[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 12th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 66 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
018/02:17:47
722 4
3 4
9 4
9
N/A 0
4 -0
0 216
3
000/00:01:35
444 -2
4 -0
0 206
9
Coasting Arc #1 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2012/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6545863
19 A = 6773439
08 meter
Y = -11983
95 meter E =
0012818
Z = 1737126
74 I = 51
57653
XDOT = 1506
801601 Wp = 244
42005
YDOT = 4930
405824 meter/sec RA = 192
04749 deg
ZDOT = -5682
027680 TA = 276
46882
MA = 276
61476
Ha = 215
626 n
mi
Hp = 204
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21475929
10 X = 6537072
28
Y = -39317
43 feet Y = 61166
66 meter
Z = 5699234
70 Z = 1768904
31
XDOT = 4943
574807 XDOT = 1479
158328
YDOT = 16175
872126 feet/sec YDOT = 4947
101563 meter/sec
ZDOT = -18641
823097 ZDOT = -5674
774707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7234318
13 X = 2205020
17
Y = 20183719
59 feet Y = 6151997
73 meter
Z = 5829275
90 Z = 1776763
29
XDOT = -12066
967109 XDOT = -3678
011575
YDOT = 9665
271345 feet/sec YDOT = 2945
974706 meter/sec
ZDOT = -18612
449695 ZDOT = -5673
074667
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 12011
53546974
00016717 00000-0 10270-3 0 9005
2 25544 51
6374 192
9485 0024229 270
6496 89
1883 15
59143181 33437
Satellite: ISS
Catalog Number: 25544
Epoch time: 12011
53546974 = yrday
fracday
Element set: 900
Inclination: 51
6374 deg
RA of node: 192
9485 deg
Eccentricity:
0024229
Arg of perigee: 270
6496 deg
Mean anomaly: 89
1883 deg
Mean motion: 15
59143181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 326
Coasting Arc #2 (Orbit 3358)
---------------------------------------
Vector Time (GMT): 2012/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6241425
70 A = 6773773
02 meter
Y = -2065366
33 meter E =
0014003
Z = 1620128
45 I = 51
60693
XDOT = 2872
669969 Wp = 304
92746
YDOT = -4219
851734 meter/sec RA = 187
04936 deg
ZDOT = 5730
108991 TA = 72
84808
MA = 72
69481
Ha = 215
666 n
mi
Hp = 204
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20477118
45 X = -6225736
57
Y = -6776136
25 feet Y = -2135074
12 meter
Z = 5315382
04 Z = 1589846
43
XDOT = 9424
770238 XDOT = 2891
808588
YDOT = -13844
657919 feet/sec YDOT = -4187
620965 meter/sec
ZDOT = 18799
570179 ZDOT = 5744
110391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -873431
16 X = -266221
82
Y = -21581620
67 feet Y = -6578077
98 meter
Z = 5191575
47 Z = 1582392
20
XDOT = 14660
560710 XDOT = 4468
538904
YDOT = 3908
195038 feet/sec YDOT = 1191
217848 meter/sec
ZDOT = 18857
131800 ZDOT = 5747
653773
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 12012
56101045
00016717 00000-0 10270-3 0 9016
2 25544 51
6371 187
7954 0024001 273
9465 85
8946 15
59124789 33590
Satellite: ISS
Catalog Number: 25544
Epoch time: 12012
56101045 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 187
7954 deg
Eccentricity:
0024001
Arg of perigee: 273
9465 deg
Mean anomaly: 85
8946 deg
Mean motion: 15
59124789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 320
Coasting Arc #3 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2012/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3838966
79 A = 6766907
96 meter
Y = 3540027
57 meter E =
0016897
Z = -4294003
40 I = 51
61547
XDOT = -6325
910103 Wp = 291
69943
YDOT = 2567
012107 meter/sec RA = 182
03464 deg
ZDOT = -3522
041090 TA = 302
42248
MA = 302
58581
Ha = 215
641 n
mi
Hp = 204
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12595035
41 X = 3819955
18
Y = 11614263
69 feet Y = 3582851
05 meter
Z = -14087937
66 Z = -4275400
23
XDOT = -20754
298239 XDOT = -6337
035748
YDOT = 8421
955731 feet/sec YDOT = 2496
209758 meter/sec
ZDOT = -11555
252920 ZDOT = -3552
798616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6133987
85 X = -1869639
50
