[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 4th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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
There are no maneuvers
Coasting Arc #1 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2012/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2499580
03 A = 6774674
38 meter
Y = -6123457
36 meter E =
0010284
Z = 1493747
54 I = 51
36538
XDOT = 5030
328807 Wp = 228
79661
YDOT = -656
744333 meter/sec RA = 237
39508 deg
ZDOT = 5744
502745 TA = 147
58424
MA = 147
52102
Ha = 217
466 n
mi
Hp = 204
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8200721
88 X = -2438176
84
Y = -20090083
21 feet Y = -6151065
98 meter
Z = 4900746
51 Z = 1481753
39
XDOT = 16503
703434 XDOT = 5009
393229
YDOT = -2154
673007 feet/sec YDOT = -600
609560 meter/sec
ZDOT = 18846
793783 ZDOT = 5768
889013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18203297
93 X = 5548365
21
Y = -11831198
80 feet Y = -3606149
39 meter
Z = 4852141
62 Z = 1478932
77
XDOT = 4308
444918 XDOT = 1313
214011
YDOT = 14373
056398 feet/sec YDOT = 4380
907590 meter/sec
ZDOT = 18946
524092 ZDOT = 5774
900543
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 12002
56122480
00016717 00000-0 10270-3 0 9000
2 25544 51
6429 238
0145 0024045 236
2407 123
6457 15
58858344 32038
Satellite: ISS
Catalog Number: 25544
Epoch time: 12002
56122480 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 238
0145 deg
Eccentricity:
0024045
Arg of perigee: 236
2407 deg
Mean anomaly: 123
6457 deg
Mean motion: 15
58858344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 282
Coasting Arc #2 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2012/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -91261
70 A = 6768185
99 meter
Y = 5325383
48 meter E =
0016509
Z = -4158057
30 I = 51
36033
XDOT = -6038
926641 Wp = 235
38442
YDOT = -2991
372177 meter/sec RA = 232
36577 deg
ZDOT = -3697
400392 TA = 356
59907
MA = 356
61028
Ha = 217
179 n
mi
Hp = 204
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -299415
03 X = -130605
46
Y = 17471730
57 feet Y = 5324143
29 meter
Z = -13641920
29 Z = -4158595
77
XDOT = -19812
751447 XDOT = -5987
066507
YDOT = -9814
213180 feet/sec YDOT = -3058
612893 meter/sec
ZDOT = -12130
578713 ZDOT = -3726
611591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17150176
06 X = -5227373
66
Y = 3339524
45 feet Y = 1017887
05 meter
Z = -13644487
72 Z = -4158839
86
XDOT = 5840
622984 XDOT = 1780
221886
YDOT = -20071
442033 feet/sec YDOT = -6117
775532 meter/sec
ZDOT = -12249
790712 ZDOT = -3733
736209
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 12003
52282363
00016717 00000-0 10270-3 0 9015
2 25544 51
6423 233
1868 0024130 240
0826 119
7933 15
58866173 32183
Satellite: ISS
Catalog Number: 25544
Epoch time: 12003
52282363 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 233
1868 deg
Eccentricity:
0024130
Arg of perigee: 240
0826 deg
Mean anomaly: 119
7933 deg
Mean motion: 15
58866173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 292
Coasting Arc #3 (Orbit 3233)
---------------------------------------
Vector Time (GMT): 2012/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2916554
25 A = 6763546
61 meter
Y = -3073182
35 meter E =
0022092
Z = 5289002
00 I = 51
36458
XDOT = 5333
479533 Wp = 239
73205
YDOT = 5495
416039 meter/sec RA = 227
30335 deg
ZDOT = 241
872955 TA = 207
89246
MA = 208
01106
Ha = 216
882 n
mi
Hp = 204
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9568747
55 X = 2925009
59
Y = -10082619
27 feet Y = -3040520
89 meter
