754
Satellite: ISS
Catalog Number: 25544
Epoch time: 13194
27819397 = yrday
fracday
Element set: 908
Inclination: 51
6518 deg
RA of node: 339
0225 deg
Eccentricity:
0004744
Arg of perigee: 179
0039 deg
Mean anomaly: 181
1122 deg
Mean motion: 15
49826046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 327
Coasting Arc #10 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2013/195/05:48:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5236286
83 A = 6800752
88 meter
Y = -4026300
79 meter E =
0004834
Z = -1618042
26 I = 51
51379
XDOT = 4095
959699 Wp = 69
27974
YDOT = 3038
406738 meter/sec RA = 333
67291 deg
ZDOT = 5710
119804 TA = 273
02465
MA = 273
07997
Ha = 228
322 n
mi
Hp = 221
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17179418
74 X = 5288780
57
Y = -13209648
25 feet Y = -3967451
72 meter
Z = -5308537
60 Z = -1592477
78
XDOT = 13438
187989 XDOT = 4033
941174
YDOT = 9968
526042 feet/sec YDOT = 3083
863277 meter/sec
ZDOT = 18733
988858 ZDOT = 5729
866964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12075955
50 X = 3680751
24
Y = -18025794
06 feet Y = -5494262
03 meter
Z = -5200947
38 Z = -1585248
76
XDOT = 14498
366069 XDOT = 4419
101978
YDOT = 4298
868401 feet/sec YDOT = 1310
295089 meter/sec
ZDOT = 18816
121003 ZDOT = 5735
153682
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 13195
24540244
00016717 00000-0 10270-3 0 9090
2 25544 51
6515 334
2321 0004668 184
7318 175
3789 15
49841832 38904
Satellite: ISS
Catalog Number: 25544
Epoch time: 13195
24540244 = yrday
fracday
Element set: 909
Inclination: 51
6515 deg
RA of node: 334
2321 deg
Eccentricity:
0004668
Arg of perigee: 184
7318 deg
Mean anomaly: 175
3789 deg
Mean motion: 15
49841832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 328
Coasting Arc #11 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2013/196/05:48:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5075068
83 A = 6801154
11 meter
Y = 4315272
92 meter E =
0016208
Z = 1321952
96 I = 51
48769
XDOT = -4035
561021 Wp = 135
90974
YDOT = -2956
899097 meter/sec RA = 328
71189 deg
ZDOT = -5808
971463 TA = 29
68629
MA = 29
59440
Ha = 228
284 n
mi
Hp = 221
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16650488
30 X = -5129367
62
Y = 14157719
55 feet Y = 4258216
61 meter
Z = 4337116
02 Z = 1297167
21
XDOT = -13240
029595 XDOT = -3973
978135
YDOT = -9701
112524 feet/sec YDOT = -3001
682634 meter/sec
ZDOT = -19058
305324 ZDOT = -5828
426342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10941398
00 X = -3334938
11
Y = 18943601
50 feet Y = 5774009
74 meter
Z = 4232745
09 Z = 1290140
70
XDOT = -14239
733170 XDOT = -4340
270670
YDOT = -3924
379290 feet/sec YDOT = -1196
150808 meter/sec
ZDOT = -19139
225869 ZDOT = -5833
636045
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 13196
27708279
00016717 00000-0 10270-3 0 9100
2 25544 51
6513 329
1230 0004732 187
5132 172
5949 15
49830603 39060
Satellite: ISS
Catalog Number: 25544
Epoch time: 13196
27708279 = yrday
fracday
Element set: 910
Inclination: 51
6513 deg
RA of node: 329
1230 deg
Eccentricity:
0004732
Arg of perigee: 187
5132 deg
Mean anomaly: 172
5949 deg
Mean motion: 15
49830603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 314
Coasting Arc #12 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2013/197/05:48:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4883217
02 A = 6801300
73 meter
Y = -4614814
24 meter E =
0005870
Z = -1046816
44 I = 51
46197
XDOT = 3978
193594 Wp = 57
58209
YDOT = 2883
562371 meter/sec RA = 323
74752 deg
ZDOT = 5872
848451 TA = 291
