Date:
September 8th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 1844)
---------------------------------------
Vector Time (GMT): 2009/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2838320
14 A = 6730379
57 meter
Y = 5724684
52 meter E =
0020609
Z = 2098063
29 I = 51
32453
XDOT = -3728
202025 Wp = 87
72560
YDOT = 3884
112469 meter/sec RA = 258
86557 deg
ZDOT = -5507
028837 TA = 68
72140
MA = 68
50146
Ha = 193
307 n
mi
Hp = 180
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9312073
96 X = 2763902
85
Y = 18781773
36 feet Y = 5756008
34 meter
Z = 6883409
74 Z = 2111670
60
XDOT = -12231
633941 XDOT = -3744
605809
YDOT = 12743
151144 feet/sec YDOT = 3842
329436 meter/sec
ZDOT = -18067
679910 ZDOT = -5525
180401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3365897
53 X = -1025925
57
Y = -20673556
71 feet Y = -6301300
09 meter
Z = 6937279
62 Z = 2114482
83
XDOT = 13818
338176 XDOT = 4211
829476
YDOT = -8388
267303 feet/sec YDOT = -2556
743874 meter/sec
ZDOT = -18138
861834 ZDOT = -5528
725087
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 09247
53598532
00020000 00000-0 20000-3 0 9001
2 25544 51
6387 259
5149 0009289 52
5929 307
6078 15
73951261 18456
Satellite: ISS
Catalog Number: 25544
Epoch time: 09247
53598532 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 259
5149 deg
Eccentricity:
0009289
Arg of perigee: 52
5929 deg
Mean anomaly: 307
6078 deg
Mean motion: 15
73951261 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1845
Checksum: 329
Coasting Arc #2 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2009/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2933406
75 A = 6722201
37 meter
Y = -3667644
36 meter E =
0013797
Z = 4797133
81 I = 51
30337
XDOT = 3835
892169 Wp = 83
55522
YDOT = 6236
345571 meter/sec RA = 253
74499 deg
ZDOT = 2417
962966 TA = 342
73062
MA = 342
77751
Ha = 193
256 n
mi
Hp = 180
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9624037
88 X = 2950897
42
Y = -12032953
94 feet Y = -3634743
11 meter
Z = 15738628
00 Z = 4811427
03
XDOT = 12584
948061 XDOT = 3754
125195
YDOT = 20460
451348 feet/sec YDOT = 6278
783779 meter/sec
ZDOT = 7932
949363 ZDOT = 2436
398572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12485885
02 X = -3805697
75
Y = 8930315
82 feet Y = 2721960
26 meter
Z = 15794639
33 Z = 4814206
07
XDOT = -5745
462961 XDOT = -1751
217110
YDOT = -22218
102598 feet/sec YDOT = -6772
077672 meter/sec
ZDOT = 8005
853615 ZDOT = 2440
184182
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 09248
55185257
00020000 00000-0 20000-3 0 9011
2 25544 51
6381 254
2976 0009253 56
1817 304
0226 15
73951561 18614
Satellite: ISS
Catalog Number: 25544
Epoch time: 09248
55185257 = yrday
fracday
Element set: 901
Inclination: 51
6381 deg
RA of node: 254
2976 deg
Eccentricity:
0009253
Arg of perigee: 56
1817 deg
Mean anomaly: 304
0226 deg
Mean motion: 15
73951561 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1861
Checksum: 297
Coasting Arc #3 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2009/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3826121
66 A = 6730187
25 meter
Y = -5114325
35 meter E =
0015427
Z = -2113518
69 I = 51
34095
XDOT = 2971
797941 Wp = 52
73342
YDOT = -4484
012016 meter/sec RA = 248
54916 deg
ZDOT = 5507
351414 TA = 283
54430
MA = 283
71612
Ha = 193
287 n
mi
Hp = 180
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12552892
59 X = -3758380
92
Y = -16779282
65 feet Y = -5156732
71 meter
Z = -6934116
44 Z = -2131941
07
XDOT = 9749
993245 XDOT = 2994
964296
YDOT = -14711
325511 feet/sec YDOT = -4450
649651 meter/sec
ZDOT = 18068
738235 ZDOT = 5521
