[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 24th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2741)
---------------------------------------
Vector Time (GMT): 2011/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2965171
13 A = 6726478
78 meter
Y = -3118524
67 meter E =
0003786
Z = 5166950
97 I = 51
32651
XDOT = 4568
821011 Wp = 106
17158
YDOT = 6107
047096 meter/sec RA = 239
59978 deg
ZDOT = 1062
316826 TA = 333
64119
MA = 333
66045
Ha = 193
446 n
mi
Hp = 186
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9728251
74 X = 2974722
59
Y = -10231380
16 feet Y = -3085312
64 meter
Z = 16951938
87 Z = 5181379
13
XDOT = 14989
570246 XDOT = 4495
030742
YDOT = 20036
243753 feet/sec YDOT = 6157
725897 meter/sec
ZDOT = 3485
291423 ZDOT = 1084
332562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9654382
39 X = 2942655
75
Y = -10204568
96 feet Y = -3110352
62 meter
Z = 17010230
04 Z = 5184718
12
XDOT = 14169
957727 XDOT = 4319
003115
YDOT = 19372
880059 feet/sec YDOT = 5904
853842 meter/sec
ZDOT = 3574
086493 ZDOT = 1089
381563
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 11082
54953807
00016717 00000-0 10270-3 0 9000
2 25544 51
6425 240
2576 0001168 25
0727 335
0492 15
71899557 27428
Satellite: ISS
Catalog Number: 25544
Epoch time: 11082
54953807 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 240
2576 deg
Eccentricity:
0001168
Arg of perigee: 25
0727 deg
Mean anomaly: 335
0492 deg
Mean motion: 15
71899557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 312
Coasting Arc #2 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2011/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4761047
98 A = 6736871
65 meter
Y = -4492360
38 meter E =
0009122
Z = -1577414
20 I = 51
37987
XDOT = 2389
603805 Wp = 36
87978
YDOT = -4538
653543 meter/sec RA = 234
43599 deg
ZDOT = 5737
637967 TA = 305
67178
MA = 305
75667
Ha = 193
446 n
mi
Hp = 186
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15620236
16 X = -4702796
94
Y = -14738715
16 feet Y = -4545275
67 meter
Z = -5175243
45 Z = -1600401
61
XDOT = 7839
907498 XDOT = 2412
305995
YDOT = -14890
595612 feet/sec YDOT = -4511
804384 meter/sec
ZDOT = 18824
271545 ZDOT = 5749
301936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15800944
10 X = -4816127
76
Y = -14511480
14 feet Y = -4423099
15 meter
Z = -5267993
60 Z = -1605684
45
XDOT = 6452
396769 XDOT = 1966
690535
YDOT = -13848
026730 feet/sec YDOT = -4220
878547 meter/sec
ZDOT = 18871
426074 ZDOT = 5752
010667
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 11083
50313007
00016717 00000-0 10270-3 0 9010
2 25544 51
6438 235
3761 0001123 30
7844 329
3383 15
71957642 27578
Satellite: ISS
Catalog Number: 25544
Epoch time: 11083
50313007 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 235
3761 deg
Eccentricity:
0001123
Arg of perigee: 30
7844 deg
Mean anomaly: 329
3383 deg
Mean motion: 15
71957642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 292
Coasting Arc #3 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2011/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1096228
99 A = 6727866
32 meter
Y = 4603542
80 meter E =
0012704
Z = -4794245
32 I = 51
36874
XDOT = -6064
992787 Wp = 68
62372
YDOT = -4022
405910 meter/sec RA = 229
33242 deg
ZDOT = -2476
325836 TA = 177
02684
MA = 177
01928
Ha = 193
433 n
mi
Hp = 186
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3596551
80 X = -1124335
82
Y = 15103486
87 feet Y = 4591126
78 meter
Z = -15729151
33 Z = -4799639
19
XDOT = -19898
270299 XDOT = -6007
533267
YDOT = -13196
869785 feet/sec YDOT = -4089
907145 meter/sec
ZDOT = -8124
428596 ZDOT = -2505
