Date:
October 25th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 349)
---------------------------------------
Vector Time (GMT): 2010/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -460287
37 A = 6733852
03 meter
Y = 5969026
76 meter E =
0020131
Z = 3061296
82 I = 51
35221
XDOT = -5581
552621 Wp = 100
64687
YDOT = 2086
720991 meter/sec RA = 298
54529 deg
ZDOT = -4884
487391 TA = 43
69548
MA = 43
53629
Ha = 195
720 n
mi
Hp = 184
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1510129
16 X = -541871
57
Y = 19583421
14 feet Y = 5963423
58 meter
Z = 10043624
73 Z = 3058862
13
XDOT = -18312
180516 XDOT = -5580
743248
YDOT = 6846
197477 feet/sec YDOT = 2024
308933 meter/sec
ZDOT = -16025
221098 ZDOT = -4911
601508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8442233
83 X = -2573192
87
Y = -17740249
02 feet Y = -5407227
90 meter
Z = 10033819
01 Z = 3058308
03
XDOT = 11051
359118 XDOT = 3368
454259
YDOT = -14428
055407 feet/sec YDOT = -4397
671288 meter/sec
ZDOT = -16133
908592 ZDOT = -4917
615339
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 10295
53810352
00016717 00000-0 10270-3 0 9001
2 25544 51
6438 299
0232 0007141 110
7438 249
4490 15
71987200 3503
Satellite: ISS
Catalog Number: 25544
Epoch time: 10295
53810352 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 299
0232 deg
Eccentricity:
0007141
Arg of perigee: 110
7438 deg
Mean anomaly: 249
4490 deg
Mean motion: 15
71987200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 350
Checksum: 288
Coasting Arc #2 (Orbit 365)
---------------------------------------
Vector Time (GMT): 2010/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4644925
46 A = 6731366
40 meter
Y = -2981896
62 meter E =
0018200
Z = 3841467
69 I = 51
33008
XDOT = 758
531082 Wp = 105
10423
YDOT = 6480
995929 meter/sec RA = 293
45453 deg
ZDOT = 4092
809943 TA = 301
91967
MA = 302
09656
Ha = 195
574 n
mi
Hp = 184
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15239256
76 X = 4659262
63
Y = -9783125
40 feet Y = -2929873
95 meter
Z = 12603240
46 Z = 3864068
38
XDOT = 2488
619037 XDOT = 666
120269
YDOT = 21263
110003 feet/sec YDOT = 6488
961756 meter/sec
ZDOT = 13427
854144 ZDOT = 4096
270252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7954881
87 X = -2424647
99
Y = 16197910
64 feet Y = 4937123
16 meter
Z = 12693845
14 Z = 3869084
00
XDOT = -11840
260768 XDOT = -3608
911482
YDOT = -16401
798007 feet/sec YDOT = -4999
268033 meter/sec
ZDOT = 13441
671030 ZDOT = 4097
021330
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 10296
55524191
00016717 00000-0 10270-3 0 9018
2 25544 51
6432 293
8158 0007075 115
2323 244
9573 15
72003155 3663
Satellite: ISS
Catalog Number: 25544
Epoch time: 10296
55524191 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 293
8158 deg
Eccentricity:
0007075
Arg of perigee: 115
2323 deg
Mean anomaly: 244
9573 deg
Mean motion: 15
72003155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 366
Checksum: 295
Coasting Arc #3 (Orbit 380)
---------------------------------------
Vector Time (GMT): 2010/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1691360
80 A = 6730827
86 meter
Y = -5140451
41 meter E =
0014258
Z = -4017783
80 I = 51
31737
XDOT = 4784
588905 Wp = 113
02529
YDOT = -4598
875658 meter/sec RA = 288
26008 deg
ZDOT = 3875
192318 TA = 197
18876
MA = 197
23709
Ha = 195
619 n
mi
Hp = 184
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5549083
99 X = -1614235
34
Y = -16864998
06 feet Y = -5158934
07 meter
Z = -13181705
39 Z = -4025813
24
XDOT = 15697
470160 XDOT = 4816
833214
YDOT = -15088
174730 feet/sec YDOT = -4545
191147 meter/sec
ZDOT = 12713
