[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 10th 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) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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 1005)
---------------------------------------
Vector Time (GMT): 2013/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5857864
90 A = 6792923
30 meter
Y = 2417877
09 meter E =
0016774
Z = -2472852
80 I = 51
67660
XDOT = -3854
979081 Wp = 120
82112
YDOT = -3917
143894 meter/sec RA = 175
53574 deg
ZDOT = 5320
389983 TA = 211
57492
MA = 211
67567
Ha = 229
758 n
mi
Hp = 213
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19218716
88 X = -5872454
35
Y = 7932667
61 feet Y = 2352289
48 meter
Z = -8113034
11 Z = -2501344
82
XDOT = -12647
569164 XDOT = -3836
735138
YDOT = -12851
521963 feet/sec YDOT = -3960
151272 meter/sec
ZDOT = 17455
347714 ZDOT = 5301
706798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13570910
44 X = -4136413
50
Y = -15690045
95 feet Y = -4782326
01 meter
Z = -8231674
45 Z = -2509014
37
XDOT = 7029
481709 XDOT = 2142
586025
YDOT = -15165
994866 feet/sec YDOT = -4622
595235 meter/sec
ZDOT = 17378
155931 ZDOT = 5296
861928
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
50503832
00016717 00000-0 10270-3 0 9006
2 25544 51
6430 176
6176 0015850 138
8384 221
3966 15
51977647 10067
Satellite: ISS
Catalog Number: 25544
Epoch time: 13009
50503832 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 176
6176 deg
Eccentricity:
0015850
Arg of perigee: 138
8384 deg
Mean anomaly: 221
3966 deg
Mean motion: 15
51977647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 307
Coasting Arc #2 (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 = 6216944
23 A = 6794509
86 meter
Y = -2239150
20 meter E =
0028844
Z = 1508646
33 I = 51
71200
XDOT = 2905
769244 Wp = 131
27059
YDOT = 4140
129821 meter/sec RA = 170
57575 deg
ZDOT = -5776
513918 TA = 32
25551
MA = 32
07943
Ha = 229
541 n
mi
Hp = 213
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20396798
64 X = 6234192
30
Y = -7346293
29 feet Y = -2169532
16 meter
Z = 4949627
07 Z = 1538889
01
XDOT = 9533
363663 XDOT = 2887
317914
YDOT = 13583
103088 feet/sec YDOT = 4172
521430 meter/sec
ZDOT = -18951
817316 ZDOT = -5762
442456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13682844
45 X = 4170530
99
Y = 16778404
74 feet Y = 5114057
77 meter
Z = 5075542
34 Z = 1547025
30
XDOT = -8390
561497 XDOT = -2557
443144
YDOT = 12609
258653 feet/sec YDOT = 3843
302037 meter/sec
ZDOT = -18893
800744 ZDOT = -5758
830467
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
53529051
00016717 00000-0 10270-3 0 9013
2 25544 51
6426 171
4975 0015653 142
6749 217
5493 15
52004284 10220
Satellite: ISS
Catalog Number: 25544
Epoch time: 13010
53529051 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 171
4975 deg
Eccentricity:
0015653
Arg of perigee: 142
6749 deg
Mean anomaly: 217
5493 deg
Mean motion: 15
52004284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 287
Coasting Arc #3 (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 = -6444055
89 A = 6795301
57 meter
Y = 2099887
44 meter E =
0016713
Z = -550096
18 I = 51
74633
XDOT = -1923
278302 Wp = 107
79546
YDOT = -4373
678872 meter/sec RA = 165
62011 deg
ZDOT = 5979
272033 TA = 246
29151
MA = 246
46696
Ha = 229
553 n
mi
Hp = 213
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21141915
66 X = -6464386
17
Y = 6889394
50 feet Y = 2027712
36 meter
Z = -1804777
49 Z = -581449
49
XDOT = -6309
968181 XDOT = -1903
273165
YDOT = -14349
