[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 13th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9321 55 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 464)
---------------------------------------
Vector Time (GMT): 2011/192/02:16:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3590917
40 A = 6770576
84 meter
Y = 5274219
19 meter E =
0012424
Z = 2239408
04 I = 51
87283
XDOT = -5237
661129 Wp = 21
94014
YDOT = 1239
105993 meter/sec RA = 39
76151 deg
ZDOT = 5481
813453 TA = 2
95683
MA = 2
94949
Ha = 212
563 n
mi
Hp = 207
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11781225
06 X = 3520794
59
Y = 17303868
73 feet Y = 5313982
56 meter
Z = 7347139
25 Z = 2256683
17
XDOT = -17183
927587 XDOT = -5277
757284
YDOT = 4065
308377 feet/sec YDOT = 1180
310190 meter/sec
ZDOT = 17984
952274 ZDOT = 5456
271841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1428742
48 X = -435480
71
Y = 20860221
90 feet Y = 6358195
63 meter
Z = 7416969
01 Z = 2260692
15
XDOT = -14599
762495 XDOT = -4450
007608
YDOT = -7355
975467 feet/sec YDOT = -2242
101322 meter/sec
ZDOT = 17881
128058 ZDOT = 5450
167832
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 11192
15422702
00016717 00000-0 10270-3 0 9004
2 25544 51
6379 40
0226 0011139 310
4566 49
5618 15
59846490 4656
Satellite: ISS
Catalog Number: 25544
Epoch time: 11192
15422702 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 40
0226 deg
Eccentricity:
0011139
Arg of perigee: 310
4566 deg
Mean anomaly: 49
5618 deg
Mean motion: 15
59846490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 294
Coasting Arc #2 (Orbit 479)
---------------------------------------
Vector Time (GMT): 2011/193/02:16:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -307703
25 A = 6763095
04 meter
Y = -4784721
16 meter E =
0011843
Z = -4777084
63 I = 51
82301
XDOT = 6849
622395 Wp = 13
69239
YDOT = 2215
323210 meter/sec RA = 34
74756 deg
ZDOT = -2650
170055 TA = 230
18560
MA = 230
28991
Ha = 212
875 n
mi
Hp = 207
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1009525
10 X = -230970
72
Y = -15697904
08 feet Y = -4787732
21 meter
Z = -15672849
83 Z = -4778393
90
XDOT = 22472
514420 XDOT = 6837
215062
YDOT = 7268
120768 feet/sec YDOT = 2291
850949 meter/sec
ZDOT = -8694
783644 ZDOT = -2616
924651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8735030
03 X = 2662437
15
Y = -13076148
76 feet Y = -3985610
14 meter
Z = -15677855
06 Z = -4778610
22
XDOT = 12634
330315 XDOT = 3850
943880
YDOT = 18741
812986 feet/sec YDOT = 5712
504598 meter/sec
ZDOT = -8559
888306 ZDOT = -2609
053956
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 11193
11523429
00016717 00000-0 10270-3 0 9010
2 25544 51
6374 35
1897 0011178 315
0256 44
9994 15
59820650 4803
Satellite: ISS
Catalog Number: 25544
Epoch time: 11193
11523429 = yrday
fracday
Element set: 901
Inclination: 51
6374 deg
RA of node: 35
1897 deg
Eccentricity:
0011178
Arg of perigee: 315
0256 deg
Mean anomaly: 44
9994 deg
Mean motion: 15
59820650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 480
Checksum: 307
Coasting Arc #3 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2011/194/02:16:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3361252
62 A = 6761443
79 meter
Y = 2772972
34 meter E =
0011731
Z = 5175659
82 I = 51
79172
XDOT = -5955
383263 Wp = 340
60247
YDOT = -4639
973547 meter/sec RA = 29
70002 deg
ZDOT = -1371
746332 TA = 122
60483
MA = 122
49153
Ha = 213
143 n
mi
Hp = 206
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11027731
71 X = -3417152
77
Y = 9097678
27 feet Y = 2735071
29 meter
Z = 16980511
21 Z = 5159195
80
XDOT = -19538
659000 XDOT = -5896
391967