845064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7724410
58 X = 2354400
35
Y = 19453486
65 feet Y = 5929422
73 meter
Z = -7006907
17 Z = -2135705
31
XDOT = -11716
057459 XDOT = -3571
054313
YDOT = 11137
713865 feet/sec YDOT = 3394
775186 meter/sec
ZDOT = 18125
485398 ZDOT = 5524
647949
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 09249
50421447
00020000 00000-0 20000-3 0 9022
2 25544 51
6386 249
4076 0009289 60
1134 300
0950 15
73999379 18767
Satellite: ISS
Catalog Number: 25544
Epoch time: 09249
50421447 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 249
4076 deg
Eccentricity:
0009289
Arg of perigee: 60
1134 deg
Mean anomaly: 300
0950 deg
Mean motion: 15
73999379 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1876
Checksum: 311
Coasting Arc #4 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2009/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2267284
51 A = 6722044
91 meter
Y = 4111078
13 meter E =
0021193
Z = -4830730
26 I = 51
32460
XDOT = -4855
092934 Wp = 68
68873
YDOT = -5463
527485 meter/sec RA = 243
42871 deg
ZDOT = -2371
669132 TA = 178
02819
MA = 178
01983
Ha = 193
353 n
mi
Hp = 180
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7438597
48 X = -2289619
82
Y = 13487789
14 feet Y = 4085598
79 meter
Z = -15848852
55 Z = -4841799
34
XDOT = -15928
782593 XDOT = -4782
116771
YDOT = -17924
958941 feet/sec YDOT = -5517
412132 meter/sec
ZDOT = -7781
066707 ZDOT = -2395
077663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10404511
65 X = 3171295
15
Y = -11297127
13 feet Y = -3443364
35 meter
Z = -15892148
10 Z = -4843926
74
XDOT = 10225
355140 XDOT = 3116
688247
YDOT = 20489
807020 feet/sec YDOT = 6245
293180 meter/sec
ZDOT = -7873
500909 ZDOT = -2399
843077
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 09250
52005368
00020000 00000-0 20000-3 0 9037
2 25544 51
6378 244
1894 0009238 63
1825 297
0282 15
73991169 18922
Satellite: ISS
Catalog Number: 25544
Epoch time: 09250
52005368 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 244
1894 deg
Eccentricity:
0009238
Arg of perigee: 63
1825 deg
Mean anomaly: 297
0282 deg
Mean motion: 15
73991169 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1892
Checksum: 311
Coasting Arc #5 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2009/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4646033
30 A = 6730199
20 meter
Y = 4413892
20 meter E =
0021639
Z = 2034941
50 I = 51
36722
XDOT = -2188
020258 Wp = 93
29946
YDOT = 4881
340245 meter/sec RA = 238
23397 deg
ZDOT = -5542
929154 TA = 63
90564
MA = 63
68310
Ha = 193
265 n
mi
Hp = 180
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15242891
41 X = 4586445
62
Y = 14481273
61 feet Y = 4465513
82 meter
Z = 6676317
27 Z = 2057367
16
XDOT = -7178
544153 XDOT = -2215
514816
YDOT = 16014
895818 feet/sec YDOT = 4856
718472 meter/sec
ZDOT = -18185
463104 ZDOT = -5553
625719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11530791
54 X = -3514585
26
Y = -17547200
15 feet Y = -5348386
61 meter
Z = 6764824
41 Z = 2061918
48
XDOT = 9234
586906 XDOT = 2814
702089
YDOT = -13157
005582 feet/sec YDOT = -4010
255301 meter/sec
ZDOT = -18227
245618 ZDOT = -5555
664464
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 09251
53587713
00020000 00000-0 20000-3 0 9049
2 25544 51
6378 238
9718 0009256 65
7177 294
4952 15
74048253 19087
Satellite: ISS
Catalog Number: 25544
Epoch time: 09251
53587713 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 238
9718 deg
Eccentricity:
0009256
Arg of perigee: 65
7177 deg
Mean anomaly: 294
4952 deg
Mean motion: 15
74048253 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1908