Z = 17352368
76 Z = 5303190
76
XDOT = 17498
292431 XDOT = 5270
457331
YDOT = 18029
580182 feet/sec YDOT = 5554
705884 meter/sec
ZDOT = 793
546441 ZDOT = 267
630275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11917358
71 X = 3632410
93
Y = 7012331
29 feet Y = 2137358
58 meter
Z = 17410589
12 Z = 5306747
56
XDOT = -13225
719302 XDOT = -4031
199243
YDOT = 20163
600763 feet/sec YDOT = 6145
865512 meter/sec
ZDOT = 898
479258 ZDOT = 273
856478
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 12004
54851085
00016717 00000-0 10270-3 0 9022
2 25544 51
6424 228
0368 0023985 243
7598 116
1092 15
58894209 32341
Satellite: ISS
Catalog Number: 25544
Epoch time: 12004
54851085 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 228
0368 deg
Eccentricity:
0023985
Arg of perigee: 243
7598 deg
Mean anomaly: 116
1092 deg
Mean motion: 15
58894209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3234
Checksum: 317
Coasting Arc #4 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2012/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5143006
41 A = 6767008
31 meter
Y = 67421
38 meter E =
0018440
Z = -4392715
93 I = 51
39681
XDOT = -2943
331480 Wp = 227
88284
YDOT = -6261
996483 meter/sec RA = 222
23731 deg
ZDOT = 3328
813323 TA = 75
91346
MA = 75
70857
Ha = 216
530 n
mi
Hp = 204
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16873380
62 X = -5122039
27
Y = 221198
74 feet Y = 10026
84 meter
Z = -14411797
67 Z = -4417649
49
XDOT = -9656
599343 XDOT = -2889
260457
YDOT = -20544
607885 feet/sec YDOT = -6294
608667 meter/sec
ZDOT = 10921
303552 ZDOT = 3314
645385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4189892
34 X = -1277079
18
Y = -16255939
16 feet Y = -4954810
26 meter
Z = -14513754
12 Z = -4423792
26
XDOT = 16471
151833 XDOT = 5020
407079
YDOT = -14006
342024 feet/sec YDOT = -4269
133049 meter/sec
ZDOT = 10863
796640 ZDOT = 3311
285216
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 12005
51007375
00016717 00000-0 10270-3 0 9036
2 25544 51
6410 223
2069 0024079 247
5634 112
2971 15
58945375 32499
Satellite: ISS
Catalog Number: 25544
Epoch time: 12005
51007375 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 223
2069 deg
Eccentricity:
0024079
Arg of perigee: 247
5634 deg
Mean anomaly: 112
2971 deg
Mean motion: 15
58945375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 299
Coasting Arc #5 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2012/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5943001
49 A = 6773711
23 meter
Y = 2649456
99 meter E =
0016401
Z = 1861386
12 I = 51
44283
XDOT = -567
650185 Wp = 217
58035
YDOT = 5196
598374 meter/sec RA = 217
20802 deg
ZDOT = -5623
209756 TA = 301
82759
MA = 301
98718
Ha = 216
248 n
mi
Hp = 204
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19498036
38 X = 5903890
87
Y = 8692444
20 feet Y = 2715696
38 meter
Z = 6106909
85 Z = 1890162
19
XDOT = -1862
369373 XDOT = -598
401200
YDOT = 17049
207265 feet/sec YDOT = 5190
079308 meter/sec
ZDOT = -18448
850905 ZDOT = -5626
041427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3474871
63 X = -1059140
87
Y = 21028750
39 feet Y = 6409563
12 meter
Z = 6224410
07 Z = 1897200
19
XDOT = -15401
510698 XDOT = -4694
380461
YDOT = 2882
266594 feet/sec YDOT = 878
514858 meter/sec
ZDOT = -18460
780743 ZDOT = -5626
845970
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 12006
53572273
00016717 00000-0 10270-3 0 9044
2 25544 51
6410 218
0577 0024017 251
7414 108
1128 15
58984518 32658
Satellite: ISS
Catalog Number: 25544
Epoch time: 12006
