[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 14th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 295)
---------------------------------------
Vector Time (GMT): 2012/072/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4196923
96 A = 6763292
60 meter
Y = -872659
27 meter E =
0017543
Z = 5219562
39 I = 51
30060
XDOT = 2535
341603 Wp = 138
24611
YDOT = 7207
810721 meter/sec RA = 245
53901 deg
ZDOT = -844
784843 TA = 319
78384
MA = 319
91351
Ha = 218
818 n
mi
Hp = 202
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13769435
57 X = 4181014
86
Y = -2863055
34 feet Y = -825815
22 meter
Z = 17124548
53 Z = 5239912
26
XDOT = 8318
049877 XDOT = 2458
657748
YDOT = 23647
672968 feet/sec YDOT = 7235
733648 meter/sec
ZDOT = -2771
603817 ZDOT = -832
655100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11991049
44 X = 3654871
87
Y = -7151433
97 feet Y = -2179757
07 meter
Z = 17208030
97 Z = 5245007
84
XDOT = 15052
008879 XDOT = 4587
852306
YDOT = 18776
022597 feet/sec YDOT = 5722
931688 meter/sec
ZDOT = -2722
339675 ZDOT = -829
769133
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 12072
62770668
00016717 00000-0 10270-3 0 9001
2 25544 51
6383 246
2205 0017148 148
9509 211
2664 15
59041045 2969
Satellite: ISS
Catalog Number: 25544
Epoch time: 12072
62770668 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 246
2205 deg
Eccentricity:
0017148
Arg of perigee: 148
9509 deg
Mean anomaly: 211
2664 deg
Mean motion: 15
59041045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 304
Coasting Arc #2 (Orbit 310)
---------------------------------------
Vector Time (GMT): 2012/073/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4972525
09 A = 6768786
01 meter
Y = -2665271
02 meter E =
0021473
Z = -3765991
48 I = 51
33428
XDOT = 242
757794 Wp = 140
64305
YDOT = -6396
233553 meter/sec RA = 240
47606 deg
ZDOT = 4203
133248 TA = 174
03658
MA = 174
01097
Ha = 218
700 n
mi
Hp = 202
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16314058
70 X = -4924057
65
Y = -8744327
51 feet Y = -2720606
09 meter
Z = -12355615
10 Z = -3790029
82
XDOT = 796
449457 XDOT = 293
845926
YDOT = -20985
018219 feet/sec YDOT = -6393
232993 meter/sec
ZDOT = 13789
807245 ZDOT = 4204
437011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18248873
98 X = -5562256
79
Y = -2673847
04 feet Y = -814988
58 meter
Z = -12454000
96 Z = -3795979
49
XDOT = -6691
193233 XDOT = -2039
475697
YDOT = -18635
388243 feet/sec YDOT = -5680
066336 meter/sec
ZDOT = 13795
560337 ZDOT = 4204
886791
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 12073
58915993
00016717 00000-0 10270-3 0 9010
2 25544 51
6394 241
3917 0017020 152
7817 207
4234 15
59102943 3114
Satellite: ISS
Catalog Number: 25544
Epoch time: 12073
58915993 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 241
3917 deg
Eccentricity:
0017020
Arg of perigee: 152
7817 deg
Mean anomaly: 207
4234 deg
Mean motion: 15
59102943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 311
Checksum: 298
Coasting Arc #3 (Orbit 326)
---------------------------------------
Vector Time (GMT): 2012/074/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4305083
30 A = 6774528
07 meter
Y = 5148739
36 meter E =
0029334
Z = 783064
74 I = 51
36929
XDOT = -3256
887563 Wp = 143
55235
YDOT = 3640
459657 meter/sec RA = 235
44980 deg
ZDOT = -5940
026273 TA = 27
91624
MA = 27
75917
Ha = 218
470 n
mi
Hp = 202
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14124289
04 X = 4243385
17
Y = 16892189
51 feet Y = 5196536
53 meter
Z = 2569110
05 Z = 803828
37
XDOT = -10685
326650 XDOT = -3268
498769
YDOT = 11943
765279 feet/sec YDOT = 3603
973919 meter/sec
ZDOT = -19488
