[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 21st 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) : 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 3654)
---------------------------------------
Vector Time (GMT): 2011/140/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2633709
79 A = 6727771
48 meter
Y = 6056562
53 meter E =
0010262
Z = 1255201
56 I = 51
37323
XDOT = -4933
601151 Wp = 124
12298
YDOT = -928
680707 meter/sec RA = 302
23689 deg
ZDOT = -5842
483081 TA = 42
04958
MA = 41
97086
Ha = 186
993 n
mi
Hp = 183
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8640780
15 X = -2707337
24
Y = 19870611
99 feet Y = 6026698
95 meter
Z = 4118115
34 Z = 1242228
96
XDOT = -16186
355481 XDOT = -4894
468010
YDOT = -3046
852712 feet/sec YDOT = -983
631624 meter/sec
ZDOT = -19168
251579 ZDOT = -5866
355636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10997888
21 X = 3352156
33
Y = 18681082
27 feet Y = 5693993
88 meter
Z = 4065316
28 Z = 1239108
40
XDOT = -10540
567231 XDOT = -3212
764892
YDOT = 10418
257997 feet/sec YDOT = 3175
485038 meter/sec
ZDOT = -19264
802345 ZDOT = -5871
911755
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
52593097
00016717 00000-0 10270-3 0 9004
2 25544 51
6445 302
7123 0003720 293
4241 66
6531 15
75314383 36558
Satellite: ISS
Catalog Number: 25544
Epoch time: 11140
52593097 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 302
7123 deg
Eccentricity:
0003720
Arg of perigee: 293
4241 deg
Mean anomaly: 66
6531 deg
Mean motion: 15
75314383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 286
Coasting Arc #2 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2011/141/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166384
64 A = 6716648
15 meter
Y = 961133
25 meter E =
0000268
Z = 5180044
80 I = 51
32032
XDOT = -2801
007630 Wp = 228
45716
YDOT = 7115
280469 meter/sec RA = 297
09040 deg
ZDOT = 932
539010 TA = 212
62118
MA = 212
62284
Ha = 186
994 n
mi
Hp = 182
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13669240
94 X = 4130163
73
Y = 3153324
30 feet Y = 1007521
12 meter
Z = 16994897
62 Z = 5200197
20
XDOT = -9189
657578 XDOT = -2884
893981
YDOT = 23344
096026 feet/sec YDOT = 7083
488752 meter/sec
ZDOT = 3059
511188 ZDOT = 918
728859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10360131
79 X = 3157768
17
Y = -9310340
04 feet Y = -2837791
65 meter
Z = 17076398
47 Z = 5204886
25
XDOT = 13174
170679 XDOT = 4015
487223
YDOT = 20168
901335 feet/sec YDOT = 6147
481127 meter/sec
ZDOT = 3003
275338 ZDOT = 915
398323
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 11141
54092133
00016717 00000-0 10270-3 0 9013
2 25544 51
6446 297
4900 0003516 297
6534 62
4273 15
75306461 36719
Satellite: ISS
Catalog Number: 25544
Epoch time: 11141
54092133 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 297
4900 deg
Eccentricity:
0003516
Arg of perigee: 297
6534 deg
Mean anomaly: 62
4273 deg
Mean motion: 15
75306461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 296
Coasting Arc #3 (Orbit 3685)
---------------------------------------
Vector Time (GMT): 2011/142/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2242586
04 A = 6728173
39 meter
Y = -6326625
66 meter E =
0011327
Z = -350571
61 I = 51
34808
XDOT = 4645
250513 Wp = 24
75283
YDOT = 1318
342707 meter/sec RA = 291
91176 deg
ZDOT = 6003
760326 TA = 331
41776
MA = 331
47981
Ha = 187
041 n
mi
Hp = 182
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7357565
76 X = 2314867
92
Y = -20756645
87 feet Y = -6301143
52 meter
Z = -1150169
34 Z = -339502
26
XDOT = 15240
323205 XDOT = 4600
998221
YDOT = 4325
271349 feet/sec YDOT = 1370
040656 meter/sec