53572273 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 218
0577 deg
Eccentricity:
0024017
Arg of perigee: 251
7414 deg
Mean anomaly: 108
1128 deg
Mean motion: 15
58984518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 296
Coasting Arc #6 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2012/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4904923
22 A = 6774317
69 meter
Y = -4446749
78 meter E =
0011231
Z = 1442850
73 I = 51
46815
XDOT = 4209
972410 Wp = 273
24440
YDOT = -2782
953909 meter/sec RA = 212
20076 deg
ZDOT = 5774
313390 TA = 102
55120
MA = 102
42555
Ha = 216
179 n
mi
Hp = 204
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16092267
78 X = -4861843
22
Y = -14589074
08 feet Y = -4501358
95 meter
Z = 4733762
25 Z = 1419127
10
XDOT = 13812
245441 XDOT = 4212
728962
YDOT = -9130
426211 feet/sec YDOT = -2735
860719 meter/sec
ZDOT = 18944
597735 ZDOT = 5794
771445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9691695
84 X = 2954028
89
Y = -19462262
71 feet Y = -5932097
67 meter
Z = 4637028
34 Z = 1413366
24
XDOT = 11070
796877 XDOT = 3374
378888
YDOT = 10015
123100 feet/sec YDOT = 3052
609521 meter/sec
ZDOT = 19028
457046 ZDOT = 5799
873708
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 12007
56135168
00016717 00000-0 10270-3 0 9057
2 25544 51
6393 212
9053 0024141 255
2719 104
5760 15
59010210 32815
Satellite: ISS
Catalog Number: 25544
Epoch time: 12007
56135168 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 212
9053 deg
Eccentricity:
0024141
Arg of perigee: 255
2719 deg
Mean anomaly: 104
5760 deg
Mean motion: 15
59010210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 276
Coasting Arc #7 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2012/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2211095
83 A = 6767805
21 meter
Y = 4852091
47 meter E =
0016448
Z = -4152485
72 I = 51
47141
XDOT = -6725
182644 Wp = 263
36006
YDOT = -125
831384 meter/sec RA = 207
17838 deg
ZDOT = -3717
258972 TA = 328
39875
MA = 328
49741
Ha = 215
989 n
mi
Hp = 204
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7254251
40 X = 2176846
04
Y = 15918935
28 feet Y = 4876626
29 meter
Z = -13623640
80 Z = -4141827
06
XDOT = -22064
247521 XDOT = -6705
218354
YDOT = -412
832624 feet/sec YDOT = -200
924443 meter/sec
ZDOT = -12195
731537 ZDOT = -3749
880745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13147024
75 X = -4007213
14
Y = 11591800
13 feet Y = 3533180
68 meter
Z = -13580359
44 Z = -4139293
56
XDOT = -5062
072782 XDOT = -1542
919784
YDOT = -20226
961174 feet/sec YDOT = -6165
177766 meter/sec
ZDOT = -12329
166032 ZDOT = -3757
929807
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 12008
52286255
00016717 00000-0 10270-3 0 9069
2 25544 51
6380 208
0766 0024026 259
0985 100
7467 15
59023881 32963
Satellite: ISS
Catalog Number: 25544
Epoch time: 12008
52286255 = yrday
fracday
Element set: 906
Inclination: 51
6380 deg
RA of node: 208
0766 deg
Eccentricity:
0024026
Arg of perigee: 259
0985 deg
Mean anomaly: 100
7467 deg
Mean motion: 15
59023881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 316
Coasting Arc #8 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2012/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1379216
72 A = 6763218
43 meter
Y = -3992959
90 meter E =
0021605
Z = 5300139
18 I = 51
48358
XDOT = 7152
180030 Wp = 260
95653
YDOT = 2737
046340 meter/sec RA = 202
12160 deg
ZDOT = 198
211972 TA = 187
13299
MA = 187
16378
Ha = 215
859 n
mi
Hp = 204
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4524989
24 X = 1398017
81
Y = -13100262
