[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 1st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17276 08 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
191/05:40:05
450 4
2 4
6 4
6
N/A 0
2 -0
7 228
8
000/00:10:10
900 2
0 -0
1 221
0
Coasting Arc #1 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2013/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3295938
43 A = 6788193
26 meter
Y = 2706754
11 meter E =
0010449
Z = 5271962
69 I = 51
84606
XDOT = -5646
592116 Wp = 98
54799
YDOT = -5112
650286 meter/sec RA = 36
80220 deg
ZDOT = -905
176074 TA =
08258
MA =
08241
Ha = 229
689 n
mi
Hp = 217
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10813446
28 X = -3351570
73
Y = 8880426
88 feet Y = 2669585
27 meter
Z = 17296465
51 Z = 5255816
46
XDOT = -18525
564685 XDOT = -5584
604586
YDOT = -16773
787026 feet/sec YDOT = -5175
447364 meter/sec
ZDOT = -2969
737774 ZDOT = -932
456641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10462444
14 X = 3188952
98
Y = 9416866
32 feet Y = 2870260
86 meter
Z = 17228470
98 Z = 5251237
96
XDOT = -13026
374639 XDOT = -3970
438990
YDOT = 20113
423776 feet/sec YDOT = 6130
571567 meter/sec
ZDOT = -3083
086339 ZDOT = -939
724716
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 13182
54676436
00016717 00000-0 10270-3 0 9003
2 25544 51
6493 37
1693 0008108 115
1831 245
0161 15
50507168 36934
Satellite: ISS
Catalog Number: 25544
Epoch time: 13182
54676436 = yrday
fracday
Element set: 900
Inclination: 51
6493 deg
RA of node: 37
1693 deg
Eccentricity:
0008108
Arg of perigee: 115
1831 deg
Mean anomaly: 245
0161 deg
Mean motion: 15
50507168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 301
Coasting Arc #2 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2013/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3564238
93 A = 6788611
78 meter
Y = -2586120
11 meter E =
0021513
Z = -5185712
60 I = 51
82117
XDOT = 5688
685617 Wp = 107
38721
YDOT = 4893
610693 meter/sec RA = 31
85271 deg
ZDOT = 1468
270644 TA = 176
75916
MA = 176
74520
Ha = 229
497 n
mi
Hp = 217
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11693697
29 X = 3618083
38
Y = -8484646
04 feet Y = -2545960
90 meter
Z = -17013492
78 Z = -5168267
35
XDOT = 18663
666722 XDOT = 5626
408942
YDOT = 16055
153191 feet/sec YDOT = 4956
876794 meter/sec
ZDOT = 4817
160907 ZDOT = 1495
755061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10383587
04 X = -3164917
33
Y = -10168851
49 feet Y = -3099465
94 meter
Z = -16940079
42 Z = -5163336
21
XDOT = 11880
844434 XDOT = 3621
281383
YDOT = -20353
540617 feet/sec YDOT = -6203
759180 meter/sec
ZDOT = 4931
388029 ZDOT = 1503
087071
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 13183
51354765
00016717 00000-0 10270-3 0 9010
2 25544 51
6480 32
3751 0008071 118
6065 241
5898 15
50529070 37089
Satellite: ISS
Catalog Number: 25544
Epoch time: 13183
51354765 = yrday
fracday
Element set: 901
Inclination: 51
6480 deg
RA of node: 32
3751 deg
Eccentricity:
0008071
Arg of perigee: 118
6065 deg
Mean anomaly: 241
5898 deg
Mean motion: 15
50529070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 303
Coasting Arc #3 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2013/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3829040
80 A = 6789213
35 meter
Y = 2483666
90 meter E =
0011827
Z = 5015797
27 I = 51
79706
XDOT = -5714
896456 Wp = 94
29115
YDOT = -4695
276231 meter/sec RA = 26
90354 deg
ZDOT = -2034
511190 TA = 15
45180
MA = 15
41573
Ha = 229
517 n
mi
Hp = 217
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12562469
82 X = -3880894
49
Y = 8148513
46 feet Y = 2440557
59 meter
Z = 16456027
79 Z = 4997070
50
XDOT = -18749
660290 XDOT = -5652
085017
YDOT = -15404
449578 feet/sec YDOT = -4758
832357 meter/sec
ZDOT = -6674
905480 ZDOT = -2062
121660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10389842
