[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 9th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 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 3433)
---------------------------------------
Vector Time (GMT): 2011/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6544281
90 A = 6729721
32 meter
Y = 456294
21 meter E =
0005878
Z = -1488202
77 I = 51
75183
XDOT = 969
968613 Wp = 27
22488
YDOT = 4967
047119 meter/sec RA = 14
28981 deg
ZDOT = 5802
410576 TA = 316
41315
MA = 316
45957
Ha = 188
545 n
mi
Hp = 183
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21470741
15 X = 6545922
64
Y = 1497028
26 feet Y = 529485
63 meter
Z = -4882555
03 Z = -1456406
29
XDOT = 3182
311721 XDOT = 886
166693
YDOT = 16296
086348 feet/sec YDOT = 4977
424885 meter/sec
ZDOT = 19036
780105 ZDOT = 5806
919561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16694414
11 X = 5088457
42
Y = -13629747
93 feet Y = -4154347
17 meter
Z = -4753911
17 Z = -1448992
12
XDOT = 12400
738402 XDOT = 3779
745065
YDOT = 8559
526339 feet/sec YDOT = 2608
943628 meter/sec
ZDOT = 19054
775315 ZDOT = 5807
895516
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 11126
50281532
00016717 00000-0 10270-3 0 9004
2 25544 51
6481 14
8127 0002878 237
0727 123
0160 15
74540090 34345
Satellite: ISS
Catalog Number: 25544
Epoch time: 11126
50281532 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 14
8127 deg
Eccentricity:
0002878
Arg of perigee: 237
0727 deg
Mean anomaly: 123
0160 deg
Mean motion: 15
74540090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 273
Coasting Arc #2 (Orbit 3449)
---------------------------------------
Vector Time (GMT): 2011/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -965289
60 A = 6718994
15 meter
Y = -4254160
65 meter E =
0011193
Z = -5120119
47 I = 51
68621
XDOT = 7552
725389 Wp = 82
75936
YDOT = 48
063262 meter/sec RA = 9
18164 deg
ZDOT = -1465
180847 TA = 173
20150
MA = 173
18631
Ha = 188
282 n
mi
Hp = 183
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3166960
62 X = -892774
24
Y = -13957219
98 feet Y = -4264549
24 meter
Z = -16798292
23 Z = -5124633
07
XDOT = 24779
282771 XDOT = 7558
744226
YDOT = 157
687867 feet/sec YDOT = 132
556188 meter/sec
ZDOT = -4807
023775 ZDOT = -1428
474840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11928869
04 X = -3635919
28
Y = -7869501
13 feet Y = -2398623
94 meter
Z = -16816339
86 Z = -5125620
39
XDOT = 17321
623071 XDOT = 5279
630712
YDOT = -16311
390233 feet/sec YDOT = -4971
711743 meter/sec
ZDOT = -4658
490676 ZDOT = -1419
907958
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 11127
51828469
00016717 00000-0 10270-3 0 9013
2 25544 51
6478 9
5938 0002952 243
8455 116
2408 15
74621217 34506
Satellite: ISS
Catalog Number: 25544
Epoch time: 11127
51828469 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 9
5938 deg
Eccentricity:
0002952
Arg of perigee: 243
8455 deg
Mean anomaly: 116
2408 deg
Mean motion: 15
74621217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3450
Checksum: 313
Coasting Arc #3 (Orbit 3465)
---------------------------------------
Vector Time (GMT): 2011/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6630094
84 A = 6729924
05 meter
Y = 365982
51 meter E =
0012483
Z = 1050997
33 I = 51
69249
XDOT = -1207
845525 Wp = 135
83884
YDOT = -4775
752191 meter/sec RA = 4
02321 deg
ZDOT = -5923
349503 TA = 32
66942
MA = 32
59226
Ha = 188
239 n
mi
Hp = 183
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21752279
65 X = -6638800
13
Y = 1200730
01 feet Y = 291792
01 meter
Z = 3448153
96 Z = 1018767
11
XDOT = -3962
747787 XDOT = -1125
577736
YDOT = -15668
478316 feet/sec YDOT = -4788