649627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3022054
72 X = -921122
28
Y = 15206254
21 feet Y = 4634866
28 meter
Z = -15750991
08 Z = -4800902
08
XDOT = -19148
685219 XDOT = -5836
519255
YDOT = -12341
211217 feet/sec YDOT = -3761
601179 meter/sec
ZDOT = -8242
782765 ZDOT = -2512
400187
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 11084
52026829
00016717 00000-0 10270-3 0 9027
2 25544 51
6439 230
1694 0001249 31
0682 329
0554 15
72011597 27736
Satellite: ISS
Catalog Number: 25544
Epoch time: 11084
52026829 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 230
1694 deg
Eccentricity:
0001249
Arg of perigee: 31
0682 deg
Mean anomaly: 329
0554 deg
Mean motion: 15
72011597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 297
Coasting Arc #4 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2011/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5643968
41 A = 6734503
41 meter
Y = 2454601
20 meter E =
0014092
Z = 2719595
31 I = 51
41168
XDOT =
654831 Wp = 96
36156
YDOT = 5725
959209 meter/sec RA = 224
15093 deg
ZDOT = -5148
106620 TA = 52
50160
MA = 52
37357
Ha = 193
351 n
mi
Hp = 186
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18516956
72 X = 5602889
97
Y = 8053153
55 feet Y = 2517485
90 meter
Z = 8922556
81 Z = 2746913
51
XDOT = 2
148396 XDOT = -38
365707
YDOT = 18785
955411 feet/sec YDOT = 5725
748158 meter/sec
ZDOT = -16890
113583 ZDOT = -5148
198439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18834807
50 X = 5740849
32
Y = 7141476
75 feet Y = 2176722
11 meter
Z = 9032846
98 Z = 2753211
76
XDOT = 1541
985521 XDOT = 469
997187
YDOT = 17384
325426 feet/sec YDOT = 5298
742390 meter/sec
ZDOT = -16890
553922 ZDOT = -5148
240835
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 11085
53737878
00016717 00000-0 10270-3 0 9033
2 25544 51
6433 224
9608 0001200 33
7899 326
3340 15
72029688 27892
Satellite: ISS
Catalog Number: 25544
Epoch time: 11085
53737878 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 224
9608 deg
Eccentricity:
0001200
Arg of perigee: 33
7899 deg
Mean anomaly: 326
3340 deg
Mean motion: 15
72029688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 329
Coasting Arc #5 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2011/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1135508
63 A = 6730115
49 meter
Y = -5175856
80 meter E =
0010819
Z = 4141083
09 I = 51
42140
XDOT = 6575
823006 Wp = 98
85549
YDOT = 1530
041753 meter/sec RA = 219
06288 deg
ZDOT = 3705
626016 TA = 313
11261
MA = 313
20307
Ha = 193
278 n
mi
Hp = 186
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3725422
00 X = -1097663
15
Y = -16981157
49 feet Y = -5188342
93 meter
Z = 13586230
62 Z = 4135659
06
XDOT = 21574
222459 XDOT = 6540
224060
YDOT = 5019
822025 feet/sec YDOT = 1603
377736 meter/sec
ZDOT = 12157
565668 ZDOT = 3737
484342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4919890
32 X = -1499582
57
Y = -16692104
93 feet Y = -5087753
58 meter
Z = 13564381
80 Z = 4134423
57
XDOT = 20568
534459 XDOT = 6269
289303
YDOT = 3947
972975 feet/sec YDOT = 1203
342163 meter/sec
ZDOT = 12286
216548 ZDOT = 3744
838804
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 11086
55445895
00016717 00000-0 10270-3 0 9042
2 25544 51
6444 219
7531 0001219 31
8556 328
2680 15
72117161 28051
Satellite: ISS
Catalog Number: 25544
Epoch time: 11086
55445895 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 219
7531 deg
Eccentricity:
0001219
Arg of perigee: 31
8556 deg
Mean anomaly: 328
2680 deg
Mean motion: 15
72117161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 307
