Date:
December 14th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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 3357)
---------------------------------------
Vector Time (GMT): 2009/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4289717
42 A = 6714054
98 meter
Y = 858649
39 meter E =
0021030
Z = -5111678
08 I = 51
89892
XDOT = -3238
675563 Wp = 72
83175
YDOT = 6793
097553 meter/sec RA = 124
94153 deg
ZDOT = -1576
035198 TA = 182
06552
MA = 182
07422
Ha = 188
973 n
mi
Hp = 177
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14073876
04 X = 4304628
87
Y = 2817091
16 feet Y = 906703
24 meter
Z = -16770597
39 Z = -5090802
16
XDOT = -10625
575993 XDOT = -3306
740295
YDOT = 22287
065463 feet/sec YDOT = 6756
500301 meter/sec
ZDOT = -5170
719154 ZDOT = -1591
933736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5795899
40 X = -1766590
14
Y = 13235596
30 feet Y = 4034209
75 meter
Z = -16688003
68 Z = -5086503
52
XDOT = -18524
758199 XDOT = -5646
346299
YDOT = -14713
663980 feet/sec YDOT = -4484
724781 meter/sec
ZDOT = -5233
351345 ZDOT = -1595
125490
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 09343
51858522
00016717 00000-0 10270-3 0 9002
2 25544 51
6425 125
7530 0007459 62
8494 297
3430 15
76422209 33581
Satellite: ISS
Catalog Number: 25544
Epoch time: 09343
51858522 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 125
7530 deg
Eccentricity:
0007459
Arg of perigee: 62
8494 deg
Mean anomaly: 297
3430 deg
Mean motion: 15
76422209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3358
Checksum: 317
Coasting Arc #2 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2009/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2944285
24 A = 6725102
37 meter
Y = -6015558
14 meter E =
0017848
Z = 553523
22 I = 51
95204
XDOT = 4504
135439 Wp = 107
59876
YDOT = 1635
355551 meter/sec RA = 119
78782 deg
ZDOT = -6032
746829 TA = 66
39755
MA = 66
21024
Ha = 188
952 n
mi
Hp = 177
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9659728
46 X = 3008644
48
Y = -19736083
12 feet Y = -5982273
59 meter
Z = 1816021
07 Z = 567982
67
XDOT = 14777
347241 XDOT = 4514
820243
YDOT = 5365
339733 feet/sec YDOT = 1685
783618 meter/sec
ZDOT = -19792
476473 ZDOT = -6010
839367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17434387
06 X = 5314001
18
Y = 13366199
09 feet Y = 4074017
48 meter
Z = 1873001
15 Z = 570890
75
XDOT = -7233
213016 XDOT = -2204
683327
YDOT = 12264
248439 feet/sec YDOT = 3738
142924 meter/sec
ZDOT = -19705
772426 ZDOT = -6006
319435
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 09344
53285675
00016717 00000-0 10270-3 0 9019
2 25544 51
6419 120
5244 0007384 66
0542 294
1395 15
76439484 33742
Satellite: ISS
Catalog Number: 25544
Epoch time: 09344
53285675 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 120
5244 deg
Eccentricity:
0007384
Arg of perigee: 66
0542 deg
Mean anomaly: 294
1395 deg
Mean motion: 15
76439484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 325
Coasting Arc #3 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2009/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3615450
91 A = 6713139
57 meter
Y = -2025634
73 meter E =
0009915
Z = 5273373
09 I = 51
92679
XDOT = 3426
626059 Wp = 71
29822
YDOT = -6903
242681 meter/sec RA = 114
65831 deg
ZDOT = -298
828277 TA = 21
54370
MA = 21
50201
Ha = 189
102 n
mi
Hp = 177
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11861715
59 X = -3618148
72
Y = -6645783
22 feet Y = -2066080
37 meter
Z = 17301092
82 Z = 5255802
21
XDOT = 11242
211480 XDOT = 3505
016330
YDOT = -22648
433992 feet/sec YDOT = -6864
485796 meter/sec
