[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 21st 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 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 2983)
---------------------------------------
Vector Time (GMT): 2011/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4562583
26 A = 6766544
22 meter
Y = -604417
84 meter E =
0023779
Z = -4963297
44 I = 51
35422
XDOT = 3119
168021 Wp = 151
62356
YDOT = -6695
255717 meter/sec RA = 307
97140 deg
ZDOT = -2076
642411 TA = 98
23524
MA = 97
96549
Ha = 221
455 n
mi
Hp = 202
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14969105
20 X = -4531374
52
Y = -1982998
18 feet Y = -655264
63 meter
Z = -16283784
27 Z = -4985386
82
XDOT = 10233
490882 XDOT = 3203
891880
YDOT = -21966
062063 feet/sec YDOT = -6659
901413 meter/sec
ZDOT = -6813
131269 ZDOT = -2061
284054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2773455
41 X = 845349
21
Y = -14743454
89 feet Y = -4493805
05 meter
Z = -16373958
14 Z = -4990782
44
XDOT = 20312
663280 XDOT = 6191
299768
YDOT = 11228
150155 feet/sec YDOT = 3422
340167 meter/sec
ZDOT = -6749
832737 ZDOT = -2057
349018
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 11353
51963988
00016717 00000-0 10270-3 0 9009
2 25544 51
6414 308
4788 0024333 182
6715 177
4314 15
58321293 29845
Satellite: ISS
Catalog Number: 25544
Epoch time: 11353
51963988 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 308
4788 deg
Eccentricity:
0024333
Arg of perigee: 182
6715 deg
Mean anomaly: 177
4314 deg
Mean motion: 15
58321293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 328
Coasting Arc #2 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2011/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2618817
36 A = 6765698
59 meter
Y = 3525432
94 meter E =
0021590
Z = 5141319
36 I = 51
33412
XDOT = -4985
214676 Wp = 177
20756
YDOT = 5678
179311 meter/sec RA = 302
90791 deg
ZDOT = -1375
215571 TA = 285
93108
MA = 286
16888
Ha = 221
223 n
mi
Hp = 203
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8591920
48 X = 2554224
86
Y = 11566381
05 feet Y = 3554356
56 meter
Z = 16867845
68 Z = 5153885
08
XDOT = -16355
691195 XDOT = -5041
658096
YDOT = 18629
197216 feet/sec YDOT = 5622
116109 meter/sec
ZDOT = -4511
862111 ZDOT = -1399
570513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11866275
61 X = -3616840
81
Y = 8066580
10 feet Y = 2458693
61 meter
Z = 16918873
33 Z = 5156872
59
XDOT = -17439
139169 XDOT = -5315
449619
YDOT = -16124
629764 feet/sec YDOT = -4914
787152 meter/sec
ZDOT = -4611
820837 ZDOT = -1405
682991
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 11354
54568261
00016717 00000-0 10270-3 0 9019
2 25544 51
6417 303
3321 0024284 186
5144 173
5699 15
58355976 30007
Satellite: ISS
Catalog Number: 25544
Epoch time: 11354
54568261 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 303
3321 deg
Eccentricity:
0024284
Arg of perigee: 186
5144 deg
Mean anomaly: 173
5699 deg
Mean motion: 15
58355976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 310
Coasting Arc #3 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2011/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -195462
70 A = 6771541
62 meter
Y = -5759655
56 meter E =
0024497
Z = -3579635
89 I = 51
33820
XDOT = 5535
408855 Wp = 177
55707
YDOT = -2937
662227 meter/sec RA = 297
85479 deg
ZDOT = 4401
531778 TA = 139
93209
MA = 139
75115
Ha = 221
061 n
mi
Hp = 203
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -641281
84 X = -113653
24
Y = -18896507
75 feet Y = -5761383
51 meter
Z = -11744212
25 Z = -3580387
40
XDOT = 18160
790208 XDOT = 5546
464998
YDOT = -9637
999432 feet/sec YDOT = -2875
700574 meter/sec
ZDOT = 14440
721057 ZDOT = 4428
449479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18904582
45 X = 5762116
73
Y = -212866
47 feet Y = -64881