Checksum: 328
Coasting Arc #6 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2009/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1541581
88 A = 6721769
98 meter
Y = -4390886
59 meter E =
0014350
Z = 4838157
28 I = 51
35531
XDOT = 5753
647698 Wp = 91
71493
YDOT = 4580
445140 meter/sec RA = 233
11605 deg
ZDOT = 2317
385277 TA = 335
61994
MA = 335
68775
Ha = 193
214 n
mi
Hp = 180
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5057683
34 X = 1567063
80
Y = -14405795
91 feet Y = -4373505
07 meter
Z = 15873219
42 Z = 4845708
42
XDOT = 18876
796909 XDOT = 5690
743180
YDOT = 15027
707151 feet/sec YDOT = 4644
434175 meter/sec
ZDOT = 7602
970070 ZDOT = 2345
183849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7874025
40 X = -2400002
94
Y = 13044975
95 feet Y = 3976108
67 meter
Z = 15902658
21 Z = 4847130
22
XDOT = -14312
989740 XDOT = -4362
599273
YDOT = -18066
866255 feet/sec YDOT = -5506
780835 meter/sec
ZDOT = 7712
633990 ZDOT = 2350
810840
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 09252
55168628
00020000 00000-0 20000-3 0 9053
2 25544 51
6375 233
7551 0009129 69
6926 290
5217 15
74053970 19247
Satellite: ISS
Catalog Number: 25544
Epoch time: 09252
55168628 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 233
7551 deg
Eccentricity:
0009129
Arg of perigee: 69
6926 deg
Mean anomaly: 290
5217 deg
Mean motion: 15
74053970 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1924
Checksum: 312
Coasting Arc #7 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2009/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5354682
24 A = 6730185
56 meter
Y = -3551342
51 meter E =
0015314
Z = -1998005
23 I = 51
40284
XDOT = 1346
657865 Wp = 60
00324
YDOT = -5141
100356 meter/sec RA = 227
92480 deg
ZDOT = 5568
292676 TA = 277
66751
MA = 277
84141
Ha = 193
288 n
mi
Hp = 180
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17567855
13 X = -5304866
50
Y = -11651386
20 feet Y = -3610943
21 meter
Z = -6555135
26 Z = -2023897
49
XDOT = 4418
168848 XDOT = 1376
996414
YDOT = -16867
127151 feet/sec YDOT = -5125
871536 meter/sec
ZDOT = 18268
676757 ZDOT = 5574
908562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14954997
11 X = 4558283
12
Y = 14811593
75 feet Y = 4514573
78 meter
Z = -6657242
99 Z = -2029127
66
XDOT = -6401
554671 XDOT = -1951
193864
YDOT = 14629
043680 feet/sec YDOT = 4458
932514 meter/sec
ZDOT = 18294
390868 ZDOT = 5576
130336
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 09253
50399306
00020000 00000-0 20000-3 0 9069
2 25544 51
6374 228
8643 0009305 73
6396 286
5790 15
74067631 19391
Satellite: ISS
Catalog Number: 25544
Epoch time: 09253
50399306 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 228
8643 deg
Eccentricity:
0009305
Arg of perigee: 73
6396 deg
Mean anomaly: 286
5790 deg
Mean motion: 15
74067631 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1939
Checksum: 322
Coasting Arc #8 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2009/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -842413
65 A = 6721537
66 meter
Y = 4548496
78 meter E =
0021601
Z = -4896383
00 I = 51
39496
XDOT = -6440
240061 Wp = 75
34559
YDOT = -3564
465331 meter/sec RA = 222
80699 deg
ZDOT = -2205
922444 TA = 173
11716
MA = 173
08744
Ha = 193
285 n
mi
Hp = 180
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2763824
30 X = -869427
20
Y = 14922889
69 feet Y = 4538925
40 meter
Z = -16064248
68 Z = -4900541
06
XDOT = -21129
396524 XDOT = -6389
186892
YDOT = -11694
440063 feet/sec YDOT = -3636
198416 meter/sec
ZDOT = -7237
278361 ZDOT = -2237
085359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5252379