ZDOT = -980
407734 ZDOT = -281
991627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8702389
28 X = 2652488
25
Y = -10561129
58 feet Y = -3219032
30 meter
Z = 17231526
54 Z = 5252169
29
XDOT = 19466
218669 XDOT = 5933
303450
YDOT = 14529
672831 feet/sec YDOT = 4428
644279 meter/sec
ZDOT = -914
040498 ZDOT = -278
599544
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 09345
54711620
00016717 00000-0 10270-3 0 9026
2 25544 51
6429 115
2973 0007449 69
4230 290
7743 15
76448794 33907
Satellite: ISS
Catalog Number: 25544
Epoch time: 09345
54711620 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 115
2973 deg
Eccentricity:
0007449
Arg of perigee: 69
4230 deg
Mean anomaly: 290
7743 deg
Mean motion: 15
76448794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 327
Coasting Arc #4 (Orbit 3405)
---------------------------------------
Vector Time (GMT): 2009/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2989256
09 A = 6724656
19 meter
Y = 5917440
10 meter E =
0021072
Z = 1071750
57 I = 51
97829
XDOT = -3854
413961 Wp = 62
49111
YDOT = -3038
153402 meter/sec RA = 109
53936 deg
ZDOT = 5945
251645 TA = 309
19686
MA = 309
38380
Ha = 188
984 n
mi
Hp = 177
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9807270
65 X = -3060410
24
Y = 19414173
56 feet Y = 5883614
52 meter
Z = 3516242
04 Z = 1057056
30
XDOT = -12645
715094 XDOT = -3849
035800
YDOT = -9967
694889 feet/sec YDOT = -3081
226298 meter/sec
ZDOT = 19505
418782 ZDOT = 5926
539303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17537071
02 X = -5345299
25
Y = -12882078
54 feet Y = -3926457
54 meter
Z = 3458300
61 Z = 1054090
03
XDOT = 10987
675771 XDOT = 3349
043575
YDOT = -9671
072960 feet/sec YDOT = -2947
743038 meter/sec
ZDOT = 19431
305128 ZDOT = 5922
661803
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 09346
56136077
00016717 00000-0 10270-3 0 9037
2 25544 51
6439 110
0702 0007480 73
6247 286
5740 15
76478820 34062
Satellite: ISS
Catalog Number: 25544
Epoch time: 09346
56136077 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 110
0702 deg
Eccentricity:
0007480
Arg of perigee: 73
6247 deg
Mean anomaly: 286
5740 deg
Mean motion: 15
76478820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3406
Checksum: 313
Coasting Arc #5 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2009/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3154565
61 A = 6714485
49 meter
Y = 3288795
15 meter E =
0019529
Z = -4948378
38 I = 51
95348
XDOT = -3425
526716 Wp = 95
14898
YDOT = 6535
845474 meter/sec RA = 104
38144 deg
ZDOT = 2165
663449 TA = 195
77294
MA = 195
83386
Ha = 188
938 n
mi
Hp = 177
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10349624
72 X = 3141594
01
Y = 10790010
33 feet Y = 3323999
47 meter
Z = -16234837
19 Z = -4933084
32
XDOT = -11238
604712 XDOT = -3508
877670
YDOT = 21443
062579 feet/sec YDOT = 6497
072896 meter/sec
ZDOT = 7105
195042 ZDOT = 2148
820326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12209556
20 X = -3721472
73
Y = 8742408
86 feet Y = 2664686
22 meter
Z = -16174239
33 Z = -4929908
15
XDOT = -18911
643290 XDOT = -5764
268875
YDOT = -13423
352476 feet/sec YDOT = -4091
437835 meter/sec
ZDOT = 7038
754201 ZDOT = 2145
412280
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 09347
51220404
00016717 00000-0 10270-3 0 9042
2 25544 51
6441 105
1706 0007468 76
6217 283
5779 15
76507517 34212
Satellite: ISS
Catalog Number: 25544
Epoch time: 09347
51220404 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 105
1706 deg
Eccentricity:
0007468
Arg of perigee: 76
6217 deg
Mean anomaly: 283
5779 deg
Mean motion: 15