340130 feet/sec YDOT = -4395
074909 meter/sec
ZDOT = 19617
034229 ZDOT = 5969
977232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13807084
91 X = -4208399
48
Y = -17416100
19 feet Y = -5308427
34 meter
Z = -1935313
12 Z = -589883
44
XDOT = 9946
389839 XDOT = 3031
659623
YDOT = -10011
660947 feet/sec YDOT = -3051
554257 meter/sec
ZDOT = 19578
884915 ZDOT = 5967
644122
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
50114226
00016717 00000-0 10270-3 0 9026
2 25544 51
6441 166
6982 0015855 146
0028 214
2143 15
52020932 10373
Satellite: ISS
Catalog Number: 25544
Epoch time: 13011
50114226 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 166
6982 deg
Eccentricity:
0015855
Arg of perigee: 146
0028 deg
Mean anomaly: 214
2143 deg
Mean motion: 15
52020932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 263
Coasting Arc #4 (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 = 6501925
05 A = 6795296
05 meter
Y = -1859633
24 meter E =
0026617
Z = -505002
68 I = 51
77573
XDOT = 891
120373 Wp = 145
21034
YDOT = 4697
790678 meter/sec RA = 160
66700 deg
ZDOT = -6002
851402 TA = 40
22901
MA = 40
03232
Ha = 229
390 n
mi
Hp = 213
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21331775
10 X = 6524689
74
Y = -6101158
93 feet Y = -1786797
32 meter
Z = -1656832
95 Z = -473362
39
XDOT = 2923
623270 XDOT = 867
682097
YDOT = 15412
699076 feet/sec YDOT = 4707
625151 meter/sec
ZDOT = -19694
394362 ZDOT = -5998
579077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13447455
66 X = 4098784
49
Y = 17659383
71 feet Y = 5382580
15 meter
Z = -1525112
52 Z = -464854
30
XDOT = -11959
732823 XDOT = -3645
326564
YDOT = 7462
275038 feet/sec YDOT = 2274
501432 meter/sec
ZDOT = -19677
149808 ZDOT = -5997
595262
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
53137020
00016717 00000-0 10270-3 0 9038
2 25544 51
6440 161
5779 0015638 149
5867 210
6195 15
52049442 10530
Satellite: ISS
Catalog Number: 25544
Epoch time: 13012
53137020 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 161
5779 deg
Eccentricity:
0015638
Arg of perigee: 149
5867 deg
Mean anomaly: 210
6195 deg
Mean motion: 15
52049442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1053
Checksum: 292
Coasting Arc #5 (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 = -6430794
40 A = 6794427
90 meter
Y = 1627007
67 meter E =
0020578
Z = 1476425
56 I = 51
80329
XDOT = 72
949453 Wp = 111
55690
YDOT = -5022
528895 meter/sec RA = 155
71587 deg
ZDOT = 5780
312687 TA = 264
49136
MA = 264
72611
Ha = 229
302 n
mi
Hp = 213
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21098406
84 X = -6455681
92
Y = 5337951
66 feet Y = 1554955
27 meter
Z = 4843915
89 Z = 1445125
63
XDOT = 239
335476 XDOT = 101
028403
YDOT = -16478
113174 feet/sec YDOT = -5021
556420 meter/sec
ZDOT = 18964
280468 ZDOT = 5780
735011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12962239
00 X = -3950890
45
Y = -17517481
74 feet Y = -5339328
43 meter
Z = 4713620
04 Z = 1436711
39
XDOT = 14011
440785 XDOT = 4270
687151
YDOT = -5198
851457 feet/sec YDOT = -1584
609924 meter/sec
ZDOT = 18966
583770 ZDOT = 5781
014733
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
56158569
00016717 00000-0 10270-3 0 9044
2 25544 51
6457 156
4591 0015806 153
6032 206
5928 15
52076456 10690
Satellite: ISS
Catalog Number: 25544
Epoch time: 13013
56158569 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 156
4591 deg
Eccentricity:
0015806
Arg of perigee: 153
6032 deg
Mean anomaly: 206
5928 deg
Mean motion: 15
52076456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1069
