[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 8th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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 974)
---------------------------------------
Vector Time (GMT): 2013/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4748816
54 A = 6788802
68 meter
Y = 2748651
92 meter E =
0022455
Z = -4023377
44 I = 51
60078
XDOT = -5444
140571 Wp = 125
01564
YDOT = -3652
925338 meter/sec RA = 185
46983 deg
ZDOT = 3933
223158 TA = 185
99982
MA = 186
02676
Ha = 229
913 n
mi
Hp = 213
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15580106
77 X = -4759655
05
Y = 9017886
88 feet Y = 2695487
40 meter
Z = -13200057
23 Z = -4046472
97
XDOT = -17861
353578 XDOT = -5421
994772
YDOT = -11984
663182 feet/sec YDOT = -3713
681615 meter/sec
ZDOT = 12904
275452 ZDOT = 3906
829410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13027330
01 X = -3970730
19
Y = -12320758
68 feet Y = -3755367
25 meter
Z = -13296281
43 Z = -4052706
58
XDOT = 5530
128006 XDOT = 1685
583016
YDOT = -19644
705623 feet/sec YDOT = -5987
706274 meter/sec
ZDOT = 12795
050354 ZDOT = 3899
931348
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 13007
50887776
00016717 00000-0 10270-3 0 9006
2 25544 51
6424 186
5359 0015760 131
9238 228
3260 15
51934022 9753
Satellite: ISS
Catalog Number: 25544
Epoch time: 13007
50887776 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 186
5359 deg
Eccentricity:
0015760
Arg of perigee: 131
9238 deg
Mean anomaly: 228
3260 deg
Mean motion: 15
51934022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 313
Coasting Arc #2 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2013/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5351883
38 A = 6791030
49 meter
Y = -2549428
28 meter E =
0026191
Z = 3279859
44 I = 51
63836
XDOT = 4715
248930 Wp = 116
63732
YDOT = 3787
161719 meter/sec RA = 180
49975 deg
ZDOT = -4732
643944 TA = 25
23543
MA = 25
10770
Ha = 229
704 n
mi
Hp = 213
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17558672
51 X = 5364061
18
Y = -8364266
00 feet Y = -2489512
40 meter
Z = 10760693
71 Z = 3305887
76
XDOT = 15469
976804 XDOT = 4695
539558
YDOT = 12425
071257 feet/sec YDOT = 3839
780855 meter/sec
ZDOT = -15527
047060 ZDOT = -4709
785164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13209641
90 X = 4026298
85
Y = 14192554
57 feet Y = 4325890
63 meter
Z = 10869094
30 Z = 3312899
94
XDOT = -6168
478015 XDOT = -1880
152099
YDOT = 17603
921377 feet/sec YDOT = 5365
675236 meter/sec
ZDOT = -15432
506759 ZDOT = -4703
828060
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 13008
53915845
00016717 00000-0 10270-3 0 9010
2 25544 51
6420 181
4163 0015636 135
8640 224
3762 15
51945070 9914
Satellite: ISS
Catalog Number: 25544
Epoch time: 13008
53915845 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 181
4163 deg
Eccentricity:
0015636
Arg of perigee: 135
8640 deg
Mean anomaly: 224
3762 deg
Mean motion: 15
51945070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 298
Coasting Arc #3 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2013/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5858696
98 A = 6792938
63 meter
Y = 2417104
04 meter E =
0016705
Z = -2471612
32 I = 51
67606
XDOT = -3853
412197 Wp = 120
98599
YDOT = -3917
814882 meter/sec RA = 175
53473 deg
ZDOT = 5321
057943 TA = 211
42481
MA = 211
52472
Ha = 229
743 n
mi
Hp = 213
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19221446
77 X = -5873283
74
Y = 7930131
35 feet Y = 2351507
14 meter
Z = -8108964
31 Z = -2500108
38
XDOT = -12642
428467 XDOT = -3835
164111
YDOT = -12853
723366 feet/sec YDOT = -3960
804714 meter/sec
ZDOT = 17457