76507517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 308
Coasting Arc #6 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2009/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3001676
73 A = 6721951
22 meter
Y = -5389804
06 meter E =
0011501
Z = -2676592
85 I = 51
98572
XDOT = 3413
287476 Wp = 97
90730
YDOT = 4491
314386 meter/sec RA = 99
28964 deg
ZDOT = -5236
794694 TA = 112
43624
MA = 112
31439
Ha = 188
953 n
mi
Hp = 177
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9848020
76 X = 3074725
96
Y = -17683084
20 feet Y = -5355828
71 meter
Z = -8781472
60 Z = -2661833
83
XDOT = 11198
449726 XDOT = 3388
250890
YDOT = 14735
283420 feet/sec YDOT = 4529
344554 meter/sec
ZDOT = -17181
084954 ZDOT = -5220
272866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16244259
42 X = 4951250
27
Y = 12116871
64 feet Y = 3693222
48 meter
Z = -8723227
51 Z = -2658839
74
XDOT = -15196
682308 XDOT = -4631
948768
YDOT = 8100
121127 feet/sec YDOT = 2468
916919 meter/sec
ZDOT = -17115
598131 ZDOT = -5216
834310
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 09348
52642407
00016717 00000-0 10270-3 0 9056
2 25544 51
6448 99
9425 0007464 80
2308 279
9699 15
76511627 34379
Satellite: ISS
Catalog Number: 25544
Epoch time: 09348
52642407 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 99
9425 deg
Eccentricity:
0007464
Arg of perigee: 80
2308 deg
Mean anomaly: 279
9699 deg
Mean motion: 15
76511627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 349
Coasting Arc #7 (Orbit 3452)
---------------------------------------
Vector Time (GMT): 2009/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2869127
13 A = 6717854
57 meter
Y = -4495663
51 meter E =
0018243
Z = 4071951
16 I = 51
97608
XDOT = 3442
550317 Wp = 79
58925
YDOT = -5715
672168 meter/sec RA = 94
11182 deg
ZDOT = -3867
031927 TA = 50
02484
MA = 49
86478
Ha = 189
069 n
mi
Hp = 177
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9413146
74 X = -2838423
59
Y = -14749552
19 feet Y = -4527576
75 meter
Z = 13359419
83 Z = 4058086
67
XDOT = 11294
456420 XDOT = 3524
993640
YDOT = -18752
205274 feet/sec YDOT = -5676
713968 meter/sec
ZDOT = -12687
112620 ZDOT = -3850
108479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15728003
45 X = 4793895
45
Y = -7762233
54 feet Y = -2365928
78 meter
Z = 13304448
79 Z = 4055195
99
XDOT = 16780
442283 XDOT = 5114
678808
YDOT = 12269
531488 feet/sec YDOT = 3739
753198 meter/sec
ZDOT = -12620
296946 ZDOT = -3846
666509
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 09349
54063187
00016717 00000-0 10270-3 0 9062
2 25544 51
6454 94
7159 0007600 83
6133 276
5897 15
76510451 34533
Satellite: ISS
Catalog Number: 25544
Epoch time: 09349
54063187 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 94
7159 deg
Eccentricity:
0007600
Arg of perigee: 83
6133 deg
Mean anomaly: 276
5897 deg
Mean motion: 15
76510451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3453
Checksum: 329
Coasting Arc #8 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2009/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3029201
05 A = 6718017
85 meter
Y = 4480723
82 meter E =
0018379
Z = 3970487
31 I = 51
97893
XDOT = -3228
561170 Wp = 95
30499
YDOT = -5746
600579 meter/sec RA = 89
03237 deg
ZDOT = 4004
530972 TA = 313
38782
MA = 313
54073
Ha = 188
935 n
mi
Hp = 177
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9938323
65 X = -3098368
17
Y = 14700537
48 feet Y = 4446462
14 meter
Z = 13026533
18 Z = 3955604
08
XDOT = -10592
392289 XDOT = -3183
515120
YDOT = -18853
676440 feet/sec YDOT = -5782
453034 meter/sec
ZDOT = 13138
224973 ZDOT = 3988