YDOT = -15223
010326 feet/sec YDOT = -4706
240182 meter/sec
ZDOT = -4500
480091 ZDOT = -1400
534701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14353363
18 X = -4374905
10
Y = 795341
00 feet Y = 242419
94 meter
Z = 16913449
54 Z = 5155219
42
XDOT = -6739
675108 XDOT = -2054
252973
YDOT = -22748
871077 feet/sec YDOT = -6933
855904 meter/sec
ZDOT = -4617
113026 ZDOT = -1407
296050
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 11194
14029915
00016717 00000-0 10270-3 0 9026
2 25544 51
6371 30
0348 0011344 318
7263 41
3034 15
59837251 4966
Satellite: ISS
Catalog Number: 25544
Epoch time: 11194
14029915 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 30
0348 deg
Eccentricity:
0011344
Arg of perigee: 318
7263 deg
Mean anomaly: 41
3034 deg
Mean motion: 15
59837251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 286
Coasting Arc #4 (Orbit 510)
---------------------------------------
Vector Time (GMT): 2011/195/02:16:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5926509
40 A = 6768357
27 meter
Y = -97660
59 meter E =
0010049
Z = -3254771
33 I = 51
78798
XDOT = 2705
660035 Wp = 346
24235
YDOT = 5376
703942 meter/sec RA = 24
66934 deg
ZDOT = 4771
841516 TA = 335
98121
MA = 336
02804
Ha = 213
415 n
mi
Hp = 206
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19443928
48 X = 5942971
77
Y = -320408
76 feet Y = -31294
16 meter
Z = -10678383
63 Z = -3225940
94
XDOT = 8876
837384 XDOT = 2622
155313
YDOT = 17640
104797 feet/sec YDOT = 5406
492569 meter/sec
ZDOT = 15655
648020 ZDOT = 4784
783442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16143115
66 X = 4920421
65
Y = 10957027
49 feet Y = 3339701
98 meter
Z = -10561262
19 Z = -3219072
72
XDOT = -2162
210874 XDOT = -659
041874
YDOT = 18305
257158 feet/sec YDOT = 5579
442382 meter/sec
ZDOT = 15707
862468 ZDOT = 4787
756480
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 11195
10129005
00016717 00000-0 10270-3 0 9035
2 25544 51
6370 25
2024 0011374 322
9242 37
1127 15
59835305 5111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11195
10129005 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 25
2024 deg
Eccentricity:
0011374
Arg of perigee: 322
9242 deg
Mean anomaly: 37
1127 deg
Mean motion: 15
59835305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 511
Checksum: 260
Coasting Arc #5 (Orbit 526)
---------------------------------------
Vector Time (GMT): 2011/196/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5679976
45 A = 6771579
33 meter
Y = -3341197
64 meter E =
0003594
Z = -1566325
60 I = 51
77194
XDOT = 3654
761219 Wp = 335
99530
YDOT = -3510
072607 meter/sec RA = 19
67457 deg
ZDOT = -5757
952793 TA = 221
12467
MA = 221
15175
Ha = 213
469 n
mi
Hp = 206
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18635093
34 X = -5634583
63
Y = -10961934
52 feet Y = -3404460
55 meter
Z = -5138863
51 Z = -1593808
55
XDOT = 11990
686413 XDOT = 3721
710344
YDOT = -11515
986243 feet/sec YDOT = -3468
827625 meter/sec
ZDOT = -18890
921236 ZDOT = -5740
036294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9591367
02 X = -2923448
67
Y = -19346286
92 feet Y = -5896748
25 meter
Z = -5250284
87 Z = -1600286
83
XDOT = 15019
552326 XDOT = 4577
959549
YDOT = -2332
564783 feet/sec YDOT = -710
965746 meter/sec
ZDOT = -18817
905365 ZDOT = -5735
697555
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 11196
12633901
00016717 00000-0 10270-3 0 9044
2 25544 51
6375 20
0470 0011512 326
8172 33
2261 15
59874700 5278
Satellite: ISS
Catalog Number: 25544
Epoch time: 11196
12633901 = yrday
fracday
Element set: 904
Inclination: 51
6375 deg
RA of node: 20
0470 deg
Eccentricity:
0011512
Arg of perigee: 326
8172 deg