Coasting Arc #6 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2011/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5623789
95 A = 6731504
43 meter
Y = -226274
04 meter E =
0006519
Z = -3698286
01 I = 51
45108
XDOT = -2578
533275 Wp = 91
25082
YDOT = -5843
738677 meter/sec RA = 213
87703 deg
ZDOT = 4284
943351 TA = 224
14861
MA = 224
20065
Ha = 193
274 n
mi
Hp = 186
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18450754
42 X = -5602876
42
Y = -742368
91 feet Y = -289045
99 meter
Z = -12133484
27 Z = -3725555
12
XDOT = -8459
754840 XDOT = -2533
810981
YDOT = -19172
370989 feet/sec YDOT = -5872
323051 meter/sec
ZDOT = 14058
213093 ZDOT = 4272
526067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18375915
73 X = -5600979
11
Y = 788821
95 feet Y = 240432
93 meter
Z = -12243625
76 Z = -3731857
13
XDOT = -10051
732839 XDOT = -3063
768169
YDOT = -17054
470072 feet/sec YDOT = -5198
202478 meter/sec
ZDOT = 14008
116144 ZDOT = 4269
673801
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 11087
50794783
00016717 00000-0 10270-3 0 9052
2 25544 51
6446 214
8713 0001406 31
2107 328
9139 15
72115757 28207
Satellite: ISS
Catalog Number: 25544
Epoch time: 11087
50794783 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 214
8713 deg
Eccentricity:
0001406
Arg of perigee: 31
2107 deg
Mean anomaly: 328
9139 deg
Mean motion: 15
72115757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 303
Coasting Arc #7 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2011/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3303713
03 A = 6732649
59 meter
Y = 4836419
06 meter E =
0005603
Z = -3325706
58 I = 51
48160
XDOT = -6041
895099 Wp = 82
00061
YDOT = 920
335864 meter/sec RA = 208
79430 deg
ZDOT = -4669
478025 TA = 137
12943
MA = 137
08573
Ha = 193
271 n
mi
Hp = 186
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10838953
52 X = 3265541
17
Y = 15867516
59 feet Y = 4873149
46 meter
Z = -10911110
83 Z = -3309750
53
XDOT = -19822
490483 XDOT = -6029
054294
YDOT = 3019
474619 feet/sec YDOT = 852
843122 meter/sec
ZDOT = -15319
809793 ZDOT = -4698
797978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12441013
41 X = 3792020
89
Y = 14692978
96 feet Y = 4478419
99 meter
Z = -10846699
53 Z = -3306074
02
XDOT = -18256
593793 XDOT = -5564
609788
YDOT = 4076
032875 feet/sec YDOT = 1242
374820 meter/sec
ZDOT = -15438
255258 ZDOT = -4705
580203
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 11088
52497395
00016717 00000-0 10270-3 0 9065
2 25544 51
6450 209
6627 0001404 36
3178 323
8080 15
72169862 28362
Satellite: ISS
Catalog Number: 25544
Epoch time: 11088
52497395 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 209
6627 deg
Eccentricity:
0001404
Arg of perigee: 36
3178 deg
Mean anomaly: 323
8080 deg
Mean motion: 15
72169862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 321
Coasting Arc #8 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2011/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4754450
22 A = 6728722
11 meter
Y = -1758285
84 meter E =
0010549
Z = 4419141
28 I = 51
49684
XDOT = 4886
979907 Wp = 64
78491
YDOT = 4974
024544 meter/sec RA = 203
61371 deg
ZDOT = -3268
234040 TA = 58
10699
MA = 58
00440
Ha = 193
200 n
mi
Hp = 186
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15598589
97 X = 4752291
24
Y = -5768654
34 feet Y = -1705130
32 meter
Z = 14498495
03 Z = 4442233
02
XDOT = 16033
398645 XDOT = 4846
872484
YDOT = 16318
978162 feet/sec YDOT = 5028
449132 meter/sec
ZDOT = -10722
552626 ZDOT = -3244
591341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14726875
16 X = 4488751
55
Y = -7549729
97 feet Y = -2301157