955017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13671717
21 X = -4167139
41
Y = -11379294
39 feet Y = -3468408
93 meter
Z = 12967746
66 Z = 3952569
18
XDOT = 18960
610080 XDOT = 5779
193952
YDOT = -7813
220772 feet/sec YDOT = -2381
469691 meter/sec
ZDOT = 13076
452945 ZDOT = 3985
702858
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 09350
55482391
00016717 00000-0 10270-3 0 9078
2 25544 51
6461 89
4885 0007494 87
0013 273
2009 15
76579648 34693
Satellite: ISS
Catalog Number: 25544
Epoch time: 09350
55482391 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 89
4885 deg
Eccentricity:
0007494
Arg of perigee: 87
0013 deg
Mean anomaly: 273
2009 deg
Mean motion: 15
76579648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 345
Coasting Arc #9 (Orbit 3483)
---------------------------------------
Vector Time (GMT): 2009/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2787331
32 A = 6721556
18 meter
Y = 5440889
93 meter E =
0011780
Z = -2800396
79 I = 51
98902
XDOT = -3568
788633 Wp = 77
57774
YDOT = 4469
420469 meter/sec RA = 83
85378 deg
ZDOT = 5152
031027 TA = 250
51255
MA = 250
63984
Ha = 188
900 n
mi
Hp = 177
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9144787
80 X = 2739887
02
Y = 17850688
73 feet Y = 5471794
68 meter
Z = -9187653
52 Z = -2786970
29
XDOT = -11708
624125 XDOT = -3643
528907
YDOT = 14663
452983 feet/sec YDOT = 4429
093458 meter/sec
ZDOT = 16902
988933 ZDOT = 5134
512984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18520192
52 X = -5644954
68
Y = 7762247
94 feet Y = 2365933
17 meter
Z = -9134395
74 Z = -2784163
82
XDOT = -13121
150073 XDOT = -3999
326542
YDOT = -11576
402942 feet/sec YDOT = -3528
487617 meter/sec
ZDOT = 16833
764789 ZDOT = 5130
931508
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 09351
50562024
00016717 00000-0 10270-3 0 9087
2 25544 51
6463 84
5889 0007415 88
7669 271
4345 15
76545306 34847
Satellite: ISS
Catalog Number: 25544
Epoch time: 09351
50562024 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 84
5889 deg
Eccentricity:
0007415
Arg of perigee: 88
7669 deg
Mean anomaly: 271
4345 deg
Mean motion: 15
76545306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3484
Checksum: 338
Coasting Arc #10 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2009/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3268762
75 A = 6714497
06 meter
Y = -3241949
84 meter E =
0019517
Z = -4905210
20 I = 51
96068
XDOT = 3145
762529 Wp = 80
72591
YDOT = 6632
513689 meter/sec RA = 78
76426 deg
ZDOT = -2291
883737 TA = 167
06423
MA = 167
01409
Ha = 188
849 n
mi
Hp = 177
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10724287
23 X = 3328600
43
Y = -10636318
36 feet Y = -3205061
30 meter
Z = -16093209
32 Z = -4889185
72
XDOT = 10320
743204 XDOT = 3082
496329
YDOT = 21760
215516 feet/sec YDOT = 6667
338064 meter/sec
ZDOT = -7519
303598 ZDOT = -2276
754336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9949049
59 X = 3032470
31
Y = 11453950
64 feet Y = 3491164
15 meter
Z = -16029860
21 Z = -4885901
39
XDOT = -21522
762604 XDOT = -6560
138042
YDOT = 8276
931909 feet/sec YDOT = 2522
808846 meter/sec
ZDOT = -7459
280546 ZDOT = -2273
588711
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 09352
51978974
00016717 00000-0 10270-3 0 9095
2 25544 51
6460 79
3616 0007424 93
3059 266
8955 15
76569893 35000
Satellite: ISS
Catalog Number: 25544
Epoch time: 09352
51978974 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 79
3616 deg
Eccentricity:
0007424
Arg of perigee: 93
3059 deg
Mean anomaly: 266
8955 deg
Mean motion: 15
76569893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 359