Y = 16063430
62 feet Y = 4896133
65 meter
Z = -14012009
68 Z = -4270860
55
XDOT = -14268
836103 XDOT = -4349
141244
YDOT = -15687
805828 feet/sec YDOT = -4781
643216 meter/sec
ZDOT = -11681
300054 ZDOT = -3560
460256
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 12013
52243703
00016717 00000-0 10270-3 0 9022
2 25544 51
6379 182
9669 0023831 277
8395 82
0055 15
59173162 33749
Satellite: ISS
Catalog Number: 25544
Epoch time: 12013
52243703 = yrday
fracday
Element set: 902
Inclination: 51
6379 deg
RA of node: 182
9669 deg
Eccentricity:
0023831
Arg of perigee: 277
8395 deg
Mean anomaly: 82
0055 deg
Mean motion: 15
59173162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 315
Coasting Arc #4 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2012/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -95297
48 A = 6762838
61 meter
Y = -4206658
46 meter E =
0021427
Z = 5312484
41 I = 51
63165
XDOT = 7653
858081 Wp = 283
52682
YDOT = -316
746293 meter/sec RA = 176
98485 deg
ZDOT = -108
987752 TA = 167
53938
MA = 167
48632
Ha = 215
705 n
mi
Hp = 204
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -312655
79 X = -74057
30
Y = -13801372
90 feet Y = -4207605
47 meter
Z = 17429410
80 Z = 5312072
98
XDOT = 25111
082943 XDOT = 7657
360582
YDOT = -1039
193876 feet/sec YDOT = -231
136559 meter/sec
ZDOT = -357
571364 ZDOT = -71
797526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12582733
81 X = 3835217
26
Y = -5683332
86 feet Y = -1732279
86 meter
Z = 17427981
69 Z = 5312048
82
XDOT = 10184
375375 XDOT = 3104
197614
YDOT = 21872
742752 feet/sec YDOT = 6666
811991 meter/sec
ZDOT = -205
318561 ZDOT = -62
581097
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 12014
54794316
00016717 00000-0 10270-3 0 9037
2 25544 51
6376 177
8140 0023755 281
6421 78
2068 15
59130946 33903
Satellite: ISS
Catalog Number: 25544
Epoch time: 12014
54794316 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 177
8140 deg
Eccentricity:
0023755
Arg of perigee: 281
6421 deg
Mean anomaly: 78
2068 deg
Mean motion: 15
59130946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 314
Coasting Arc #5 (Orbit 3404)
---------------------------------------
Vector Time (GMT): 2012/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3647473
16 A = 6767027
79 meter
Y = 3855341
64 meter E =
0015787
Z = -4182573
01 I = 51
67808
XDOT = -6417
269647 Wp = 282
95418
YDOT = -2046
235712 meter/sec RA = 171
93932 deg
ZDOT = 3701
868444 TA = 24
95771
MA = 24
88146
Ha = 215
664 n
mi
Hp = 204
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11966775
45 X = -3669995
40
Y = 12648758
66 feet Y = 3814427
52 meter
Z = -13722352
38 Z = -4200346
77
XDOT = -21054
034274 XDOT = -6411
894011
YDOT = -6713
371759 feet/sec YDOT = -2117
967602 meter/sec
ZDOT = 12145
237678 ZDOT = 3670
706842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16343271
41 X = -4981429
13
Y = -5838116
52 feet Y = -1779457
92 meter
Z = -13795348
50 Z = -4204822
22
XDOT = -2716
251521 XDOT = -827
913463
YDOT = -20857
597165 feet/sec YDOT = -6357
395616 meter/sec
ZDOT = 12017
794861 ZDOT = 3663
023873
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 12015
50933514
00016717 00000-0 10270-3 0 9040
2 25544 51
6387 172
9843 0023789 285
0622 74
7901 15
59210251 34051
Satellite: ISS
Catalog Number: 25544
Epoch time: 12015
50933514 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 172
9843 deg
Eccentricity:
0023789
Arg of perigee: 285
0622 deg
Mean anomaly: 74
7901 deg
Mean motion: 15
59210251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3405
Checksum: 305
Coasting Arc #6 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2012/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6115215
27 A = 6773600
50 meter
Y = -2558210
71 meter E =
0010518
Z = 1405980
25 I = 51
72947
XDOT = 3003
059696 Wp = 276
25380
YDOT = 4006
560237 meter/sec RA = 166
93146 deg