539184 ZDOT = 5302
382379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13569372
37 X = -4135944
70
Y = -15693459
86 feet Y = -4783366
56 meter
Z = -8227621
33 Z = -2507778
98
XDOT = 7032
938205 XDOT = 2143
639565
YDOT = -15161
935392 feet/sec YDOT = -4621
357907 meter/sec
ZDOT = 17380
379141 ZDOT = 5297
539562
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 13009
50503567
00016717 00000-0 10270-3 0 9023
2 25544 51
6424 176
6165 0015804 139
0939 221
1402 15
51973294 10063
Satellite: ISS
Catalog Number: 25544
Epoch time: 13009
50503567 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 176
6165 deg
Eccentricity:
0015804
Arg of perigee: 139
0939 deg
Mean anomaly: 221
1402 deg
Mean motion: 15
51973294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 290
Coasting Arc #4 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2013/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6216892
14 A = 6794519
45 meter
Y = -2239329
91 meter E =
0028783
Z = 1508700
05 I = 51
71145
XDOT = 2905
871309 Wp = 131
38770
YDOT = 4140
111215 meter/sec RA = 170
57469 deg
ZDOT = -5776
447703 TA = 32
13773
MA = 31
96260
Ha = 229
524 n
mi
Hp = 213
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20396627
75 X = 6234141
97
Y = -7346882
89 feet Y = -2169712
45 meter
Z = 4949803
31 Z = 1538942
48
XDOT = 9533
698519 XDOT = 2887
419857
YDOT = 13583
042045 feet/sec YDOT = 4172
503965 meter/sec
ZDOT = -18951
600076 ZDOT = -5762
375746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13683343
67 X = 4170683
15
Y = 16778047
02 feet Y = 5113948
73 meter
Z = 5075717
56 Z = 1547078
71
XDOT = -8390
419430 XDOT = -2557
399842
YDOT = 12609
516664 feet/sec YDOT = 3843
380679 meter/sec
ZDOT = -18893
581444 ZDOT = -5758
763624
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 13010
53529036
00016717 00000-0 10270-3 0 9038
2 25544 51
6420 171
4963 0015605 142
9323 217
2910 15
52000961 10228
Satellite: ISS
Catalog Number: 25544
Epoch time: 13010
53529036 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 171
4963 deg
Eccentricity:
0015605
Arg of perigee: 142
9323 deg
Mean anomaly: 217
2910 deg
Mean motion: 15
52000961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 260
Coasting Arc #5 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2013/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6443755
64 A = 6795307
85 meter
Y = 2100601
42 meter E =
0016629
Z = -550891
35 I = 51
74577
XDOT = -1924
533721 Wp = 107
87985
YDOT = -4373
324829 meter/sec RA = 165
61900 deg
ZDOT = 5979
131058 TA = 246
19849
MA = 246
37293
Ha = 229
534 n
mi
Hp = 213
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21140930
58 X = -6464090
06
Y = 6891736
96 feet Y = 2028429
67 meter
Z = -1807386
32 Z = -582243
21
XDOT = -6314
087010 XDOT = -1904
531765
YDOT = -14348
178573 feet/sec YDOT = -4394
734923 meter/sec
ZDOT = 19616
571711 ZDOT = 5969
830150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13808932
88 X = -4208962
74
Y = -17414347
07 feet Y = -5307892
99 meter
Z = -1937916
00 Z = -590676
80
XDOT = 9943
997403 XDOT = 3030
930408
YDOT = -10014
981335 feet/sec YDOT = -3052
566311 meter/sec
ZDOT = 19578
396982 ZDOT = 5967
495400
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 13011
50114380
00016717 00000-0 10270-3 0 9049
2 25544 51
6435 166
6970 0015805 146
2539 213
9621 15
52018645 10372
Satellite: ISS
Catalog Number: 25544
Epoch time: 13011
50114380 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 166
6970 deg
Eccentricity:
0015805
Arg of perigee: 146
2539 deg
Mean anomaly: 213
9621 deg
Mean motion: 15
52018645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 285
Coasting Arc #6 (Orbit 1052)