Coasting Arc #11 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2009/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2711791
80 A = 6724235
39 meter
Y = -6035844
24 meter E =
0020955
Z = 1148486
07 I = 51
98610
XDOT = 3968
195896 Wp = 113
28328
YDOT = -2925
044694 meter/sec RA = 73
60397 deg
ZDOT = -5926
352717 TA = 54
18068
MA = 53
98615
Ha = 188
876 n
mi
Hp = 177
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8896954
74 X = -2649675
50
Y = -19802638
57 feet Y = -6065821
94 meter
Z = 3767998
92 Z = 1135462
31
XDOT = 13019
015407 XDOT = 4029
398351
YDOT = -9596
603328 feet/sec YDOT = -2880
326985 meter/sec
ZDOT = -19443
414425 ZDOT = -5906
927039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20179937
78 X = 6150845
04
Y = -8028522
15 feet Y = -2447093
55 meter
Z = 3716323
03 Z = 1132735
26
XDOT = 8417
527593 XDOT = 2565
662410
YDOT = 12075
318769 feet/sec YDOT = 3680
557161 meter/sec
ZDOT = -19366
590669 ZDOT = -5902
936836
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 09353
53394702
00016717 00000-0 10270-3 0 9101
2 25544 51
6454 74
1343 0007604 96
4141 263
7890 15
76599522 35162
Satellite: ISS
Catalog Number: 25544
Epoch time: 09353
53394702 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 74
1343 deg
Eccentricity:
0007604
Arg of perigee: 96
4141 deg
Mean anomaly: 263
7890 deg
Mean motion: 15
76599522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 317
Coasting Arc #12 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2009/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3706798
12 A = 6712546
53 meter
Y = 1853461
01 meter E =
0009922
Z = 5272175
99 I = 51
93806
XDOT = -3064
339431 Wp = 100
75879
YDOT = -7070
894541 meter/sec RA = 68
48495 deg
ZDOT = 328
980138 TA = 346
12233
MA = 346
14959
Ha = 188
828 n
mi
Hp = 177
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12161411
14 X = -3752859
48
Y = 6080908
84 feet Y = 1811751
24 meter
Z = 17297165
33 Z = 5254056
80
XDOT = -10053
607057 XDOT = -2986
641816
YDOT = -23198
472904 feet/sec YDOT = -7104
727402 meter/sec
ZDOT = 1079
331163 ZDOT = 314
281549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5744006
89 X = -1750773
30
Y = -12424102
79 feet Y = -3786866
53 meter
Z = 17225485
67 Z = 5250328
03
XDOT = 22558
678595 XDOT = 6875
885236
YDOT = -9003
266834 feet/sec YDOT = -2744
195731 meter/sec
ZDOT = 1021
005297 ZDOT = 311
202414
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 09354
54808962
00016717 00000-0 10270-3 0 9112
2 25544 51
6458 68
9062 0007421 99
8222 260
3789 15
76659140 35320
Satellite: ISS
Catalog Number: 25544
Epoch time: 09354
54808962 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 68
9062 deg
Eccentricity:
0007421
Arg of perigee: 99
8222 deg
Mean anomaly: 260
3789 deg
Mean motion: 15
76659140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 336
Coasting Arc #13 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2009/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2580906
35 A = 6724579
11 meter
Y = 6174921
01 meter E =
0019051
Z = 591084
66 I = 51
96545
XDOT = -4608
075445 Wp = 68
88470
YDOT = 1334
626098 meter/sec RA = 63
35511 deg
ZDOT = 6030
291043 TA = 297
52844
MA = 297
72191
Ha = 188
811 n
mi
Hp = 177
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8467540
53 X = 2508794
12
Y = 20258927
18 feet Y = 6203378
96 meter
Z = 1939254
12 Z = 603448
10
XDOT = -15118
357758 XDOT = -4651
950903
YDOT = 4378
694548 feet/sec YDOT = 1282
849949 meter/sec
ZDOT = 19784
419434 ZDOT = 6007
798682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20343555
65 X = -6200715
76
Y = 8250479