275174 ZDOT = -5955
876344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19216345
93 X = 5857142
24
Y = 10729896
20 feet Y = 3270472
36 meter
Z = 2653923
58 Z = 808915
91
XDOT = -4814
672269 XDOT = -1467
512108
YDOT = 13530
426413 feet/sec YDOT = 4124
073971 meter/sec
ZDOT = -19553
495334 ZDOT = -5959
905378
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 12074
61468716
00016717 00000-0 10270-3 0 9022
2 25544 51
6389 236
2398 0016971 156
7526 203
4401 15
59142798 3270
Satellite: ISS
Catalog Number: 25544
Epoch time: 12074
61468716 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 236
2398 deg
Eccentricity:
0016971
Arg of perigee: 156
7526 deg
Mean anomaly: 203
4401 deg
Mean motion: 15
59142798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 327
Checksum: 326
Coasting Arc #4 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2012/075/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2291606
50 A = 6772001
88 meter
Y = -5874846
14 meter E =
0022648
Z = 2472649
81 I = 51
38067
XDOT = 5551
618848 Wp = 123
30467
YDOT = 81
871667 meter/sec RA = 230
43634 deg
ZDOT = 5292
277072 TA = 264
54999
MA = 264
80839
Ha = 218
310 n
mi
Hp = 202
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7518394
03 X = -2237753
90
Y = -19274429
61 feet Y = -5900171
07 meter
Z = 8112368
14 Z = 2461648
53
XDOT = 18213
972597 XDOT = 5524
582350
YDOT = 268
607830 feet/sec YDOT = 143
802398 meter/sec
ZDOT = 17363
113753 ZDOT = 5319
180589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14220715
97 X = -4334474
23
Y = -15050753
11 feet Y = -4587469
55 meter
Z = 8067618
63 Z = 2459010
16
XDOT = 15799
969672 XDOT = 4815
830756
YDOT = -5478
580657 feet/sec YDOT = -1669
871384 meter/sec
ZDOT = 17473
433988 ZDOT = 5325
902680
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 12075
64018745
00016717 00000-0 10270-3 0 9030
2 25544 51
6399 231
0888 0016942 160
5878 199
5926 15
59218367 3430
Satellite: ISS
Catalog Number: 25544
Epoch time: 12075
64018745 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 231
0888 deg
Eccentricity:
0016942
Arg of perigee: 160
5878 deg
Mean anomaly: 199
5926 deg
Mean motion: 15
59218367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 344
Coasting Arc #5 (Orbit 357)
---------------------------------------
Vector Time (GMT): 2012/076/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -739920
03 A = 6764729
09 meter
Y = 4714383
62 meter E =
0019928
Z = -4802994
18 I = 51
37649
XDOT = -6319
752668 Wp = 129
09297
YDOT = -3539
730220 meter/sec RA = 225
39299 deg
ZDOT = -2520
202234 TA = 116
13689
MA = 115
93175
Ha = 218
078 n
mi
Hp = 202
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2427559
16 X = -769250
72
Y = 15467137
86 feet Y = 4705945
07 meter
Z = -15757854
93 Z = -4806660
17
XDOT = -20734
096680 XDOT = -6267
458607
YDOT = -11613
288124 feet/sec YDOT = -3610
109367 meter/sec
ZDOT = -8268
380033 ZDOT = -2550
775587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3876875
05 X = 1181671
51
Y = 15152958
11 feet Y = 4618621
63 meter
Z = -15773176
26 Z = -4807664
13
XDOT = -22468
686446 XDOT = -6848
455629
YDOT = -2922
455425 feet/sec YDOT = -890
764414 meter/sec
ZDOT = -8393
552641 ZDOT = -2558
354845
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 12076
60157277
00016717 00000-0 10270-3 0 9042
2 25544 51
6399 226
2592 0016710 164
2248 195
9431 15
59214852 3585
Satellite: ISS
Catalog Number: 25544
Epoch time: 12076
60157277 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 226
2592 deg
Eccentricity:
0016710
Arg of perigee: 164
2248 deg
Mean anomaly: 195
9431 deg
Mean motion: 15
59214852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 358