70 meter
Z = 14591794
45 Z = 4447578
95
XDOT = 17351
686473 XDOT = 5288
794037
YDOT = 13241
394607 feet/sec YDOT = 4035
977076 meter/sec
ZDOT = -10627
080590 ZDOT = -3239
134164
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 11089
54197214
00016717 00000-0 10270-3 0 9076
2 25544 51
6455 204
4549 0001593 41
7821 318
3463 15
72195815 28526
Satellite: ISS
Catalog Number: 25544
Epoch time: 11089
54197214 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 204
4549 deg
Eccentricity:
0001593
Arg of perigee: 41
7821 deg
Mean anomaly: 318
3463 deg
Mean motion: 15
72195815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 316
Coasting Arc #9 (Orbit 2867)
---------------------------------------
Vector Time (GMT): 2011/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5107686
94 A = 6734734
01 meter
Y = -3687816
88 meter E =
0015381
Z = 2359478
67 I = 51
54680
XDOT = 4637
591970 Wp = 70
23370
YDOT = -2959
829339 meter/sec RA = 198
52746 deg
ZDOT = 5389
807603 TA = 316
37351
MA = 316
49502
Ha = 193
230 n
mi
Hp = 186
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16757503
08 X = -5077531
26
Y = -12099136
76 feet Y = -3744765
26 meter
Z = 7741071
76 Z = 2334739
44
XDOT = 15215
196752 XDOT = 4644
162215
YDOT = -9710
726178 feet/sec YDOT = -2907
931634 meter/sec
ZDOT = 17683
095812 ZDOT = 5412
353086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18278107
64 X = -5571167
21
Y = -9728864
66 feet Y = -2965357
95 meter
Z = 7641150
77 Z = 2329022
75
XDOT = 12956
422959 XDOT = 3949
117718
YDOT = -10321
075777 feet/sec YDOT = -3145
863897 meter/sec
ZDOT = 17774
201738 ZDOT = 5417
576690
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 11090
55893906
00016717 00000-0 10270-3 0 9081
2 25544 51
6462 199
2462 0001648 41
3167 318
8120 15
72277479 28688
Satellite: ISS
Catalog Number: 25544
Epoch time: 11090
55893906 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 199
2462 deg
Eccentricity:
0001648
Arg of perigee: 41
3167 deg
Mean anomaly: 318
8120 deg
Mean motion: 15
72277479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2868
Checksum: 333
Coasting Arc #10 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2011/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3223591
01 A = 6726296
01 meter
Y = 3260752
23 meter E =
0013629
Z = -4933554
60 I = 51
54879
XDOT = -6604
112404 Wp = 99
27224
YDOT = -3308
269845 meter/sec RA = 193
36223 deg
ZDOT = 2131
431183 TA = 191
44585
MA = 191
47688
Ha = 193
131 n
mi
Hp = 185
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10576085
99 X = -3235847
59
Y = 10698006
00 feet Y = 3224634
98 meter
Z = -16186202
75 Z = -4949244
86
XDOT = -21667
035446 XDOT = -6576
981914
YDOT = -10853
903691 feet/sec YDOT = -3381
969096 meter/sec
ZDOT = 6992
884460 ZDOT = 2099
414878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8737161
34 X = -2663086
78
Y = 12161661
48 feet Y = 3706874
42 meter
Z = -16249618
10 Z = -4952883
60
XDOT = -22215
567684 XDOT = -6771
305030
YDOT = -6801
853662 feet/sec YDOT = -2073
204996 meter/sec
ZDOT = 6863
552069 ZDOT = 2092
010671
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 11091
51232132
00016717 00000-0 10270-3 0 9097
2 25544 51
6464 194
3642 0001753 42
0636 318
0661 15
72335688 28838
Satellite: ISS
Catalog Number: 25544
Epoch time: 11091
51232132 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 194
3642 deg
Eccentricity:
0001753
Arg of perigee: 42
0636 deg
Mean anomaly: 318
0661 deg
Mean motion: 15
72335688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 299
Coasting Arc #11 (Orbit 2898)
---------------------------------------