Checksum: 318
Coasting Arc #6 (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 = 6196103
66 A = 6792813
31 meter
Y = -1242473
16 meter E =
0020764
Z = -2470096
60 I = 51
82535
XDOT = -1035
117035 Wp = 150
91427
YDOT = 5398
020155 meter/sec RA = 150
76419 deg
ZDOT = -5348
276290 TA = 56
67250
MA = 56
47387
Ha = 229
236 n
mi
Hp = 214
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20328424
07 X = 6221535
58
Y = -4076355
52 feet Y = -1173042
19 meter
Z = -8103991
46 Z = -2439935
32
XDOT = -3396
053266 XDOT = -1069
421929
YDOT = 17710
039878 feet/sec YDOT = 5386
253159 meter/sec
ZDOT = -17546
838221 ZDOT = -5353
387879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11806510
83 X = 3598624
50
Y = 17102241
98 feet Y = 5212763
35 meter
Z = -7978458
39 Z = -2431834
12
XDOT = -16317
614564 XDOT = -4973
608919
YDOT = 3125
539050 feet/sec YDOT = 952
664303 meter/sec
ZDOT = -17568
677836 ZDOT = -5354
933004
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
52740231
00016717 00000-0 10270-3 0 9055
2 25544 51
6458 151
6592 0015637 156
8874 203
2984 15
52069364 10843
Satellite: ISS
Catalog Number: 25544
Epoch time: 13014
52740231 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 151
6592 deg
Eccentricity:
0015637
Arg of perigee: 156
8874 deg
Mean anomaly: 203
2984 deg
Mean motion: 15
52069364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1084
Checksum: 312
Coasting Arc #7 (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 = -5869555
71 A = 6790648
59 meter
Y = 844375
42 meter E =
0022818
Z = 3309095
66 I = 51
84586
XDOT = 1854
990038 Wp = 128
93040
YDOT = -5742
702811 meter/sec RA = 145
81180 deg
ZDOT = 4719
795837 TA = 269
36290
MA = 269
62436
Ha = 229
020 n
mi
Hp = 214
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19257072
53 X = -5894635
88
Y = 2770260
57 feet Y = 778598
11 meter
Z = 10856613
04 Z = 3280521
44
XDOT = 6085
925323 XDOT = 1896
141173
YDOT = -18840
888489 feet/sec YDOT = -5721
729107 meter/sec
ZDOT = 15484
894479 ZDOT = 4728
906961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10474913
22 X = -3192753
55
Y = -16472795
31 feet Y = -5020908
01 meter
Z = 10737711
14 Z = 3272854
36
XDOT = 18434
952942 XDOT = 5618
973657
YDOT = -1526
209140 feet/sec YDOT = -465
188546 meter/sec
ZDOT = 15523
404465 ZDOT = 4731
533681
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
55759184
00016717 00000-0 10270-3 0 9067
2 25544 51
6469 146
5403 0015644 160
9370 199
2370 15
52122030 11006
Satellite: ISS
Catalog Number: 25544
Epoch time: 13015
55759184 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 146
5403 deg
Eccentricity:
0015644
Arg of perigee: 160
9370 deg
Mean anomaly: 199
2370 deg
Mean motion: 15
52122030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1100
Checksum: 287
Coasting Arc #8 (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 = 5412338
74 A = 6788284
79 meter
Y = -265954
21 meter E =
0016801
Z = -4088780
21 I = 51
86249
XDOT = -2619
774047 Wp = 139
34272
YDOT = 6063
943399 meter/sec RA = 140
85671 deg
ZDOT = -3883
609582 TA = 90
63482
MA = 90
44230
Ha = 228
958 n
mi
Hp = 214
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17757016
86 X = 5434772
37
Y = -872553
20 feet Y = -205304
61 meter
Z = -13414633
23 Z = -4062433
41
XDOT = -8595
059210 XDOT = -2668
522359
YDOT = 19894
827424 feet/sec YDOT = 6034
374887 meter/sec
ZDOT = -12741
501253 ZDOT = -3896
454431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8407093
28 X = 2562482
03
Y = 15758232
19 feet Y = 4803109
17 meter
Z = -13305047