Checksum: 321
Coasting Arc #6 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2012/077/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3732130
99 A = 6762879
15 meter
Y = -2242912
01 meter E =
0015515
Z = 5166176
93 I = 51
39356
XDOT = 5087
367906 Wp = 153
79320
YDOT = 5623
017400 meter/sec RA = 220
32271 deg
ZDOT = -1246
203857 TA = 308
11420
MA = 308
25399
Ha = 217
778 n
mi
Hp = 203
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12244524
25 X = 3731838
61
Y = -7358635
21 feet Y = -2201178
23 meter
Z = 16949399
39 Z = 5184306
62
XDOT = 16690
839588 XDOT = 5030
165761
YDOT = 18448
219817 feet/sec YDOT = 5679
587552 meter/sec
ZDOT = -4088
595333 ZDOT = -1221
629489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8117206
77 X = 2474124
62
Y = -11647233
12 feet Y = -3550076
65 meter
Z = 17023893
23 Z = 5188882
66
XDOT = 21908
666248 XDOT = 6677
761472
YDOT = 9497
977757 feet/sec YDOT = 2894
983620 meter/sec
ZDOT = -3988
134620 ZDOT = -1215
583432
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 12077
62702405
00016717 00000-0 10270-3 0 9055
2 25544 51
6402 221
1075 0016554 167
6237 192
5328 15
59273843 3742
Satellite: ISS
Catalog Number: 25544
Epoch time: 12077
62702405 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 221
1075 deg
Eccentricity:
0016554
Arg of perigee: 167
6237 deg
Mean anomaly: 192
5328 deg
Mean motion: 15
59273843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 301
Coasting Arc #7 (Orbit 388)
---------------------------------------
Vector Time (GMT): 2012/078/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5788306
54 A = 6769181
93 meter
Y = -716364
35 meter E =
0018178
Z = -3458868
09 I = 51
43899
XDOT = -1993
563506 Wp = 156
05380
YDOT = -5840
630968 meter/sec RA = 215
26835 deg
ZDOT = 4537
924797 TA = 163
22878
MA = 163
16859
Ha = 217
671 n
mi
Hp = 203
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18990507
04 X = -5763063
70
Y = -2350276
72 feet Y = -780951
98 meter
Z = -11347992
40 Z = -3486925
55
XDOT = -6540
562685 XDOT = -1950
148068
YDOT = -19162
175093 feet/sec YDOT = -5862
681009 meter/sec
ZDOT = 14888
204714 ZDOT = 4528
346378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18152580
43 X = -5532906
52
Y = 5832889
31 feet Y = 1777864
66 meter
Z = -11463041
30 Z = -3493934
99
XDOT = -13655
804816 XDOT = -4162
289308
YDOT = -13265
589711 feet/sec YDOT = -4043
351744 meter/sec
ZDOT = 14849
252710 ZDOT = 4526
052226
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 12078
58836056
00016717 00000-0 10270-3 0 9062
2 25544 51
6404 216
2777 0016428 171
5224 188
6212 15
59287563 3896
Satellite: ISS
Catalog Number: 25544
Epoch time: 12078
58836056 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 216
2777 deg
Eccentricity:
0016428
Arg of perigee: 171
5224 deg
Mean anomaly: 188
6212 deg
Mean motion: 15
59287563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 389
Checksum: 332
Coasting Arc #8 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2012/079/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5949853
02 A = 6774225
11 meter
Y = 3187689
96 meter E =
0027198
Z = 306665
13 I = 51
48166
XDOT = -2017
172758 Wp = 156
41614
YDOT = 4358
232767 meter/sec RA = 210
25298 deg
ZDOT = -6006
557838 TA = 20
25843
MA = 20
15072
Ha = 217
484 n
mi
Hp = 203
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19520515
14 X = 5912275
73
Y = 10458300
39 feet Y = 3254014
82 meter
Z = 1006119
18 Z = 335477
15
XDOT = -6618
020861 XDOT = -2036
579406
YDOT = 14298
663935 feet/sec YDOT = 4335
566260 meter/sec
ZDOT = -19706
554585 ZDOT = -6016
404689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22121955
99 X = 6742772