798642 meter/sec
ZDOT = -19433
561362 ZDOT = -5929
017749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14494451
69 X = -4417908
88
Y = 16291005
38 feet Y = 4965498
44 meter
Z = 3317710
35 Z = 1011238
11
XDOT = -12638
257043 XDOT = -3852
140747
YDOT = -7259
166263 feet/sec YDOT = -2212
593877 meter/sec
ZDOT = -19456
253975 ZDOT = -5930
266212
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 11128
53370797
00016717 00000-0 10270-3 0 9023
2 25544 51
6478 4
3750 0003046 244
6134 115
4715 15
74636446 34668
Satellite: ISS
Catalog Number: 25544
Epoch time: 11128
53370797 = yrday
fracday
Element set: 902
Inclination: 51
6478 deg
RA of node: 4
3750 deg
Eccentricity:
0003046
Arg of perigee: 244
6134 deg
Mean anomaly: 115
4715 deg
Mean motion: 15
74636446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3466
Checksum: 305
Coasting Arc #4 (Orbit 3481)
---------------------------------------
Vector Time (GMT): 2011/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1107844
07 A = 6718232
82 meter
Y = 4101361
03 meter E =
0002671
Z = 5204850
97 I = 51
62339
XDOT = -7596
323137 Wp = 181
48391
YDOT = 876
971265 meter/sec RA = 358
90100 deg
ZDOT = 923
209162 TA = 259
70632
MA = 259
73643
Ha = 187
901 n
mi
Hp = 183
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3634659
03 X = 1036615
29
Y = 13455908
88 feet Y = 4113351
05 meter
Z = 17076282
72 Z = 5210060
11
XDOT = -24922
320004 XDOT = -7610
049804
YDOT = 2877
202312 feet/sec YDOT = 791
947766 meter/sec
ZDOT = 3028
901449 ZDOT = 886
272912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12153606
66 X = 3704419
31
Y = 6771179
64 feet Y = 2063855
55 meter
Z = 17097152
78 Z = 5211212
17
XDOT = -14702
562726 XDOT = -4481
341119
YDOT = 19097
623609 feet/sec YDOT = 5820
955676 meter/sec
ZDOT = 2879
388103 ZDOT = 877
637494
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 11129
54908087
00016717 00000-0 10270-3 0 9035
2 25544 51
6477 359
1552 0003110 252
6431 107
4393 15
74742218 34825
Satellite: ISS
Catalog Number: 25544
Epoch time: 11129
54908087 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 359
1552 deg
Eccentricity:
0003110
Arg of perigee: 252
6431 deg
Mean anomaly: 107
4393 deg
Mean motion: 15
74742218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3482
Checksum: 304
Coasting Arc #5 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2011/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6604461
35 A = 6729716
91 meter
Y = -1148629
18 meter E =
0008793
Z = -533368
26 I = 51
63154
XDOT = 1288
954955 Wp = 27
77892
YDOT = 4643
519539 meter/sec RA = 353
74546 deg
ZDOT = 6007
754695 TA = 326
41505
MA = 326
47076
Ha = 187
712 n
mi
Hp = 183
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21668180
28 X = 6619405
69
Y = -3768468
45 feet Y = -1074690
51 meter
Z = -1749895
87 Z = -501247
53
XDOT = 4228
854840 XDOT = 1207
749842
YDOT = 15234
644156 feet/sec YDOT = 4657
479131 meter/sec
ZDOT = 19710
481283 ZDOT = 6013
819379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11978824
16 X = 3651145
61
Y = -18456905
46 feet Y = -5625664
78 meter
Z = -1619857
76 Z = -493732
65
XDOT = 12619
936411 XDOT = 3846
556618
YDOT = 6473
210140 feet/sec YDOT = 1973
034451 meter/sec
ZDOT = 19734
787139 ZDOT = 6015
163120
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 11130
50095011
00016717 00000-0 10270-3 0 9048
2 25544 51
6472 354
2612 0003283 258
4380 101
6415 15
74826202 34974
Satellite: ISS
Catalog Number: 25544
Epoch time: 11130
50095011 = yrday
fracday
Element set: 904
Inclination: 51
6472 deg
RA of node: 354
2612 deg
Eccentricity:
0003283
Arg of perigee: 258
4380 deg
Mean anomaly: 101
6415 deg