95 X = 3166824
13
Y = 10901884
47 feet Y = 3322894
39 meter
Z = 16377266
21 Z = 4991790
74
XDOT = -10809
451698 XDOT = -3294
720878
YDOT = 20517
665419 feet/sec YDOT = 6253
784420 meter/sec
ZDOT = -6789
684213 ZDOT = -2069
495748
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 13184
54477007
00016717 00000-0 10270-3 0 9020
2 25544 51
6483 27
2630 0007970 122
7337 237
4584 15
50543962 37246
Satellite: ISS
Catalog Number: 25544
Epoch time: 13184
54477007 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 27
2630 deg
Eccentricity:
0007970
Arg of perigee: 122
7337 deg
Mean anomaly: 237
4584 deg
Mean motion: 15
50543962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 310
Coasting Arc #4 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2013/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4123940
64 A = 6790017
41 meter
Y = -2439590
58 meter E =
0019128
Z = -4829326
77 I = 51
77063
XDOT = 5652
211101 Wp = 115
31110
YDOT = 4462
708124 meter/sec RA = 21
95102 deg
ZDOT = 2572
258223 TA = 180
04201
MA = 180
04217
Ha = 229
357 n
mi
Hp = 217
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13529988
98 X = 4174373
67
Y = -8003906
09 feet Y = -2393191
42 meter
Z = -15844247
92 Z = -4809170
91
XDOT = 18543
999675 XDOT = 5589
392743
YDOT = 14641
430853 feet/sec YDOT = 4525
563128 meter/sec
ZDOT = 8439
167399 ZDOT = 2599
564124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10632081
55 X = -3240658
46
Y = -11694440
84 feet Y = -3564465
57 meter
Z = -15759511
47 Z = -4803499
10
XDOT = 9681
802567 XDOT = 2951
013422
YDOT = -20327
894368 feet/sec YDOT = -6195
942203 meter/sec
ZDOT = 8552
703596 ZDOT = 2606
864056
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 13185
51152964
00016717 00000-0 10270-3 0 9031
2 25544 51
6469 22
4684 0008040 126
1314 234
0582 15
50561949 37390
Satellite: ISS
Catalog Number: 25544
Epoch time: 13185
51152964 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 22
4684 deg
Eccentricity:
0008040
Arg of perigee: 126
1314 deg
Mean anomaly: 234
0582 deg
Mean motion: 15
50561949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 305
Coasting Arc #5 (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 = -4405055
59 A = 6790976
52 meter
Y = 2411563
65 meter E =
0014275
Z = 4558243
44 I = 51
74537
XDOT = -5563
633312 Wp = 96
49372
YDOT = -4266
979982 meter/sec RA = 16
99875 deg
ZDOT = -3112
401679 TA = 24
64938
MA = 24
58122
Ha = 229
352 n
mi
Hp = 217
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14452282
13 X = -4453837
42
Y = 7911954
23 feet Y = 2362030
13 meter
Z = 14954866
92 Z = 4536726
03
XDOT = -18253
390130 XDOT = -5500
386388
YDOT = -13999
278156 feet/sec YDOT = -4328
841964 meter/sec
ZDOT = -10211
291598 ZDOT = -3139
276165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10945537
27 X = 3336199
76
Y = 12424140
96 feet Y = 3786878
16 meter
Z = 14864436
02 Z = 4530680
10
XDOT = -8705
023889 XDOT = -2653
291281
YDOT = 20046
495023 feet/sec YDOT = 6110
171683 meter/sec
ZDOT = -10323
050760 ZDOT = -3146
465872
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
54272616
00016717 00000-0 10270-3 0 9043
2 25544 51
6471 17
3557 0007913 130
3009 229
8835 15
50578252 37557
Satellite: ISS
Catalog Number: 25544
Epoch time: 13186
54272616 = yrday
fracday
Element set: 904
Inclination: 51
6471 deg
RA of node: 17
3557 deg
Eccentricity:
0007913
Arg of perigee: 130
3009 deg
Mean anomaly: 229
8835 deg
Mean motion: 15
50578252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 314
Coasting Arc #6 (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 = 4693626
08 A = 6792035
68 meter
Y = -2446944
64 meter E =
0015794
Z = -4273082
31 I = 51
71846
XDOT = 5392
035855 Wp = 121
28260
YDOT = 4056
781482 meter/sec RA = 12
04365 deg
ZDOT = 3601
490619 TA = 185
56745
MA = 185
58503
Ha = 229
217 n
mi
Hp = 217