ZDOT = -5807
745549 TA = 248
42183
MA = 248
53395
Ha = 215
904 n
mi
Hp = 204
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20063042
22 X = 6136537
29
Y = -8393079
77 feet Y = -2489707
46 meter
Z = 4612796
09 Z = 1435739
25
XDOT = 9852
558059 XDOT = 2986
246948
YDOT = 13144
882668 feet/sec YDOT = 4040
048536 meter/sec
ZDOT = -19054
283297 ZDOT = -5793
197548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15956395
82 X = 4863509
44
Y = 14738470
80 feet Y = 4492285
90 meter
Z = 4734791
44 Z = 1443164
43
XDOT = -6741
155974 XDOT = -2054
704341
YDOT = 13363
291713 feet/sec YDOT = 4073
131314 meter/sec
ZDOT = -18994
968816 ZDOT = -5789
666495
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 12016
53480305
00016717 00000-0 10270-3 0 9050
2 25544 51
6378 167
8326 0023930 289
1306 70
7259 15
59245031 34216
Satellite: ISS
Catalog Number: 25544
Epoch time: 12016
53480305 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 167
8326 deg
Eccentricity:
0023930
Arg of perigee: 289
1306 deg
Mean anomaly: 70
7259 deg
Mean motion: 15
59245031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 300
Coasting Arc #7 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2012/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6450359
05 A = 6772744
24 meter
Y = 452021
54 meter E =
0017036
Z = 1991432
31 I = 51
75748
XDOT = 1360
206696 Wp = 328
37924
YDOT = -5081
309524 meter/sec RA = 161
94407 deg
ZDOT = 5594
910728 TA = 53
63012
MA = 53
47304
Ha = 216
059 n
mi
Hp = 204
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21162595
32 X = -6464608
13
Y = 1483010
29 feet Y = 379809
86 meter
Z = 6533570
57 Z = 1960062
29
XDOT = 4462
620393 XDOT = 1389
747115
YDOT = -16670
963005 feet/sec YDOT = -5065
934049 meter/sec
ZDOT = 18356
006324 ZDOT = 5601
589949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10475646
06 X = -3192976
92
Y = -18492644
72 feet Y = -5636558
11 meter
Z = 6405094
52 Z = 1952272
81
XDOT = 15569
172759 XDOT = 4745
483857
YDOT = -2493
661702 feet/sec YDOT = -760
068087 meter/sec
ZDOT = 18383
673577 ZDOT = 5603
343706
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 12017
56025261
00016717 00000-0 10270-3 0 9061
2 25544 51
6391 162
6801 0023795 292
7844 67
0798 15
59287987 34378
Satellite: ISS
Catalog Number: 25544
Epoch time: 12017
56025261 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 162
6801 deg
Eccentricity:
0023795
Arg of perigee: 292
7844 deg
Mean anomaly: 67
0798 deg
Mean motion: 15
59287987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 343
Coasting Arc #8 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2012/018/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3011736
84 A = 6770131
08 meter
Y = -4554440
49 meter E =
0013133
Z = 4017325
39 I = 51
75800
XDOT = 6515
979187 Wp = 323
26870
YDOT = 822
857542 meter/sec RA = 158
91582 deg
ZDOT = -3948
462525 TA = 167
74491
MA = 167
71293
Ha = 216
330 n
mi
Hp = 206
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9881026
38 X = 3042926
50
Y = -14942390
05 feet Y = -4520587
32 meter
Z = 13180201
43 Z = 4032031
61
XDOT = 21377
884471 XDOT = 6525
474187
YDOT = 2699
663851 feet/sec YDOT = 895
776624 meter/sec
ZDOT = -12954
273377 ZDOT = -3916
785224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15850115
70 X = -4831115
26
Y = 8251353
14 feet Y = 2515012
44 meter
Z = 13240710
55 Z = 4035768
58
XDOT = -16802
907847 XDOT = -5121
526312
YDOT = -11678
691752 feet/sec YDOT = -3559
665246 meter/sec
ZDOT = -12824
609775 ZDOT = -3908
941059
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 12018
13709180
00016717 00000-0 10270-3 0 9075
2 25544 51
6399 159
7879 0020241 294
1954 65
7085 15
58361027 34460
Satellite: ISS
Catalog Number: 25544
Epoch time: 12018
13709180 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 159
7879 deg
Eccentricity:
0020241
Arg of perigee: 294
1954 deg
Mean anomaly: 65