70 meter
Z = -11746796
12 Z = -3580423
46
XDOT = 9278
275419 XDOT = 2828
018348
YDOT = 16873
465456 feet/sec YDOT = 5143
032271 meter/sec
ZDOT = 14550
918639 ZDOT = 4435
120001
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 11355
50757499
00016717 00000-0 10270-3 0 9020
2 25544 51
6417 298
5051 0024227 190
2606 169
8058 15
58385957 30159
Satellite: ISS
Catalog Number: 25544
Epoch time: 11355
50757499 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 298
5051 deg
Eccentricity:
0024227
Arg of perigee: 190
2606 deg
Mean anomaly: 169
8058 deg
Mean motion: 15
58385957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 333
Coasting Arc #4 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2011/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2010082
82 A = 6776659
50 meter
Y = 6400548
42 meter E =
0031947
Z = 789122
16 I = 51
34346
XDOT = -4826
254367 Wp = 170
98538
YDOT = -783
077486 meter/sec RA = 292
83374 deg
ZDOT = -5940
598748 TA =
41110
MA =
40848
Ha = 220
802 n
mi
Hp = 203
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6594759
91 X = -2085339
05
Y = 20999174
61 feet Y = 6377649
55 meter
Z = 2588983
46 Z = 779175
23
XDOT = -15834
167870 XDOT = -4788
280709
YDOT = -2569
151858 feet/sec YDOT = -836
834487 meter/sec
ZDOT = -19490
153374 ZDOT = -5963
952627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20988036
28 X = -6397153
46
Y = -6646052
09 feet Y = -2025716
68 meter
Z = 2547813
32 Z = 776573
50
XDOT = 2112
394184 XDOT = 643
857747
YDOT = -14181
042648 feet/sec YDOT = -4322
381799 meter/sec
ZDOT = -19585
485227 ZDOT = -5969
655897
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 11356
53357177
00016717 00000-0 10270-3 0 9034
2 25544 51
6428 293
3573 0024288 193
9369 166
1119 15
58414482 30318
Satellite: ISS
Catalog Number: 25544
Epoch time: 11356
53357177 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 293
3573 deg
Eccentricity:
0024288
Arg of perigee: 193
9369 deg
Mean anomaly: 166
1119 deg
Mean motion: 15
58414482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 326
Coasting Arc #5 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2011/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3609820
36 A = 6774480
69 meter
Y = -5273567
53 meter E =
0019781
Z = 2277166
00 I = 51
32590
XDOT = 3100
754823 Wp = 162
69268
YDOT = 4465
596121 meter/sec RA = 287
82102 deg
ZDOT = 5395
544988 TA = 222
77045
MA = 222
92454
Ha = 220
547 n
mi
Hp = 203
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11843242
65 X = 3657460
12
Y = -17301730
73 feet Y = -5232934
28 meter
Z = 7471017
06 Z = 2294817
39
XDOT = 10173
080128 XDOT = 3024
378675
YDOT = 14650
905910 feet/sec YDOT = 4499
842811 meter/sec
ZDOT = 17701
919253 ZDOT = 5410
423572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17482071
49 X = 5328535
39
Y = 11528233
32 feet Y = 3513805
52 meter
Z = 7543566
24 Z = 2299278
99
XDOT = -13653
509761 XDOT = -4161
589775
YDOT = 9016
811230 feet/sec YDOT = 2748
324063 meter/sec
ZDOT = 17762
328032 ZDOT = 5413
957584
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 11357
55954339
00016717 00000-0 10270-3 0 9041
2 25544 51
6426 288
2092 0024239 197
9720 162
0580 15
58472568 30479
Satellite: ISS
Catalog Number: 25544
Epoch time: 11357
55954339 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 288
2092 deg
Eccentricity:
0024239
Arg of perigee: 197
9720 deg
Mean anomaly: 162
0580 deg
Mean motion: 15
58472568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3047
Checksum: 334
Coasting Arc #6 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2011/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4320713
38 A = 6767538
17 meter
Y = 2471981
61 meter E =
0018974
Z = -4576120
31 I = 51
29550
XDOT = -866
727053 Wp = 177
25329
YDOT = -7020
687474 meter/sec RA = 282
78168 deg
