Date:
August 1st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8794 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
213/08:18:49
534 2
7 4
1 4
1
N/A 2
0 -0
1 189
1
000/00:07:39
068 -2
4 0
2 187
8
Coasting Arc #1 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2009/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -218914
23 A = 6731527
59 meter
Y = -6692660
24 meter E =
0005228
Z = -654696
73 I = 51
99368
XDOT = 4779
848410 Wp = 169
73798
YDOT = 431
339402 meter/sec RA = 83
74463 deg
ZDOT = -6019
976333 TA = 17
35586
MA = 17
33800
Ha = 188
785 n
mi
Hp = 185
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -718222
54 X = -140879
11
Y = -21957546
73 feet Y = -6694671
88 meter
Z = -2147955
16 Z = -655571
43
XDOT = 15681
917355 XDOT = 4803
913628
YDOT = 1415
155520 feet/sec YDOT = 484
925709 meter/sec
ZDOT = -19750
578520 ZDOT = -5996
697463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16992530
53 X = -5179323
30
Y = 13924347
22 feet Y = 4244141
03 meter
Z = -2151714
24 Z = -655842
50
XDOT = -7476
583701 XDOT = -2278
862712
YDOT = -12155
668780 feet/sec YDOT = -3705
047844 meter/sec
ZDOT = -19659
015272 ZDOT = -5992
067855
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 09211
53049514
00010596 00000-0 82463-4 0 9004
2 25544 51
6423 84
3170 0006762 297
3050 62
7425 15
74161341 12780
Satellite: ISS
Catalog Number: 25544
Epoch time: 09211
53049514 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 84
3170 deg
Eccentricity:
0006762
Arg of perigee: 297
3050 deg
Mean anomaly: 62
7425 deg
Mean motion: 15
74161341 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1278
Checksum: 284
Coasting Arc #2 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2009/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4207550
58 A = 6719673
12 meter
Y = -113848
48 meter E =
0006144
Z = 5241282
67 I = 51
94996
XDOT = -854
980445 Wp = 330
92197
YDOT = -7604
381394 meter/sec RA = 78
61689 deg
ZDOT = -846
693686 TA = 127
13399
MA = 127
07785
Ha = 189
027 n
mi
Hp = 185
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13804299
80 X = -4231425
77
Y = -373518
62 feet Y = -161033
92 meter
Z = 17195809
30 Z = 5220784
56
XDOT = -2805
053953 XDOT = -765
770359
YDOT = -24948
757853 feet/sec YDOT = -7613
443381 meter/sec
ZDOT = -2777
866424 ZDOT = -850
631403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8359043
17 X = 2547836
36
Y = 11117134
53 feet Y = 3388502
60 meter
Z = 17115191
61 Z = 5216710
40
XDOT = -16985
384317 XDOT = -5177
145140
YDOT = 17096
970405 feet/sec YDOT = 5211
156579 meter/sec
ZDOT = -2793
704576 ZDOT = -851
521155
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 09212
54619255
00010596 00000-0 82463-4 0 9012
2 25544 51
6423 79
0989 0006901 302
5107 57
5389 15
74233039 12949
Satellite: ISS
Catalog Number: 25544
Epoch time: 09212
54619255 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 79
0989 deg
Eccentricity:
0006901
Arg of perigee: 302
5107 deg
Mean anomaly: 57
5389 deg
Mean motion: 15
74233039 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1294
Checksum: 311
Coasting Arc #3 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2009/213/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2092863
08 A = 6725958
45 meter
Y = -4793276
47 meter E =
0004405
Z = -4231890
56 I = 51
95719
XDOT = 4409
371387 Wp = 3
65659
YDOT = 5147
455099 meter/sec RA = 74
30615 deg
ZDOT = -3645
570836 TA = 229
34843
MA = 229
38673
Ha = 189
120 n
mi
Hp = 187
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6866348
67 X = 2166864
28
Y = -15725972
66 feet Y = -4769458
54 meter
Z = -13884155
37 Z = -4221544
41
XDOT = 14466
441557 XDOT = 4369
193266
YDOT = 16887
976045 feet/sec YDOT = 5196
539093 meter/sec
ZDOT = -11960
534238 ZDOT = -3624
247286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13387993
97 X = -4080660
56
Y = -10785953
74 feet Y = -3287558
70 meter
Z = -13843682
68 Z = -4219554
48
XDOT = 19291