ZDOT = 19697
376397 ZDOT = 6026
219531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13095717
35 X = -3991574
65
Y = -17708077
73 feet Y = -5397422
09 meter
Z = -1105070
69 Z = -336825
55
XDOT = 10748
100300 XDOT = 3276
020971
YDOT = -9166
420051 feet/sec YDOT = -2793
924832 meter/sec
ZDOT = 19788
199282 ZDOT = 6031
443141
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 11142
49244047
00016717 00000-0 10270-3 0 9022
2 25544 51
6457 292
5945 0003491 299
9494 60
1323 15
75389906 36860
Satellite: ISS
Catalog Number: 25544
Epoch time: 11142
49244047 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 292
5945 deg
Eccentricity:
0003491
Arg of perigee: 299
9494 deg
Mean anomaly: 60
1323 deg
Mean motion: 15
75389906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3686
Checksum: 336
Coasting Arc #4 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2011/143/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3971842
20 A = 6715963
29 meter
Y = -1386519
57 meter E =
0012320
Z = -5245555
76 I = 51
29723
XDOT = 2342
765661 Wp = 82
00778
YDOT = -7327
444071 meter/sec RA = 286
74611 deg
ZDOT = 164
928648 TA = 189
55436
MA = 189
57782
Ha = 187
059 n
mi
Hp = 182
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13030978
34 X = -3930560
79
Y = -4548948
73 feet Y = -1430703
85 meter
Z = -17209828
60 Z = -5264750
75
XDOT = 7686
239045 XDOT = 2423
727236
YDOT = -24040
170835 feet/sec YDOT = -7300
793176 meter/sec
ZDOT = 541
104487 ZDOT = 176
505792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10855991
95 X = -3308906
35
Y = 8364764
39 feet Y = 2549580
19 meter
Z = -17287443
04 Z = -5269212
64
XDOT = -15368
809121 XDOT = -4684
413020
YDOT = -18743
809678 feet/sec YDOT = -5713
113190 meter/sec
ZDOT = 588
296472 ZDOT = 179
312765
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 11143
50736216
00016717 00000-0 10270-3 0 9030
2 25544 51
6459 287
3732 0003509 305
7856 54
2981 15
75455393 37023
Satellite: ISS
Catalog Number: 25544
Epoch time: 11143
50736216 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 287
3732 deg
Eccentricity:
0003509
Arg of perigee: 305
7856 deg
Mean anomaly: 54
2981 deg
Mean motion: 15
75455393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 317
Coasting Arc #5 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2011/144/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1854737
34 A = 6727682
82 meter
Y = 6429804
53 meter E =
0007093
Z = -657160
44 I = 51
32888
XDOT = -4484
519703 Wp = 144
78947
YDOT = -1899
490275 meter/sec RA = 281
58301 deg
ZDOT = -5965
817258 TA = 42
40150
MA = 42
34671
Ha = 187
083 n
mi
Hp = 182
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6085096
27 X = -1923306
44
Y = 21095159
21 feet Y = 6408680
38 meter
Z = -2156038
19 Z = -666336
84
XDOT = -14712
991152 XDOT = -4433
965115
YDOT = -6231
923474 feet/sec YDOT = -1949
355809 meter/sec
ZDOT = -19572
891267 ZDOT = -5987
480365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14668992
28 X = 4471108
85
Y = 16330707
83 feet Y = 4977599
75 meter
Z = -2193464
50 Z = -668567
98
XDOT = -11830
880798 XDOT = -3606
052467
YDOT = 8002
653610 feet/sec YDOT = 2439
208820 meter/sec
ZDOT = -19660
474055 ZDOT = -5992
512492
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 11144
52224883
00016717 00000-0 10270-3 0 9046
2 25544 51
6452 282
1493 0003729 310
7024 49
3815 15
75511038 37187
Satellite: ISS
Catalog Number: 25544
Epoch time: 11144
52224883 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 282
1493 deg
Eccentricity:
0003729
Arg of perigee: 310
7024 deg
Mean anomaly: 49
3815 deg
Mean motion: 15
75511038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 297