68 X = 1600925
33
Y = -14220653
04 feet Y = -4334455
05 meter
Z = -16080329
03 Z = -4901284
29
XDOT = 17665
082693 XDOT = 5384
317205
YDOT = 14837
058422 feet/sec YDOT = 4522
335407 meter/sec
ZDOT = -7360
140350 ZDOT = -2243
370779
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 09254
51977125
00020000 00000-0 20000-3 0 9073
2 25544 51
6378 223
6461 0009200 77
0891 283
1299 15
74083944 19558
Satellite: ISS
Catalog Number: 25544
Epoch time: 09254
51977125 = yrday
fracday
Element set: 907
Inclination: 51
6378 deg
RA of node: 223
6461 deg
Eccentricity:
0009200
Arg of perigee: 77
0891 deg
Mean anomaly: 283
1299 deg
Mean motion: 15
74083944 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1955
Checksum: 313
Coasting Arc #9 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2009/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5885231
95 A = 6730266
54 meter
Y = 2662994
76 meter E =
0022361
Z = 1861122
41 I = 51
44767
XDOT = -567
980735 Wp = 100
46888
YDOT = 5227
890002 meter/sec RA = 217
62003 deg
ZDOT = -5631
115540 TA = 58
79816
MA = 58
57918
Ha = 193
183 n
mi
Hp = 180
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19308503
76 X = 5845975
46
Y = 8736859
45 feet Y = 2728587
36 meter
Z = 6106044
66 Z = 1889617
61
XDOT = -1863
453854 XDOT = -599
042683
YDOT = 17151
870084 feet/sec YDOT = 5221
364904 meter/sec
ZDOT = -18474
788516 ZDOT = -5633
950178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17639756
01 X = -5376597
63
Y = -11687845
79 feet Y = -3562455
40 meter
Z = 6218366
39 Z = 1895358
07
XDOT = 3606
009107 XDOT = 1099
111576
YDOT = -15368
490782 feet/sec YDOT = -4684
315990 meter/sec
ZDOT = -18485
617217 ZDOT = -5634
416128
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 09255
53553250
00020000 00000-0 20000-3 0 9086
2 25544 51
6377 218
4288 0009151 80
1529 280
0667 15
74125434 19718
Satellite: ISS
Catalog Number: 25544
Epoch time: 09255
53553250 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 218
4288 deg
Eccentricity:
0009151
Arg of perigee: 80
1529 deg
Mean anomaly: 280
0667 deg
Mean motion: 15
74125434 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1971
Checksum: 296
Coasting Arc #10 (Orbit 1986)
---------------------------------------
Vector Time (GMT): 2009/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 147794
16 A = 6721076
81 meter
Y = -4559885
48 meter E =
0014353
Z = 4924124
57 I = 51
44197
XDOT = 6994
566707 Wp = 100
43762
YDOT = 2486
394144 meter/sec RA = 212
50502 deg
ZDOT = 2084
842557 TA = 329
29134
MA = 329
37525
Ha = 193
069 n
mi
Hp = 180
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 484888
96 X = 174852
16
Y = -14960254
21 feet Y = -4558081
51 meter
Z = 16155264
35 Z = 4924908
25
XDOT = 22948
053501 XDOT = 6956
115805
YDOT = 8157
461104 feet/sec YDOT = 2564
396498 meter/sec
ZDOT = 6840
034637 ZDOT = 2118
728689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2509028
82 X = -764751
99
Y = 14753263
35 feet Y = 4496794
67 meter
Z = 16158059
43 Z = 4924976
51
XDOT = -20443
001573 XDOT = -6231
026880
YDOT = -11141
907901 feet/sec YDOT = -3396
053528 meter/sec
ZDOT = 6973
582166 ZDOT = 2125
547844
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 09256
55127595
00020000 00000-0 20000-3 0 9099
2 25544 51
6381 213
2121 0008970 84
3424 275
8762 15
74180560 19876
Satellite: ISS
Catalog Number: 25544
Epoch time: 09256
55127595 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 213
2121 deg
Eccentricity:
0008970
Arg of perigee: 84
3424 deg
Mean anomaly: 275
8762 deg
Mean motion: 15
74180560 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1987
Checksum: 307