838861 XDOT = 5880
152485
YDOT = -8685
285636 feet/sec YDOT = -2647
275062 meter/sec
ZDOT = -11876
437437 ZDOT = -3619
938131
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 09213
37145007
00010596 00000-0 82463-4 0 9024
2 25544 51
6415 74
8592 0007620 281
6185 78
4123 15
73467383 13078
Satellite: ISS
Catalog Number: 25544
Epoch time: 09213
37145007 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 74
8592 deg
Eccentricity:
0007620
Arg of perigee: 281
6185 deg
Mean anomaly: 78
4123 deg
Mean motion: 15
73467383 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1307
Checksum: 302
Coasting Arc #4 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2009/214/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4291465
14 A = 6729030
19 meter
Y = -3983447
47 meter E =
0005598
Z = 3313073
74 I = 51
95763
XDOT = 1743
555175 Wp = 73
11303
YDOT = -5818
494264 meter/sec RA = 69
14742 deg
ZDOT = -4729
248971 TA = 68
18280
MA = 68
12326
Ha = 189
369 n
mi
Hp = 187
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14079610
03 X = -4262696
66
Y = -13069053
38 feet Y = -4031276
71 meter
Z = 10869664
51 Z = 3292295
50
XDOT = 5720
325378 XDOT = 1831
462472
YDOT = -19089
548110 feet/sec YDOT = -5798
504697 meter/sec
ZDOT = -15515
908698 ZDOT = -4720
566118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16108974
59 X = -4910015
46
Y = 10550368
60 feet Y = 3215752
35 meter
Z = 10787763
49 Z = 3288110
31
XDOT = -16341
023667 XDOT = -4980
744014
YDOT = -9092
681990 feet/sec YDOT = -2771
449471 meter/sec
ZDOT = -15482
017018 ZDOT = -4718
918787
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 09214
38763304
00010596 00000-0 82463-4 0 9033
2 25544 51
6411 69
6451 0007646 285
2142 74
8175 15
73455198 13237
Satellite: ISS
Catalog Number: 25544
Epoch time: 09214
38763304 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 69
6451 deg
Eccentricity:
0007646
Arg of perigee: 285
2142 deg
Mean anomaly: 74
8175 deg
Mean motion: 15
73455198 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1323
Checksum: 310
Coasting Arc #5 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2009/215/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -931473
75 A = 6726632
23 meter
Y = 5302768
21 meter E =
0003308
Z = 4029427
68 I = 51
93850
XDOT = -5330
443806 Wp = 85
28060
YDOT = -3926
087901 meter/sec RA = 64
08776 deg
ZDOT = 3932
063983 TA = 324
27341
MA = 324
29554
Ha = 189
700 n
mi
Hp = 187
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3056016
23 X = -1010274
84
Y = 17397533
48 feet Y = 5291910
85 meter
Z = 13219907
08 Z = 4024711
88
XDOT = -17488
332698 XDOT = -5305
246350
YDOT = -12880
865816 feet/sec YDOT = -3985
555619 meter/sec
ZDOT = 12900
472384 ZDOT = 3906
229910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16240799
40 X = 4950195
66
Y = 6980957
12 feet Y = 2127795
73 meter
Z = 13201591
65 Z = 4023845
13
XDOT = -16005
150154 XDOT = -4878
369767
YDOT = 13016
237848 feet/sec YDOT = 3967
349296 meter/sec
ZDOT = 12798
685157 ZDOT = 3901
039236
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 09215
40380510
00010596 00000-0 82463-4 0 9042
2 25544 51
6415 64
4302 0007695 289
7678 70
2655 15
73474699 13393
Satellite: ISS
Catalog Number: 25544
Epoch time: 09215
40380510 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 64
4302 deg
Eccentricity:
0007695
Arg of perigee: 289
7678 deg
Mean anomaly: 70
2655 deg
Mean motion: 15
73474699 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1339
Checksum: 325
Coasting Arc #6 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2009/216/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4957498
93 A = 6728187
09 meter
Y = 2837453
70 meter E =
0003232
Z = -3551254
23 I = 51
93013
XDOT = -351
122722 Wp = 322
58395
YDOT = 6240
345014 meter/sec RA = 58
92550 deg
ZDOT = 4496
262465 TA = 355
29763
MA = 355
30066
Ha = 189
959 n
mi
Hp = 187
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16264760