7085 deg
Mean motion: 15
58361027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 329
Coasting Arc #9 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2012/019/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5390310
43 A = 6776155
35 meter
Y = 3845315
29 meter E =
0020749
Z = -1377823
43 I = 51
80628
XDOT = -3811
447870 Wp = 322
52468
YDOT = -3242
578703 meter/sec RA = 153
91934 deg
ZDOT = 5831
695337 TA = 22
45172
MA = 22
36105
Ha = 216
577 n
mi
Hp = 206
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17684745
52 X = -5426215
80
Y = 12615863
81 feet Y = 3784836
90 meter
Z = -4520418
08 Z = -1404095
94
XDOT = -12504
750229 XDOT = -3803
234239
YDOT = -10638
381570 feet/sec YDOT = -3285
155281 meter/sec
ZDOT = 19132
858718 ZDOT = 5813
199302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21525146
53 X = 6560864
66
Y = -2755297
26 feet Y = -839814
60 meter
Z = -4628263
98 Z = -1410694
86
XDOT = 5881
348098 XDOT = 1792
634900
YDOT = 13774
249523 feet/sec YDOT = 4198
391255 meter/sec
ZDOT = 19057
317392 ZDOT = 5808
670341
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 12019
09898895
00016717 00000-0 10270-3 0 9084
2 25544 51
6400 154
9609 0020350 298
1077 61
8021 15
58380503 34616
Satellite: ISS
Catalog Number: 25544
Epoch time: 12019
09898895 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 154
9609 deg
Eccentricity:
0020350
Arg of perigee: 298
1077 deg
Mean anomaly: 61
8021 deg
Mean motion: 15
58380503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 314
Coasting Arc #10 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2012/020/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6190921
64 A = 6775708
75 meter
Y = -2157538
57 meter E =
0013319
Z = -1712108
38 I = 51
83285
XDOT = 194
588478 Wp = 290
49523
YDOT = 5119
581961 meter/sec RA = 148
94180 deg
ZDOT = -5707
480268 TA = 268
25123
MA = 268
40379
Ha = 216
802 n
mi
Hp = 206
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20311422
71 X = 6222904
46
Y = -7078538
63 feet Y = -2088128
88 meter
Z = -5617153
46 Z = -1681956
11
XDOT = 638
413642 XDOT = 165
051088
YDOT = 16796
528743 feet/sec YDOT = 5121
593388 meter/sec
ZDOT = -18725
328964 ZDOT = -5706
606211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21327573
25 X = -6500644
33
Y = -3027873
18 feet Y = -922895
75 meter
Z = -5493506
86 Z = -1674420
89
XDOT = 6804
945168 XDOT = 2074
147287
YDOT = -13718
651112 feet/sec YDOT = -4181
444859 meter/sec
ZDOT = -18722
082544 ZDOT = -5706
490759
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 12020
12499545
00016717 00000-0 10270-3 0 9090
2 25544 51
6410 149
8131 0020315 301
9068 58
0111 15
58412703 34777
Satellite: ISS
Catalog Number: 25544
Epoch time: 12020
12499545 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 149
8131 deg
Eccentricity:
0020315
Arg of perigee: 301
9068 deg
Mean anomaly: 58
0111 deg
Mean motion: 15
58412703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 281
Coasting Arc #11 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2012/021/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5253339
88 A = 6769204
90 meter
Y = -313983
10 meter E =
0011347
Z = 4257285
83 I = 51
83696
XDOT = 3281
009071 Wp = 323
87538
YDOT = -5913
617681 meter/sec RA = 143
94564 deg
ZDOT = 3626
351730 TA = 89
24565
MA = 89
11564
Ha = 217
122 n
mi
Hp = 206
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17235367
07 X = -5270118
95
Y = -1030128
29 feet Y = -372823
40 meter
Z = 13967473
19 Z = 4231725
05
XDOT = 10764
465457 XDOT = 3329
276819
YDOT = -19401
632813 feet/sec YDOT = -5876
657885 meter/sec
ZDOT = 11897
479428 ZDOT = 3642
407094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15073922
78 X = 4594531
66
Y = 8591248
03 feet Y = 2618612
40 meter
Z = 13862779
63 Z = 4225375
23
XDOT = -17550
327795 XDOT = -5349
339912
YDOT = 11562
620090 feet/sec YDOT = 3524
286603 meter/sec