Coasting Arc #11 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2009/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6277472
55 A = 6730285
04 meter
Y = -1664454
06 meter E =
0015011
Z = -1763185
31 I = 51
49871
XDOT = -206
271313 Wp = 65
95098
YDOT = -5191
133334 meter/sec RA = 207
32230 deg
ZDOT = 5678
793586 TA = 274
48890
MA = 274
66037
Ha = 193
111 n
mi
Hp = 180
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20595382
37 X = -6249828
60
Y = -5460807
28 feet Y = -1734497
91 meter
Z = -5784728
70 Z = -1793613
89
XDOT = -676
743153 XDOT = -175
794200
YDOT = -17031
277343 feet/sec YDOT = -5193
269499 meter/sec
ZDOT = 18631
212554 ZDOT = 5677
865625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19718902
67 X = 6010321
53
Y = 7984578
82 feet Y = 2433699
62 meter
Z = -5904630
04 Z = -1799731
24
XDOT = -764
270751 XDOT = -232
949725
YDOT = 15557
895304 feet/sec YDOT = 4742
046489 meter/sec
ZDOT = 18627
223515 ZDOT = 5677
577727
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 09257
50352199
00020000 00000-0 20000-3 0 9107
2 25544 51
6378 208
3203 0009103 87
5415 272
6790 15
74166727 20026
Satellite: ISS
Catalog Number: 25544
Epoch time: 09257
50352199 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 208
3203 deg
Eccentricity:
0009103
Arg of perigee: 87
5415 deg
Mean anomaly: 272
6790 deg
Mean motion: 15
74166727 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2002
Checksum: 285
Coasting Arc #12 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2009/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 463966
79 A = 6720788
63 meter
Y = 4487178
55 meter E =
0021903
Z = -5001357
65 I = 51
49492
XDOT = -7321
510974 Wp = 82
31994
YDOT = -1356
092205 meter/sec RA = 202
20695 deg
ZDOT = -1900
102121 TA = 169
28437
MA = 169
23763
Ha = 193
072 n
mi
Hp = 180
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1522200
75 X = 438051
38
Y = 14721714
40 feet Y = 4492221
79 meter
Z = -16408653
71 Z = -4999166
86
XDOT = -24020
705296 XDOT = -7296
572493
YDOT = -4449
121408 feet/sec YDOT = -1437
826290 meter/sec
ZDOT = -6233
930844 ZDOT = -1935
609077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22485
53 X = -6853
59
Y = -14810070
02 feet Y = -4514109
34 meter
Z = -16399731
92 Z = -4998638
29
XDOT = 22285
076312 XDOT = 6792
491260
YDOT = 7008
778075 feet/sec YDOT = 2136
275557 meter/sec
ZDOT = -6373
821744 ZDOT = -1942
740867
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 09258
51923314
00020000 00000-0 20000-3 0 9113
2 25544 51
6388 203
1018 0009030 91
3316 268
8882 15
74199766 20181
Satellite: ISS
Catalog Number: 25544
Epoch time: 09258
51923314 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 203
1018 deg
Eccentricity:
0009030
Arg of perigee: 91
3316 deg
Mean anomaly: 268
8882 deg
Mean motion: 15
74199766 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2018
Checksum: 296
Coasting Arc #13 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2009/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6500569
90 A = 6730442
83 meter
Y = 695382
80 meter E =
0022745
Z = 1560919
50 I = 51
55681
XDOT = 858
179626 Wp = 108
77997
YDOT = 5045
686781 meter/sec RA = 197
03125 deg
ZDOT = -5760
831643 TA = 53
97217
MA = 53
76160
Ha = 193
014 n
mi
Hp = 180
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21327329
06 X = 6484728
26
Y = 2281439
62 feet Y = 767987
53 meter
Z = 5121126
98 Z = 1592460
50
XDOT = 2815
549954 XDOT = 829
678970
YDOT = 16554
090488 feet/sec YDOT = 5055
123684 meter/sec
ZDOT = -18900
366284 ZDOT = -5756
732226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21002752
84 X = -6401639
07
Y = -4201943
98 feet Y = -1280752