---------------------------------------
Vector Time (GMT): 2013/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6501662
91 A = 6795300
26 meter
Y = -1860976
49 meter E =
0026564
Z = -503446
29 I = 51
77517
XDOT = 893
324243 Wp = 145
34385
YDOT = 4697
228582 meter/sec RA = 160
66584 deg
ZDOT = -6002
964659 TA = 40
07872
MA = 39
88303
Ha = 229
368 n
mi
Hp = 213
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21330915
07 X = 6524435
09
Y = -6105565
91 feet Y = -1788143
46 meter
Z = -1651726
68 Z = -471807
26
XDOT = 2930
853815 XDOT = 869
892639
YDOT = 15410
854928 feet/sec YDOT = 4707
087737 meter/sec
ZDOT = -19694
765942 ZDOT = -5998
681613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13451235
99 X = 4099936
73
Y = 17656950
19 feet Y = 5381838
42 meter
Z = -1520011
32 Z = -463299
45
XDOT = -11955
561151 XDOT = -3644
055039
YDOT = 7468
065502 feet/sec YDOT = 2276
266365 meter/sec
ZDOT = -19677
476760 ZDOT = -5997
694917
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 13012
53137287
00016717 00000-0 10270-3 0 9055
2 25544 51
6434 161
5767 0015587 149
8395 210
3657 15
52048210 10534
Satellite: ISS
Catalog Number: 25544
Epoch time: 13012
53137287 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 161
5767 deg
Eccentricity:
0015587
Arg of perigee: 149
8395 deg
Mean anomaly: 210
3657 deg
Mean motion: 15
52048210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1053
Checksum: 303
Coasting Arc #7 (Orbit 1068)
---------------------------------------
Vector Time (GMT): 2013/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6430790
27 A = 6794430
31 meter
Y = 1628461
91 meter E =
0020489
Z = 1474885
07 I = 51
80273
XDOT = 70
592454 Wp = 111
59360
YDOT = -5022
015286 meter/sec RA = 155
71465 deg
ZDOT = 5780
775201 TA = 264
43757
MA = 264
67128
Ha = 229
278 n
mi
Hp = 213
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21098393
29 X = -6455686
57
Y = 5342722
79 feet Y = 1556409
50 meter
Z = 4838861
77 Z = 1443585
13
XDOT = 231
602538 XDOT = 98
663589
YDOT = -16476
428103 feet/sec YDOT = -5021
069211 meter/sec
ZDOT = 18965
797902 ZDOT = 5781
186056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12966635
37 X = -3952230
46
Y = -17515628
60 feet Y = -5338763
60 meter
Z = 4708565
75 Z = 1435170
84
XDOT = 14007
076699 XDOT = 4269
356978
YDOT = -5205
052939 feet/sec YDOT = -1586
500136 meter/sec
ZDOT = 18968
053473 ZDOT = 5781
462699
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 13013
56158876
00016717 00000-0 10270-3 0 9067
2 25544 51
6451 156
4578 0015754 153
8513 206
3438 15
52076257 10690
Satellite: ISS
Catalog Number: 25544
Epoch time: 13013
56158876 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 156
4578 deg
Eccentricity:
0015754
Arg of perigee: 153
8513 deg
Mean anomaly: 206
3438 deg
Mean motion: 15
52076257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1069
Checksum: 321
Coasting Arc #8 (Orbit 1083)
---------------------------------------
Vector Time (GMT): 2013/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6196356
60 A = 6792813
79 meter
Y = -1244059
19 meter E =
0020708
Z = -2468613
44 I = 51
82479
XDOT = -1032
874269 Wp = 151
09039
YDOT = 5397
679825 meter/sec RA = 150
76292 deg
ZDOT = -5349
083110 TA = 56
47872
MA = 56
28106
Ha = 229
209 n
mi
Hp = 214
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20329253
94 X = 6221799
03
Y = -4081559
03 feet Y = -1174625
33 meter
Z = -8099125
46 Z = -2438450
91
XDOT = -3388
695108 XDOT = -1067
171605
YDOT = 17708
923312 feet/sec YDOT = 5385
937952 meter/sec
ZDOT = -17549
485270 ZDOT = -5354
183787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11811605
93 X = 3600177
49
Y = 17100918
