[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 30th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 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 2173)
---------------------------------------
Vector Time (GMT): 2011/301/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1969869
42 A = 6762435
39 meter
Y = -3725001
60 meter E =
0021734
Z = 5288615
30 I = 51
45459
XDOT = 6771
198138 Wp =
99656
YDOT = 3619
172836 meter/sec RA = 208
41193 deg
ZDOT = 48
377305 TA = 88
66634
MA = 88
41736
Ha = 219
057 n
mi
Hp = 202
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6462826
19 X = 1985684
93
Y = -12221133
85 feet Y = -3702884
93 meter
Z = 17351100
08 Z = 5298223
55
XDOT = 22215
216989 XDOT = 6729
989562
YDOT = 11873
926627 feet/sec YDOT = 3694
662112 meter/sec
ZDOT = 158
718193 ZDOT = 81
172548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6023682
23 X = 1836018
34
Y = 12388439
04 feet Y = 3775996
22 meter
Z = 17390420
90 Z = 5300600
29
XDOT = -21870
342895 XDOT = -6666
080514
YDOT = 10321
944662 feet/sec YDOT = 3146
128733 meter/sec
ZDOT = 292
194687 ZDOT = 89
060940
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 11301
59735602
00016717 00000-0 10270-3 0 9000
2 25544 51
6426 209
2012 0022003 354
5225 5
5686 15
59263770 21744
Satellite: ISS
Catalog Number: 25544
Epoch time: 11301
59735602 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 209
2012 deg
Eccentricity:
0022003
Arg of perigee: 354
5225 deg
Mean anomaly: 5
5686 deg
Mean motion: 15
59263770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 278
Coasting Arc #2 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2011/302/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5018585
60 A = 6766467
92 meter
Y = 1530685
87 meter E =
0020360
Z = -4266937
26 I = 51
49546
XDOT = -4551
926936 Wp = 21
09665
YDOT = -5054
238446 meter/sec RA = 203
35291 deg
ZDOT = 3564
566086 TA = 285
17208
MA = 285
39716
Ha = 219
149 n
mi
Hp = 202
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16465175
86 X = -5014600
60
Y = 5021935
26 feet Y = 1474587
36 meter
Z = -13999138
01 Z = -4291308
33
XDOT = -14934
143491 XDOT = -4512
387502
YDOT = -16582
147132 feet/sec YDOT = -5104
919895 meter/sec
ZDOT = 11694
770622 ZDOT = 3542
548288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5451682
07 X = 1661672
69
Y = -16242175
87 feet Y = -4950615
20 meter
Z = -14098531
86 Z = -4297232
51
XDOT = 21032
363916 XDOT = 6410
664522
YDOT = -2946
500301 feet/sec YDOT = -898
093292 meter/sec
ZDOT = 11605
266223 ZDOT = 3537
285145
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 11302
55871142
00016717 00000-0 10270-3 0 9018
2 25544 51
6423 204
3719 0022039 357
9611 2
1451 15
59289096 21894
Satellite: ISS
Catalog Number: 25544
Epoch time: 11302
55871142 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 204
3719 deg
Eccentricity:
0022039
Arg of perigee: 357
9611 deg
Mean anomaly: 2
1451 deg
Mean motion: 15
59289096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 296
Coasting Arc #3 (Orbit 2204)
---------------------------------------
Vector Time (GMT): 2011/303/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6552704
28 A = 6773314
70 meter
Y = 945095
42 meter E =
0020069
Z = 1465344
72 I = 51
54635
XDOT = 579
267371 Wp = 40
79774
YDOT = 5014
782472 meter/sec RA = 198
33034 deg
ZDOT = -5765
091531 TA = 123
18328
MA = 122
99065
Ha = 219
300 n
mi
Hp = 201
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21498373
62 X = 6534530
53
Y = 3100706
77 feet Y = 1018270
12 meter
Z = 4807561
42 Z = 1497134
13
XDOT = 1900
483502 XDOT = 551
154235
YDOT = 16452
698399 feet/sec YDOT = 5021
103169 meter/sec