Mean motion: 15
74826202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 276
Coasting Arc #6 (Orbit 3512)
---------------------------------------
Vector Time (GMT): 2011/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1105253
27 A = 6717526
70 meter
Y = -4038623
79 meter E =
0011690
Z = -5262947
11 I = 51
55982
XDOT = 7495
477360 Wp = 89
36335
YDOT = -1717
870204 meter/sec RA = 348
60691 deg
ZDOT = -256
219470 TA = 178
20204
MA = 178
19783
Ha = 187
501 n
mi
Hp = 183
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3626159
01 X = -1034443
96
Y = -13250078
06 feet Y = -4050587
37 meter
Z = -17266886
85 Z = -5268144
54
XDOT = 24591
461156 XDOT = 7515
374500
YDOT = -5636
057099 feet/sec YDOT = -1633
939968 meter/sec
ZDOT = -840
615058 ZDOT = -219
758079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12219593
84 X = -3724532
20
Y = -6218955
50 feet Y = -1895537
64 meter
Z = -17287715
24 Z = -5269295
61
XDOT = 11762
258369 XDOT = 3585
136351
YDOT = -21188
491816 feet/sec YDOT = -6458
252305 meter/sec
ZDOT = -692
988361 ZDOT = -211
222852
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 11131
51623144
00016717 00000-0 10270-3 0 9055
2 25544 51
6462 349
0404 0003372 263
4213 96
6572 15
74907661 35139
Satellite: ISS
Catalog Number: 25544
Epoch time: 11131
51623144 = yrday
fracday
Element set: 905
Inclination: 51
6462 deg
RA of node: 349
0404 deg
Eccentricity:
0003372
Arg of perigee: 263
4213 deg
Mean anomaly: 96
6572 deg
Mean motion: 15
74907661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3513
Checksum: 288
Coasting Arc #7 (Orbit 3528)
---------------------------------------
Vector Time (GMT): 2011/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6468713
86 A = 6729486
54 meter
Y = 1830545
67 meter E =
0010091
Z = -109410
55 I = 51
57072
XDOT = -1213
136462 Wp = 150
84453
YDOT = -4633
116852 meter/sec RA = 343
45944 deg
ZDOT = -6033
056045 TA = 30
34572
MA = 30
28734
Ha = 187
377 n
mi
Hp = 183
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21222814
50 X = -6488171
10
Y = 6005727
27 feet Y = 1758099
80 meter
Z = -358958
51 Z = -140882
99
XDOT = -3980
106501 XDOT = -1131
930233
YDOT = -15200
514607 feet/sec YDOT = -4646
228754 meter/sec
ZDOT = -19793
490962 ZDOT = -6038
752305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9345532
53 X = -2848518
31
Y = 19975732
94 feet Y = 6088603
40 meter
Z = -486397
06 Z = -148253
82
XDOT = -12564
711915 XDOT = -3829
724192
YDOT = -6346
628653 feet/sec YDOT = -1934
452414 meter/sec
ZDOT = -19816
308445 ZDOT = -6040
010814
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 11132
53146592
00016717 00000-0 10270-3 0 9066
2 25544 51
6464 343
8210 0003469 266
1621 93
9146 15
74942599 35291
Satellite: ISS
Catalog Number: 25544
Epoch time: 11132
53146592 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 343
8210 deg
Eccentricity:
0003469
Arg of perigee: 266
1621 deg
Mean anomaly: 93
9146 deg
Mean motion: 15
74942599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3529
Checksum: 321
Coasting Arc #8 (Orbit 3544)
---------------------------------------
Vector Time (GMT): 2011/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 998436
17 A = 6717281
71 meter
Y = 4086651
84 meter E =
0001563
Z = 5237758
66 I = 51
50045
XDOT = -7283
387889 Wp = 320
72119
YDOT = 2450
670690 meter/sec RA = 338
30242 deg
ZDOT = -522
599255 TA = 134
25875
MA = 134
24593
Ha = 187
198 n
mi
Hp = 183
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3275709
22 X = 927219
88
Y = 13407650
38 feet Y = 4097418
69 meter
Z = 17184247
58 Z = 5242436
19
XDOT = -23895
629557 XDOT = -7307
711716
YDOT = 8040
258170 feet/sec YDOT = 2369