07 feet Y = 5212359
83 meter
Z = -7973587
01 Z = -2430349
32
XDOT = -16313
767931 XDOT = -4972
436465
YDOT = 3131
498301 feet/sec YDOT = 954
480682 meter/sec
ZDOT = -17571
279478 ZDOT = -5355
725985
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 13014
52740510
00016717 00000-0 10270-3 0 9077
2 25544 51
6452 151
6579 0015584 157
1358 203
0491 15
52070259 10840
Satellite: ISS
Catalog Number: 25544
Epoch time: 13014
52740510 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 151
6579 deg
Eccentricity:
0015584
Arg of perigee: 157
1358 deg
Mean anomaly: 203
0491 deg
Mean motion: 15
52070259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1084
Checksum: 291
Coasting Arc #9 (Orbit 1099)
---------------------------------------
Vector Time (GMT): 2013/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5869866
38 A = 6790645
14 meter
Y = 845418
69 meter E =
0022735
Z = 3308310
42 I = 51
84529
XDOT = 1853
558131 Wp = 128
99251
YDOT = -5742
590700 meter/sec RA = 145
81046 deg
ZDOT = 4720
462769 TA = 269
29031
MA = 269
55081
Ha = 228
991 n
mi
Hp = 214
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19258091
80 X = -5894954
38
Y = 2773683
38 feet Y = 779637
86 meter
Z = 10854036
80 Z = 3279734
67
XDOT = 6081
227463 XDOT = 1894
704879
YDOT = -18840
520668 feet/sec YDOT = -5721
633032 meter/sec
ZDOT = 15487
082575 ZDOT = 4729
566926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10478445
60 X = -3193830
22
Y = -16472301
89 feet Y = -5020757
62 meter
Z = 10735128
43 Z = 3272067
14
XDOT = 18432
715440 XDOT = 5618
291666
YDOT = -1530
094311 feet/sec YDOT = -466
372746 meter/sec
ZDOT = 15525
563585 ZDOT = 4732
191781
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 13015
55759365
00016717 00000-0 10270-3 0 9080
2 25544 51
6463 146
5389 0015590 161
1842 198
9889 15
52123952 11005
Satellite: ISS
Catalog Number: 25544
Epoch time: 13015
55759365 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 146
5389 deg
Eccentricity:
0015590
Arg of perigee: 161
1842 deg
Mean anomaly: 198
9889 deg
Mean motion: 15
52123952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1100
Checksum: 329
Coasting Arc #10 (Orbit 1114)
---------------------------------------
Vector Time (GMT): 2013/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5412464
90 A = 6788276
85 meter
Y = -266363
75 meter E =
0016722
Z = -4088529
25 I = 51
86191
XDOT = -2619
307192 Wp = 139
47143
YDOT = 6064
050787 meter/sec RA = 140
85529 deg
ZDOT = -3883
824810 TA = 90
50282
MA = 90
31120
Ha = 228
926 n
mi
Hp = 214
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17757430
77 X = 5434901
88
Y = -873896
83 feet Y = -205712
71 meter
Z = -13413809
87 Z = -4062181
83
XDOT = -8593
527534 XDOT = -2668
055694
YDOT = 19895
179749 feet/sec YDOT = 6034
487495 meter/sec
ZDOT = -12742
207382 ZDOT = -3896
667392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8408482
79 X = 2562905
55
Y = 15758028
19 feet Y = 4803046
99 meter
Z = -13304221
26 Z = -4055126
64
XDOT = -20476
216466 XDOT = -6241
150779
YDOT = 181
855010 feet/sec YDOT = 55
429407 meter/sec
ZDOT = -12796
275438 ZDOT = -3900
304753
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 13016
52338539
00016717 00000-0 10270-3 0 9095
2 25544 51
6463 141
7392 0015461 164
5873 195
5753 15
52097899 11153
Satellite: ISS
Catalog Number: 25544
Epoch time: 13016
52338539 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 141
7392 deg
Eccentricity:
0015461
Arg of perigee: 164
5873 deg
Mean anomaly: 195
5753 deg
Mean motion: 15
52097899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1115
Checksum: 332
Coasting Arc #11 (Orbit 1130)
---------------------------------------