Coasting Arc #6 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2011/145/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3901836
55 A = 6716392
63 meter
Y = 1947535
06 meter E =
0005245
Z = 5108267
92 I = 51
28652
XDOT = -1903
869678 Wp = 10
83236
YDOT = 7343
334460 meter/sec RA = 276
39461 deg
ZDOT = -1340
120348 TA = 92
07977
MA = 92
01971
Ha = 187
102 n
mi
Hp = 182
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12801301
00 X = 3854953
76
Y = 6389550
71 feet Y = 1990905
31 meter
Z = 16759409
18 Z = 5127109
32
XDOT = -6246
291596 XDOT = -1979
332681
YDOT = 24092
304659 feet/sec YDOT = 7321
622381 meter/sec
ZDOT = -4396
720302 ZDOT = -1349
552202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12022130
71 X = 3664345
44
Y = -7590077
47 feet Y = -2313455
61 meter
Z = 16835574
21 Z = 5131483
02
XDOT = 16886
401409 XDOT = 5146
975149
YDOT = 16870
613110 feet/sec YDOT = 5142
162876 meter/sec
ZDOT = -4435
212883 ZDOT = -1351
852887
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 11145
53710358
00016717 00000-0 10270-3 0 9056
2 25544 51
6460 276
9266 0003669 315
7620 44
3250 15
75512308 37342
Satellite: ISS
Catalog Number: 25544
Epoch time: 11145
53710358 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 276
9266 deg
Eccentricity:
0003669
Arg of perigee: 315
7620 deg
Mean anomaly: 44
3250 deg
Mean motion: 15
75512308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3734
Checksum: 302
Coasting Arc #7 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2011/146/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1486255
34 A = 6726338
88 meter
Y = -6332036
36 meter E =
0013583
Z = 1683388
88 I = 51
31963
XDOT = 4505
635116 Wp = 48
92775
YDOT = 2577
662769 meter/sec RA = 271
25060 deg
ZDOT = 5696
834295 TA = 329
79376
MA = 329
87200
Ha = 187
073 n
mi
Hp = 182
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4876165
81 X = 1548773
28
Y = -20774397
49 feet Y = -6315066
70 meter
Z = 5522929
38 Z = 1690760
60
XDOT = 14782
267441 XDOT = 4448
801990
YDOT = 8456
898850 feet/sec YDOT = 2627
729389 meter/sec
ZDOT = 18690
401229 ZDOT = 5718
584899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15559509
88 X = -4742538
61
Y = -14591805
81 feet Y = -4447582
41 meter
Z = 5553034
19 Z = 1692564
82
XDOT = 13601
328251 XDOT = 4145
684851
YDOT = -7331
028615 feet/sec YDOT = -2234
497522 meter/sec
ZDOT = 18778
315901 ZDOT = 5723
630687
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 11146
55192007
00016717 00000-0 10270-3 0 9065
2 25544 51
6469 271
7036 0003744 318
5650 41
5230 15
75616133 37503
Satellite: ISS
Catalog Number: 25544
Epoch time: 11146
55192007 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 271
7036 deg
Eccentricity:
0003744
Arg of perigee: 318
5650 deg
Mean anomaly: 41
5230 deg
Mean motion: 15
75616133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3750
Checksum: 292
Coasting Arc #8 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2011/147/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4001089
37 A = 6717493
66 meter
Y = -2554559
33 meter E =
0008815
Z = -4760702
54 I = 51
29069
XDOT = 1536
992615 Wp = 93
38100
YDOT = -7106
491169 meter/sec RA = 266
04392 deg
ZDOT = 2525
049729 TA = 201
46160
MA = 201
49858
Ha = 187
123 n
mi
Hp = 181
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13126933
64 X = -3949099
60
Y = -8381100
18 feet Y = -2599010
92 meter
Z = -15619102
81 Z = -4780013
89
XDOT = 5042
626689 XDOT = 1604
078190
YDOT = -23315
259742 feet/sec YDOT = -7088
928665 meter/sec
ZDOT = 8284
283887 ZDOT = 2532
678959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13656291
04 X = -4162437
51
Y = 7322621