26 X = 4942652
57
Y = 9309231
29 feet Y = 2892808
71 meter
Z = -11651096
55 Z = -3527206
97
XDOT = -1151
977435 XDOT = -442
718801
YDOT = 20473
572881 feet/sec YDOT = 6235
905955 meter/sec
ZDOT = 14751
517275 ZDOT = 4494
334901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12517503
23 X = 3815334
99
Y = -14025491
39 feet Y = -4274969
78 meter
Z = -11556382
15 Z = -3522385
28
XDOT = 18739
978981 XDOT = 5711
945593
YDOT = 4577
579734 feet/sec YDOT = 1395
246303 meter/sec
ZDOT = 14744
208310 ZDOT = 4494
034693
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 09216
35645664
00010596 00000-0 82463-4 0 9052
2 25544 51
6419 59
5415 0007808 293
5367 66
4976 15
73505554 13546
Satellite: ISS
Catalog Number: 25544
Epoch time: 09216
35645664 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 59
5415 deg
Eccentricity:
0007808
Arg of perigee: 293
5367 deg
Mean anomaly: 66
4976 deg
Mean motion: 15
73505554 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1354
Checksum: 338
Coasting Arc #7 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2009/217/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -318560
53 A = 6727186
51 meter
Y = -5524852
23 meter E =
0005398
Z = -3828367
43 I = 51
91070
XDOT = 5929
582681 Wp = 349
62486
YDOT = 2560
970460 meter/sec RA = 53
86501 deg
ZDOT = -4183
129247 TA = 236
66553
MA = 236
71722
Ha = 190
036 n
mi
Hp = 187
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1045146
11 X = -238159
91
Y = -18126155
61 feet Y = -5527964
70 meter
Z = -12560260
58 Z = -3829720
13
XDOT = 19454
011419 XDOT = 5920
825207
YDOT = 8402
134054 feet/sec YDOT = 2627
229913 meter/sec
ZDOT = -13724
177319 ZDOT = -4154
345027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17975264
13 X = -5478860
51
Y = -2529814
00 feet Y = -771087
31 meter
Z = -12565823
26 Z = -3830062
93
XDOT = 11814
949903 XDOT = 3601
196731
YDOT = -16243
888330 feet/sec YDOT = -4951
137163 meter/sec
ZDOT = -13610
839131 ZDOT = -4148
583767
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 09217
37260856
00010596 00000-0 82463-4 0 9062
2 25544 51
6421 54
3269 0007962 297
3630 62
6722 15
73514951 13701
Satellite: ISS
Catalog Number: 25544
Epoch time: 09217
37260856 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 54
3269 deg
Eccentricity:
0007962
Arg of perigee: 297
3630 deg
Mean anomaly: 62
6722 deg
Mean motion: 15
73514951 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1370
Checksum: 313
Coasting Arc #8 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2009/218/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5342927
78 A = 6727455
15 meter
Y = -1621858
58 meter E =
0007382
Z = 3753004
98 I = 51
89281
XDOT = -1089
262693 Wp = 41
63759
YDOT = -6311
938640 meter/sec RA = 48
69966 deg
ZDOT = -4268
247749 TA = 93
21301
MA = 93
12855
Ha = 190
233 n
mi
Hp = 186
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17529290
61 X = -5342625
80
Y = -5321058
32 feet Y = -1681604
87 meter
Z = 12313008
45 Z = 3727050
23
XDOT = -3573
696498 XDOT = -997
866633
YDOT = -20708
460106 feet/sec YDOT = -6323
608126 meter/sec
ZDOT = -14003
437496 ZDOT = -4273
317670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8323538
09 X = -2537014
41
Y = 16395546
92 feet Y = 4997362
70 meter
Z = 12210840
39 Z = 3721864
15
XDOT = -19804
611729 XDOT = -6036
445655
YDOT = 415
176436 feet/sec YDOT = 126
545778 meter/sec
ZDOT = -14023
657271 ZDOT = -4274
410736
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 09218
38875062
00010596 00000-0 82463-4 0 9076
2 25544 51
6418 49
1120 0007939 302
1922 57
8471 15
73544949 13862
Satellite: ISS
Catalog Number: 25544
Epoch time: 09218
38875062 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 49
1120 deg
Eccentricity:
0007939
Arg of perigee: 302
1922 deg
Mean anomaly: 57
8471 deg
Mean motion: 15
73544949 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1386
Checksum: 328
Coasting Arc #9 (Orbit 1401)