ZDOT = -18914
342292 ZDOT = -5762
345552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14746582
76 X = -4494758
43
Y = 15908189
42 feet Y = 4848816
14 meter
Z = 4937094
66 Z = 1504826
45
XDOT = -13524
485502 XDOT = -4122
263181
YDOT = -6611
170123 feet/sec YDOT = -2015
084653 meter/sec
ZDOT = -18903
377232 ZDOT = -5761
749380
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 11303
58412319
00016717 00000-0 10270-3 0 9020
2 25544 51
6418 199
2197 0021874 2
0102 358
1137 15
59317928 22059
Satellite: ISS
Catalog Number: 25544
Epoch time: 11303
58412319 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 199
2197 deg
Eccentricity:
0021874
Arg of perigee: 2
0102 deg
Mean anomaly: 358
1137 deg
Mean motion: 15
59317928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2205
Checksum: 293
Coasting Arc #4 (Orbit 2220)
---------------------------------------
Vector Time (GMT): 2011/304/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5773016
88 A = 6772591
48 meter
Y = -2930052
55 meter E =
0031221
Z = 1916136
32 I = 51
57312
XDOT = 3743
215808 Wp = 28
82242
YDOT = -3693
783225 meter/sec RA = 193
32922 deg
ZDOT = 5618
248129 TA = 352
41729
MA = 352
46439
Ha = 219
402 n
mi
Hp = 201
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18940344
09 X = -5749131
73
Y = -9613033
32 feet Y = -2994476
46 meter
Z = 6286536
48 Z = 1888148
64
XDOT = 12280
891757 XDOT = 3756
949471
YDOT = -12118
711368 feet/sec YDOT = -3651
847618 meter/sec
ZDOT = 18432
572602 ZDOT = 5636
466161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18513515
78 X = 5642919
61
Y = -10479344
35 feet Y = -3194104
16 meter
Z = 6172573
22 Z = 1881400
32
XDOT = 2587
069361 XDOT = 788
538741
YDOT = 15493
460799 feet/sec YDOT = 4722
406852 meter/sec
ZDOT = 18507
008006 ZDOT = 5640
936040
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 11304
60949837
00016717 00000-0 10270-3 0 9035
2 25544 51
6415 194
0667 0022035 5
3941 354
7448 15
59384775 22217
Satellite: ISS
Catalog Number: 25544
Epoch time: 11304
60949837 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 194
0667 deg
Eccentricity:
0022035
Arg of perigee: 5
3941 deg
Mean anomaly: 354
7448 deg
Mean motion: 15
59384775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2221
Checksum: 316
Coasting Arc #5 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2011/305/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2958122
59 A = 6765239
20 meter
Y = 4073670
74 meter E =
0027970
Z = -4543139
74 I = 51
57812
XDOT = -6840
980535 Wp = 26
67317
YDOT = 1488
490170 meter/sec RA = 188
30498 deg
ZDOT = -3102
583881 TA = 212
10076
MA = 212
27138
Ha = 219
385 n
mi
Hp = 201
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9705126
61 X = 2934420
09
Y = 13365061
47 feet Y = 4106617
77 meter
Z = -14905314
12 Z = -4528826
61
XDOT = -22444
161860 XDOT = -6842
044760
YDOT = 4883
497934 feet/sec YDOT = 1411
984202 meter/sec
ZDOT = -10179
080973 ZDOT = -3135
820230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16536733
93 X = -5040396
50
Y = 1040004
15 feet Y = 316993
26 meter
Z = -14847139
86 Z = -4525408
23
XDOT = 8036
014302 XDOT = 2449
377159
YDOT = -20275
418284 feet/sec YDOT = -6179
947493 meter/sec
ZDOT = -10314
657769 ZDOT = -3143
907688
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 11305
57075609
00016717 00000-0 10270-3 0 9040
2 25544 51
6409 189
2361 0021929 8
5402 351
6123 15
59440992 22361
Satellite: ISS
Catalog Number: 25544
Epoch time: 11305
57075609 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 189
2361 deg
Eccentricity:
0021929
Arg of perigee: 8
5402 deg
Mean anomaly: 351
6123 deg
Mean motion: 15