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15399035
69 X = 4741396
81
Y = -8028033
60 feet Y = -2394189
84 meter
Z = -14019298
93 Z = -4250165
60
XDOT = 17690
406349 XDOT = 5328
776373
YDOT = 13309
650531 feet/sec YDOT = 4116
724410 meter/sec
ZDOT = 11815
914103 ZDOT = 3627
531369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11494989
41 X = -3503672
77
Y = -13120041
59 feet Y = -3998988
68 meter
Z = -13923005
90 Z = -4243732
20
XDOT = 7761
570598 XDOT = 2365
726718
YDOT = -19447
664008 feet/sec YDOT = -5927
647990 meter/sec
ZDOT = 11924
217007 ZDOT = 3634
501344
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
50946173
00016717 00000-0 10270-3 0 9057
2 25544 51
6461 12
5610 0008062 133
4983 226
6839 15
50597464 37706
Satellite: ISS
Catalog Number: 25544
Epoch time: 13187
50946173 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 12
5610 deg
Eccentricity:
0008062
Arg of perigee: 133
4983 deg
Mean anomaly: 226
6839 deg
Mean motion: 15
50597464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3770
Checksum: 317
Coasting Arc #7 (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 = -4956869
44 A = 6793224
85 meter
Y = 2490837
07 meter E =
0017004
Z = 3903320
89 I = 51
69243
XDOT = -5188
408903 Wp = 103
78993
YDOT = -3900
227503 meter/sec RA = 7
08858 deg
ZDOT = -4088
965043 TA = 29
04312
MA = 28
94863
Ha = 229
189 n
mi
Hp = 217
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16262695
02 X = -5003315
18
Y = 8172037
64 feet Y = 2435145
99 meter
Z = 12806170
90 Z = 3879128
66
XDOT = -17022
338921 XDOT = -5124
547235
YDOT = -12796
021993 feet/sec YDOT = -3957
889926 meter/sec
ZDOT = -13415
239644 ZDOT = -4114
015024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12076829
19 X = 3681017
54
Y = 13711327
12 feet Y = 4179212
51 meter
Z = 12704533
32 Z = 3872341
76
XDOT = -7044
966134 XDOT = -2147
305677
YDOT = 18765
541584 feet/sec YDOT = 5719
737075 meter/sec
ZDOT = -13519
421828 ZDOT = -4120
719773
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
54063224
00016717 00000-0 10270-3 0 9060
2 25544 51
6462 7
4478 0007933 137
6857 222
4907 15
50612114 37861
Satellite: ISS
Catalog Number: 25544
Epoch time: 13188
54063224 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 7
4478 deg
Eccentricity:
0007933
Arg of perigee: 137
6857 deg
Mean anomaly: 222
4907 deg
Mean motion: 15
50612114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3786
Checksum: 315
Coasting Arc #8 (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 = 5205770
40 A = 6794359
13 meter
Y = -2596057
38 meter E =
0012087
Z = -3525746
76 I = 51
66588
XDOT = 4917
361630 Wp = 122
28782
YDOT = 3748
202046 meter/sec RA = 2
13147 deg
ZDOT = 4505
666394 TA = 196
35270
MA = 196
39174
Ha = 229
067 n
mi
Hp = 218
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17079299
20 X = 5251540
06
Y = -8517248
63 feet Y = -2537586
80 meter
Z = -11567410
64 Z = -3500347
11
XDOT = 16133
076213 XDOT = 4853
195943
YDOT = 12297
250807 feet/sec YDOT = 3802
831730 meter/sec
ZDOT = 14782
370059 ZDOT = 4529
398812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12863074
65 X = -3920665
15
Y = -14186068
19 feet Y = -4323913
58 meter
Z = -11460704
79 Z = -3493222
82
XDOT = 6435
610472 XDOT = 1961
574072
YDOT = -17844
152894 feet/sec YDOT = -5438
897802 meter/sec
ZDOT = 14881
064186 ZDOT = 4535
748364
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
50734348
00016717 00000-0 10270-3 0 9070
2 25544 51
6462 2
6533 0008104 140
6352 219
5389 15
50635834 38018
Satellite: ISS
Catalog Number: 25544
Epoch time: 13189
50734348 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 2
6533 deg
Eccentricity:
0008104
Arg of perigee: 140
6352 deg
Mean anomaly: 219
5389 deg
Mean motion: 15
50635834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3801
Checksum: 302
Coasting Arc #9 (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 = -5418375