Mean anomaly: 33
2261 deg
Mean motion: 15
59874700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 527
Checksum: 276
Coasting Arc #6 (Orbit 542)
---------------------------------------
Vector Time (GMT): 2011/197/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2727375
06 A = 6764133
87 meter
Y = 4322834
23 meter E =
0007177
Z = 4424263
32 I = 51
71887
XDOT = -6859
173822 Wp = 21
68236
YDOT = 923
018968 meter/sec RA = 14
66222 deg
ZDOT = 3331
343276 TA = 34
80159
MA = 34
75466
Ha = 213
510 n
mi
Hp = 205
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8948080
92 X = 2657341
86
Y = 14182527
00 feet Y = 4352941
23 meter
Z = 14515299
59 Z = 4437343
04
XDOT = -22503
851121 XDOT = -6885
168067
YDOT = 3028
277455 feet/sec YDOT = 846
169727 meter/sec
ZDOT = 10929
603925 ZDOT = 3297
959223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -41135
68 X = -12538
15
Y = 16723442
78 feet Y = 5097305
36 meter
Z = 14568147
31 Z = 4440371
30
XDOT = -19503
092207 XDOT = -5944
542505
YDOT = -9437
109253 feet/sec YDOT = -2876
430900 meter/sec
ZDOT = 10793
926064 ZDOT = 3289
988664
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 11197
15137845
00016717 00000-0 10270-3 0 9055
2 25544 51
6378 14
8924 0011543 329
5836 30
4649 15
59911453 5431
Satellite: ISS
Catalog Number: 25544
Epoch time: 11197
15137845 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 14
8924 deg
Eccentricity:
0011543
Arg of perigee: 329
5836 deg
Mean anomaly: 30
4649 deg
Mean motion: 15
59911453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 543
Checksum: 320
Coasting Arc #7 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2011/198/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1351231
97 A = 6760778
94 meter
Y = -4006233
88 meter E =
0013247
Z = -5283013
14 I = 51
67791
XDOT = 7448
339554 Wp = 45
66124
YDOT = 1739
025937 meter/sec RA = 9
60924 deg
ZDOT = 596
286064 TA = 229
96619
MA = 230
08249
Ha = 213
823 n
mi
Hp = 205
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4433175
74 X = 1421593
30
Y = -13143811
93 feet Y = -3990729
58 meter
Z = -17332720
29 Z = -5276278
56
XDOT = 24436
809561 XDOT = 7425
443276
YDOT = 5705
465673 feet/sec YDOT = 1822
189718 meter/sec
ZDOT = 1956
319109 ZDOT = 632
413772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10682501
93 X = 3256026
59
Y = -8902455
98 feet Y = -2713468
58 meter
Z = -17305099
30 Z = -5274594
27
XDOT = 17302
600824 XDOT = 5273
832731
YDOT = 16738
107933 feet/sec YDOT = 5101
775298 meter/sec
ZDOT = 2102
965445 ZDOT = 640
983868
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 11198
11234770
00016717 00000-0 10270-3 0 9068
2 25544 51
6381 10
0592 0011638 333
9512 26
1057 15
59883630 5585
Satellite: ISS
Catalog Number: 25544
Epoch time: 11198
11234770 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 10
0592 deg
Eccentricity:
0011638
Arg of perigee: 333
9512 deg
Mean anomaly: 26
1057 deg
Mean motion: 15
59883630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 558
Checksum: 297
Coasting Arc #8 (Orbit 573)
---------------------------------------
Vector Time (GMT): 2011/199/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5028036
28 A = 6766704
13 meter
Y = 2563198
92 meter E =
0014003
Z = 3737583
07 I = 51
66856
XDOT = -5122
136077 Wp = 30
55999
YDOT = -3794
982720 meter/sec RA = 4
56319 deg
ZDOT = -4269
234845 TA = 104
70036
MA = 104
54510
Ha = 213
999 n
mi
Hp = 205
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16496182
02 X = -5074480
85
Y = 8409445
27 feet Y = 2506712
34 meter
Z = 12262411
65 Z = 3713044
86
XDOT = -16804
908390 XDOT = -5058
580477
YDOT = -12450
730708 feet/sec YDOT = -3851
905824 meter/sec