ZDOT = 11963
641895 ZDOT = 3646
518050
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 12021
15098383
00016717 00000-0 10270-3 0 9101
2 25544 51
6411 144
6642 0020306 306
1114 53
8161 15
58441247 34938
Satellite: ISS
Catalog Number: 25544
Epoch time: 12021
15098383 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 144
6642 deg
Eccentricity:
0020306
Arg of perigee: 306
1114 deg
Mean anomaly: 53
8161 deg
Mean motion: 15
58441247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 273
Coasting Arc #12 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2012/022/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3009705
02 A = 6764696
37 meter
Y = 2912569
43 meter E =
0013763
Z = -5312207
28 I = 51
84742
XDOT = -5619
615874 Wp = 356
98704
YDOT = 5220
029629 meter/sec RA = 138
92121 deg
ZDOT = -308
387832 TA = 270
00566
MA = 270
16337
Ha = 217
316 n
mi
Hp = 206
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9874360
31 X = 3002717
29
Y = 9555673
97 feet Y = 2946187
16 meter
Z = -17428501
59 Z = -5297603
36
XDOT = -18437
059954 XDOT = -5676
071585
YDOT = 17126
081459 feet/sec YDOT = 5156
871992 meter/sec
ZDOT = -1011
771104 ZDOT = -335
823729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4940735
10 X = -1505936
06
Y = -12902653
42 feet Y = -3932728
76 meter
Z = -17368858
21 Z = -5294027
98
XDOT = 23040
014145 XDOT = 7022
596311
YDOT = -7249
174253 feet/sec YDOT = -2209
548312 meter/sec
ZDOT = -1124
527321 ZDOT = -342
755927
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 12022
11283066
00016717 00000-0 10270-3 0 9113
2 25544 51
6421 139
8382 0020367 309
8693 50
0670 15
58496741 35085
Satellite: ISS
Catalog Number: 25544
Epoch time: 12022
11283066 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 139
8382 deg
Eccentricity:
0020367
Arg of perigee: 309
8693 deg
Mean anomaly: 50
0670 deg
Mean motion: 15
58496741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 302
Coasting Arc #13 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2012/023/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -112189
97 A = 6767803
72 meter
Y = -5026980
32 meter E =
0018836
Z = 4544950
44 I = 51
88052
XDOT = 6311
077935 Wp = 339
22130
YDOT = -2998
010674 meter/sec RA = 133
89412 deg
ZDOT = -3147
009363 TA = 142
31177
MA = 142
17967
Ha = 217
486 n
mi
Hp = 206
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -368077
32 X = -78046
68
Y = -16492717
58 feet Y = -5028044
27 meter
Z = 14911254
73 Z = 4544488
07
XDOT = 20705
636270 XDOT = 6359
420292
YDOT = -9835
993026 feet/sec YDOT = -2927
165831 meter/sec
ZDOT = -10324
833868 ZDOT = -3116
234007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6370953
71 X = -1941866
69
Y = 15218500
02 feet Y = 4638598
81 meter
Z = 14909692
74 Z = 4544474
35
XDOT = -21866
100564 XDOT = -6664
787452
YDOT = 880
095283 feet/sec YDOT = 268
253042 meter/sec
ZDOT = -10198
526226 ZDOT = -3108
510794
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 12023
13878317
00016717 00000-0 10270-3 0 9126
2 25544 51
6422 134
6900 0020501 313
7989 46
1470 15
58525778 35242
Satellite: ISS
Catalog Number: 25544
Epoch time: 12023
13878317 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 134
6900 deg
Eccentricity:
0020501
Arg of perigee: 313
7989 deg
Mean anomaly: 46
1470 deg
Mean motion: 15
58525778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 302
Coasting Arc #14 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2012/024/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2540232
56 A = 6774480
19 meter
Y = 5871649
29 meter E =
0021902
Z = -2182620
65 I = 51
92408
XDOT = -5345
225840 Wp = 333
88532
YDOT = -260
376978 meter/sec RA = 128
89677 deg
ZDOT = 5518
829761 TA = 1
89868
MA = 1
89038
Ha = 217
719 n
mi
Hp = 206
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8334096
32 X = -2595099
33
Y = 19263941
23 feet Y = 5842936
15 meter
Z = -7160828