06721
MA = 291
12998
Ha = 228
041 n
mi
Hp = 221
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16021053
20 X = 4939543
08
Y = -15140466
65 feet Y = -4559892
01 meter
Z = -3434437
15 Z = -1022957
77
XDOT = 13051
816252 XDOT = 3917
124668
YDOT = 9460
506467 feet/sec YDOT = 2927
707195 meter/sec
ZDOT = 19267
875496 ZDOT = 5892
025973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9673204
24 X = 2948392
65
Y = -19824667
63 feet Y = -6042558
69 meter
Z = -3333902
79 Z = -1016173
57
XDOT = 13992
231640 XDOT = 4264
832204
YDOT = 3589
139168 feet/sec YDOT = 1093
969618 meter/sec
ZDOT = 19347
645973 ZDOT = 5897
162493
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 13197
24427112
00016717 00000-0 10270-3 0 9113
2 25544 51
6504 324
3320 0004570 193
5750 166
5279 15
49867948 39218
Satellite: ISS
Catalog Number: 25544
Epoch time: 13197
24427112 = yrday
fracday
Element set: 911
Inclination: 51
6504 deg
RA of node: 324
3320 deg
Eccentricity:
0004570
Arg of perigee: 193
5750 deg
Mean anomaly: 166
5279 deg
Mean motion: 15
49867948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 315
Coasting Arc #13 (Orbit 3936)
---------------------------------------
Vector Time (GMT): 2013/198/05:48:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4675013
14 A = 6801530
24 meter
Y = 4872556
40 meter E =
0015445
Z = 733553
36 I = 51
43838
XDOT = -3918
771531 Wp = 143
23298
YDOT = -2858
286686 meter/sec RA = 318
78281 deg
ZDOT = -5936
064185 TA = 28
82824
MA = 28
74298
Ha = 227
940 n
mi
Hp = 221
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15337969
62 X = -4732715
06
Y = 15986077
41 feet Y = 4819954
75 meter
Z = 2406671
14 Z = 710702
86
XDOT = -12856
861978 XDOT = -3857
682543
YDOT = -9377
580992 feet/sec YDOT = -2901
766797 meter/sec
ZDOT = -19475
276196 ZDOT = -5954
953060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8378183
00 X = -2553670
18
Y = 20519954
51 feet Y = 6254482
14 meter
Z = 2310317
22 Z = 704184
69
XDOT = -13800
135370 XDOT = -4206
281261
YDOT = -3412
660692 feet/sec YDOT = -1040
178979 meter/sec
ZDOT = -19553
842894 ZDOT = -5960
011314
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 13198
27593028
00016717 00000-0 10270-3 0 9128
2 25544 51
6502 319
2225 0004601 196
6172 163
4829 15
49870462 39379
Satellite: ISS
Catalog Number: 25544
Epoch time: 13198
27593028 = yrday
fracday
Element set: 912
Inclination: 51
6502 deg
RA of node: 319
2225 deg
Eccentricity:
0004601
Arg of perigee: 196
6172 deg
Mean anomaly: 163
4829 deg
Mean motion: 15
49870462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3937
Checksum: 321
Coasting Arc #14 (Orbit 3951)
---------------------------------------
Vector Time (GMT): 2013/199/05:48:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4436501
11 A = 6801587
70 meter
Y = -5133242
22 meter E =
0007129
Z = -441913
08 I = 51
41526
XDOT = 3872
228293 Wp = 54
64489
YDOT = 2839
280760 meter/sec RA = 313
81466 deg
ZDOT = 5965
816463 TA = 300
58557
MA = 300
65588
Ha = 227
770 n
mi
Hp = 221
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14555449
83 X = 4495719
09
Y = -16841345
87 feet Y = -5083299
31 meter
Z = -1449846
08 Z = -420217
70
XDOT = 12704
161065 XDOT = 3811
210790
YDOT = 9315
225589 feet/sec YDOT = 2882
240673 meter/sec
ZDOT = 19572
888657 ZDOT = 5984
479448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6967288
41 X = 2123629
51
Y = -21147247
04 feet Y = -6445680
90 meter
Z = -1358285
33 Z = -414005
37
XDOT = 13655
845394 XDOT = 4162
301676
YDOT = 3253
238596 feet/sec YDOT = 991
587124 meter/sec
ZDOT = 19650