Vector Time (GMT): 2011/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6278043
36 A = 6736105
25 meter
Y = 2010604
13 meter E =
0008749
Z = -1372268
28 I = 51
61156
XDOT = -2637
849797 Wp = 131
69942
YDOT = 4280
668165 meter/sec RA = 188
26541 deg
ZDOT = -5825
623065 TA = 63
37106
MA = 63
28146
Ha = 193
157 n
mi
Hp = 185
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20597255
10 X = 6261760
02
Y = 6596470
25 feet Y = 2080717
82 meter
Z = -4502192
53 Z = -1341809
38
XDOT = -8654
362852 XDOT = -2657
221204
YDOT = 14044
186892 feet/sec YDOT = 4251
061158 meter/sec
ZDOT = -19112
936564 ZDOT = -5838
485256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21440423
38 X = 6535041
05
Y = 3026794
38 feet Y = 922566
93 meter
Z = -4379136
45 Z = -1334760
79
XDOT = -5830
660225 XDOT = -1777
185237
YDOT = 13718
149487 feet/sec YDOT = 4181
291964 meter/sec
ZDOT = -19164
935587 ZDOT = -5841
472367
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 11092
52923458
00016717 00000-0 10270-3 0 9109
2 25544 51
6462 189
1555 0001751 43
8870 316
2431 15
72347924 28996
Satellite: ISS
Catalog Number: 25544
Epoch time: 11092
52923458 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 189
1555 deg
Eccentricity:
0001751
Arg of perigee: 43
8870 deg
Mean anomaly: 316
2431 deg
Mean motion: 15
72347924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2899
Checksum: 319
Coasting Arc #12 (Orbit 2914)
---------------------------------------
Vector Time (GMT): 2011/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1316619
46 A = 6724854
14 meter
Y = -4053797
07 meter E =
0005264
Z = 5198465
24 I = 51
60553
XDOT = 7545
946540 Wp = 53
00858
YDOT = 1189
070967 meter/sec RA = 183
11936 deg
ZDOT = -980
130247 TA = 46
35801
MA = 46
31437
Ha = 192
977 n
mi
Hp = 185
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4319617
65 X = 1336598
66
Y = -13299859
16 feet Y = -4038961
58 meter
Z = 17055332
16 Z = 5204910
35
XDOT = 24757
042454 XDOT = 7536
850596
YDOT = 3901
151465 feet/sec YDOT = 1273
403358 meter/sec
ZDOT = -3215
650418 ZDOT = -943
494163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1678233
57 X = 511525
59
Y = -13850590
61 feet Y = -4221660
02 meter
Z = 17081404
43 Z = 5206412
07
XDOT = 24059
527680 XDOT = 7333
344037
YDOT = -883
281838 feet/sec YDOT = -269
224304 meter/sec
ZDOT = -3067
621047 ZDOT = -935
010895
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 11093
54611777
00016717 00000-0 10270-3 0 9111
2 25544 51
6466 183
9464 0001843 42
2184 317
9120 15
72431806 29159
Satellite: ISS
Catalog Number: 25544
Epoch time: 11093
54611777 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 183
9464 deg
Eccentricity:
0001843
Arg of perigee: 42
2184 deg
Mean anomaly: 317
9120 deg
Mean motion: 15
72431806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2915
Checksum: 304
Coasting Arc #13 (Orbit 2930)
---------------------------------------
Vector Time (GMT): 2011/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6720653
23 A = 6736648
35 meter
Y = -37618
60 meter E =
0014851
Z = 343047
07 I = 51
67525
XDOT = 342
452708 Wp = 48
24568
YDOT = -4779
463665 meter/sec RA = 178
00836 deg
ZDOT = 6027
769252 TA = 315
47997
MA = 315
59919
Ha = 193
114 n
mi
Hp = 185
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22049387
24 X = -6721399
55
Y = -123420
62 feet Y = -112777
17 meter
Z = 1125482
53 Z = 310396
14
XDOT = 1123
532505 XDOT = 366
590135
YDOT = -15680
655068 feet/sec YDOT = -4775
498635 meter/sec
ZDOT = 19776
145839 ZDOT = 6029
491968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21624612
45 X = -6591181
87
Y = 4341248
46 feet Y = 1323212
53 meter