---------------------------------------
Vector Time (GMT): 2009/219/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1574050
01 A = 6727760
10 meter
Y = 5436462
57 meter E =
0006612
Z = 3629246
83 I = 51
87345
XDOT = -6212
410091 Wp = 55
18296
YDOT = -1144
461136 meter/sec RA = 43
63548 deg
ZDOT = 4406
819375 TA = 348
14653
MA = 348
16209
Ha = 190
456 n
mi
Hp = 186
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5164206
08 X = 1495511
69
Y = 17836163
30 feet Y = 5453625
25 meter
Z = 11906977
80 Z = 3636702
87
XDOT = -20381
922871 XDOT = -6220
557922
YDOT = -3754
793754 feet/sec YDOT = -1213
977687 meter/sec
ZDOT = 14458
068817 ZDOT = 4376
620243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18418014
24 X = 5613810
74
Y = -2206693
47 feet Y = -672600
17 meter
Z = 11936545
62 Z = 3638259
10
XDOT = -7108
251204 XDOT = -2166
594967
YDOT = 18270
149739 feet/sec YDOT = 5568
741640 meter/sec
ZDOT = 14339
226554 ZDOT = 4370
596254
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 09219
40488258
00010596 00000-0 82463-4 0 9088
2 25544 51
6420 43
8963 0008005 306
4344 53
6080 15
73528705 14022
Satellite: ISS
Catalog Number: 25544
Epoch time: 09219
40488258 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 43
8963 deg
Eccentricity:
0008005
Arg of perigee: 306
4344 deg
Mean anomaly: 53
6080 deg
Mean motion: 15
73528705 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1402
Checksum: 300
Coasting Arc #10 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2009/220/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5438858
62 A = 6726773
38 meter
Y = 369446
45 meter E =
0003242
Z = -3938586
76 I = 51
84769
XDOT = 2513
428740 Wp =
64098
YDOT = 6052
122939 meter/sec RA = 38
46705 deg
ZDOT = 4041
740246 TA = 311
22312
MA = 311
25107
Ha = 190
688 n
mi
Hp = 186
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17844024
34 X = 5453455
81
Y = 1212094
65 feet Y = 430348
66 meter
Z = -12921872
58 Z = -3912129
75
XDOT = 8246
157282 XDOT = 2425
932338
YDOT = 19856
046389 feet/sec YDOT = 6079
740266 meter/sec
ZDOT = 13260
302643 ZDOT = 4053
737892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3731886
15 X = 1137478
90
Y = -17567883
57 feet Y = -5354690
91 meter
Z = -12817786
93 Z = -3906861
46
XDOT = 19530
290432 XDOT = 5952
832524
YDOT = -5553
049328 feet/sec YDOT = -1692
569435 meter/sec
ZDOT = 13307
761124 ZDOT = 4056
205591
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 09220
35749503
00010596 00000-0 82463-4 0 9098
2 25544 51
6419 39
0071 0008203 309
1579 50
8854 15
73565336 14172
Satellite: ISS
Catalog Number: 25544
Epoch time: 09220
35749503 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 39
0071 deg
Eccentricity:
0008203
Arg of perigee: 309
1579 deg
Mean anomaly: 50
8854 deg
Mean motion: 15
73565336 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1417
Checksum: 310
Coasting Arc #11 (Orbit 1432)
---------------------------------------
Vector Time (GMT): 2009/221/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2782178
15 A = 6728238
17 meter
Y = -5072927
04 meter E =
0005939
Z = -3439143
34 I = 51
82848
XDOT = 6165
624774 Wp = 349
25931
YDOT = -261
462592 meter/sec RA = 33
40016 deg
ZDOT = -4595
179741 TA = 231
27791
MA = 231
33102
Ha = 190
729 n
mi
Hp = 186
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9127881
06 X = -2708538
50
Y = -16643461
43 feet Y = -5103627
22 meter
Z = -11283278
67 Z = -3452480
18
XDOT = 20228
427735 XDOT = 6190
412534
YDOT = -857
816902 feet/sec YDOT = -192
376314 meter/sec
ZDOT = -15076
049018 ZDOT = -4565
167292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17640717
46 X = -5376890
68
Y = 6923620
19 feet Y = 2110319
43 meter
Z = -11335959
14 Z = -3455200
35
XDOT = 2177
964810 XDOT = 663
843674
YDOT = -18978
640786 feet/sec YDOT = -5784
689712 meter/sec
ZDOT = -14958
009519 ZDOT = -4559
201301
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 09221
37360600
00010596 00000-0 82463-4 0 9100