885557 ZDOT = 3898
514977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13577316
74 X = 4138366
14
Y = 11403008
08 feet Y = 3475636
86 meter
Z = -13213846
01 Z = -4027580
26
XDOT = -4420
100703 XDOT = -1347
246694
YDOT = 20083
547519 feet/sec YDOT = 6121
465284 meter/sec
ZDOT = 12807
397908 ZDOT = 3903
694882
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 10297
50878765
00016717 00000-0 10270-3 0 9024
2 25544 51
6433 288
9335 0007076 117
9476 242
2403 15
72009286 3816
Satellite: ISS
Catalog Number: 25544
Epoch time: 10297
50878765 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 288
9335 deg
Eccentricity:
0007076
Arg of perigee: 117
9476 deg
Mean anomaly: 242
2403 deg
Mean motion: 15
72009286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 381
Checksum: 324
Coasting Arc #4 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2010/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3548848
56 A = 6733953
32 meter
Y = 4925968
19 meter E =
0011643
Z = -2914917
44 I = 51
31972
XDOT = -2929
275387 Wp = 118
11472
YDOT = -5057
879756 meter/sec RA = 283
16517 deg
ZDOT = -5001
667139 TA = 95
55737
MA = 95
42457
Ha = 195
480 n
mi
Hp = 184
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11643203
93 X = -3589507
33
Y = 16161312
97 feet Y = 4886055
51 meter
Z = -9563377
42 Z = -2932257
00
XDOT = -9610
483553 XDOT = -2848
201614
YDOT = -16594
093689 feet/sec YDOT = -5090
183352 meter/sec
ZDOT = -16409
669092 ZDOT = -5015
701058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 919112
03 X = 280145
35
Y = -19863851
94 feet Y = -6054502
07 meter
Z = -9632914
49 Z = -2936112
34
XDOT = 15566
003410 XDOT = 4744
517839
YDOT = 8672
787211 feet/sec YDOT = 2643
465542 meter/sec
ZDOT = -16465
878269 ZDOT = -5018
799696
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 10298
52588023
00016717 00000-0 10270-3 0 9033
2 25544 51
6430 283
7246 0007115 121
7040 238
4816 15
72062165 3978
Satellite: ISS
Catalog Number: 25544
Epoch time: 10298
52588023 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 283
7246 deg
Eccentricity:
0007115
Arg of perigee: 121
7040 deg
Mean anomaly: 238
4816 deg
Mean motion: 15
72062165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 295
Coasting Arc #5 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2010/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3288107
94 A = 6727967
82 meter
Y = 3534092
94 meter E =
0012538
Z = 4675616
17 I = 51
29401
XDOT = -3112
547244 Wp = 91
75661
YDOT = 6503
095847 meter/sec RA = 277
97588 deg
ZDOT = -2720
618118 TA = 25
17351
MA = 25
11244
Ha = 195
237 n
mi
Hp = 184
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10787755
70 X = 3225630
77
Y = 11594793
10 feet Y = 3570513
12 meter
Z = 15339948
07 Z = 4691438
53
XDOT = -10211
769173 XDOT = -3171
818111
YDOT = 21335
616295 feet/sec YDOT = 6467
958125 meter/sec
ZDOT = -8925
912459 ZDOT = -2735
883120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15350148
93 X = -4678725
39
Y = -3638528
72 feet Y = -1109023
55 meter
Z = 15403341
96 Z = 4694938
63
XDOT = -3763
455065 XDOT = -1147
101104
YDOT = -22250
607181 feet/sec YDOT = -6781
985069 meter/sec
ZDOT = -8987
148207 ZDOT = -2739
282773
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 10299
54294770
00016717 00000-0 10270-3 0 9040
2 25544 51
6428 278
5168 0006925 125
7264 234
4537 15
72109634 4138
Satellite: ISS
Catalog Number: 25544
Epoch time: 10299
54294770 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 278
5168 deg
Eccentricity:
0006925
Arg of perigee: 125
7264 deg
Mean anomaly: 234
4537 deg
Mean motion: 15
72109634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 322