52 meter
Z = 5245370
62 Z = 1598788
97
XDOT = -1720
090720 XDOT = -524
283651
YDOT = -15219
260169 feet/sec YDOT = -4638
830499 meter/sec
ZDOT = -18883
885099 ZDOT = -5755
808178
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 09259
53492705
00020000 00000-0 20000-3 0 9122
2 25544 51
6396 197
8840 0009051 95
1244 265
0952 15
74222048 20342
Satellite: ISS
Catalog Number: 25544
Epoch time: 09259
53492705 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 197
8840 deg
Eccentricity:
0009051
Arg of perigee: 95
1244 deg
Mean anomaly: 265
0952 deg
Mean motion: 15
74222048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2034
Checksum: 296
Coasting Arc #14 (Orbit 2049)
---------------------------------------
Vector Time (GMT): 2009/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1029779
02 A = 6720264
50 meter
Y = -4309282
89 meter E =
0013810
Z = 5042866
89 I = 51
55251
XDOT = 7517
086886 Wp = 109
44831
YDOT = 205
330850 meter/sec RA = 191
91784 deg
ZDOT = 1702
193610 TA = 324
13209
MA = 324
22474
Ha = 192
884 n
mi
Hp = 180
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3378540
10 X = -1006012
59
Y = -14138067
24 feet Y = -4320665
13 meter
Z = 16544838
87 Z = 5037922
37
XDOT = 24662
358549 XDOT = 7505
963234
YDOT = 673
657644 feet/sec YDOT = 289
329304 meter/sec
ZDOT = 5584
624704 ZDOT = 1738
684437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2426870
58 X = 739710
15
Y = 14354908
30 feet Y = 4375376
05 meter
Z = 16525074
23 Z = 5036842
63
XDOT = -23466
534566 XDOT = -7152
599736
YDOT = -2658
407593 feet/sec YDOT = -810
282634 meter/sec
ZDOT = 5728
335598 ZDOT = 1745
996690
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 09260
55060099
00020000 00000-0 20000-3 0 9134
2 25544 51
6401 192
6668 0008851 99
5698 260
6466 15
74294865 20503
Satellite: ISS
Catalog Number: 25544
Epoch time: 09260
55060099 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 192
6668 deg
Eccentricity:
0008851
Arg of perigee: 99
5698 deg
Mean anomaly: 260
6466 deg
Mean motion: 15
74294865 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2050
Checksum: 319
Coasting Arc #15 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2009/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6575452
95 A = 6730506
07 meter
Y = 333681
89 meter E =
0014728
Z = -1393815
95 I = 51
61655
XDOT = -1466
736980 Wp = 70
86882
YDOT = -4816
631770 meter/sec RA = 186
74858 deg
ZDOT = 5820
959949 TA = 273
81093
MA = 273
97932
Ha = 192
865 n
mi
Hp = 180
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21573008
35 X = -6571924
61
Y = 1094756
85 feet Y = 260170
89 meter
Z = -4572886
97 Z = -1425751
02
XDOT = -4812
129201 XDOT = -1441
044793
YDOT = -15802
597670 feet/sec YDOT = -4832
889434 meter/sec
ZDOT = 19097
637628 ZDOT = 5813
897430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21573431
23 X = 6575581
84
Y = 120175
74 feet Y = 36629
57 meter
Z = -4698627
45 Z = -1432141
65
XDOT = 4034
634655 XDOT = 1229
756643
YDOT = 14481
285155 feet/sec YDOT = 4413
895715 meter/sec
ZDOT = 19069
494287 ZDOT = 5812
381859
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 09261
50278229
00020000 00000-0 20000-3 0 9147
2 25544 51
6401 187
7748 0008902 102
2365 257
9796 15
74270477 20651
Satellite: ISS
Catalog Number: 25544
Epoch time: 09261
50278229 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 187
7748 deg
Eccentricity:
0008902
Arg of perigee: 102
2365 deg
Mean anomaly: 257
9796 deg
Mean motion: 15
74270477 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2065
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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