14 feet Y = -3977432
07 meter
Z = 17388908
08 Z = 5306884
51
XDOT = 23465
157579 XDOT = 7120
079413
YDOT = 8979
810826 feet/sec YDOT = 2816
846907 meter/sec
ZDOT = 650
301744 ZDOT = 232
878709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13822613
51 X = 4213132
60
Y = 241358
44 feet Y = 73566
05 meter
Z = 17416762
67 Z = 5308629
26
XDOT = -1429
052398 XDOT = -435
575171
YDOT = 24070
984909 feet/sec YDOT = 7336
836200 meter/sec
ZDOT = 791
952606 ZDOT = 241
387154
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 12009
54845541
00016717 00000-0 10270-3 0 9072
2 25544 51
6381 202
9246 0023954 262
8479 96
9952 15
59006193 33120
Satellite: ISS
Catalog Number: 25544
Epoch time: 12009
54845541 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 202
9246 deg
Eccentricity:
0023954
Arg of perigee: 262
8479 deg
Mean anomaly: 96
9952 deg
Mean motion: 15
59006193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 326
Coasting Arc #9 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2012/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4687595
94 A = 6766748
98 meter
Y = 2181473
19 meter E =
0016180
Z = -4354717
28 I = 51
52416
XDOT = -5253
381465 Wp = 253
43023
YDOT = -4448
532241 meter/sec RA = 197
06304 deg
ZDOT = 3411
463453 TA = 51
19664
MA = 51
05227
Ha = 215
579 n
mi
Hp = 204
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15379251
79 X = -4690487
37
Y = 7157064
26 feet Y = 2129037
79 meter
Z = -14287130
19 Z = -4377495
85
XDOT = -17235
503495 XDOT = -5219
818469
YDOT = -14594
922049 feet/sec YDOT = -4507
091392 meter/sec
ZDOT = 11192
465398 ZDOT = 3386
024387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11666304
12 X = -3555889
50
Y = -12205179
61 feet Y = -3720138
75 meter
Z = -14380472
26 Z = -4383167
94
XDOT = 7412
341670 XDOT = 2259
281741
YDOT = -20207
725292 feet/sec YDOT = -6159
314669 meter/sec
ZDOT = 11088
658227 ZDOT = 3379
823028
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 12010
50992808
00016717 00000-0 10270-3 0 9080
2 25544 51
6373 198
0937 0023965 266
2968 93
5446 15
59083108 33274
Satellite: ISS
Catalog Number: 25544
Epoch time: 12010
50992808 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 198
0937 deg
Eccentricity:
0023965
Arg of perigee: 266
2968 deg
Mean anomaly: 93
5446 deg
Mean motion: 15
59083108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 338
Coasting Arc #10 (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 = 6544648
32 A = 6773410
45 meter
Y = -16485
29 meter E =
0012699
Z = 1741676
88 I = 51
57708
XDOT = 1514
041874 Wp = 244
52443
YDOT = 4930
196664 meter/sec RA = 192
04242 deg
ZDOT = -5680
256270 TA = 276
31259
MA = 276
45722
Ha = 215
582 n
mi
Hp = 204
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21471943
31 X = 6535885
73
Y = -54085
58 feet Y = 56651
90 meter
Z = 5714163
00 Z = 1773448
62
XDOT = 4967
328984 XDOT = 1486
391797
YDOT = 16175
185906 feet/sec YDOT = 4946
973330 meter/sec
ZDOT = -18636
011385 ZDOT = -5672
968141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7246860
16 X = 2208842
98
Y = 20174922
66 feet Y = 6149316
43 meter
Z = 5844180
62 Z = 1781306
25
XDOT = -12059
000367 XDOT = -3675
583312
YDOT = 9686
468690 feet/sec YDOT = 2952
435657 meter/sec
ZDOT = -18606
494100 ZDOT = -5671
259402
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
53547919
00016717 00000-0 10270-3 0 9094
2 25544 51
6380 192
9430 0024139 270
7942 89
0447 15
59150707 33438
Satellite: ISS
Catalog Number: 25544
Epoch time: 12011
53547919 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 192
9430 deg
Eccentricity:
0024139
Arg of perigee: 270
7942 deg
Mean anomaly: 89
0447 deg
Mean motion: 15
59150707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 316
Coasting Arc #11 (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 = -6242385
92 A = 6773741
70 meter
Y = -2063508
90 meter E =
0013962
Z = 1618404
46 I = 51
60749
XDOT = 2869
973377 Wp = 305
35537
YDOT = -4220
873040 meter/sec RA = 187
04430 deg
ZDOT = 5730
825993 TA = 72
40074
MA = 72
24829
Ha = 215
616 n
mi
Hp = 204
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20480268
76 X = -6226709
11
Y = -6770042
31 feet Y = -2133227
50 meter
Z = 5309725
92 Z = 1588117
75
XDOT = 9415
923153 XDOT = 2889
120134
YDOT = -13848
008661 feet/sec YDOT = -4188
672381 meter/sec
ZDOT = 18801
922550 ZDOT = 5744
814314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -880231
48 X = -268294
55
Y = -21582393
38 feet Y = -6578313
50 meter
Z = 5185900
02 Z = 1580662
33
XDOT = 14660
522952 XDOT = 4468
527396
YDOT = 3899
217450 feet/sec YDOT = 1188
481479 meter/sec
ZDOT = 18859
430703 ZDOT = 5748
354478
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
56101347
00016717 00000-0 10270-3 0 9101
2 25544 51
6376 187
7899 0023909 274
1002 85
7420 15
59136437 33598
Satellite: ISS
Catalog Number: 25544
Epoch time: 12012
56101347 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 187
7899 deg
Eccentricity:
0023909
Arg of perigee: 274
1002 deg
Mean anomaly: 85
7420 deg
Mean motion: 15
59136437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 313
Coasting Arc #12 (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 = 3836290
51 A = 6766855
86 meter
Y = 3540885
09 meter E =
0016817
Z = -4295729
16 I = 51
61598
XDOT = -6327
975212 Wp = 292
02389
YDOT = 2565
355509 meter/sec RA = 182
02954 deg
ZDOT = -3519
408051 TA = 302
12900
MA = 302
29209
Ha = 215
587 n
mi
Hp = 204
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12586254
96 X = 3817277
90
Y = 11617077
08 feet Y = 3583678
64 meter
Z = -14093599
59 Z = -4277138
99
XDOT = -20761
073529 XDOT = -6339
094969
YDOT = 8416
520700 feet/sec YDOT = 2494
530100 meter/sec
ZDOT = -11546
614341 ZDOT = -3550
175595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6139821
23 X = -1871417
51
Y = 16056332
95 feet Y = 4893970
28 meter
Z = -14017724
88 Z = -4272602
54
XDOT = -14266
812091 XDOT = -4348
524325
YDOT = -15695
728481 feet/sec YDOT = -4784
058041 meter/sec
ZDOT = -11672
702385 ZDOT = -3557
839687
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
52243151
00016717 00000-0 10270-3 0 9119
2 25544 51
6384 182
9614 0023738 278
0047 81
8415 15
59188979 33747
Satellite: ISS
Catalog Number: 25544
Epoch time: 12013
52243151 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 182
9614 deg
Eccentricity:
0023738
Arg of perigee: 278
0047 deg
Mean anomaly: 81
8415 deg
Mean motion: 15
59188979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 320
Coasting Arc #13 (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 = -84399
73 A = 6762781
14 meter
Y = -4206983
86 meter E =
0021340
Z = 5312253
27 I = 51
63216
XDOT = 7654
111373 Wp = 283
77947
YDOT = -309
549245 meter/sec RA = 176
97960 deg
ZDOT = -118
972136 TA = 167
38219
MA = 167
32868
Ha = 215
646 n
mi
Hp = 204
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -276901
99 X = -63155
59
Y = -13802440
48 feet Y = -4207808
98 meter
Z = 17428652
46 Z = 5311894
79
XDOT = 25111
913955 XDOT = 7657
581878
YDOT = -1015
581513 feet/sec YDOT = -223
936857 meter/sec
ZDOT = -390
328529 ZDOT = -81
780757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12597444