59440992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 305
Coasting Arc #6 (Orbit 2251)
---------------------------------------
Vector Time (GMT): 2011/306/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1060587
38 A = 6761893
75 meter
Y = -4113369
69 meter E =
0023876
Z = 5256908
72 I = 51
59819
XDOT = 7581
382100 Wp = 18
36917
YDOT = 1003
045788 meter/sec RA = 183
24744 deg
ZDOT = -721
592284 TA = 78
64956
MA = 78
38141
Ha = 219
341 n
mi
Hp = 200
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3479617
39 X = 1080967
75
Y = -13495307
39 feet Y = -4101395
55 meter
Z = 17247075
84 Z = 5262110
64
XDOT = 24873
300854 XDOT = 7573
107766
YDOT = 3290
832638 feet/sec YDOT = 1087
779177 meter/sec
ZDOT = -2367
428753 ZDOT = -684
781753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9715477
58 X = 2961277
57
Y = 9955004
37 feet Y = 3034285
33 meter
Z = 17268470
32 Z = 5263429
75
XDOT = -15135
773678 XDOT = -4613
383817
YDOT = 18749
310777 feet/sec YDOT = 5714
789925 meter/sec
ZDOT = -2217
373694 ZDOT = -675
855502
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 11306
59606513
00016717 00000-0 10270-3 0 9058
2 25544 51
6412 184
0827 0021863 12
4390 347
7301 15
59504351 22524
Satellite: ISS
Catalog Number: 25544
Epoch time: 11306
59606513 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 184
0827 deg
Eccentricity:
0021863
Arg of perigee: 12
4390 deg
Mean anomaly: 347
7301 deg
Mean motion: 15
59504351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2252
Checksum: 286
Coasting Arc #7 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2011/307/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4643406
05 A = 6767404
31 meter
Y = 3141646
36 meter E =
0022839
Z = -3784211
89 I = 51
64663
XDOT = -5568
399171 Wp = 31
81204
YDOT = -3173
022066 meter/sec RA = 178
20091 deg
ZDOT = 4229
016666 TA = 282
67386
MA = 282
92910
Ha = 219
341 n
mi
Hp = 200
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15234271
83 X = -4659808
28
Y = 10307238
70 feet Y = 3089629
13 meter
Z = -12415393
32 Z = -3806809
67
XDOT = -18269
026150 XDOT = -5553
047927
YDOT = -10410
177381 feet/sec YDOT = -3235
205373 meter/sec
ZDOT = 13874
726594 ZDOT = 4202
002526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1132854
97 X = -345294
19
Y = -18295863
18 feet Y = -5576579
10 meter
Z = -12507686
81 Z = -3812342
94
XDOT = 16980
421965 XDOT = 5175
632615
YDOT = -10393
381208 feet/sec YDOT = -3167
902592 meter/sec
ZDOT = 13764
702340 ZDOT = 4195
481273
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 11307
55726196
00016717 00000-0 10270-3 0 9066
2 25544 51
6402 179
2513 0021831 15
7189 344
4640 15
59546538 22677
Satellite: ISS
Catalog Number: 25544
Epoch time: 11307
55726196 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 179
2513 deg
Eccentricity:
0021831
Arg of perigee: 15
7189 deg
Mean anomaly: 344
4640 deg
Mean motion: 15
59546538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 317
Coasting Arc #8 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2011/308/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6625166
42 A = 6773277
00 meter
Y = -1294471
19 meter E =
0021696
Z = 633560
67 I = 51
69695
XDOT = 1479
277259 Wp = 55
34466
YDOT = 4572
092595 meter/sec RA = 173
19567 deg
ZDOT = -5969
766295 TA = 117
81656
MA = 117
59651
Ha = 219
457 n
mi
Hp = 200
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21736110
31 X = 6636071
30
Y = -4246952
72 feet Y = -1220323
52 meter
Z = 2078611
14 Z = 665772
61
XDOT = 4853
271846 XDOT = 1457
041632
YDOT = 15000
303788 feet/sec YDOT = 4588
510224 meter/sec
ZDOT = -19585
847425 ZDOT = -5962
634077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7067744