ZDOT = -2993
315316 TA = 62
88562
MA = 62
69221
Ha = 220
125 n
mi
Hp = 203
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14175568
84 X = -4325804
68
Y = 8110175
88 feet Y = 2423636
97 meter
Z = -15013518
08 Z = -4597122
15
XDOT = -2843
592692 XDOT = -773
615057
YDOT = -23033
751554 feet/sec YDOT = -7029
858674 meter/sec
ZDOT = -9820
588307 ZDOT = -2997
300740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8565471
94 X = -2610755
85
Y = -13811750
79 feet Y = -4209821
64 meter
Z = -15099525
18 Z = -4602335
27
XDOT = 21923
806960 XDOT = 6682
376361
YDOT = -2911
127006 feet/sec YDOT = -887
311511 meter/sec
ZDOT = -9836
292110 ZDOT = -2998
101835
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 11358
52137109
00016717 00000-0 10270-3 0 9058
2 25544 51
6433 283
3827 0024135 201
4779 158
5366 15
58517973 30628
Satellite: ISS
Catalog Number: 25544
Epoch time: 11358
52137109 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 283
3827 deg
Eccentricity:
0024135
Arg of perigee: 201
4779 deg
Mean anomaly: 158
5366 deg
Mean motion: 15
58517973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 320
Coasting Arc #7 (Orbit 3077)
---------------------------------------
Vector Time (GMT): 2011/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4119323
45 A = 6764522
23 meter
Y = 1049924
21 meter E =
0022398
Z = 5267362
44 I = 51
27993
XDOT = -1379
642530 Wp = 200
54147
YDOT = 7533
311128 meter/sec RA = 277
71503 deg
ZDOT = -443
837029 TA = 253
58796
MA = 253
83428
Ha = 219
873 n
mi
Hp = 203
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13514840
72 X = 4081689
30
Y = 3444633
25 feet Y = 1095777
84 meter
Z = 17281372
83 Z = 5287282
57
XDOT = -4526
386254 XDOT = -1461
622925
YDOT = 24715
587690 feet/sec YDOT = 7517
424804 meter/sec
ZDOT = -1456
158231 ZDOT = -450
737290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2772412
67 X = -845031
38
Y = 13565153
09 feet Y = 4134658
66 meter
Z = 17362678
78 Z = 5292144
49
XDOT = -23920
893026 XDOT = -7291
088194
YDOT = -3076
805985 feet/sec YDOT = -937
810464 meter/sec
ZDOT = -1484
961538 ZDOT = -452
616277
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 11359
54729708
00016717 00000-0 10270-3 0 9064
2 25544 51
6431 278
2356 0024208 205
6455 154
3501 15
58566304 30788
Satellite: ISS
Catalog Number: 25544
Epoch time: 11359
54729708 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 278
2356 deg
Eccentricity:
0024208
Arg of perigee: 205
6455 deg
Mean anomaly: 154
3501 deg
Mean motion: 15
58566304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3078
Checksum: 316
Coasting Arc #8 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2011/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3083583
32 A = 6769206
30 meter
Y = -4428637
81 meter E =
0024026
Z = -4099345
90 I = 51
29283
XDOT = 3292
199441 Wp = 190
94839
YDOT = -5805
845549 meter/sec RA = 272
64993 deg
ZDOT = 3768
927286 TA = 118
23151
MA = 117
98874
Ha = 219
685 n
mi
Hp = 204
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10116743
16 X = -3013918
70
Y = -14529651
60 feet Y = -4462730
30 meter
Z = -13449297
58 Z = -4114157
03
XDOT = 10801
179268 XDOT = 3338
568437
YDOT = -19048
049700 feet/sec YDOT = -5768
771361 meter/sec
ZDOT = 12365
247002 ZDOT = 3785
032411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13824811
45 X = 4213802
53
Y = -10986889
28 feet Y = -3348803
85 meter
Z = -13509468
01 Z = -4117685
85
XDOT = 18922
534135 XDOT = 5767
588404
YDOT = 8416
616220 feet/sec YDOT = 2565
384624 meter/sec
ZDOT = 12431
514939 ZDOT = 3789
125753
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 11360
50908303
00016717 00000-0 10270-3 0 9073
2 25544 51
6432 273
4079 0024134 208
9871 150
9945 15
58582947 30936
Satellite: ISS
Catalog Number: 25544
Epoch time: 11360