77 X = 3839701
17
Y = -5650723
92 feet Y = -1722340
65 meter
Z = 17427440
12 Z = 5311883
75
XDOT = 10165
346467 XDOT = 3098
397603
YDOT = 21881
683248 feet/sec YDOT = 6669
537054 meter/sec
ZDOT = -238
071433 ZDOT = -72
564173
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
54792580
00016717 00000-0 10270-3 0 9128
2 25544 51
6381 177
8085 0023662 281
8155 78
0346 15
59150869 33903
Satellite: ISS
Catalog Number: 25544
Epoch time: 12014
54792580 = yrday
fracday
Element set: 912
Inclination: 51
6381 deg
RA of node: 177
8085 deg
Eccentricity:
0023662
Arg of perigee: 281
8155 deg
Mean anomaly: 78
0346 deg
Mean motion: 15
59150869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 325
Coasting Arc #14 (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 = -3664215
16 A = 6766992
84 meter
Y = 3850140
87 meter E =
0015740
Z = -4172690
13 I = 51
67869
XDOT = -6404
821720 Wp = 283
27392
YDOT = -2058
932153 meter/sec RA = 171
93400 deg
ZDOT = 3716
358196 TA = 24
81189
MA = 24
73628
Ha = 215
601 n
mi
Hp = 204
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12021703
29 X = -3686726
02
Y = 12631695
76 feet Y = 3809039
60 meter
Z = -13689928
25 Z = -4190545
19
XDOT = -21013
194621 XDOT = -6399
375423
YDOT = -6755
026749 feet/sec YDOT = -2130
524448 meter/sec
ZDOT = 12192
776232 ZDOT = 3685
257236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16349662
97 X = -4983377
27
Y = -5895464
68 feet Y = -1796937
63 meter
Z = -13763256
89 Z = -4195040
70
XDOT = -2666
045698 XDOT = -812
610729
YDOT = -20836
606615 feet/sec YDOT = -6350
997696 meter/sec
ZDOT = 12065
582433 ZDOT = 3677
589526
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
50930411
00016717 00000-0 10270-3 0 9133
2 25544 51
6392 172
9788 0023695 285
2472 74
6064 15
59234486 34051
Satellite: ISS
Catalog Number: 25544
Epoch time: 12015
50930411 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 172
9788 deg
Eccentricity:
0023695
Arg of perigee: 285
2472 deg
Mean anomaly: 74
6064 deg
Mean motion: 15
59234486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3405
Checksum: 318
Coasting Arc #15 (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 = 6127368
02 A = 6773546
26 meter
Y = -2542001
94 meter E =
0010448
Z = 1381756
77 I = 51
73004
XDOT = 2970
795553 Wp = 276
23991
YDOT = 4019
855137 meter/sec RA = 166
92624 deg
ZDOT = -5815
262831 TA = 248
70593
MA = 248
81751
Ha = 215
837 n
mi
Hp = 204
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20102913
46 X = 6148625
56
Y = -8339901
38 feet Y = -2473363
14 meter
Z = 4533322
74 Z = 1411574
66
XDOT = 9746
704571 XDOT = 2953
873054
YDOT = 13188
501106 feet/sec YDOT = 4052
982025 meter/sec
ZDOT = -19078
946295 ZDOT = -5800
871833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15924787
30 X = 4853875
17
Y = 14797264
18 feet Y = 4510206
12 meter
Z = 4655558
17 Z = 1419014
13
XDOT = -6820
450655 XDOT = -2078
873360
YDOT = 13287
561882 feet/sec YDOT = 4050
048862 meter/sec
ZDOT = -19020
275423 ZDOT = -5797
379949
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
53475463
00016717 00000-0 10270-3 0 9149
2 25544 51
6383 167
8270 0023837 289
3297 70
5281 15
59273983 34217
Satellite: ISS
Catalog Number: 25544
Epoch time: 12016
53475463 = yrday
fracday
Element set: 914
Inclination: 51
6383 deg
RA of node: 167
8270 deg
Eccentricity:
0023837
Arg of perigee: 289
3297 deg
Mean anomaly: 70
5281 deg
Mean motion: 15
59273983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 330
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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