Coasting Arc #6 (Orbit 428)
---------------------------------------
Vector Time (GMT): 2010/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1767788
41 A = 6735896
45 meter
Y = -6235751
09 meter E =
0018293
Z = 1815361
24 I = 51
31864
XDOT = 4372
851889 Wp = 86
45791
YDOT = 2894
327376 meter/sec RA = 272
86943 deg
ZDOT = 5635
976496 TA = 293
75410
MA = 293
94586
Ha = 195
204 n
mi
Hp = 184
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5799830
73 X = 1828567
45
Y = -20458500
96 feet Y = -6215642
84 meter
Z = 5955909
58 Z = 1824096
81
XDOT = 14346
626931 XDOT = 4312
782806
YDOT = 9495
824723 feet/sec YDOT = 2942
891213 meter/sec
ZDOT = 18490
736535 ZDOT = 5657
074459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6998389
14 X = 2133109
01
Y = 20069678
22 feet Y = 6117237
92 meter
Z = 5990970
09 Z = 1826047
68
XDOT = -15645
616668 XDOT = -4768
783960
YDOT = -135
680424 feet/sec YDOT = -41
355393 meter/sec
ZDOT = 18575
288820 ZDOT = 5661
748032
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 10300
55998989
00016717 00000-0 10270-3 0 9058
2 25544 51
6430 273
3092 0007067 130
8859 229
2916 15
72188440 4297
Satellite: ISS
Catalog Number: 25544
Epoch time: 10300
55998989 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 273
3092 deg
Eccentricity:
0007067
Arg of perigee: 130
8859 deg
Mean anomaly: 229
2916 deg
Mean motion: 15
72188440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 429
Checksum: 329
Coasting Arc #7 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2010/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4151645
69 A = 6726059
49 meter
Y = -1469956
52 meter E =
0020145
Z = -5101357
96 I = 51
28503
XDOT = 864
276012 Wp = 111
49532
YDOT = -7494
415618 meter/sec RA = 267
69431 deg
ZDOT = 1453
485227 TA = 172
55165
MA = 172
52168
Ha = 195
174 n
mi
Hp = 184
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13620884
80 X = -4110117
87
Y = -4822692
01 feet Y = -1516150
39 meter
Z = -16736738
70 Z = -5121426
19
XDOT = 2835
551220 XDOT = 940
954824
YDOT = -24587
977748 feet/sec YDOT = -7484
322067 meter/sec
ZDOT = 4768
652320 ZDOT = 1457
870019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13777816
03 X = 4199478
33
Y = -4032307
23 feet Y = -1229047
24 meter
Z = -16817180
71 Z = -5125876
68
XDOT = 11866
682951 XDOT = 3616
964963
YDOT = 20548
899902 feet/sec YDOT = 6263
304690 meter/sec
ZDOT = 4786
275354 ZDOT = 1458
856728
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 10301
51344762
00016717 00000-0 10270-3 0 9060
2 25544 51
6432 268
4259 0006921 132
7381 227
4365 15
72161652 4449
Satellite: ISS
Catalog Number: 25544
Epoch time: 10301
51344762 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 268
4259 deg
Eccentricity:
0006921
Arg of perigee: 132
7381 deg
Mean anomaly: 227
4365 deg
Mean motion: 15
72161652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 444
Checksum: 293
Coasting Arc #8 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2010/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 284684
57 A = 6737019
23 meter
Y = 6683847
76 meter E =
0017416
Z = -727437
93 I = 51
32532
XDOT = -4863
245873 Wp = 138
75790
YDOT = -430
782019 meter/sec RA = 262
56799 deg
ZDOT = -5955
166506 TA = 49
20105
MA = 49
05010
Ha = 194
989 n
mi
Hp = 184
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 934004
49 X = 213457
20
Y = 21928634
38 feet Y = 6686633
03 meter
Z = -2386607
37 Z = -726227
83
XDOT = -15955
531078 XDOT = -4829
137790
YDOT = -1413
326833 feet/sec YDOT = -484
974963 meter/sec
ZDOT = -19537
947854 ZDOT = -5978
709657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13933727