Vector Time (GMT): 2013/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4920057
71 A = 6785981
59 meter
Y = -326194
20 meter E =
0021438
Z = 4661963
88 I = 51
87847
XDOT = 3214
020445 Wp = 150
30717
YDOT = -6312
546724 meter/sec RA = 135
89832 deg
ZDOT = 2926
354936 TA = 270
53550
MA = 270
78114
Ha = 228
693 n
mi
Hp = 214
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16141921
62 X = -4938690
80
Y = -1070190
93 feet Y = -381317
57 meter
Z = 15295157
07 Z = 4638017
66
XDOT = 10544
686500 XDOT = 3270
154508
YDOT = -20710
455130 feet/sec YDOT = -6276
291684 meter/sec
ZDOT = 9600
902022 ZDOT = 2942
104513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6225308
01 X = -1897473
88
Y = -15032887
66 feet Y = -4582024
16 meter
Z = 15195611
23 Z = 4631622
30
XDOT = 22115
433561 XDOT = 6740
784149
YDOT = 693
287388 feet/sec YDOT = 211
313996 meter/sec
ZDOT = 9667
096482 ZDOT = 2946
531008
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 13017
55354722
00016717 00000-0 10270-3 0 9103
2 25544 51
6468 136
6198 0015392 168
2920 191
8592 15
52162069 11312
Satellite: ISS
Catalog Number: 25544
Epoch time: 13017
55354722 = yrday
fracday
Element set: 910
Inclination: 51
6468 deg
RA of node: 136
6198 deg
Eccentricity:
0015392
Arg of perigee: 168
2920 deg
Mean anomaly: 191
8592 deg
Mean motion: 15
52162069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1131
Checksum: 309
Coasting Arc #12 (Orbit 1145)
---------------------------------------
Vector Time (GMT): 2013/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4349321
09 A = 6784240
10 meter
Y = 1090889
32 meter E =
0019177
Z = -5100668
26 I = 51
89375
XDOT = -3716
230091 Wp = 129
03292
YDOT = 6446
403025 meter/sec RA = 130
93865 deg
ZDOT = -1806
411232 TA = 123
61207
MA = 123
42891
Ha = 228
539 n
mi
Hp = 214
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14269426
14 X = 4361576
75
Y = 3579033
20 feet Y = 1139594
75 meter
Z = -16734475
91 Z = -5079510
03
XDOT = -12192
355940 XDOT = -3779
263947
YDOT = 21149
616225 feet/sec YDOT = 6404
493395 meter/sec
ZDOT = -5926
546036 ZDOT = -1824
617208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3399385
70 X = 1036132
76
Y = 14415389
47 feet Y = 4393810
71 meter
Z = -16646603
51 Z = -5073884
75
XDOT = -23316
520121 XDOT = -7106
875333
YDOT = -1371
628519 feet/sec YDOT = -418
072373 meter/sec
ZDOT = -6002
984465 ZDOT = -1829
709665
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 13018
51931352
00016717 00000-0 10270-3 0 9111
2 25544 51
6468 131
8201 0015261 171
8247 188
3156 15
52141096 11461
Satellite: ISS
Catalog Number: 25544
Epoch time: 13018
51931352 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 131
8201 deg
Eccentricity:
0015261
Arg of perigee: 171
8247 deg
Mean anomaly: 188
3156 deg
Mean motion: 15
52141096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1146
Checksum: 286
Coasting Arc #13 (Orbit 1161)
---------------------------------------
Vector Time (GMT): 2013/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3801649
71 A = 6783105
02 meter
Y = -1841710
19 meter E =
0016951
Z = 5305370
07 I = 51
91025
XDOT = 4065
159266 Wp = 166
76292
YDOT = -6468
290084 meter/sec RA = 125
97840 deg
ZDOT = 651
061041 TA = 276
94706
MA = 277
13984
Ha = 228
342 n
mi
Hp = 215
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12472604
04 X = -3806544
64
Y = -6042356
25 feet Y = -1884250
13 meter
Z = 17406069
78 Z = 5286890
19
XDOT = 13337
136699 XDOT = 4134
024266
YDOT = -21221
424160 feet/sec YDOT = -6422
445897 meter/sec
ZDOT = 2136
027036 ZDOT = 670
976167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -628593
51 X = -191595
30
Y = -13940708
87 feet Y = -4249128
06 meter