514855 ZDOT = 5989
476928
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 13199
24309971
00016717 00000-0 10270-3 0 9139
2 25544 51
6491 314
4309 0004532 201
9585 158
1371 15
49894304 39528
Satellite: ISS
Catalog Number: 25544
Epoch time: 13199
24309971 = yrday
fracday
Element set: 913
Inclination: 51
6491 deg
RA of node: 314
4309 deg
Eccentricity:
0004532
Arg of perigee: 201
9585 deg
Mean anomaly: 158
1371 deg
Mean motion: 15
49894304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 321
Coasting Arc #15 (Orbit 3967)
---------------------------------------
Vector Time (GMT): 2013/200/05:48:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4188302
41 A = 6801604
02 meter
Y = 5346966
69 meter E =
0014296
Z = 115057
68 I = 51
39501
XDOT = -3831
282907 Wp = 150
65683
YDOT = -2865
650582 meter/sec RA = 308
84673 deg
ZDOT = -5988
429266 TA = 28
10124
MA = 28
02415
Ha = 227
591 n
mi
Hp = 221
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13741149
65 X = -4248340
99
Y = 17542541
64 feet Y = 5299794
74 meter
Z = 377485
83 Z = 94566
21
XDOT = -12569
825811 XDOT = -3769
863817
YDOT = -9401
740756 feet/sec YDOT = -2908
150270 meter/sec
ZDOT = -19647
077643 ZDOT = -6006
892362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5569521
14 X = -1697590
04
Y = 21577725
80 feet Y = 6576890
82 meter
Z = 290929
22 Z = 88675
23
XDOT = -13598
025050 XDOT = -4144
678035
YDOT = -3226
443040 feet/sec YDOT = -983
419839 meter/sec
ZDOT = -19723
867244 ZDOT = -6011
834736
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 13200
27473805
00016717 00000-0 10270-3 0 9144
2 25544 51
6491 309
3212 0004492 205
5337 154
5592 15
49915277 39689
Satellite: ISS
Catalog Number: 25544
Epoch time: 13200
27473805 = yrday
fracday
Element set: 914
Inclination: 51
6491 deg
RA of node: 309
3212 deg
Eccentricity:
0004492
Arg of perigee: 205
5337 deg
Mean anomaly: 154
5592 deg
Mean motion: 15
49915277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3968
Checksum: 317
Coasting Arc #16 (Orbit 3983)
---------------------------------------
Vector Time (GMT): 2013/201/05:48:54
582
Vector Time (MET): N/A
Weight (LBS) : 921297
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3912397
33 A = 6801563
49 meter
Y = -5556500
24 meter E =
0008288
Z = 189137
89 I = 51
37542
XDOT = 3811
760700 Wp = 57
10540
YDOT = 2893
811335 meter/sec RA = 303
87561 deg
ZDOT = 5979
658226 TA = 304
93540
MA = 305
01323
Ha = 227
515 n
mi
Hp = 221
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12835949
25 X = 3973321
77
Y = -18229987
68 feet Y = -5512408
72 meter
Z = 620531
13 Z = 208291
04
XDOT = 12505
776574 XDOT = 3750
070912
YDOT = 9494
131675 feet/sec YDOT = 2936
091153 meter/sec
ZDOT = 19618
301268 ZDOT = 5998
025764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4082792
88 X = 1244435
27
Y = -21916153
30 feet Y = -6680043
53 meter
Z = 701519
41 Z = 213823
12
XDOT = 13613
943476 XDOT = 4149
529971
YDOT = 3183
941235 feet/sec YDOT = 970
465288 meter/sec
ZDOT = 19694
692879 ZDOT = 6002
942390
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 13201
30636605
00016717 00000-0 10270-3 0 9159
2 25544 51
6481 304
2099 0004522 209
7345 150
3550 15
49921964 39840
Satellite: ISS
Catalog Number: 25544
Epoch time: 13201
30636605 = yrday
fracday
Element set: 915
Inclination: 51
6481 deg
RA of node: 304
2099 deg
Eccentricity:
0004522
Arg of perigee: 209
7345 deg
Mean anomaly: 150
3550 deg
Mean motion: 15
49921964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3984
Checksum: 303
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