48 X = -2154248
52
Y = 20975662
79 feet Y = 6393382
02 meter
Z = 2210041
14 Z = 673620
54
XDOT = -13963
361049 XDOT = -4256
032448
YDOT = -2593
170382 feet/sec YDOT = -790
398332 meter/sec
ZDOT = -19556
961640 ZDOT = -5960
961908
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 11308
58250609
00016717 00000-0 10270-3 0 9072
2 25544 51
6403 174
0981 0021843 19
6295 340
5697 15
59596280 22830
Satellite: ISS
Catalog Number: 25544
Epoch time: 11308
58250609 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 174
0981 deg
Eccentricity:
0021843
Arg of perigee: 19
6295 deg
Mean anomaly: 340
5697 deg
Mean motion: 15
59596280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 326
Coasting Arc #9 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2011/309/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6092104
80 A = 6770164
90 meter
Y = -943248
65 meter E =
0031364
Z = 2748067
02 I = 51
71584
XDOT = 3079
078633 Wp = 44
21324
YDOT = -4806
302741 meter/sec RA = 168
20067 deg
ZDOT = 5162
930706 TA = 347
03192
MA = 347
11239
Ha = 219
476 n
mi
Hp = 200
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19987220
48 X = -6094454
23
Y = -3094647
80 feet Y = -1011387
32 meter
Z = 9015967
93 Z = 2718465
50
XDOT = 10101
964019 XDOT = 3107
513875
YDOT = -15768
709781 feet/sec YDOT = -4771
711376 meter/sec
ZDOT = 16938
749034 ZDOT = 5177
958363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12337604
03 X = 3760501
71
Y = -16093822
73 feet Y = -4905397
17 meter
Z = 8895274
15 Z = 2711279
56
XDOT = 7855
880539 XDOT = 2394
472388
YDOT = 15443
008810 feet/sec YDOT = 4707
029085 meter/sec
ZDOT = 17000
256448 ZDOT = 5181
678165
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 11309
60771580
00016717 00000-0 10270-3 0 9083
2 25544 51
6393 168
9437 0021697 23
0773 337
1352 15
59656619 22993
Satellite: ISS
Catalog Number: 25544
Epoch time: 11309
60771580 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 168
9437 deg
Eccentricity:
0021697
Arg of perigee: 23
0773 deg
Mean anomaly: 337
1352 deg
Mean motion: 15
59656619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 340
Coasting Arc #10 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2011/310/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3393106
45 A = 6762732
20 meter
Y = 3090613
73 meter E =
0031571
Z = -4993046
24 I = 51
71938
XDOT = -6401
281278 Wp = 44
28199
YDOT = 3648
797585 meter/sec RA = 163
17301 deg
ZDOT = -2077
420088 TA = 205
41597
MA = 205
57157
Ha = 219
473 n
mi
Hp = 199
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11132239
00 X = 3382550
16
Y = 10139808
83 feet Y = 3128498
29 meter
Z = -16381385
31 Z = -4976588
02
XDOT = -21001
578997 XDOT = -6431
515179
YDOT = 11971
120687 feet/sec YDOT = 3577
045395 meter/sec
ZDOT = -6815
682703 ZDOT = -2108
591660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14198660
28 X = -4327751
65
Y = 5227897
48 feet Y = 1593463
15 meter
Z = -16314392
03 Z = -4972626
69
XDOT = -469
572434 XDOT = -143
125678
YDOT = -23087
190289 feet/sec YDOT = -7036
975600 meter/sec
ZDOT = -6942
996542 ZDOT = -2116
225346
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 11310
56882128
00016717 00000-0 10270-3 0 9092
2 25544 51
6379 164
1116 0021705 26
8617 333
3657 15
59686825 23143
Satellite: ISS
Catalog Number: 25544
Epoch time: 11310
56882128 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 164
1116 deg
Eccentricity:
0021705
Arg of perigee: 26
8617 deg
Mean anomaly: 333
3657 deg
Mean motion: 15
59686825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2314
Checksum: 319