Z = 17329416
97 Z = 5282006
29
XDOT = 23982
947661 XDOT = 7310
002447
YDOT = 1745
269933 feet/sec YDOT = 531
958276 meter/sec
ZDOT = 2219
592322 ZDOT = 676
531740
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 13019
54944878
00016717 00000-0 10270-3 0 9123
2 25544 51
6471 126
7003 0015188 175
4790 184
6501 15
52205870 11621
Satellite: ISS
Catalog Number: 25544
Epoch time: 13019
54944878 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 126
7003 deg
Eccentricity:
0015188
Arg of perigee: 175
4790 deg
Mean anomaly: 184
6501 deg
Mean motion: 15
52205870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1162
Checksum: 308
Coasting Arc #14 (Orbit 1176)
---------------------------------------
Vector Time (GMT): 2013/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3233015
71 A = 6783081
69 meter
Y = 2715171
47 meter E =
0022055
Z = -5323244
04 I = 51
92732
XDOT = -4313
115245 Wp = 137
35853
YDOT = 6295
635951 meter/sec RA = 121
01800 deg
ZDOT = 577
248268 TA = 138
22385
MA = 138
05526
Ha = 228
112 n
mi
Hp = 215
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10607006
91 X = 3228272
48
Y = 8908042
89 feet Y = 2751298
77 meter
Z = -17464711
41 Z = -5307549
87
XDOT = -14150
640566 XDOT = -4385
997910
YDOT = 20654
973592 feet/sec YDOT = 6246
996460 meter/sec
ZDOT = 1893
859146 ZDOT = 556
118927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2543247
17 X = -775181
74
Y = 13698861
74 feet Y = 4175413
06 meter
Z = -17399742
79 Z = -5303441
60
XDOT = -23941
210143 XDOT = -7297
280852
YDOT = -2091
696162 feet/sec YDOT = -637
548990 meter/sec
ZDOT = 1805
245839 ZDOT = 550
238932
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 13020
51519014
00016717 00000-0 10270-3 0 9133
2 25544 51
6472 121
9008 0015062 178
7297 181
3896 15
52200347 11774
Satellite: ISS
Catalog Number: 25544
Epoch time: 13020
51519014 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 121
9008 deg
Eccentricity:
0015062
Arg of perigee: 178
7297 deg
Mean anomaly: 181
3896 deg
Mean motion: 15
52200347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1177
Checksum: 291
Coasting Arc #15 (Orbit 1192)
---------------------------------------
Vector Time (GMT): 2013/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2727868
63 A = 6783831
32 meter
Y = -3524365
16 meter E =
0012509
Z = 5108229
66 I = 51
94553
XDOT = 4460
789524 Wp = 163
18366
YDOT = -5987
128017 meter/sec RA = 116
05938 deg
ZDOT = -1759
212415 TA = 303
68996
MA = 303
80916
Ha = 227
959 n
mi
Hp = 215
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8949700
24 X = -2713069
86
Y = -11562877
83 feet Y = -3554787
41 meter
Z = 16759283
68 Z = 5095013
82
XDOT = 14635
136234 XDOT = 4535
953017
YDOT = -19642
808456 feet/sec YDOT = -5936
824323 meter/sec
ZDOT = -5771
694274 ZDOT = -1737
360232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5437613
48 X = 1657384
59
Y = -13640221
44 feet Y = -4157539
49 meter
Z = 16704717
49 Z = 5091597
89
XDOT = 23362
212922 XDOT = 7120
802499
YDOT = 2399
704299 feet/sec YDOT = 731
429870 meter/sec
ZDOT = -5680
092190 ZDOT = -1731
292100
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 13021
54529972
00016717 00000-0 10270-3 0 9142
2 25544 51
6475 116
7807 0014964 182
5625 177
5453 15
52238370 11935
Satellite: ISS
Catalog Number: 25544
Epoch time: 13021
54529972 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node: 116
7807 deg
Eccentricity:
0014964
Arg of perigee: 182
5625 deg
Mean anomaly: 177
5453 deg
Mean motion: 15
52238370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1193
Checksum: 321
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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