2 25544 51
6417 33
7923 0008261 312
4672 47
5792 15
73562470 14330
Satellite: ISS
Catalog Number: 25544
Epoch time: 09221
37360600 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 33
7923 deg
Eccentricity:
0008261
Arg of perigee: 312
4672 deg
Mean anomaly: 47
5792 deg
Mean motion: 15
73562470 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1433
Checksum: 290
Coasting Arc #12 (Orbit 1448)
---------------------------------------
Vector Time (GMT): 2009/222/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5281071
70 A = 6726053
30 meter
Y = 815483
98 meter E =
0009771
Z = 4086798
21 I = 51
79656
XDOT = -3820
108181 Wp = 28
32259
YDOT = -5473
780154 meter/sec RA = 28
22855 deg
ZDOT = -3832
050969 TA = 101
04699
MA = 100
93708
Ha = 190
893 n
mi
Hp = 185
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17326350
71 X = -5309650
85
Y = 2675472
37 feet Y = 756268
11 meter
Z = 13408130
61 Z = 4061073
55
XDOT = -12533
163322 XDOT = -3740
000243
YDOT = -17958
596307 feet/sec YDOT = -5516
050909 meter/sec
ZDOT = -12572
345698 ZDOT = -3850
414376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 794973
62 X = 242307
96
Y = 17590643
22 feet Y = 5361628
05 meter
Z = 13306984
48 Z = 4055968
87
XDOT = -17908
016482 XDOT = -5458
363424
YDOT = 10405
264176 feet/sec YDOT = 3171
524521 meter/sec
ZDOT = -12644
809764 ZDOT = -3854
138016
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 09222
38970498
00010596 00000-0 82463-4 0 9115
2 25544 51
6423 28
5769 0008415 317
2518 42
7989 15
73641052 14496
Satellite: ISS
Catalog Number: 25544
Epoch time: 09222
38970498 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 28
5769 deg
Eccentricity:
0008415
Arg of perigee: 317
2518 deg
Mean anomaly: 42
7989 deg
Mean motion: 15
73641052 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1449
Checksum: 331
Coasting Arc #13 (Orbit 1464)
---------------------------------------
Vector Time (GMT): 2009/223/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3857597
61 A = 6728626
84 meter
Y = 4438704
27 meter E =
0010179
Z = 3255789
39 I = 51
77736
XDOT = -5843
944755 Wp = 46
61916
YDOT = 1582
041137 meter/sec RA = 23
15631 deg
ZDOT = 4764
909004 TA = 351
44450
MA = 351
46184
Ha = 191
035 n
mi
Hp = 185
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12656160
14 X = 3791860
57
Y = 14562678
07 feet Y = 4481474
59 meter
Z = 10681723
71 Z = 3274369
93
XDOT = -19173
047098 XDOT = -5884
348062
YDOT = 5190
423678 feet/sec YDOT = 1516
464738 meter/sec
ZDOT = 15632
903557 ZDOT = 4736
421103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15637844
44 X = 4766414
99
Y = -11231081
19 feet Y = -3423233
55 meter
Z = 10754991
39 Z = 3278121
37
XDOT = 2615
750544 XDOT = 797
280766
YDOT = 18512
593741 feet/sec YDOT = 5642
638572 meter/sec
ZDOT = 15520
924997 ZDOT = 4730
777939
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 09223
40579598
00010596 00000-0 82463-4 0 9126
2 25544 51
6414 23
3610 0008423 321
1223 38
9333 15
73604369 14658
Satellite: ISS
Catalog Number: 25544
Epoch time: 09223
40579598 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 23
3610 deg
Eccentricity:
0008423
Arg of perigee: 321
1223 deg
Mean anomaly: 38
9333 deg
Mean motion: 15
73604369 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1465
Checksum: 294
Coasting Arc #14 (Orbit 1479)
---------------------------------------
Vector Time (GMT): 2009/224/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4863090
13 A = 6725542
25 meter
Y = -1926695
52 meter E =
0004857
Z = -4227220
86 I = 51
73838
XDOT = 4976
971547 Wp = 34
60501
YDOT = 4621
269688 meter/sec RA = 17
98137 deg
ZDOT = 3625
267950 TA = 272
21727
MA = 272
27289
Ha = 191
243 n
mi
Hp = 185
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15955020
12 X = 4904808
40
Y = -6321179
51 feet Y = -1872080
20 meter
Z = -13868834
84 Z = -4203494
71
XDOT = 16328
646808 XDOT = 4907
314932
YDOT = 15161
645957 feet/sec YDOT = 4676