32 feet Y = 2231934
98 meter
Z = -15697150
43 Z = -4784491
45
XDOT = -17422
463152 XDOT = -5310
366769
YDOT = -14691
050216 feet/sec YDOT = -4477
832106 meter/sec
ZDOT = 8315
458951 ZDOT = 2534
551888
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 11147
50328214
00016717 00000-0 10270-3 0 9073
2 25544 51
6468 266
8077 0003897 323
1497 36
9399 15
75659098 37659
Satellite: ISS
Catalog Number: 25544
Epoch time: 11147
50328214 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 266
8077 deg
Eccentricity:
0003897
Arg of perigee: 323
1497 deg
Mean anomaly: 36
9399 deg
Mean motion: 15
75659098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3765
Checksum: 356
Coasting Arc #9 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2011/148/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1243892
33 A = 6724092
96 meter
Y = 6022653
38 meter E =
0002081
Z = -2721910
84 I = 51
31704
XDOT = -4692
973637 Wp = 68
38420
YDOT = -3290
650389 meter/sec RA = 260
91429 deg
ZDOT = -5138
816038 TA = 142
84603
MA = 142
83163
Ha = 187
230 n
mi
Hp = 181
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4081011
58 X = -1297923
64
Y = 19759361
47 feet Y = 6008441
54 meter
Z = -8930153
66 Z = -2728084
48
XDOT = -15396
895134 XDOT = -4630
864431
YDOT = -10796
097078 feet/sec YDOT = -3342
782375 meter/sec
ZDOT = -16859
632672 ZDOT = -5161
464176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15540165
30 X = 4736642
38
Y = 12850639
03 feet Y = 3916874
78 meter
Z = -8955389
69 Z = -2729602
78
XDOT = -15786
788523 XDOT = -4811
813142
YDOT = 7283
303914 feet/sec YDOT = 2219
951033 meter/sec
ZDOT = -16951
158133 ZDOT = -5166
712999
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 11148
51803467
00016717 00000-0 10270-3 0 9084
2 25544 51
6473 261
5836 0003963 327
6088 32
4833 15
75700959 37814
Satellite: ISS
Catalog Number: 25544
Epoch time: 11148
51803467 = yrday
fracday
Element set: 908
Inclination: 51
6473 deg
RA of node: 261
5836 deg
Eccentricity:
0003963
Arg of perigee: 327
6088 deg
Mean anomaly: 32
4833 deg
Mean motion: 15
75700959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3781
Checksum: 332
Coasting Arc #10 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2011/149/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4233325
99 A = 6719680
37 meter
Y = 3167301
70 meter E =
0010291
Z = 4144650
73 I = 51
30887
XDOT = -1349
011470 Wp = 52
12805
YDOT = 6633
026457 meter/sec RA = 255
69441 deg
ZDOT = -3678
574783 TA = 75
64640
MA = 75
53217
Ha = 187
278 n
mi
Hp = 181
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13888864
80 X = 4177459
75
Y = 10391409
77 feet Y = 3214328
54 meter
Z = 13597935
46 Z = 4165081
12
XDOT = -4425
890651 XDOT = -1405
212896
YDOT = 21761
897825 feet/sec YDOT = 6617
627118 meter/sec
ZDOT = -12068
814905 ZDOT = -3685
264225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15538531
50 X = 4736144
40
Y = -7562003
70 feet Y = -2304898
73 meter
Z = 13680495
24 Z = 4169814
95
XDOT = 16841
877753 XDOT = 5133
404339
YDOT = 12650
260867 feet/sec YDOT = 3855
799512 meter/sec
ZDOT = -12096
162523 ZDOT = -3686
910337
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 11149
53275415
00016717 00000-0 10270-3 0 9094
2 25544 51
6477 256
3604 0003993 333
6754 26
4207 15
75729428 37970
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
53275415 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 256
3604 deg
Eccentricity:
0003993
Arg of perigee: 333
6754 deg
Mean anomaly: 26
4207 deg
Mean motion: 15
75729428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3797
Checksum: 338