35 A = 6795577
77 meter
Y = 2696584
94 meter E =
0019320
Z = 3065361
13 I = 51
63920
XDOT = -4613
029066 Wp = 113
91263
YDOT = -3665
393312 meter/sec RA = 357
17399 deg
ZDOT = -4912
805521 TA = 30
90166
MA = 30
78810
Ha = 229
001 n
mi
Hp = 218
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17776822
01 X = -5463016
91
Y = 8847063
46 feet Y = 2635743
28 meter
Z = 10056959
10 Z = 3038931
43
XDOT = -15134
609798 XDOT = -4547
834280
YDOT = -12025
568608 feet/sec YDOT = -3716
614017 meter/sec
ZDOT = -16118
128350 ZDOT = -4935
056939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13619450
07 X = 4151208
38
Y = 14526438
69 feet Y = 4427658
51 meter
Z = 9945929
70 Z = 3031519
37
XDOT = -6117
111316 XDOT = -1864
495529
YDOT = 16872
443266 feet/sec YDOT = 5142
720707 meter/sec
ZDOT = -16210
639641 ZDOT = -4941
002963
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
53848784
00016717 00000-0 10270-3 0 9086
2 25544 51
6461 357
5398 0007974 144
8244 215
3435 15
50649492 38176
Satellite: ISS
Catalog Number: 25544
Epoch time: 13190
53848784 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 357
5398 deg
Eccentricity:
0007974
Arg of perigee: 144
8244 deg
Mean anomaly: 215
3435 deg
Mean motion: 15
50649492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3817
Checksum: 346
Coasting Arc #10 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2013/191/05:45:10
900
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4595370
50 A = 6796418
38 meter
Y = -3435684
55 meter E =
0008361
Z = -3653304
29 I = 51
61612
XDOT = 5600
129672 Wp = 129
68219
YDOT = 2845
930845 meter/sec RA = 353
50592 deg
ZDOT = 4369
280094 TA = 187
06831
MA = 187
08011
Ha = 228
790 n
mi
Hp = 220
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15076674
88 X = 4651194
02
Y = -11271930
95 feet Y = -3383983
71 meter
Z = -11985906
46 Z = -3630845
51
XDOT = 18373
128846 XDOT = 5546
665201
YDOT = 9337
043455 feet/sec YDOT = 2908
255639 meter/sec
ZDOT = 14334
908446 ZDOT = 4396
355031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12024898
24 X = 3665188
98
Y = -14560958
34 feet Y = -4438180
10 meter
Z = -11891375
91 Z = -3624491
38
XDOT = 18921
671321 XDOT = 5767
325419
YDOT = 3831
162852 feet/sec YDOT = 1167
738437 meter/sec
ZDOT = 14447
736030 ZDOT = 4403
669942
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
24739223
00016717 00000-0 10270-3 0 9093
2 25544 51
6511 354
0272 0004745 167
3040 192
8231 15
49796952 38289
Satellite: ISS
Catalog Number: 25544
Epoch time: 13191
24739223 = yrday
fracday
Element set: 909
Inclination: 51
6511 deg
RA of node: 354
0272 deg
Eccentricity:
0004745
Arg of perigee: 167
3040 deg
Mean anomaly: 192
8231 deg
Mean motion: 15
49796952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 316
Coasting Arc #11 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2013/192/05:45:10
900
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4542900
33 A = 6797032
14 meter
Y = 3697080
35 meter E =
0014003
Z = 3432513
20 I = 51
58780
XDOT = -5574
976994 Wp = 109
04663
YDOT = -2581
796440 meter/sec RA = 348
55097 deg
ZDOT = -4586
789818 TA = 30
76728
MA = 30
68527
Ha = 228
769 n
mi
Hp = 221
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14904528
66 X = -4600578
21
Y = 12129528
70 feet Y = 3645955
97 meter
Z = 11261526
24 Z = 3410304
77
XDOT = -18290
606936 XDOT = -5523
411409
YDOT = -8470
460762 feet/sec YDOT = -2643
850638 meter/sec
ZDOT = -15048
523026 ZDOT = -4613
747110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11383054
28 X = -3469554
95
Y = 15549730
31 feet Y = 4739557
80 meter
Z = 11168006
82 Z = 3404008
48
XDOT = -18622
419352 XDOT = -5676
113419
YDOT = -2717
869240 feet/sec YDOT = -828
406544 meter/sec
ZDOT = -15160
900060 ZDOT = -4621
042338
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
27910164
00016717 00000-0 10270-3 0 9104