91 Z = -2195093
70
XDOT = -17536
830185 XDOT = -5368
725482
YDOT = -854
255178 feet/sec YDOT = -320
282182 meter/sec
ZDOT = 18106
396854 ZDOT = 5492
806515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15239685
91 X = 4645056
26
Y = -14407229
77 feet Y = -4391323
63 meter
Z = -7212334
42 Z = -2198319
53
XDOT = 14816
039610 XDOT = 4515
928873
YDOT = 6658
528477 feet/sec YDOT = 2029
519480 meter/sec
ZDOT = 17999
767118 ZDOT = 5486
329018
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 12024
10059754
00016717 00000-0 10270-3 0 9131
2 25544 51
6430 129
8630 0020529 317
4122 42
5440 15
58538352 35392
Satellite: ISS
Catalog Number: 25544
Epoch time: 12024
10059754 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 129
8630 deg
Eccentricity:
0020529
Arg of perigee: 317
4122 deg
Mean anomaly: 42
5440 deg
Mean motion: 15
58538352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 287
Coasting Arc #15 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2012/025/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4337665
72 A = 6776200
29 meter
Y = -5125870
82 meter E =
0010485
Z = -943280
65 I = 51
94792
XDOT = 3098
683995 Wp = 320
90030
YDOT = 3723
283231 meter/sec RA = 123
92604 deg
ZDOT = -5939
578424 TA = 229
27488
MA = 229
36598
Ha = 217
952 n
mi
Hp = 206
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14231186
76 X = 4399243
98
Y = -16817161
48 feet Y = -5077020
05 meter
Z = -3094752
80 Z = -922059
52
XDOT = 10166
286074 XDOT = 3085
671573
YDOT = 12215
496165 feet/sec YDOT = 3757
861949 meter/sec
ZDOT = -19486
805854 ZDOT = -5924
557105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19571945
90 X = -5965529
11
Y = 10139790
09 feet Y = 3090608
02 meter
Z = -3007437
83 Z = -916667
05
XDOT = -4131
060733 XDOT = -1259
147311
YDOT = -13779
245510 feet/sec YDOT = -4199
914032 meter/sec
ZDOT = -19425
489176 ZDOT = -5920
889101
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 12025
12651545
00016717 00000-0 10270-3 0 9141
2 25544 51
6429 124
7151 0020476 320
9728 38
9948 15
58529111 35557
Satellite: ISS
Catalog Number: 25544
Epoch time: 12025
12651545 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 124
7151 deg
Eccentricity:
0020476
Arg of perigee: 320
9728 deg
Mean anomaly: 38
9948 deg
Mean motion: 15
58529111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 312
Coasting Arc #16 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2012/026/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4893806
23 A = 6770502
02 meter
Y = 2760804
20 meter E =
0015741
Z = 3763867
86 I = 51
94502
XDOT = -310
051676 Wp = 359
70206
YDOT = -6368
539740 meter/sec RA = 118
94347 deg
ZDOT = 4283
622956 TA = 45
27212
MA = 45
14408
Ha = 218
341 n
mi
Hp = 205
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16055794
72 X = -4942597
97
Y = 9057756
56 feet Y = 2705805
86 meter
Z = 12348647
83 Z = 3739976
01
XDOT = -1017
229908 XDOT = -259
622728
YDOT = -20894
159251 feet/sec YDOT = -6371
724942 meter/sec
ZDOT = 14053
881088 ZDOT = 4282
239296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18321340
98 X = 5584344
73
Y = -2563865
42 feet Y = -781466
18 meter
Z = 12250537
13 Z = 3733963
72
XDOT = -6767
179269 XDOT = -2062
636241
YDOT = 18524
720498 feet/sec YDOT = 5646
334808 meter/sec
ZDOT = 14048
636570 ZDOT = 4282
024427
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 12026
15241456
00016717 00000-0 10270-3 0 9152
2 25544 51
6427 119
5654 0020639 325
5766 34
4051 15
58565191 35711
Satellite: ISS
Catalog Number: 25544
Epoch time: 12026
15241456 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 119
5654 deg
Eccentricity:
0020639
Arg of perigee: 325
5766 deg
Mean anomaly: 34
4051 deg
Mean motion: 15
58565191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 307
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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