Coasting Arc #11 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2011/150/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1166637
22 A = 6721095
71 meter
Y = -5506214
16 meter E =
0010514
Z = 3662297
27 I = 51
32376
XDOT = 5040
540136 Wp = 75
47893
YDOT = 3935
331952 meter/sec RA = 250
57363 deg
ZDOT = 4303
354329 TA = 328
83554
MA = 328
89785
Ha = 187
219 n
mi
Hp = 181
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3827549
94 X = 1210331
04
Y = -18065007
08 feet Y = -5492924
24 meter
Z = 12015411
01 Z = 3668070
36
XDOT = 16537
205170 XDOT = 4975
254665
YDOT = 12911
194069 feet/sec YDOT = 3991
332790 meter/sec
ZDOT = 14118
616566 ZDOT = 4327
683502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14570877
15 X = -4441203
36
Y = -11318862
73 feet Y = -3449989
36 meter
Z = 12039003
55 Z = 3669488
28
XDOT = 18007
270686 XDOT = 5488
616105
YDOT = -8032
713785 feet/sec YDOT = -2448
371162 meter/sec
ZDOT = 14216
931746 ZDOT = 4333
320796
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 11150
54743699
00016717 00000-0 10270-3 0 9103
2 25544 51
6482 251
1362 0004123 336
7048 23
3929 15
75831224 38130
Satellite: ISS
Catalog Number: 25544
Epoch time: 11150
54743699 = yrday
fracday
Element set: 910
Inclination: 51
6482 deg
RA of node: 251
1362 deg
Eccentricity:
0004123
Arg of perigee: 336
7048 deg
Mean anomaly: 23
3929 deg
Mean motion: 15
75831224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3813
Checksum: 297
Coasting Arc #12 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2011/151/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4577432
14 A = 6722134
46 meter
Y = -3656808
20 meter E =
0005434
Z = -3293950
98 I = 51
33884
XDOT = 1391
252013 Wp = 37
19558
YDOT = -5953
060045 meter/sec RA = 245
35159 deg
ZDOT = 4683
778486 TA = 283
92965
MA = 283
99009
Ha = 187
316 n
mi
Hp = 181
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15017821
98 X = -4520199
18
Y = -11997402
23 feet Y = -3707675
36 meter
Z = -10806925
79 Z = -3316049
92
XDOT = 4564
475108 XDOT = 1434
963637
YDOT = -19531
036892 feet/sec YDOT = -5937
258466 meter/sec
ZDOT = 15366
727316 ZDOT = 4690
642624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17209505
35 X = -5245457
23
Y = 8447917
37 feet Y = 2574925
22 meter
Z = -10896233
30 Z = -3321171
91
XDOT = -15170
519155 XDOT = -4623
974238
YDOT = -11082
747713 feet/sec YDOT = -3378
021503 meter/sec
ZDOT = 15394
755202 ZDOT = 4692
321386
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 11151
49867467
00016717 00000-0 10270-3 0 9119
2 25544 51
6482 246
2398 0004369 340
1009 19
9984 15
75839493 38286
Satellite: ISS
Catalog Number: 25544
Epoch time: 11151
49867467 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 246
2398 deg
Eccentricity:
0004369
Arg of perigee: 340
1009 deg
Mean anomaly: 19
9984 deg
Mean motion: 15
75839493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 349
Coasting Arc #13 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2011/152/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1343037
57 A = 6718093
97 meter
Y = 4846581
19 meter E =
0010994
Z = -4465076
54 I = 51
33904
XDOT = -5444
287112 Wp = 46
51835
YDOT = -4423
718379 meter/sec RA = 240
23007 deg
ZDOT = -3161
526729 TA = 191
72007
MA = 191
74568
Ha = 187
415 n
mi
Hp = 181
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4406291
24 X = -1375442
40
Y = 15900856
93 feet Y = 4831382
04 meter
Z = -14649201
24 Z = -4471679
03
XDOT = -17861
834356 XDOT = -5379
057330
YDOT = -14513
511742 feet/sec YDOT = -4484
234489 meter/sec
ZDOT = -10372
463023 ZDOT = -3187
817593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12746270
21 X = 3885063
16
Y = 10440098
81 feet Y = 3182142
12 meter
Z = -14676126
30 Z = -4473283