30 X = -4247000
08
Y = -16959115
45 feet Y = -5169138
39 meter
Z = -2381787
51 Z = -725968
83
XDOT = 12274
160443 XDOT = 3741
164103
YDOT = -7370
626233 feet/sec YDOT = -2246
566876 meter/sec
ZDOT = -19632
334193 ZDOT = -5983
935462
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 10302
53044281
00016717 00000-0 10270-3 0 9077
2 25544 51
6436 263
2174 0006845 136
4171 223
7533 15
72220022 4606
Satellite: ISS
Catalog Number: 25544
Epoch time: 10302
53044281 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 263
2174 deg
Eccentricity:
0006845
Arg of perigee: 136
4171 deg
Mean anomaly: 223
7533 deg
Mean motion: 15
72220022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 460
Checksum: 267
Coasting Arc #9 (Orbit 475)
---------------------------------------
Vector Time (GMT): 2010/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4142468
28 A = 6725065
06 meter
Y = -725507
93 meter E =
0008319
Z = 5241955
85 I = 51
29055
XDOT = 1539
602491 Wp = 126
18880
YDOT = 7546
560307 meter/sec RA = 257
41467 deg
ZDOT = -176
854653 TA = 325
47000
MA = 325
52401
Ha = 194
749 n
mi
Hp = 184
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13590775
18 X = 4124808
36
Y = -2380275
35 feet Y = -679283
07 meter
Z = 17198017
88 Z = 5262037
32
XDOT = 5051
189276 XDOT = 1455
960165
YDOT = 24759
056126 feet/sec YDOT = 7563
309398 meter/sec
ZDOT = -580
231801 ZDOT = -169
578375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9178731
13 X = -2797677
25
Y = 10166110
19 feet Y = 3098630
39 meter
Z = 17278535
77 Z = 5266497
70
XDOT = -18460
983480 XDOT = -5626
907765
YDOT = -15757
170813 feet/sec YDOT = -4802
785664 meter/sec
ZDOT = -551
082521 ZDOT = -167
969953
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 10303
54741289
00016717 00000-0 10270-3 0 9082
2 25544 51
6435 258
0096 0006798 140
5877 219
5781 15
72258568 4767
Satellite: ISS
Catalog Number: 25544
Epoch time: 10303
54741289 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 258
0096 deg
Eccentricity:
0006798
Arg of perigee: 140
5877 deg
Mean anomaly: 219
5781 deg
Mean motion: 15
72258568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 476
Checksum: 343
Coasting Arc #10 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2010/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2351104
86 A = 6736929
82 meter
Y = -6299192
53 meter E =
0011925
Z = -400847
72 I = 51
33834
XDOT = 4389
147191 Wp = 76
11078
YDOT = -2009
733593 meter/sec RA = 252
26635 deg
ZDOT = 5990
523622 TA = 279
51822
MA = 279
65297
Ha = 194
759 n
mi
Hp = 184
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7713598
62 X = -2278544
11
Y = -20666642
17 feet Y = -6325078
30 meter
Z = -1315117
19 Z = -412093
12
XDOT = 14400
089210 XDOT = 4382
192924
YDOT = -6593
614150 feet/sec YDOT = -1960
690233 meter/sec
ZDOT = 19653
948890 ZDOT = 6011
829541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18975204
01 X = 5783642
18
Y = 11244142
19 feet Y = 3427214
54 meter
Z = -1360196
57 Z = -414587
92
XDOT = -6155
132290 XDOT = -1876
084322
YDOT = 12716
705123 feet/sec YDOT = 3876
051721 meter/sec
ZDOT = 19739
381989 ZDOT = 6016
563630
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 10304
50079879
00016717 00000-0 10270-3 0 9099
2 25544 51
6432 253
1261 0006846 144
3826 215
7795 15
72302325 4915
Satellite: ISS
Catalog Number: 25544
Epoch time: 10304
50079879 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 253
1261 deg
Eccentricity:
0006846
Arg of perigee: 144
3826 deg
Mean anomaly: 215
7795 deg
Mean motion: 15
72302325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 308