50908303 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 273
4079 deg
Eccentricity:
0024134
Arg of perigee: 208
9871 deg
Mean anomaly: 150
9945 deg
Mean motion: 15
58582947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 323
Coasting Arc #9 (Orbit 3108)
---------------------------------------
Vector Time (GMT): 2011/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1464187
05 A = 6775445
67 meter
Y = 6426298
68 meter E =
0026954
Z = 1493483
74 I = 51
31326
XDOT = -4516
885417 Wp = 181
63655
YDOT = 2360
625523 meter/sec RA = 267
61893 deg
ZDOT = -5758
272241 TA = 341
91726
MA = 342
01294
Ha = 219
418 n
mi
Hp = 204
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4803763
29 X = 1384963
14
Y = 21083657
09 feet Y = 6442229
00 meter
Z = 4899881
04 Z = 1500404
85
XDOT = -14819
177876 XDOT = -4514
974592
YDOT = 7744
834393 feet/sec YDOT = 2310
126211 meter/sec
ZDOT = -18891
969293 ZDOT = -5780
209965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20607041
38 X = -6281026
21
Y = 6532496
37 feet Y = 1991104
89 meter
Z = 4927667
68 Z = 1501953
11
XDOT = -8478
127644 XDOT = -2584
133306
YDOT = -12497
507487 feet/sec YDOT = -3809
240282 meter/sec
ZDOT = -18981
798954 ZDOT = -5785
652321
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 11361
53496536
00016717 00000-0 10270-3 0 9088
2 25544 51
6431 268
2600 0024185 212
7419 147
2238 15
58586784 31099
Satellite: ISS
Catalog Number: 25544
Epoch time: 11361
53496536 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 268
2600 deg
Eccentricity:
0024185
Arg of perigee: 212
7419 deg
Mean anomaly: 147
2238 deg
Mean motion: 15
58586784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3109
Checksum: 321
Coasting Arc #10 (Orbit 3124)
---------------------------------------
Vector Time (GMT): 2011/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 504266
16 A = 6775043
20 meter
Y = -6553746
02 meter E =
0013335
Z = 1678011
70 I = 51
31450
XDOT = 4815
792177 Wp = 187
83302
YDOT = 1824
467173 meter/sec RA = 262
60460 deg
ZDOT = 5670
902390 TA = 190
64120
MA = 190
66944
Ha = 219
122 n
mi
Hp = 204
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1654416
54 X = 569362
65
Y = -21501791
40 feet Y = -6547743
16 meter
Z = 5505287
72 Z = 1680618
97
XDOT = 15799
843099 XDOT = 4767
485004
YDOT = 5985
784687 feet/sec YDOT = 1878
049766 meter/sec
ZDOT = 18605
322803 ZDOT = 5694
179878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21555062
00 X = 6569982
90
Y = -566174
52 feet Y = -172569
99 meter
Z = 5516436
28 Z = 1681409
78
XDOT = -4407
671764 XDOT = -1343
458354
YDOT = 14641
004228 feet/sec YDOT = 4462
578089 meter/sec
ZDOT = 18700
312980 ZDOT = 5699
855396
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 11362
56082350
00016717 00000-0 10270-3 0 9098
2 25544 51
6429 263
1106 0024081 216
8728 143
0772 15
58637052 31254
Satellite: ISS
Catalog Number: 25544
Epoch time: 11362
56082350 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 263
1106 deg
Eccentricity:
0024081
Arg of perigee: 216
8728 deg
Mean anomaly: 143
0772 deg
Mean motion: 15
58637052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3125
Checksum: 296
Coasting Arc #11 (Orbit 3139)
---------------------------------------
Vector Time (GMT): 2011/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2454966
14 A = 6768342
48 meter
Y = 4652551
62 meter E =
0017289
Z = -4242113
44 I = 51
29797
XDOT = -4121
209595 Wp = 207
16021
YDOT = -5418
799158 meter/sec RA = 257
57066 deg
ZDOT = -3567
481752 TA = 26
38846
MA = 26
30051
Ha = 218
686 n
mi
Hp = 204
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8054350
85 X = -2486202
37
Y = 15264276
97 feet Y = 4624924
29 meter
Z = -13917695
02 Z = -4254115
05
XDOT = -13521
028855 XDOT = -4042
979321
YDOT = -17778
212459 feet/sec YDOT = -5464
447425 meter/sec
ZDOT = -11704