ZDOT = -14006
676000 ZDOT = -4293
963563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18551804
90 X = -5654590
13
Y = -1054535
25 feet Y = -321422
34 meter
Z = 12162566
38 Z = 3707150
23
XDOT = -8276
699349 XDOT = -2522
737962
YDOT = -17814
126182 feet/sec YDOT = -5429
745660 meter/sec
ZDOT = -14106
880721 ZDOT = -4299
777244
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 11199
13737194
00016717 00000-0 10270-3 0 9070
2 25544 51
6387 4
9045 0011760 337
7486 22
3158 15
59913995 5740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11199
13737194 = yrday
fracday
Element set: 907
Inclination: 51
6387 deg
RA of node: 4
9045 deg
Eccentricity:
0011760
Arg of perigee: 337
7486 deg
Mean anomaly: 22
3158 deg
Mean motion: 15
59913995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 574
Checksum: 334
Coasting Arc #9 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2011/200/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6725014
00 A = 6772477
43 meter
Y = -454623
13 meter E =
0019822
Z = -508913
34 I = 51
65791
XDOT = 770
490668 Wp = 10
13174
YDOT = 4740
713312 meter/sec RA = 359
55623 deg
ZDOT = 6001
091139 TA = 344
35987
MA = 344
42102
Ha = 214
139 n
mi
Hp = 205
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22063694
21 X = 6732070
02
Y = -1491545
69 feet Y = -379380
43 meter
Z = -1669663
19 Z = -476226
80
XDOT = 2527
856521 XDOT = 688
270222
YDOT = 15553
521364 feet/sec YDOT = 4748
869249 meter/sec
ZDOT = 19688
619223 ZDOT = 6004
634743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19999613
79 X = 6095882
28
Y = 9458995
35 feet Y = 2883101
78 meter
Z = -1536860
83 Z = -468435
18
XDOT = -4789
802486 XDOT = -1459
931798
YDOT = 13296
995715 feet/sec YDOT = 4052
924294 meter/sec
ZDOT = 19702
706590 ZDOT = 6005
384968
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 11200
09832474
00016717 00000-0 10270-3 0 9086
2 25544 51
6388
0719 0011778 341
3299 18
7423 15
59913808 5891
Satellite: ISS
Catalog Number: 25544
Epoch time: 11200
09832474 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node:
0719 deg
Eccentricity:
0011778
Arg of perigee: 341
3299 deg
Mean anomaly: 18
7423 deg
Mean motion: 15
59913808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 321
Coasting Arc #10 (Orbit 604)
---------------------------------------
Vector Time (GMT): 2011/201/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5814228
96 A = 6768636
27 meter
Y = -1808768
45 meter E =
0009997
Z = -2969647
71 I = 51
61632
XDOT = 3896
709698 Wp = 6
50643
YDOT = -4334
859566 meter/sec RA = 354
55483 deg
ZDOT = -4980
931209 TA = 207
49473
MA = 207
54765
Ha = 214
269 n
mi
Hp = 204
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19075554
33 X = -5779145
08
Y = -5934279
71 feet Y = -1873590
35 meter
Z = -9742938
68 Z = -2997807
64
XDOT = 12784
480635 XDOT = 3969
089364
YDOT = -14221
980205 feet/sec YDOT = -4290
879166 meter/sec
ZDOT = -16341
637825 ZDOT = -4961
825797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13956780
45 X = -4254026
68
Y = -14214820
88 feet Y = -4332677
40 meter
Z = -9857202
94 Z = -3004475
46
XDOT = 17037
005214 XDOT = 5192
879189
YDOT = -5431
537044 feet/sec YDOT = -1655
532491 meter/sec
ZDOT = -16263
756050 ZDOT = -4957
192844
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 11201
12333278
00016717 00000-0 10270-3 0 9090
2 25544 51
6398 354
9170 0011880 345
2869 14
7939 15
59940999 6052
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
12333278 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 354
9170 deg
Eccentricity:
0011880
Arg of perigee: 345
2869 deg
Mean anomaly: 14
7939 deg
Mean motion: 15
59940999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 605