25 Z = -4055378
40
XDOT = -20476
538901 XDOT = -6241
249057
YDOT = 180
416986 feet/sec YDOT = 54
991097 meter/sec
ZDOT = -12795
578722 ZDOT = -3900
092394
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
52338518
00016717 00000-0 10270-3 0 9070
2 25544 51
6469 141
7407 0015517 164
3404 195
8230 15
52094897 11154
Satellite: ISS
Catalog Number: 25544
Epoch time: 13016
52338518 = yrday
fracday
Element set: 907
Inclination: 51
6469 deg
RA of node: 141
7407 deg
Eccentricity:
0015517
Arg of perigee: 164
3404 deg
Mean anomaly: 195
8230 deg
Mean motion: 15
52094897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1115
Checksum: 308
Coasting Arc #9 (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 = -4920563
31 A = 6785995
22 meter
Y = -325184
32 meter E =
0021514
Z = 4661476
41 I = 51
87906
XDOT = 3213
165146 Wp = 150
17942
YDOT = -6312
534157 meter/sec RA = 135
89984 deg
ZDOT = 2927
390794 TA = 270
65193
MA = 270
89844
Ha = 228
727 n
mi
Hp = 214
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16143580
41 X = -4939205
28
Y = -1066877
68 feet Y = -380313
40 meter
Z = 15293557
78 Z = 4637527
72
XDOT = 10541
880401 XDOT = 3269
294100
YDOT = -20710
413902 feet/sec YDOT = -6276
288711 meter/sec
ZDOT = 9604
300504 ZDOT = 2943
136203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6229008
78 X = -1898601
88
Y = -15032900
37 feet Y = -4582028
03 meter
Z = 15194001
52 Z = 4631131
66
XDOT = 22114
144561 XDOT = 6740
391262
YDOT = 691
040452 feet/sec YDOT = 210
629130 meter/sec
ZDOT = 9670
477629 ZDOT = 2947
561581
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
55354939
00016717 00000-0 10270-3 0 9080
2 25544 51
6474 136
6214 0015449 168
0463 192
1058 15
52158046 11312
Satellite: ISS
Catalog Number: 25544
Epoch time: 13017
55354939 = yrday
fracday
Element set: 908
Inclination: 51
6474 deg
RA of node: 136
6214 deg
Eccentricity:
0015449
Arg of perigee: 168
0463 deg
Mean anomaly: 192
1058 deg
Mean motion: 15
52158046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1131
Checksum: 306
Coasting Arc #10 (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 = 4350795
66 A = 6784258
08 meter
Y = 1088361
07 meter E =
0019258
Z = -5100013
77 I = 51
89435
XDOT = -3714
118430 Wp = 129
01248
YDOT = 6446
816269 meter/sec RA = 130
94028 deg
ZDOT = -1809
094070 TA = 123
60620
MA = 123
42225
Ha = 228
575 n
mi
Hp = 214
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14274263
99 X = 4363076
31
Y = 3570738
42 feet Y = 1137083
13 meter
Z = -16732328
64 Z = -5078848
32
XDOT = -12185
427919 XDOT = -3777
144032
YDOT = 21150
972011 feet/sec YDOT = 6404
930299 meter/sec
ZDOT = -5935
347999 ZDOT = -1827
289768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3408968
78 X = 1039053
68
Y = 14415881
00 feet Y = 4393960
53 meter
Z = -16644425
92 Z = -5073221
02
XDOT = -23314
492363 XDOT = -7106
257272
YDOT = -1365
499603 feet/sec YDOT = -416
204279 meter/sec
ZDOT = -6011
743725 ZDOT = -1832
379487
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
51931859
00016717 00000-0 10270-3 0 9090
2 25544 51
6474 131
8218 0015319 171
5792 188
5620 15
52135961 11464
Satellite: ISS
Catalog Number: 25544
Epoch time: 13018
51931859 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 131
8218 deg
Eccentricity:
0015319
Arg of perigee: 171
5792 deg
Mean anomaly: 188
5620 deg
Mean motion: 15
52135961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1146
Checksum: 318
Coasting Arc #11 (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 = -3804567
27 A = 6783124
97 meter
Y = -1836957
60 meter E =