336457 ZDOT = -3587
312565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16099963
44 X = -4907268
86
Y = -6106114
28 feet Y = -1861143
63 meter
Z = -13967086
29 Z = -4257167
90
XDOT = 15615
565228 XDOT = 4759
624281
YDOT = -14286
840237 feet/sec YDOT = -4354
628904 meter/sec
ZDOT = -11784
983871 ZDOT = -3592
063084
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 11363
52254437
00016717 00000-0 10270-3 0 9104
2 25544 51
6433 258
2836 0024082 220
7031 139
2325 15
58689201 31407
Satellite: ISS
Catalog Number: 25544
Epoch time: 11363
52254437 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 258
2836 deg
Eccentricity:
0024082
Arg of perigee: 220
7031 deg
Mean anomaly: 139
2325 deg
Mean motion: 15
58689201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3140
Checksum: 285
Coasting Arc #12 (Orbit 3155)
---------------------------------------
Vector Time (GMT): 2011/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3978658
85 A = 6764002
03 meter
Y = -1463095
16 meter E =
0022801
Z = 5283788
45 I = 51
29110
XDOT = 2430
126476 Wp = 219
44597
YDOT = 7267
776766 meter/sec RA = 252
50448 deg
ZDOT = 165
695414 TA = 228
86807
MA = 229
06508
Ha = 218
431 n
mi
Hp = 204
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13053342
67 X = 3969056
44
Y = -4800180
98 feet Y = -1418657
32 meter
Z = 17335263
93 Z = 5303093
09
XDOT = 7972
855893 XDOT = 2347
871230
YDOT = 23844
411962 feet/sec YDOT = 7294
492010 meter/sec
ZDOT = 543
620124 ZDOT = 177
301381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6509356
92 X = 1984051
99
Y = 12178439
57 feet Y = 3711988
38 meter
Z = 17414268
58 Z = 5307869
06
XDOT = -21656
650637 XDOT = -6600
947114
YDOT = 10652
098304 feet/sec YDOT = 3246
759563 meter/sec
ZDOT = 590
530607 ZDOT = 179
993729
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 11364
54835846
00016717 00000-0 10270-3 0 9117
2 25544 51
6431 253
1343 0024139 224
5304 135
3912 15
58730869 31563
Satellite: ISS
Catalog Number: 25544
Epoch time: 11364
54835846 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 253
1343 deg
Eccentricity:
0024139
Arg of perigee: 224
5304 deg
Mean anomaly: 135
3912 deg
Mean motion: 15
58730869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3156
Checksum: 304
Coasting Arc #13 (Orbit 3170)
---------------------------------------
Vector Time (GMT): 2011/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4691999
07 A = 6767631
26 meter
Y = -2141572
00 meter E =
0021435
Z = -4384648
59 I = 51
31369
XDOT = 17
353807 Wp = 206
34261
YDOT = -6911
145652 meter/sec RA = 247
43550 deg
ZDOT = 3331
830367 TA = 97
58183
MA = 97
33830
Ha = 218
118 n
mi
Hp = 204
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15393697
73 X = -4646403
28
Y = -7026154
86 feet Y = -2193785
65 meter
Z = -14385330
03 Z = -4407331
42
XDOT = 56
935061 XDOT = 78
449079
YDOT = -22674
362374 feet/sec YDOT = -6910
610158 meter/sec
ZDOT = 10931
201992 ZDOT = 3332
062717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4610261
18 X = 1405207
61
Y = -16198973
22 feet Y = -4937447
04 meter
Z = -14477888
67 Z = -4412860
47
XDOT = 21225
804993 XDOT = 6469
625362
YDOT = -3803
528266 feet/sec YDOT = -1159
315415 meter/sec
ZDOT = 10932
641410 ZDOT = 3332
269102
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 11365
51003934
00016717 00000-0 10270-3 0 9121
2 25544 51
6431 248
3059 0024113 228
3843 131
5246 15
58750446 31713
Satellite: ISS
Catalog Number: 25544
Epoch time: 11365
51003934 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 248
3059 deg
Eccentricity:
0024113
Arg of perigee: 228
3843 deg
Mean anomaly: 131
5246 deg
Mean motion: 15
58750446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3171
Checksum: 288
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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