Checksum: 336
Coasting Arc #11 (Orbit 620)
---------------------------------------
Vector Time (GMT): 2011/202/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2603274
75 A = 6761264
25 meter
Y = 3618511
66 meter E =
0008846
Z = 5080100
89 I = 51
56219
XDOT = -7001
084917 Wp = 10
53167
YDOT = 2665
669230 meter/sec RA = 349
51295 deg
ZDOT = 1697
001921 TA = 63
13061
MA = 63
04021
Ha = 214
275 n
mi
Hp = 204
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8540927
65 X = 2537940
51
Y = 11871757
42 feet Y = 3647257
43 meter
Z = 16666997
67 Z = 5092588
96
XDOT = -22969
438703 XDOT = -7038
616222
YDOT = 8745
633957 feet/sec YDOT = 2587
168876 meter/sec
ZDOT = 5567
591603 ZDOT = 1662
900137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2078472
33 X = 633518
37
Y = 14418059
62 feet Y = 4394624
57 meter
Z = 16717487
56 Z = 5095490
21
XDOT = -23404
829140 XDOT = -7133
791922
YDOT = -2890
174325 feet/sec YDOT = -880
925134 meter/sec
ZDOT = 5428
911614 ZDOT = 1654
732260
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 11202
14833101
00016717 00000-0 10270-3 0 9105
2 25544 51
6400 349
7626 0011855 348
2778 11
8100 15
59977898 6212
Satellite: ISS
Catalog Number: 25544
Epoch time: 11202
14833101 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 349
7626 deg
Eccentricity:
0011855
Arg of perigee: 348
2778 deg
Mean anomaly: 11
8100 deg
Mean motion: 15
59977898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 621
Checksum: 301
Coasting Arc #12 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2011/203/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1506655
45 A = 6762323
87 meter
Y = -4441169
81 meter E =
0012896
Z = -4877218
01 I = 51
53594
XDOT = 7302
967472 Wp = 49
33039
YDOT = -92
651759 meter/sec RA = 344
44601 deg
ZDOT = 2352
688309 TA = 243
65676
MA = 243
78925
Ha = 214
558 n
mi
Hp = 204
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4943095
32 X = 1579897
87
Y = -14570767
09 feet Y = -4423911
60 meter
Z = -16001371
41 Z = -4869721
17
XDOT = 23959
867033 XDOT = 7292
031940
YDOT = -303
975587 feet/sec YDOT = -11
046839 meter/sec
ZDOT = 7718
793664 ZDOT = 2388
139164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10958967
90 X = 3340293
42
Y = -10845508
41 feet Y = -3305710
96 meter
Z = -15970638
74 Z = -4867850
69
XDOT = 20795
488767 XDOT = 6338
464976
YDOT = 9494
221898 feet/sec YDOT = 2893
838834 meter/sec
ZDOT = 7862
781996 ZDOT = 2396
575952
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 11203
10926165
00016717 00000-0 10270-3 0 9116
2 25544 51
6402 344
9297 0011981 352
4834 7
6140 15
59955663 6364
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
10926165 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 344
9297 deg
Eccentricity:
0011981
Arg of perigee: 352
4834 deg
Mean anomaly: 7
6140 deg
Mean motion: 15
59955663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 304
Coasting Arc #13 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2011/204/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4968639
06 A = 6769977
68 meter
Y = 3915682
02 meter E =
0014883
Z = 2414015
10 I = 51
53308
XDOT = -4772
929939 Wp = 56
59608
YDOT = -2742
227487 meter/sec RA = 339
40744 deg
ZDOT = -5343
968117 TA = 96
31690
MA = 96
14737
Ha = 214
691 n
mi
Hp = 204
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16301309
26 X = -5023782
44
Y = 12846725
78 feet Y = 3859811
15 meter
Z = 7919997
05 Z = 2389744
04
XDOT = -15659
218960 XDOT = -4715
951289
YDOT = -8996
809340 feet/sec YDOT = -2795
282276 meter/sec
ZDOT = -17532
703796 ZDOT = -5367
016627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20265637