93 feet Y = 2514746
28 meter
Z = 1988316
94 Z = 606039
00
XDOT = -3623
079255 XDOT = -1104
314557
YDOT = -13794
067894 feet/sec YDOT = -4204
431894 meter/sec
ZDOT = 19695
416245 ZDOT = 6003
162871
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 09355
56222372
00016717 00000-0 10270-3 0 9121
2 25544 51
6452 63
6787 0007557 101
7145 258
4868 15
76618955 35489
Satellite: ISS
Catalog Number: 25544
Epoch time: 09355
56222372 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 63
6787 deg
Eccentricity:
0007557
Arg of perigee: 101
7145 deg
Mean anomaly: 258
4868 deg
Mean motion: 15
76618955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 344
Coasting Arc #14 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2009/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4381954
60 A = 6713531
83 meter
Y = -489909
37 meter E =
0021037
Z = -5081295
38 I = 51
91309
XDOT = 2753
536762 Wp = 103
46662
YDOT = 6974
298031 meter/sec RA = 58
20054 deg
ZDOT = 1703
220220 TA = 182
87300
MA = 182
88510
Ha = 188
716 n
mi
Hp = 177
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14376491
47 X = 4411791
11
Y = -1607314
22 feet Y = -440740
51 meter
Z = -16670916
60 Z = -5059935
48
XDOT = 9033
913262 XDOT = 2667
070378
YDOT = 22881
555220 feet/sec YDOT = 7004
606100 meter/sec
ZDOT = 5587
992847 ZDOT = 1716
387437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1710113
97 X = 521242
74
Y = 14462157
91 feet Y = 4408065
73 meter
Z = -16586377
69 Z = -5055527
92
XDOT = -21762
824757 XDOT = -6633
308986
YDOT = 9038
028417 feet/sec YDOT = 2754
791061 meter/sec
ZDOT = 5640
250104 ZDOT = 1719
148232
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 09356
51296028
00016717 00000-0 10270-3 0 9137
2 25544 51
6445 58
7773 0007512 105
0410 255
1587 15
76653148 35636
Satellite: ISS
Catalog Number: 25544
Epoch time: 09356
51296028 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 58
7773 deg
Eccentricity:
0007512
Arg of perigee: 105
0410 deg
Mean anomaly: 255
1587 deg
Mean motion: 15
76653148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 317
Coasting Arc #15 (Orbit 3578)
---------------------------------------
Vector Time (GMT): 2009/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2144394
79 A = 6722107
92 meter
Y = -5921348
31 meter E =
0012982
Z = -2349513
92 I = 51
92580
XDOT = 5452
712504 Wp = 119
08351
YDOT = 170
670321 meter/sec RA = 53
09915 deg
ZDOT = -5435
373206 TA = 87
27749
MA = 87
12891
Ha = 188
690 n
mi
Hp = 176
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7035415
98 X = -2066608
35
Y = -19426995
77 feet Y = -5944893
09 meter
Z = -7708378
99 Z = -2359742
90
XDOT = 17889
476719 XDOT = 5476
802833
YDOT = 559
941997 feet/sec YDOT = 231
780886 meter/sec
ZDOT = -17832
589258 ZDOT = -5408
825404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19251763
01 X = 5867937
36
Y = -7459709
54 feet Y = -2273719
47 meter
Z = -7748980
83 Z = -2361889
36
XDOT = -666
483705 XDOT = -203
144233
YDOT = 16598
050345 feet/sec YDOT = 5059
085745 meter/sec
ZDOT = -17727
502370 ZDOT = -5403
342723
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 09357
52706912
00016717 00000-0 10270-3 0 9148
2 25544 51
6447 53
5487 0007646 108
4635 251
7361 15
76684640 35797
Satellite: ISS
Catalog Number: 25544
Epoch time: 09357
52706912 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 53
5487 deg
Eccentricity:
0007646
Arg of perigee: 108
4635 deg
Mean anomaly: 251
7361 deg
Mean motion: 15
76684640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
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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