Coasting Arc #11 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2011/311/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 547905
52 A = 6762281
75 meter
Y = -4486962
63 meter E =
0026841
Z = 5022217
62 I = 51
74732
XDOT = 7322
384460 Wp = 35
92623
YDOT = -1298
630102 meter/sec RA = 158
12032 deg
ZDOT = -1932
570810 TA = 72
90089
MA = 72
60708
Ha = 219
434 n
mi
Hp = 199
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1797590
29 X = 573641
36
Y = -14721006
02 feet Y = -4480691
54 meter
Z = 16477091
92 Z = 5024942
08
XDOT = 24023
571064 XDOT = 7345
750055
YDOT = -4260
597448 feet/sec YDOT = -1216
616135 meter/sec
ZDOT = -6340
455412 ZDOT = -1896
941110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12383882
27 X = 3774607
31
Y = 8136681
82 feet Y = 2480060
62 meter
Z = 16488413
40 Z = 5025668
40
XDOT = -6421
995045 XDOT = -1957
424090
YDOT = 22504
056660 feet/sec YDOT = 6859
236470 meter/sec
ZDOT = -6195
051244 ZDOT = -1888
251619
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 11311
59396732
00016717 00000-0 10270-3 0 9109
2 25544 51
6380 158
9569 0021622 30
4948 329
7460 15
59730704 23309
Satellite: ISS
Catalog Number: 25544
Epoch time: 11311
59396732 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 158
9569 deg
Eccentricity:
0021622
Arg of perigee: 30
4948 deg
Mean anomaly: 329
7460 deg
Mean motion: 15
59730704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 312
Coasting Arc #12 (Orbit 2344)
---------------------------------------
Vector Time (GMT): 2011/312/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4038205
69 A = 6769307
83 meter
Y = 4595726
25 meter E =
0025635
Z = -2885454
69 I = 51
79817
XDOT = -5511
126677 Wp = 39
95371
YDOT = -1683
074104 meter/sec RA = 153
09340 deg
ZDOT = 5076
234008 TA = 287
16937
MA = 287
44987
Ha = 219
399 n
mi
Hp = 199
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13248706
33 X = -4075278
52
Y = 15077842
04 feet Y = 4550361
21 meter
Z = -9466714
87 Z = -2905162
93
XDOT = -18081
124270 XDOT = -5516
556627
YDOT = -5521
896666 feet/sec YDOT = -1744
733144 meter/sec
ZDOT = 16654
311050 ZDOT = 5049
447161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7852299
10 X = -2393380
76
Y = -18430355
75 feet Y = -5617572
43 meter
Z = -9547335
55 Z = -2910027
87
XDOT = 11525
305660 XDOT = 3512
913165
YDOT = -13406
875376 feet/sec YDOT = -4086
415615 meter/sec
ZDOT = 16545
111339 ZDOT = 5042
949936
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 11312
55501206
00016717 00000-0 10270-3 0 9111
2 25544 51
6369 154
1241 0021597 34
2643 325
9901 15
59784765 23456
Satellite: ISS
Catalog Number: 25544
Epoch time: 11312
55501206 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 154
1241 deg
Eccentricity:
0021597
Arg of perigee: 34
2643 deg
Mean anomaly: 325
9901 deg
Mean motion: 15
59784765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2345
Checksum: 301
Coasting Arc #13 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2011/313/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5975506
98 A = 6772500
96 meter
Y = -3142569
28 meter E =
0022313
Z = -622340
63 I = 51
83607
XDOT = 1738
223183 Wp = 66
41178
YDOT = 4458
588569 meter/sec RA = 148
10540 deg
ZDOT = -5985
266950 TA = 120
29243
MA = 120
07147
Ha = 219
447 n
mi
Hp = 199
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19604681
69 X = 6013226
99
Y = -10310266
65 feet Y = -3075536
59 meter
Z = -2041799
96 Z = -593219
22
XDOT = 5702
831965 XDOT = 1717
313271
YDOT = 14627
915253 feet/sec YDOT = 4477
909494 meter/sec
ZDOT = -19636
702592 ZDOT = -5976
873264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1148704
61 X = 350125
17
Y = 22131364
31 feet Y = 6745639
84 meter
Z = -1922831