19
Y = 891191
80 feet Y = 271635
26 meter
Z = 1124132
84 Z = 342635
69
XDOT = 459
714153 XDOT = 140
120874
YDOT = 14086
864914 feet/sec YDOT = 4293
676426 meter/sec
ZDOT = -19747
195725 ZDOT = -6018
945257
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 12079
61376120
00016717 00000-0 10270-3 0 9079
2 25544 51
6405 211
1256 0016502 175
0709 185
0612 15
59326780 4052
Satellite: ISS
Catalog Number: 25544
Epoch time: 12079
61376120 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 211
1256 deg
Eccentricity:
0016502
Arg of perigee: 175
0709 deg
Mean anomaly: 185
0612 deg
Mean motion: 15
59326780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 285
Coasting Arc #9 (Orbit 420)
---------------------------------------
Vector Time (GMT): 2012/080/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4087819
67 A = 6770403
95 meter
Y = -4523168
06 meter E =
0019820
Z = 2951412
64 I = 51
49701
XDOT = 5562
786362 Wp = 137
23671
YDOT = -1756
335814 meter/sec RA = 205
24344 deg
ZDOT = 4979
060357 TA = 256
59736
MA = 256
81837
Ha = 217
240 n
mi
Hp = 203
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13411481
84 X = -4051274
00
Y = -14839790
22 feet Y = -4568675
85 meter
Z = 9683112
33 Z = 2931643
80
XDOT = 18250
611425 XDOT = 5557
825750
YDOT = -5762
256608 feet/sec YDOT = -1694
156370 meter/sec
ZDOT = 16335
499858 ZDOT = 5006
071989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18722298
95 X = -5706556
72
Y = -7149962
86 feet Y = -2179308
68 meter
Z = 9602262
07 Z = 2926769
48
XDOT = 13066
623222 XDOT = 3982
706758
YDOT = -11977
107093 feet/sec YDOT = -3650
622242 meter/sec
ZDOT = 16446
413330 ZDOT = 5012
866783
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 12080
63913379
00016717 00000-0 10270-3 0 9087
2 25544 51
6411 205
9731 0016322 178
8091 181
3106 15
59399822 4215
Satellite: ISS
Catalog Number: 25544
Epoch time: 12080
63913379 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 205
9731 deg
Eccentricity:
0016322
Arg of perigee: 178
8091 deg
Mean anomaly: 181
3106 deg
Mean motion: 15
59399822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 421
Checksum: 306
Coasting Arc #10 (Orbit 435)
---------------------------------------
Vector Time (GMT): 2012/081/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 597923
36 A = 6763246
33 meter
Y = 4485487
14 meter E =
0017545
Z = -5032799
20 I = 51
50119
XDOT = -7353
855892 Wp = 137
98983
YDOT = -1111
633602 meter/sec RA = 200
20102 deg
ZDOT = -1880
989424 TA = 113
84440
MA = 113
66041
Ha = 216
998 n
mi
Hp = 203
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1961690
81 X = 572169
32
Y = 14716165
15 feet Y = 4492028
78 meter
Z = -16511808
40 Z = -5029957
72
XDOT = -24126
823794 XDOT = -7331
741470
YDOT = -3647
091871 feet/sec YDOT = -1193
745579 meter/sec
ZDOT = -6171
225144 ZDOT = -1916
659978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8698126
28 X = 2651188
89
Y = 12047118
00 feet Y = 3671961
57 meter
Z = -16500397
31 Z = -5029321
10
XDOT = -22123
783374 XDOT = -6743
329172
YDOT = 7395
255743 feet/sec YDOT = 2254
073951 meter/sec
ZDOT = -6317
511831 ZDOT = -1925
577606
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 12081
60039825
00016717 00000-0 10270-3 0 9091
2 25544 51
6411 201
1432 0016187 182
8147 177
2920 15
59403736 4361
Satellite: ISS
Catalog Number: 25544
Epoch time: 12081
60039825 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 201
1432 deg
Eccentricity:
0016187
Arg of perigee: 182
8147 deg
Mean anomaly: 177
2920 deg
Mean motion: 15
59403736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 296
Coasting Arc #11 (Orbit 451)
---------------------------------------