91 X = -6176966
43
Y = 4650867
46 feet Y = 1417584
40 meter
Z = 7821173
34 Z = 2383893
63
XDOT = -9893
837040 XDOT = -3015
641530
YDOT = -13292
270765 feet/sec YDOT = -4051
484129 meter/sec
ZDOT = -17626
135761 ZDOT = -5372
446180
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 11204
13424458
00016717 00000-0 10270-3 0 9129
2 25544 51
6404 339
7747 0012012 356
3473 3
7593 15
59970317 6526
Satellite: ISS
Catalog Number: 25544
Epoch time: 11204
13424458 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 339
7747 deg
Eccentricity:
0012012
Arg of perigee: 356
3473 deg
Mean anomaly: 3
7593 deg
Mean motion: 15
59970317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 299
Coasting Arc #14 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2011/205/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6341670
37 A = 6771833
75 meter
Y = -2039796
14 meter E =
0022659
Z = 1132611
69 I = 51
51145
XDOT = 529
692652 Wp = 30
46115
YDOT = 4928
304542 meter/sec RA = 334
40035 deg
ZDOT = 5877
665555 TA = 341
90393
MA = 341
98445
Ha = 214
785 n
mi
Hp = 203
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20806005
14 X = 6358506
46
Y = -6692244
54 feet Y = -1968785
69 meter
Z = 3715917
63 Z = 1163459
98
XDOT = 1737
836784 XDOT = 445
991625
YDOT = 16168
978157 feet/sec YDOT = 4933
759332 meter/sec
ZDOT = 19283
679642 ZDOT = 5880
035941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21697952
74 X = 6613536
00
Y = 2434554
00 feet Y = 742052
06 meter
Z = 3841331
06 Z = 1170837
71
XDOT = -4985
081085 XDOT = -1519
452715
YDOT = 13826
984324 feet/sec YDOT = 4214
464822 meter/sec
ZDOT = 19292
990663 ZDOT = 5880
503554
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 11205
15921947
00016717 00000-0 10270-3 0 9138
2 25544 51
6403 334
6195 0012125
1722 359
9436 15
59967857 6686
Satellite: ISS
Catalog Number: 25544
Epoch time: 11205
15921947 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 334
6195 deg
Eccentricity:
0012125
Arg of perigee:
1722 deg
Mean anomaly: 359
9436 deg
Mean motion: 15
59967857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 668
Checksum: 318
Coasting Arc #15 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2011/206/02:20:17
209
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5278063
64 A = 6764724
79 meter
Y = -746371
05 meter E =
0017049
Z = -4182094
68 I = 51
46219
XDOT = 3714
230850 Wp = 28
85602
YDOT = -5604
318113 meter/sec RA = 329
37370 deg
ZDOT = -3679
028780 TA = 203
24814
MA = 203
32535
Ha = 214
899 n
mi
Hp = 203
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17316481
77 X = -5249009
62
Y = -2448723
90 feet Y = -805230
66 meter
Z = -13720783
08 Z = -4207664
80
XDOT = 12185
796751 XDOT = 3794
495269
YDOT = -18386
870450 feet/sec YDOT = -5562
334136 meter/sec
ZDOT = -12070
304397 ZDOT = -3660
790856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14864933
71 X = -4530831
80
Y = -9057116
72 feet Y = -2760609
18 meter
Z = -13824581
74 Z = -4213732
52
XDOT = 17863
639738 XDOT = 5444
837392
YDOT = -10966
746399 feet/sec YDOT = -3342
664302 meter/sec
ZDOT = -11995
877466 ZDOT = -3656
343452
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 11206
12012418
00016717 00000-0 10270-3 0 9141
2 25544 51
6411 329
7866 0012157 3
7654 356
3591 15
60011500 6830
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
12012418 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 329
7866 deg
Eccentricity:
0012157
Arg of perigee: 3
7654 deg
Mean anomaly: 356
3591 deg
Mean motion: 15
60011500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 275
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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