0017031
Z = 5304906
51 I = 51
91085
XDOT = 4061
786738 Wp = 166
57094
YDOT = -6469
934709 meter/sec RA = 125
98016 deg
ZDOT = 656
088124 TA = 277
09067
MA = 277
28430
Ha = 228
381 n
mi
Hp = 214
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12482176
07 X = -3809512
87
Y = -6026763
77 feet Y = -1879530
45 meter
Z = 17404548
92 Z = 5286412
34
XDOT = 13326
071974 XDOT = 4130
645959
YDOT = -21226
819911 feet/sec YDOT = -6424
128268 meter/sec
ZDOT = 2152
520092 ZDOT = 675
986853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -646854
51 X = -197161
25
Y = -13941757
40 feet Y = -4249447
66 meter
Z = 17327836
10 Z = 5281524
44
XDOT = 23982
341658 XDOT = 7309
817737
YDOT = 1734
211999 feet/sec YDOT = 528
587817 meter/sec
ZDOT = 2236
017360 ZDOT = 681
538091
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
54945763
00016717 00000-0 10270-3 0 9105
2 25544 51
6477 126
7020 0015248 175
2344 184
8955 15
52199751 11621
Satellite: ISS
Catalog Number: 25544
Epoch time: 13019
54945763 = yrday
fracday
Element set: 910
Inclination: 51
6477 deg
RA of node: 126
7020 deg
Eccentricity:
0015248
Arg of perigee: 175
2344 deg
Mean anomaly: 184
8955 deg
Mean motion: 15
52199751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1162
Checksum: 320
Coasting Arc #12 (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 = 3237656
88 A = 6783100
15 meter
Y = 2708345
73 meter E =
0022137
Z = -5323972
76 I = 51
92791
XDOT = -4308
739614 Wp = 137
30433
YDOT = 6299
246592 meter/sec RA = 121
01989 deg
ZDOT = 569
777470 TA = 138
20701
MA = 138
03775
Ha = 228
153 n
mi
Hp = 215
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10622233
85 X = 3232993
17
Y = 8885648
72 feet Y = 2744525
37 meter
Z = -17467102
23 Z = -5308255
85
XDOT = -14136
284822 XDOT = -4381
626689
YDOT = 20666
819526 feet/sec YDOT = 6250
656007 meter/sec
ZDOT = 1869
348654 ZDOT = 548
669375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2516262
20 X = -766956
72
Y = 13701231
88 feet Y = 4176135
48 meter
Z = -17402038
24 Z = -5304141
26
XDOT = -23944
293089 XDOT = -7298
220534
YDOT = -2075
221657 feet/sec YDOT = -632
527561 meter/sec
ZDOT = 1780
823308 ZDOT = 542
794944
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
51520318
00016717 00000-0 10270-3 0 9110
2 25544 51
6478 121
9026 0015123 178
4881 181
6319 15
52193030 11777
Satellite: ISS
Catalog Number: 25544
Epoch time: 13020
51520318 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 121
9026 deg
Eccentricity:
0015123
Arg of perigee: 178
4881 deg
Mean anomaly: 181
6319 deg
Mean motion: 15
52193030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1177
Checksum: 281
Coasting Arc #13 (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 = -2734600
88 A = 6783843
23 meter
Y = -3515134
39 meter E =
0012594
Z = 5110968
25 I = 51
94610
XDOT = 4455
608253 Wp = 163
11568
YDOT = -5993
967491 meter/sec RA = 116
06140 deg
ZDOT = -1749
132894 TA = 303
65739
MA = 303
77745
Ha = 228
002 n
mi
Hp = 215
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8971787
66 X = -2719918
13
Y = -11532593
14 feet Y = -3545632
57 meter
Z = 16768268
52 Z = 5097719
41
XDOT = 14618
137313 XDOT = 4530
799649
YDOT = -19665
247673 feet/sec YDOT = -5943
721581 meter/sec
ZDOT = -5738
624979 ZDOT = -1727
305813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5400300
27 X = 1646011
52
Y = -13644121
14 feet Y = -4158728
12 meter
Z = 16713564
04 Z = 5094294
32
XDOT = 23372
664886 XDOT = 7123
988257
YDOT = 2376
270754 feet/sec YDOT = 724
287326 meter/sec
ZDOT = -5647
126527 ZDOT = -1721
244165