535522 meter/sec
ZDOT = 11893
923720 ZDOT = 3649
277008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5135382
78 X = -1565264
67
Y = -16453730
21 feet Y = -5015096
97 meter
Z = -13775600
28 Z = -4198802
97
XDOT = 15107
164681 XDOT = 4604
663795
YDOT = -14735
867847 feet/sec YDOT = -4491
492520 meter/sec
ZDOT = 11988
543400 ZDOT = 3654
108028
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 09224
35836958
00010596 00000-0 82463-4 0 9138
2 25544 51
6406 18
4713 0008369 324
3655 35
6948 15
73636358 14807
Satellite: ISS
Catalog Number: 25544
Epoch time: 09224
35836958 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 18
4713 deg
Eccentricity:
0008369
Arg of perigee: 324
3655 deg
Mean anomaly: 35
6948 deg
Mean motion: 15
73636358 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1480
Checksum: 335
Coasting Arc #15 (Orbit 1495)
---------------------------------------
Vector Time (GMT): 2009/225/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4778897
10 A = 6728968
72 meter
Y = -3596783
11 meter E =
0006120
Z = -3090129
80 I = 51
72084
XDOT = 5249
864320 Wp = 359
34542
YDOT = -2762
299222 meter/sec RA = 12
90527 deg
ZDOT = -4897
637213 TA = 216
43740
MA = 216
47907
Ha = 191
320 n
mi
Hp = 185
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15678796
26 X = -4723310
78
Y = -11800469
51 feet Y = -3649912
58 meter
Z = -10138221
11 Z = -3113210
85
XDOT = 17223
964303 XDOT = 5304
154477
YDOT = -9062
661491 feet/sec YDOT = -2703
288356 meter/sec
ZDOT = -16068
363559 ZDOT = -4872
001640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12653025
43 X = -3856642
15
Y = 14937363
29 feet Y = 4552908
33 meter
Z = -10229143
94 Z = -3117843
07
XDOT = -6994
204491 XDOT = -2131
833529
YDOT = -16872
857880 feet/sec YDOT = -5142
847082 meter/sec
ZDOT = -15967
652585 ZDOT = -4866
940508
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 09225
37443809
00010596 00000-0 82463-4 0 9141
2 25544 51
6400 13
2567 0008434 328
4066 31
6590 15
73643925 14969
Satellite: ISS
Catalog Number: 25544
Epoch time: 09225
37443809 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 13
2567 deg
Eccentricity:
0008434
Arg of perigee: 328
4066 deg
Mean anomaly: 31
6590 deg
Mean motion: 15
73643925 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1496
Checksum: 310
Coasting Arc #16 (Orbit 1511)
---------------------------------------
Vector Time (GMT): 2009/226/08:22:39
068
Vector Time (MET): N/A
Weight (LBS) : 701318
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4271944
05 A = 6725053
53 meter
Y = 2873072
31 meter E =
0011746
Z = 4328854
65 I = 51
67861
XDOT = -5895
557620 Wp = 25
78154
YDOT = -3550
046595 meter/sec RA = 7
72681 deg
ZDOT = -3447
999995 TA = 99
10238
MA = 98
96945
Ha = 191
459 n
mi
Hp = 185
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14015564
47 X = -4324782
50
Y = 9426090
25 feet Y = 2825005
18 meter
Z = 14202279
04 Z = 4307973
44
XDOT = -19342
380643 XDOT = -5838
672483
YDOT = -11647
134497 feet/sec YDOT = -3615
655868 meter/sec
ZDOT = -11312
335942 ZDOT = -3476
502656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8875640
40 X = 2705295
19
Y = 14451054
77 feet Y = 4404681
49 meter
Z = 14120268
36 Z = 4303857
80
XDOT = -11328
240148 XDOT = -3452
847597
YDOT = 18165
454465 feet/sec YDOT = 5536
830521 meter/sec
ZDOT = -11424
577572 ZDOT = -3482
211244
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 09226
39049462
00010596 00000-0 82463-4 0 9152
2 25544 51
6403 8
0404 0008494 331
5968 28
4731 15
73675548 15122
Satellite: ISS
Catalog Number: 25544
Epoch time: 09226
39049462 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 8
0404 deg
Eccentricity:
0008494
Arg of perigee: 331
5968 deg
Mean anomaly: 28
4731 deg
Mean motion: 15
73675548 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1512
Checksum: 314
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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