Vector Time (GMT): 2012/082/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3186067
37 A = 6763009
99 meter
Y = -3250342
97 meter E =
0012996
Z = 4995936
45 I = 51
53090
XDOT = 6586
606299 Wp = 167
19066
YDOT = 3418
197805 meter/sec RA = 195
13725 deg
ZDOT = -1988
057559 TA = 302
04669
MA = 302
17285
Ha = 216
601 n
mi
Hp = 203
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10452976
95 X = 3197907
51
Y = -10663854
90 feet Y = -3214647
50 meter
Z = 16390867
62 Z = 5011443
38
XDOT = 21609
600719 XDOT = 6557
551292
YDOT = 11214
559728 feet/sec YDOT = 3491
690577 meter/sec
ZDOT = -6522
498552 ZDOT = -1956
131283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3926010
08 X = 1196647
87
Y = -14334340
85 feet Y = -4369107
09 meter
Z = 16454670
67 Z = 5015383
62
XDOT = 23327
815813 XDOT = 7110
318260
YDOT = -905
012418 feet/sec YDOT = -275
847785 meter/sec
ZDOT = -6391
691975 ZDOT = -1948
187714
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 12082
62571972
00016717 00000-0 10270-3 0 9100
2 25544 51
6416 195
9907 0015987 186
5902 173
5045 15
59493140 4523
Satellite: ISS
Catalog Number: 25544
Epoch time: 12082
62571972 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 195
9907 deg
Eccentricity:
0015987
Arg of perigee: 186
5902 deg
Mean anomaly: 173
5045 deg
Mean motion: 15
59493140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 452
Checksum: 327
Coasting Arc #12 (Orbit 466)
---------------------------------------
Vector Time (GMT): 2012/083/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6015228
07 A = 6770178
68 meter
Y = 1239296
17 meter E =
0013764
Z = -2868541
07 I = 51
58406
XDOT = -3376
655206 Wp = 174
72685
YDOT = -4670
482455 meter/sec RA = 190
09915 deg
ZDOT = 5051
444433 TA = 152
58218
MA = 152
50948
Ha = 216
475 n
mi
Hp = 204
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19735000
24 X = -6014704
33
Y = 4065932
31 feet Y = 1172032
72 meter
Z = -9411223
99 Z = -2897761
68
XDOT = -11078
265110 XDOT = -3348
716759
YDOT = -15323
105167 feet/sec YDOT = -4708
085424 meter/sec
ZDOT = 16572
980424 ZDOT = 5035
109265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15049397
37 X = -4587056
32
Y = 13313346
51 feet Y = 4057908
02 meter
Z = -9531191
98 Z = -2905107
31
XDOT = -16347
713008 XDOT = -4982
782925
YDOT = -6635
788884 feet/sec YDOT = -2022
588452 meter/sec
ZDOT = 16506
209025 ZDOT = 5031
092511
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 12083
58693631
00016717 00000-0 10270-3 0 9114
2 25544 51
6410 191
1606 0015893 190
1164 169
9674 15
59494750 4679
Satellite: ISS
Catalog Number: 25544
Epoch time: 12083
58693631 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 191
1606 deg
Eccentricity:
0015893
Arg of perigee: 190
1164 deg
Mean anomaly: 169
9674 deg
Mean motion: 15
59494750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 467
Checksum: 327
Coasting Arc #13 (Orbit 482)
---------------------------------------
Vector Time (GMT): 2012/084/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6667134
99 A = 6773600
05 meter
Y = 986985
13 meter E =
0024003
Z = -493274
46 I = 51
62523
XDOT = -1131
018289 Wp = 171
35155
YDOT = 4670
855695 meter/sec RA = 185
09827 deg
ZDOT = -6002
075152 TA = 13
99085
MA = 13
92447
Ha = 216
253 n
mi
Hp = 204
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21873802
47 X = 6657999
03
Y = 3238140
19 feet Y = 1061490
01 meter
Z = -1618354
53 Z = -460908
02
XDOT = -3710
689925 XDOT = -1154
007847
YDOT = 15324
329709 feet/sec YDOT = 4658
078693 meter/sec
ZDOT = -19691
847611 ZDOT = -6007
626004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20453405
09 X = 6234197
87
Y = -8427282
86 feet Y = -2568635