30
XDOT = -19760
148506 XDOT = -6022
893265
YDOT = 9382
731203 feet/sec YDOT = 2859
856471 meter/sec
ZDOT = -10478
720122 ZDOT = -3193
913893
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 11152
51329519
00016717 00000-0 10270-3 0 9125
2 25544 51
6478 241
0160 0004330 344
3305 15
7724 15
75891803 38441
Satellite: ISS
Catalog Number: 25544
Epoch time: 11152
51329519 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 241
0160 deg
Eccentricity:
0004330
Arg of perigee: 344
3305 deg
Mean anomaly: 15
7724 deg
Mean motion: 15
75891803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 290
Coasting Arc #14 (Orbit 3859)
---------------------------------------
Vector Time (GMT): 2011/153/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4929774
66 A = 6724523
76 meter
Y = 4019027
47 meter E =
0012579
Z = 2171432
48 I = 51
37707
XDOT = -1754
090170 Wp = 90
93930
YDOT = 5125
240442 meter/sec RA = 235
01722 deg
ZDOT = -5476
752797 TA = 64
63327
MA = 64
50308
Ha = 187
478 n
mi
Hp = 180
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16173801
38 X = 4873918
24
Y = 13185785
68 feet Y = 4073842
53 meter
Z = 7124122
31 Z = 2195246
48
XDOT = -5754
889009 XDOT = -1784
665986
YDOT = 16815
093314 feet/sec YDOT = 5105
455099 meter/sec
ZDOT = -17968
349070 ZDOT = -5485
347633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18464293
31 X = 5627916
60
Y = -9651211
18 feet Y = -2941689
17 meter
Z = 7220381
52 Z = 2200772
29
XDOT = 12538
597146 XDOT = 3821
764410
YDOT = 10453
837439 feet/sec YDOT = 3186
329651 meter/sec
ZDOT = -18003
352609 ZDOT = -5487
421875
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 11153
52788301
00016717 00000-0 10270-3 0 9136
2 25544 51
6471 235
7920 0004430 350
6417 9
4664 15
75950348 38604
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
52788301 = yrday
fracday
Element set: 913
Inclination: 51
6471 deg
RA of node: 235
7920 deg
Eccentricity:
0004430
Arg of perigee: 350
6417 deg
Mean anomaly: 9
4664 deg
Mean motion: 15
75950348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3860
Checksum: 304
Coasting Arc #15 (Orbit 3875)
---------------------------------------
Vector Time (GMT): 2011/154/11:48:10
839
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1788845
04 A = 6715393
90 meter
Y = -4092665
20 meter E =
0004099
Z = 5010957
52 I = 51
36556
XDOT = 5829
986218 Wp = 71
08881
YDOT = 4719
265569 meter/sec RA = 229
88201 deg
ZDOT = 1773
331972 TA = 1
78185
MA = 1
78039
Ha = 187
367 n
mi
Hp = 180
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5868914
17 X = 1810134
69
Y = -13427379
26 feet Y = -4072543
06 meter
Z = 16440149
35 Z = 5019698
77
XDOT = 19127
251370 XDOT = 5768
166640
YDOT = 15483
154755 feet/sec YDOT = 4784
114061 meter/sec
ZDOT = 5818
018280 ZDOT = 1801
504749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10259402
37 X = -3127065
84
Y = -10407350
77 feet Y = -3172160
52 meter
Z = 16475706
08 Z = 5021795
21
XDOT = 20781
014365 XDOT = 6334
053178
YDOT = -11095
560476 feet/sec YDOT = -3381
926833 meter/sec
ZDOT = 5931
915317 ZDOT = 1808
047789
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 11154
54243620
00016717 00000-0 10270-3 0 9140
2 25544 51
6471 230
5669 0004519 352
8591 7
2509 15
76028443 38766
Satellite: ISS
Catalog Number: 25544
Epoch time: 11154
54243620 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 230
5669 deg
Eccentricity:
0004519
Arg of perigee: 352
8591 deg
Mean anomaly: 7
2509 deg
Mean motion: 15
76028443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3876
Checksum: 310
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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