Coasting Arc #11 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2010/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3369096
62 A = 6725237
90 meter
Y = 2684931
75 meter E =
0018220
Z = -5179022
17 I = 51
31030
XDOT = -3709
527278 Wp = 101
84112
YDOT = -6650
149612 meter/sec RA = 247
13362 deg
ZDOT = -1041
225542 TA = 158
20243
MA = 158
12480
Ha = 194
593 n
mi
Hp = 184
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11053466
59 X = -3373710
46
Y = 8808831
21 feet Y = 2647230
46 meter
Z = -16991542
56 Z = -5195400
83
XDOT = -12170
365084 XDOT = -3629
830200
YDOT = -21818
076156 feet/sec YDOT = -6691
186213 meter/sec
ZDOT = -3416
094297 ZDOT = -1059
052830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2755151
52 X = 839770
18
Y = -13782146
10 feet Y = -4200798
13 meter
Z = -17057219
54 Z = -5199040
52
XDOT = 22309
295930 XDOT = 6799
873399
YDOT = 8748
721665 feet/sec YDOT = 2666
610363 meter/sec
ZDOT = -3487
576315 ZDOT = -1063
013261
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 10305
51771916
00016717 00000-0 10270-3 0 9104
2 25544 51
6439 247
9165 0006742 148
4457 211
7111 15
72330563 5077
Satellite: ISS
Catalog Number: 25544
Epoch time: 10305
51771916 = yrday
fracday
Element set: 910
Inclination: 51
6439 deg
RA of node: 247
9165 deg
Eccentricity:
0006742
Arg of perigee: 148
4457 deg
Mean anomaly: 211
7111 deg
Mean motion: 15
72330563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 295
Coasting Arc #12 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2010/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4040567
60 A = 6735944
37 meter
Y = 5186851
36 meter E =
0020049
Z = 1411977
07 I = 51
36030
XDOT = -3111
788698 Wp = 129
75049
YDOT = 4013
018675 meter/sec RA = 241
96673 deg
ZDOT = -5795
108461 TA = 34
65600
MA = 34
52551
Ha = 194
463 n
mi
Hp = 184
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13256455
37 X = 3975407
68
Y = 17017228
89 feet Y = 5231671
17 meter
Z = 4632470
70 Z = 1431448
01
XDOT = -10209
280504 XDOT = -3128
279568
YDOT = 13166
071767 feet/sec YDOT = 3978
128279 meter/sec
ZDOT = -19012
823034 ZDOT = -5810
266104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21138984
11 X = -6443162
36
Y = -4211119
11 feet Y = -1283549
10 meter
Z = 4710551
92 Z = 1435776
22
XDOT = -1288
099817 XDOT = -392
612824
YDOT = -15020
452387 feet/sec YDOT = -4578
233888 meter/sec
ZDOT = -19073
602702 ZDOT = -5813
634103
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 10306
53461430
00016717 00000-0 10270-3 0 9115
2 25544 51
6446 242
7075 0006774 151
9821 208
1707 15
72365571 5233
Satellite: ISS
Catalog Number: 25544
Epoch time: 10306
53461430 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 242
7075 deg
Eccentricity:
0006774
Arg of perigee: 151
9821 deg
Mean anomaly: 208
1707 deg
Mean motion: 15
72365571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 292
Coasting Arc #13 (Orbit 538)
---------------------------------------
Vector Time (GMT): 2010/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1935594
92 A = 6726158
74 meter
Y = -4189331
32 meter E =
0012633
Z = 4889632
70 I = 51
34365
XDOT = 5386
018347 Wp = 140
51207
YDOT = 5052
565391 meter/sec RA = 236
85474 deg
ZDOT = 2184
127369 TA = 288
12354
MA = 288
26107
Ha = 194
240 n
mi
Hp = 184
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6350377
02 X = 1958543
37
Y = -13744525
32 feet Y = -4167557
80 meter
Z = 16042102
02 Z = 4899091
99
XDOT = 17670
663869 XDOT = 5318
508945
YDOT = 16576
658106 feet/sec YDOT = 5112
417719 meter/sec
ZDOT = 7165
772207 ZDOT = 2210
129113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4512708
51 X = 1375473
56
Y = 14410287
12 feet Y = 4392255