82 meter
Z = -1485591
38 Z = -452808
25
XDOT = 4149
689391 XDOT = 1264
825327
YDOT = 13508
472595 feet/sec YDOT = 4117
382447 meter/sec
ZDOT = -19714
883979 ZDOT = -6009
096637
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 12084
61220824
00016717 00000-0 10270-3 0 9120
2 25544 51
6404 186
0081 0015792 193
4964 166
5771 15
59529090 4839
Satellite: ISS
Catalog Number: 25544
Epoch time: 12084
61220824 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 186
0081 deg
Eccentricity:
0015792
Arg of perigee: 193
4964 deg
Mean anomaly: 166
5771 deg
Mean motion: 15
59529090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 483
Checksum: 313
Coasting Arc #14 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2012/085/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4926759
69 A = 6767946
91 meter
Y = -2888812
20 meter E =
0017341
Z = 3639676
04 I = 51
63729
XDOT = 5271
083090 Wp = 155
67206
YDOT = -3452
241287 meter/sec RA = 180
09178 deg
ZDOT = 4372
135622 TA = 247
59572
MA = 247
77953
Ha = 215
971 n
mi
Hp = 204
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16163909
74 X = -4911771
06
Y = -9477730
33 feet Y = -2943822
09 meter
Z = 11941194
36 Z = 3615778
65
XDOT = 17293
579692 XDOT = 5288
056023
YDOT = -11326
250940 feet/sec YDOT = -3393
201424 meter/sec
ZDOT = 14344
276974 ZDOT = 4397
784025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18793040
46 X = -5728118
73
Y = 499741
65 feet Y = 152321
26 meter
Z = 11843283
39 Z = 3609832
78
XDOT = 8693
273144 XDOT = 2649
709654
YDOT = -17321
159046 feet/sec YDOT = -5279
489277 meter/sec
ZDOT = 14449
728433 ZDOT = 4404
277226
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 12085
63745189
00016717 00000-0 10270-3 0 9130
2 25544 51
6404 180
8548 0015699 197
6659 162
3952 15
59591613 4994
Satellite: ISS
Catalog Number: 25544
Epoch time: 12085
63745189 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 180
8548 deg
Eccentricity:
0015699
Arg of perigee: 197
6659 deg
Mean anomaly: 162
3952 deg
Mean motion: 15
59591613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 358
Coasting Arc #15 (Orbit 513)
---------------------------------------
Vector Time (GMT): 2012/086/13:56:39
729
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1310356
60 A = 6761741
14 meter
Y = 4058589
36 meter E =
0015462
Z = -5252990
99 I = 51
64633
XDOT = -7507
387338 Wp = 145
82688
YDOT = 1331
650779 meter/sec RA = 175
04764 deg
ZDOT = -857
585753 TA = 116
05846
MA = 115
89921
Ha = 215
707 n
mi
Hp = 204
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4299070
22 X = 1290393
25
Y = 13315581
90 feet Y = 4073130
50 meter
Z = -17234222
41 Z = -5246674
15
XDOT = -24630
535885 XDOT = -7517
554173
YDOT = 4368
933002 feet/sec YDOT = 1247
641613 meter/sec
ZDOT = -2813
601552 ZDOT = -894
081327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10911334
96 X = 3325774
90
Y = 8809911
22 feet Y = 2685260
94 meter
Z = -17208526
43 Z = -5245158
86
XDOT = -17685
463228 XDOT = -5390
529192
YDOT = 16203
552645 feet/sec YDOT = 4938
842846 meter/sec
ZDOT = -2963
465242 ZDOT = -903
264206
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 12086
59859622
00016717 00000-0 10270-3 0 9145
2 25544 51
6395 176
0234 0015528 201
2936 158
7575 15
59595891 5143
Satellite: ISS
Catalog Number: 25544
Epoch time: 12086
59859622 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 176
0234 deg
Eccentricity:
0015528
Arg of perigee: 201
2936 deg
Mean anomaly: 158
7575 deg
Mean motion: 15
59595891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 514
Checksum: 342
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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