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
54531792
00016717 00000-0 10270-3 0 9123
2 25544 51
6481 116
7826 0015027 182
3211 177
7874 15
52230269 11931
Satellite: ISS
Catalog Number: 25544
Epoch time: 13021
54531792 = yrday
fracday
Element set: 912
Inclination: 51
6481 deg
RA of node: 116
7826 deg
Eccentricity:
0015027
Arg of perigee: 182
3211 deg
Mean anomaly: 177
7874 deg
Mean motion: 15
52230269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1193
Checksum: 298
Coasting Arc #14 (Orbit 1207)
---------------------------------------
Vector Time (GMT): 2013/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2254824
25 A = 6785554
62 meter
Y = 4363731
31 meter E =
0020380
Z = -4697662
91 I = 51
96436
XDOT = -4523
948346 Wp = 155
24709
YDOT = 5456
222593 meter/sec RA = 111
10614 deg
ZDOT = 2883
453333 TA = 143
40607
MA = 143
26668
Ha = 227
752 n
mi
Hp = 215
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7397717
36 X = 2228680
21
Y = 14316703
78 feet Y = 4388800
25 meter
Z = -15412279
90 Z = -4686772
57
XDOT = -14842
350217 XDOT = -4598
631621
YDOT = 17900
992758 feet/sec YDOT = 5405
215229 meter/sec
ZDOT = 9460
148730 ZDOT = 2861
295560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8366045
97 X = -2549970
81
Y = 13823248
33 feet Y = 4213326
09 meter
Z = -15367487
80 Z = -4684010
28
XDOT = -22022
623002 XDOT = -6712
495491
YDOT = -2865
379313 feet/sec YDOT = -873
367614 meter/sec
ZDOT = 9367
320780 ZDOT = 2855
159374
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 13022
51104001
00016717 00000-0 10270-3 0 9131
2 25544 51
6479 111
9832 0015009 185
4428 174
6563 15
52248629 12083
Satellite: ISS
Catalog Number: 25544
Epoch time: 13022
51104001 = yrday
fracday
Element set: 913
Inclination: 51
6479 deg
RA of node: 111
9832 deg
Eccentricity:
0015009
Arg of perigee: 185
4428 deg
Mean anomaly: 174
6563 deg
Mean motion: 15
52248629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1208
Checksum: 288
Coasting Arc #15 (Orbit 1223)
---------------------------------------
Vector Time (GMT): 2013/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1848974
62 A = 6787747
72 meter
Y = -5085799
92 meter E =
0014684
Z = 4081689
28 I = 51
98222
XDOT = 4560
111711 Wp = 147
24102
YDOT = -4783
590099 meter/sec RA = 106
15481 deg
ZDOT = -3900
166489 TA = 342
90896
MA = 342
95836
Ha = 227
602 n
mi
Hp = 215
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6066189
70 X = -1811794
16
Y = -16685695
29 feet Y = -5106268
66 meter
Z = 13391369
04 Z = 4072797
29
XDOT = 14960
996427 XDOT = 4632
209581
YDOT = -15694
193239 feet/sec YDOT = -4732
192729 meter/sec
ZDOT = -12795
821814 ZDOT = -3877
839355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10847980
98 X = 3306464
60
Y = -14089204
59 feet Y = -4294389
56 meter
Z = 13354979
31 Z = 4070597
69
XDOT = 20266
056277 XDOT = 6177
093953
YDOT = 3580
571727 feet/sec YDOT = 1091
358262 meter/sec
ZDOT = -12702
353919 ZDOT = -3871
677475
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 13023
54113089
00016717 00000-0 10270-3 0 9142
2 25544 51
6482 106
8633 0014844 189
4541 170
6334 15
52255185 12240
Satellite: ISS
Catalog Number: 25544
Epoch time: 13023
54113089 = yrday
fracday
Element set: 914
Inclination: 51
6482 deg
RA of node: 106
8633 deg
Eccentricity:
0014844
Arg of perigee: 189
4541 deg
Mean anomaly: 170
6334 deg
Mean motion: 15
52255185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1224
Checksum: 296
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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