2 25544 51
6510 348
9182 0004699 170
4702 189
6539 15
49805622 38446
Satellite: ISS
Catalog Number: 25544
Epoch time: 13192
27910164 = yrday
fracday
Element set: 910
Inclination: 51
6510 deg
RA of node: 348
9182 deg
Eccentricity:
0004699
Arg of perigee: 170
4702 deg
Mean anomaly: 189
6539 deg
Mean motion: 15
49805622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 324
Coasting Arc #12 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2013/193/05:45:10
900
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4471333
35 A = 6797545
86 meter
Y = -3984124
02 meter E =
0006042
Z = -3224029
72 I = 51
56045
XDOT = 5511
978757 Wp = 127
21690
YDOT = 2325
992916 meter/sec RA = 343
59340 deg
ZDOT = 4772
685861 TA = 195
54118
MA = 195
55974
Ha = 228
503 n
mi
Hp = 221
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14669728
85 X = 4531213
61
Y = -13071273
02 feet Y = -3933787
70 meter
Z = -10577525
33 Z = -3202163
53
XDOT = 18083
919806 XDOT = 5462
375253
YDOT = 7631
210355 feet/sec YDOT = 2387
353661 meter/sec
ZDOT = 15658
418179 ZDOT = 4799
341859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10627944
13 X = 3239397
37
Y = -16584522
28 feet Y = -5054962
39 meter
Z = -10485398
87 Z = -3195949
58
XDOT = 18174
459387 XDOT = 5539
575221
YDOT = 1682
147841 feet/sec YDOT = 512
718662 meter/sec
ZDOT = 15769
573630 ZDOT = 4806
566043
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
24631607
00016717 00000-0 10270-3 0 9115
2 25544 51
6516 344
1280 0004558 176
1198 183
9988 15
49831028 38595
Satellite: ISS
Catalog Number: 25544
Epoch time: 13193
24631607 = yrday
fracday
Element set: 911
Inclination: 51
6516 deg
RA of node: 344
1280 deg
Eccentricity:
0004558
Arg of perigee: 176
1198 deg
Mean anomaly: 183
9988 deg
Mean motion: 15
49831028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 334
Coasting Arc #13 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2013/194/05:45:10
900
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4379402
81 A = 6798136
19 meter
Y = 4250962
95 meter E =
0014603
Z = 2974705
17 I = 51
53336
XDOT = -5439
021789 Wp = 115
18219
YDOT = -2114
504995 meter/sec RA = 338
63481 deg
ZDOT = -4972
633444 TA = 30
79178
MA = 30
70619
Ha = 228
455 n
mi
Hp = 221
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14368119
46 X = -4441062
65
Y = 13946728
85 feet Y = 4201644
77 meter
Z = 9759531
39 Z = 2953281
15
XDOT = -17844
559676 XDOT = -5390
817273
YDOT = -6937
352347 feet/sec YDOT = -2175
057757 meter/sec
ZDOT = -16314
414187 ZDOT = -4998
938452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9795090
79 X = -2985543
67
Y = 17514706
26 feet Y = 5338482
47 meter
Z = 9669220
05 Z = 2947178
27
XDOT = -17712
930877 XDOT = -5398
901331
YDOT = -814
907475 feet/sec YDOT = -248
383798 meter/sec
ZDOT = -16424
131897 ZDOT = -5006
075402
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
27800050
00016717 00000-0 10270-3 0 9120
2 25544 51
6515 339
0190 0004518 178
8577 181
2584 15
49847828 38759
Satellite: ISS
Catalog Number: 25544
Epoch time: 13194
27800050 = yrday
fracday
Element set: 912
Inclination: 51
6515 deg
RA of node: 339
0190 deg
Eccentricity:
0004518
Arg of perigee: 178
8577 deg
Mean anomaly: 181
2584 deg
Mean motion: 15
49847828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 333
Coasting Arc #14 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2013/195/05:49:10
900
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5373279
63 A = 6800910
84 meter
Y = -3918565
21 meter E =
0005462
Z = -1419650
44 I = 51
51443
XDOT = 3863
799872 Wp = 63
50087
YDOT = 3212
358223 meter/sec RA = 333
66907 deg
ZDOT = 5777
021824 TA = 281
03094
MA = 281
09237
Ha = 228
216 n
mi
Hp = 221
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17628870
18 X = 5423594
74
Y = -12856185
07 feet Y = -3858196
40 meter
Z = -4657645
81 Z = -1393425
75
XDOT = 12676