53 Z = -586079
05
XDOT = -14106
536751 XDOT = -4299
672402
YDOT = -922
206269 feet/sec YDOT = -281
088471 meter/sec
ZDOT = -19602
676168 ZDOT = -5974
895696
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 11313
58009313
00016717 00000-0 10270-3 0 9128
2 25544 51
6368 148
9691 0021792 37
6633 322
6043 15
59879453 23616
Satellite: ISS
Catalog Number: 25544
Epoch time: 11313
58009313 = yrday
fracday
Element set: 912
Inclination: 51
6368 deg
RA of node: 148
9691 deg
Eccentricity:
0021792
Arg of perigee: 37
6633 deg
Mean anomaly: 322
6043 deg
Mean motion: 15
59879453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 318
Coasting Arc #14 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2011/314/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5562049
98 A = 6766528
60 meter
Y = 448153
01 meter E =
0029659
Z = 3792979
43 I = 51
84047
XDOT = 2410
093331 Wp = 60
67085
YDOT = -5963
187366 meter/sec RA = 143
10901 deg
ZDOT = 4228
244927 TA = 344
96828
MA = 345
05623
Ha = 219
491 n
mi
Hp = 198
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18248195
47 X = -5585074
01
Y = 1470318
27 feet Y = 385825
97 meter
Z = 12444158
23 Z = 3765902
36
XDOT = 7907
130351 XDOT = 2456
055156
YDOT = -19564
263012 feet/sec YDOT = -5935
979293 meter/sec
ZDOT = 13872
194644 ZDOT = 4240
065035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6038972
97 X = 1840678
96
Y = -17361663
96 feet Y = -5291835
17 meter
Z = 12333652
25 Z = 3759297
21
XDOT = 13484
858385 XDOT = 4110
184836
YDOT = 14604
411623 feet/sec YDOT = 4451
424663 meter/sec
ZDOT = 13920
728403 ZDOT = 4243
038017
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 11314
60514228
00016717 00000-0 10270-3 0 9139
2 25544 51
6359 143
8134 0021480 41
8734 318
4060 15
59903140 23775
Satellite: ISS
Catalog Number: 25544
Epoch time: 11314
60514228 = yrday
fracday
Element set: 913
Inclination: 51
6359 deg
RA of node: 143
8134 deg
Eccentricity:
0021480
Arg of perigee: 41
8734 deg
Mean anomaly: 318
4060 deg
Mean motion: 15
59903140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 288
Coasting Arc #15 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2011/315/13:10:42
147
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3232252
08 A = 6760616
17 meter
Y = 2706823
77 meter E =
0034265
Z = -5312298
46 I = 51
84514
XDOT = -5399
919165 Wp = 62
10350
YDOT = 5399
774572 meter/sec RA = 138
07405 deg
ZDOT = -521
123142 TA = 202
85307
MA = 203
00593
Ha = 219
445 n
mi
Hp = 198
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10604501
58 X = 3227550
44
Y = 8880655
41 feet Y = 2742942
68 meter
Z = -17428800
74 Z = -5296607
12
XDOT = -17716
270227 XDOT = -5457
367586
YDOT = 17715
795839 feet/sec YDOT = 5339
068171 meter/sec
ZDOT = -1709
721595 ZDOT = -547
495979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12334185
05 X = -3759459
60
Y = 6435240
43 feet Y = 1961461
28 meter
Z = -17364911
43 Z = -5292825
00
XDOT = -9007
597771 XDOT = -2745
515800
YDOT = -22285
143046 feet/sec YDOT = -6792
511600 meter/sec
ZDOT = -1817
627188 ZDOT = -554
012767
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 11315
56609655
00016717 00000-0 10270-3 0 9145
2 25544 51
6364 138
9808 0021616 45
7963 314
4964 15
59937154 23920
Satellite: ISS
Catalog Number: 25544
Epoch time: 11315
56609655 = yrday
fracday
Element set: 914
Inclination: 51
6364 deg
RA of node: 138
9808 deg
Eccentricity:
0021616
Arg of perigee: 45
7963 deg
Mean anomaly: 314
4964 deg
Mean motion: 15
59937154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 339
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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