Z = 993538
94 Z = 302830
67
XDOT = -1871
212030 XDOT = -570
345427
YDOT = -13982
093121 feet/sec YDOT = -4261
741983 meter/sec
ZDOT = 19783
144871 ZDOT = 6029
902557
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 11094
56297585
00016717 00000-0 10270-3 0 9122
2 25544 51
6462 178
7380 0002049 45
3468 314
7861 15
72417806 29311
Satellite: ISS
Catalog Number: 25544
Epoch time: 11094
56297585 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 178
7380 deg
Eccentricity:
0002049
Arg of perigee: 45
3468 deg
Mean anomaly: 314
7861 deg
Mean motion: 15
72417806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2931
Checksum: 327
Coasting Arc #14 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2011/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 693076
90 A = 6724508
98 meter
Y = 4122344
93 meter E =
0016551
Z = -5281508
15 I = 51
66421
XDOT = -7609
130105 Wp = 84
21913
YDOT = 1075
485038 meter/sec RA = 172
88584 deg
ZDOT = -157
870876 TA = 184
27335
MA = 184
28750
Ha = 193
048 n
mi
Hp = 185
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2273874
34 X = 672585
36
Y = 13524753
72 feet Y = 4129980
37 meter
Z = -17327782
66 Z = -5278191
24
XDOT = -24964
337616 XDOT = -7619
823937
YDOT = 3528
494219 feet/sec YDOT = 990
335325 meter/sec
ZDOT = -517
949068 ZDOT = -194
862383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5283189
59 X = 1610316
19
Y = 12674403
00 feet Y = 3863158
03 meter
Z = -17314414
10 Z = -5277433
42
XDOT = -22656
757227 XDOT = -6905
779603
YDOT = 8526
990572 feet/sec YDOT = 2599
026726 meter/sec
ZDOT = -667
454676 ZDOT = -203
440185
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 11095
51625194
00016717 00000-0 10270-3 0 9130
2 25544 51
6451 173
8547 0001989 46
3270 313
8057 15
72460544 29464
Satellite: ISS
Catalog Number: 25544
Epoch time: 11095
51625194 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 173
8547 deg
Eccentricity:
0001989
Arg of perigee: 46
3270 deg
Mean anomaly: 313
8057 deg
Mean motion: 15
72460544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 318
Coasting Arc #15 (Orbit 2961)
---------------------------------------
Vector Time (GMT): 2011/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6433543
36 A = 6736199
63 meter
Y = -1883087
38 meter E =
0013978
Z = 603689
67 I = 51
73398
XDOT = 1872
087961 Wp = 119
88757
YDOT = 4440
157341 meter/sec RA = 167
75880 deg
ZDOT = -6004
308709 TA = 53
55275
MA = 53
42398
Ha = 193
051 n
mi
Hp = 185
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21107425
73 X = 6451189
60
Y = -6178108
19 feet Y = -1811044
89 meter
Z = 1980609
17 Z = 634987
07
XDOT = 6142
020871 XDOT = 1851
466241
YDOT = 14567
445343 feet/sec YDOT = 4460
976527 meter/sec
ZDOT = -19699
175554 ZDOT = -5995
264364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19042711
63 X = 5804218
51
Y = -10979545
45 feet Y = -3346565
45 meter
Z = 2107123
55 Z = 642251
26
XDOT = 8718
430126 XDOT = 2657
377503
YDOT = 11290
472767 feet/sec YDOT = 3441
336099 meter/sec
ZDOT = -19662
664650 ZDOT = -5993
180185
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 11096
53305383
00016717 00000-0 10270-3 0 9149
2 25544 51
6446 168
6451 0002194 51
6361 308
4998 15
72525129 29626
Satellite: ISS
Catalog Number: 25544
Epoch time: 11096
53305383 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 168
6451 deg
Eccentricity:
0002194
Arg of perigee: 51
6361 deg
Mean anomaly: 308
4998 deg
Mean motion: 15
72525129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2962
Checksum: 319
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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