508766 XDOT = 3799
528449
YDOT = 10539
233014 feet/sec YDOT = 3255
206003 meter/sec
ZDOT = 18953
483673 ZDOT = 5795
635719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12589879
46 X = 3837395
26
Y = -17848504
81 feet Y = -5440224
26 meter
Z = -4547310
64 Z = -1386020
28
XDOT = 13978
273099 XDOT = 4260
577641
YDOT = 5028
209221 feet/sec YDOT = 1532
598170 meter/sec
ZDOT = 19030
847095 ZDOT = 5800
602195
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
24519150
00016717 00000-0 10270-3 0 9137
2 25544 51
6513 334
2284 0004428 184
7834 175
3275 15
49873146 38900
Satellite: ISS
Catalog Number: 25544
Epoch time: 13195
24519150 = yrday
fracday
Element set: 913
Inclination: 51
6513 deg
RA of node: 334
2284 deg
Eccentricity:
0004428
Arg of perigee: 184
7834 deg
Mean anomaly: 175
3275 deg
Mean motion: 15
49873146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 321
Coasting Arc #15 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2013/196/05:49:10
900
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5216920
63 A = 6801284
40 meter
Y = 4204826
88 meter E =
0016055
Z = 1110228
46 I = 51
48819
XDOT = -3797
958756 Wp = 137
50036
YDOT = -3153
432976 meter/sec RA = 328
70800 deg
ZDOT = -5865
201731 TA = 30
44142
MA = 30
34830
Ha = 228
177 n
mi
Hp = 221
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17115881
33 X = -5268945
34
Y = 13795363
78 feet Y = 4146197
02 meter
Z = 3642481
82 Z = 1084759
13
XDOT = -12460
494607 XDOT = -3733
922695
YDOT = -10345
908713 feet/sec YDOT = -3195
545774 meter/sec
ZDOT = -19242
787831 ZDOT = -5883
496418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11475201
32 X = -3497641
36
Y = 18771115
03 feet Y = 5721435
86 meter
Z = 3535268
65 Z = 1077549
89
XDOT = -13740
745780 XDOT = -4188
179314
YDOT = -4737
349067 feet/sec YDOT = -1443
943995 meter/sec
ZDOT = -19318
823754 ZDOT = -5888
377480
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
27685143
00016717 00000-0 10270-3 0 9148
2 25544 51
6510 329
1192 0004501 187
6758 172
4324 15
49858676 39069
Satellite: ISS
Catalog Number: 25544
Epoch time: 13196
27685143 = yrday
fracday
Element set: 914
Inclination: 51
6510 deg
RA of node: 329
1192 deg
Eccentricity:
0004501
Arg of perigee: 187
6758 deg
Mean anomaly: 172
4324 deg
Mean motion: 15
49858676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 331
Coasting Arc #16 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2013/197/05:49:10
900
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5029809
97 A = 6801362
40 meter
Y = -4500835
48 meter E =
0006675
Z = -822016
37 I = 51
46235
XDOT = 3738
587898 Wp = 55
92030
YDOT = 3104
051253 meter/sec RA = 323
74355 deg
ZDOT = 5918
375970 TA = 295
18855
MA = 295
25775
Ha = 227
928 n
mi
Hp = 221
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16502001
22 X = 5083758
59
Y = -14766520
60 feet Y = -4444287
26 meter
Z = -2696904
12 Z = -797451
33
XDOT = 12265
708327 XDOT = 3674
850066
YDOT = 10183
895187 feet/sec YDOT = 3145
501729 meter/sec
ZDOT = 19417
243995 ZDOT = 5936
383043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10227469
65 X = 3117332
75
Y = -19654832
42 feet Y = -5990792
92 meter
Z = -2593432
80 Z = -790478
32
XDOT = 13529
445573 XDOT = 4123
775011
YDOT = 4485
359789 feet/sec YDOT = 1367
137664 meter/sec
ZDOT = 19492
083432 ZDOT = 5941
187030
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
24401868
00016717 00000-0 10270-3 0 9157
2 25544 51
6502 324
3280 0004324 193
7344 166
3690 15
49905793 39215
Satellite: ISS
Catalog Number: 25544
Epoch time: 13197
24401868 = yrday
fracday
Element set: 915
Inclination: 51
6502 deg
RA of node: 324
3280 deg
Eccentricity:
0004324
Arg of perigee: 193
7344 deg
Mean anomaly: 166
3690 deg
Mean motion: 15
49905793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 316
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