087429 meter/sec
ZDOT = -1714
564484 ZDOT = -558
041378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12322755
74 X = 3755975
95
Y = 6164515
44 feet Y = 1878944
31 meter
Z = 17202969
65 Z = 5243465
15
XDOT = -8698
839719 XDOT = -2651
406346
YDOT = 22584
203051 feet/sec YDOT = 6883
665090 meter/sec
ZDOT = -1858
089398 ZDOT = -566
345649
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 11133
54665145
00016717 00000-0 10270-3 0 9079
2 25544 51
6457 338
5995 0003562 271
4153 88
6603 15
75023936 35450
Satellite: ISS
Catalog Number: 25544
Epoch time: 11133
54665145 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 338
5995 deg
Eccentricity:
0003562
Arg of perigee: 271
4153 deg
Mean anomaly: 88
6603 deg
Mean motion: 15
75023936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3545
Checksum: 323
Coasting Arc #9 (Orbit 3560)
---------------------------------------
Vector Time (GMT): 2011/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6220178
31 A = 6728691
74 meter
Y = -2412299
42 meter E =
0011113
Z = 824810
30 I = 51
51033
XDOT = 1056
193236 Wp = 41
18457
YDOT = 4772
208939 meter/sec RA = 333
16128 deg
ZDOT = 5954
916367 TA = 327
83411
MA = 327
90186
Ha = 187
066 n
mi
Hp = 183
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20407409
17 X = 6242683
96
Y = -7914368
16 feet Y = -2342615
79 meter
Z = 2706070
53 Z = 855082
99
XDOT = 3465
200906 XDOT = 973
822629
YDOT = 15656
853474 feet/sec YDOT = 4783
559204 meter/sec
ZDOT = 19537
127187 ZDOT = 5959
847487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6646746
35 X = 2025928
29
Y = -20838468
38 feet Y = -6351565
16 meter
Z = 2828672
59 Z = 862179
40
XDOT = 12767
976153 XDOT = 3891
679132
YDOT = 6743
052140 feet/sec YDOT = 2055
282292 meter/sec
ZDOT = 19556
838910 ZDOT = 5960
924500
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 11134
56178869
00016717 00000-0 10270-3 0 9085
2 25544 51
6444 333
3773 0003667 275
7576 84
3169 15
75113121 35619
Satellite: ISS
Catalog Number: 25544
Epoch time: 11134
56178869 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 333
3773 deg
Eccentricity:
0003667
Arg of perigee: 275
7576 deg
Mean anomaly: 84
3169 deg
Mean motion: 15
75113121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3561
Checksum: 328
Coasting Arc #10 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2011/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -835740
94 A = 6717393
98 meter
Y = -4284917
79 meter E =
0010340
Z = -5114458
88 I = 51
44487
XDOT = 6937
144096 Wp = 101
13333
YDOT = -3022
395435 meter/sec RA = 327
98439 deg
ZDOT = 1399
017461 TA = 182
30760
MA = 182
31237
Ha = 186
989 n
mi
Hp = 183
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2741932
22 X = -762918
47
Y = -14058129
24 feet Y = -4293856
11 meter
Z = -16779720
74 Z = -5118342
33
XDOT = 22759
659109 XDOT = 6963
629212
YDOT = -9915
995521 feet/sec YDOT = -2944
672067 meter/sec
ZDOT = 4589
952300 ZDOT = 1432
782906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12714128
60 X = -3875266
40
Y = -6555905
00 feet Y = -1998239
84 meter
Z = -16795215
44 Z = -5119181
67
XDOT = 5668
815814 XDOT = 1727
855060
YDOT = -23099
330582 feet/sec YDOT = -7040
675962 meter/sec
ZDOT = 4726
713839 ZDOT = 1440
702378
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 11135
51343657
00016717 00000-0 10270-3 0 9091
2 25544 51
6434 328
4812 0003644 279
4892 80
5860 15
75190330 35763
Satellite: ISS
Catalog Number: 25544
Epoch time: 11135
51343657 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 328
4812 deg
Eccentricity:
0003644
Arg of perigee: 279
4892 deg
Mean anomaly: 80
5860 deg
Mean motion: 15
75190330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3576