51 meter
Z = 16080030
74 Z = 4901193
37
XDOT = -23139
935532 XDOT = -7053
052350
YDOT = -912
381690 feet/sec YDOT = -278
093939 meter/sec
ZDOT = 7270
048027 ZDOT = 2215
910638
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 10307
55148157
00016717 00000-0 10270-3 0 9127
2 25544 51
6448 237
4987 0006758 157
3831 202
7631 15
72447081 5391
Satellite: ISS
Catalog Number: 25544
Epoch time: 10307
55148157 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 237
4987 deg
Eccentricity:
0006758
Arg of perigee: 157
3831 deg
Mean anomaly: 202
7631 deg
Mean motion: 15
72447081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 539
Checksum: 322
Coasting Arc #14 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2010/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5214836
11 A = 6734105
88 meter
Y = -3549891
88 meter E =
0006759
Z = -2365903
01 I = 51
38825
XDOT = 1222
549223 Wp = 111
31453
YDOT = -5367
614908 meter/sec RA = 231
67275 deg
ZDOT = 5368
983151 TA = 221
98050
MA = 222
03233
Ha = 194
182 n
mi
Hp = 184
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17109042
36 X = -5163259
50
Y = -11646626
90 feet Y = -3607918
99 meter
Z = -7762148
99 Z = -2391112
08
XDOT = 4010
988266 XDOT = 1256
397685
YDOT = -17610
285130 feet/sec YDOT = -5353
754238 meter/sec
ZDOT = 17614
774118 ZDOT = 5375
004827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20430367
78 X = 6227176
10
Y = -3063264
22 feet Y = -933682
93 meter
Z = -7863249
36 Z = -2396718
41
XDOT = 8887
326479 XDOT = 2708
857111
YDOT = 14077
920779 feet/sec YDOT = 4290
950253 meter/sec
ZDOT = 17638
917420 ZDOT = 5376
342030
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 10308
50477424
00016717 00000-0 10270-3 0 9136
2 25544 51
6449 232
6145 0006656 160
1835 199
9587 15
72445750 5543
Satellite: ISS
Catalog Number: 25544
Epoch time: 10308
50477424 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 232
6145 deg
Eccentricity:
0006656
Arg of perigee: 160
1835 deg
Mean anomaly: 199
9587 deg
Mean motion: 15
72445750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 554
Checksum: 323
Coasting Arc #15 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2010/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -157252
87 A = 6727748
81 meter
Y = 5030236
92 meter E =
0011389
Z = -4472653
76 I = 51
38801
XDOT = -6330
360972 Wp = 105
40900
YDOT = -3006
827005 meter/sec RA = 226
57517 deg
ZDOT = -3168
785531 TA = 132
81822
MA = 132
72244
Ha = 194
007 n
mi
Hp = 185
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -515921
49 X = -191762
18
Y = 16503401
97 feet Y = 5028285
48 meter
Z = -14674060
89 Z = -4473501
53
XDOT = -20768
900826 XDOT = -6280
873691
YDOT = -9864
917994 feet/sec YDOT = -3077
340202 meter/sec
ZDOT = -10396
277989 ZDOT = -3199
419224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11119346
22 X = -3389176
73
Y = -12202003
63 feet Y = -3719170
71 meter
Z = -14677457
60 Z = -4473689
08
XDOT = 20879
928659 XDOT = 6364
202255
YDOT = -6412
304459 feet/sec YDOT = -1954
470399 meter/sec
ZDOT = -10519
139570 ZDOT = -3206
233741
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 10309
52159345
00016717 00000-0 10270-3 0 9149
2 25544 51
6459 227
4048 0006661 163
4220 196
7162 15
72507416 5708
Satellite: ISS
Catalog Number: 25544
Epoch time: 10309
52159345 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 227
4048 deg
Eccentricity:
0006661
Arg of perigee: 163
4220 deg
Mean anomaly: 196
7162 deg
Mean motion: 15
72507416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 301
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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