Checksum: 318
Coasting Arc #11 (Orbit 3591)
---------------------------------------
Vector Time (GMT): 2011/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5881422
16 A = 6727335
75 meter
Y = 2818007
62 meter E =
0005280
Z = -1638198
80 I = 51
45390
XDOT = -843
278080 Wp = 167
37057
YDOT = -5082
469381 meter/sec RA = 322
85416 deg
ZDOT = -5723
815838 TA = 30
77892
MA = 30
74797
Ha = 186
890 n
mi
Hp = 183
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19296004
46 X = -5904538
31
Y = 9245431
83 feet Y = 2752108
88 meter
Z = -5374667
98 Z = -1666827
21
XDOT = -2766
660368 XDOT = -758
576465
YDOT = -16674
768311 feet/sec YDOT = -5091
425356 meter/sec
ZDOT = -18778
923354 ZDOT = -5727
707244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4184729
02 X = -1275505
40
Y = 20953324
48 feet Y = 6386573
30 meter
Z = -5490636
60 Z = -1673546
03
XDOT = -13396
412520 XDOT = -4083
226536
YDOT = -7593
214042 feet/sec YDOT = -2314
411640 meter/sec
ZDOT = -18794
406563 ZDOT = -5728
535120
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 11136
52848007
00016717 00000-0 10270-3 0 9104
2 25544 51
6434 323
2597 0003769 285
8175 74
2573 15
75272456 35928
Satellite: ISS
Catalog Number: 25544
Epoch time: 11136
52848007 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 323
2597 deg
Eccentricity:
0003769
Arg of perigee: 285
8175 deg
Mean anomaly: 74
2573 deg
Mean motion: 15
75272456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3592
Checksum: 326
Coasting Arc #12 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2011/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 651405
56 A = 6718255
42 meter
Y = 4623454
41 meter E =
0005256
Z = 4830354
54 I = 51
39920
XDOT = -6506
159467 Wp = 25
42185
YDOT = 3384
100867 meter/sec RA = 317
65812 deg
ZDOT = -2356
123023 TA = 87
64939
MA = 87
58921
Ha = 186
843 n
mi
Hp = 183
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2137157
36 X = 576191
42
Y = 15168813
68 feet Y = 4630317
74 meter
Z = 15847619
89 Z = 4833336
94
XDOT = -21345
667542 XDOT = -6532
071764
YDOT = 11102
693132 feet/sec YDOT = 3311
200422 meter/sec
ZDOT = -7730
062410 ZDOT = -2387
793042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13479514
58 X = 4108556
04
Y = 7251760
39 feet Y = 2210336
57 meter
Z = 15859447
16 Z = 4833959
49
XDOT = -2986
302666 XDOT = -910
225053
YDOT = 22777
344858 feet/sec YDOT = 6942
534713 meter/sec
ZDOT = -7858
369425 ZDOT = -2395
231001
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 11137
54347546
00016717 00000-0 10270-3 0 9110
2 25544 51
6430 318
0364 0003818 287
6774 72
3973 15
75313768 36081
Satellite: ISS
Catalog Number: 25544
Epoch time: 11137
54347546 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 318
0364 deg
Eccentricity:
0003818
Arg of perigee: 287
6774 deg
Mean anomaly: 72
3973 deg
Mean motion: 15
75313768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 325
Coasting Arc #13 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2011/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5462712
68 A = 6725409
53 meter
Y = -3027246
66 meter E =
0010973
Z = 2478919
35 I = 51
40218
XDOT = 659
726641 Wp = 63
83669
YDOT = 5547
292683 meter/sec RA = 312
53497 deg
ZDOT = 5307
162410 TA = 324
33002
MA = 324
40329
Ha = 186
702 n
mi
Hp = 182
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17922285
69 X = 5484115
64
Y = -9931911
62 feet Y = -2966039
95 meter
Z = 8132937
51 Z = 2505509
13
XDOT = 2164
457485 XDOT = 571
865173
YDOT = 18199
779144 feet/sec YDOT = 5554
178191 meter/sec
ZDOT = 17411
950163 ZDOT = 5310
154710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2102387
77 X = 640807
79
Y = -20338807
27 feet Y = -6199268
46 meter
Z = 8240676
55 Z = 2511758
21
XDOT = 14613
463346 XDOT = 4454
183628
YDOT = 8587
675909 feet/sec YDOT = 2617
523617 meter/sec
ZDOT = 17423
769496 ZDOT = 5310
764942
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 11138
55842074
00016717 00000-0 10270-3 0 9129
2 25544 51
6427 312
8128 0003813 291
6108 68
4650 15
75414301 36249
Satellite: ISS
Catalog Number: 25544
Epoch time: 11138
55842074 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 312
8128 deg
Eccentricity:
0003813
Arg of perigee: 291
6108 deg
Mean anomaly: 68
4650 deg
Mean motion: 15
75414301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 292
Coasting Arc #14 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2011/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -519806
63 A = 6719619
65 meter
Y = -5081323
59 meter E =
0005446
Z = -4371533
33 I = 51
36391
XDOT = 6003
296422 Wp = 106
74507
YDOT = -3479
849313 meter/sec RA = 307
32375 deg
ZDOT = 3332
901019 TA = 196
90708
MA = 196
92523
Ha = 186
764 n
mi
Hp = 182
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1705402
33 X = -441711
40
Y = -16671009
14 feet Y = -5086699
11 meter
Z = -14342300
97 Z = -4373869
59
XDOT = 19695
854404 XDOT = 6025
571846
YDOT = -11416
828455 feet/sec YDOT = -3412
592727 meter/sec
ZDOT = 10934
714629 ZDOT = 3362
118854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14730423
20 X = -4489832
99
Y = -7973821
98 feet Y = -2430420
94 meter
Z = -14351492
45 Z = -4374334
90
XDOT = 921
193443 XDOT = 280
779761
YDOT = -21584
378129 feet/sec YDOT = -6578
918454 meter/sec
ZDOT = 11053
114701 ZDOT = 3368
989361
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 11139
50988772
00016717 00000-0 10270-3 0 9132
2 25544 51
6434 307
9160 0003752 296
1556 63
9222 15
75485662 36396
Satellite: ISS
Catalog Number: 25544
Epoch time: 11139
50988772 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 307
9160 deg
Eccentricity:
0003752
Arg of perigee: 296
1556 deg
Mean anomaly: 63
9222 deg
Mean motion: 15
75485662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 332
Coasting Arc #15 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2011/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5025183
42 A = 6722743
27 meter
Y = 2970408
06 meter E =
0002594
Z = -3338102
47 I = 51
35813
XDOT = -532
561125 Wp = 37
79520
YDOT = -6117
828047 meter/sec RA = 302
20714 deg
ZDOT = -4642
109707 TA = 181
66603
MA = 181
66689
Ha = 186
776 n
mi
Hp = 182
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16486822
24 X = -5041809
68
Y = 9745433
27 feet Y = 2914120
90 meter
Z = -10951779
74 Z = -3362554
83
XDOT = -1747
247785 XDOT = -441
560248
YDOT = -20071
614327 feet/sec YDOT = -6123
274020 meter/sec
ZDOT = -15230
018723 ZDOT = -4644
476688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -767274
40 X = -233865
24
Y = 19079300
98 feet Y = 5815370
94 meter
Z = -11050874
22 Z = -3368306
46
XDOT = -16346
354492 XDOT = -4982
368849
YDOT = -9484
298362 feet/sec YDOT = -2890
814141 meter/sec
ZDOT = -15239
286644 ZDOT = -4644
934569
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 11140
52473664
00016717 00000-0 10270-3 0 9146
2 25544 51
6438 302
6932 0003867 302
8997 57
1795 15
75579819 36556
Satellite: ISS
Catalog Number: 25544
Epoch time: 11140
52473664 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 302
6932 deg
Eccentricity:
0003867
Arg of perigee: 302
8997 deg
Mean anomaly: 57
1795 deg
Mean motion: 15
75579819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 346
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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