Date:
November 19th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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 2994)
---------------------------------------
Vector Time (GMT): 2009/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4552721
49 A = 6721857
67 meter
Y = -4050930
82 meter E =
0008173
Z = -2827348
23 I = 51
35309
XDOT = 1772
145974 Wp = 12
47929
YDOT = -5523
664973 meter/sec RA = 243
43888 deg
ZDOT = 5071
125726 TA = 314
91391
MA = 314
98021
Ha = 186
837 n
mi
Hp = 180
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14936750
30 X = -4493349
72
Y = -13290455
46 feet Y = -4101509
88 meter
Z = -9276076
86 Z = -2849322
11
XDOT = 5814
127211 XDOT = 1809
145458
YDOT = -18122
260411 feet/sec YDOT = -5503
641271 meter/sec
ZDOT = 16637
551593 ZDOT = 5079
824572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19429282
15 X = 5922045
20
Y = -4541681
65 feet Y = -1384304
57 meter
Z = -9362929
08 Z = -2853820
78
XDOT = 11214
232539 XDOT = 3418
098078
YDOT = 13675
845118 feet/sec YDOT = 4168
397592 meter/sec
ZDOT = 16671
645269 ZDOT = 5081
517478
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 09320
50577560
00016717 00000-0 10270-3 0 9006
2 25544 51
6451 244
3179 0006373 337
9041 22
1847 15
76378503 29954
Satellite: ISS
Catalog Number: 25544
Epoch time: 09320
50577560 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 244
3179 deg
Eccentricity:
0006373
Arg of perigee: 337
9041 deg
Mean anomaly: 22
1847 deg
Mean motion: 15
76378503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 314
Coasting Arc #2 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2009/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1858400
15 A = 6715111
04 meter
Y = 4314015
79 meter E =
0013543
Z = -4810604
04 I = 51
34603
XDOT = -5341
498109 Wp = 44
73587
YDOT = -4989
221705 meter/sec RA = 238
30769 deg
ZDOT = -2405
325687 TA = 201
63975
MA = 201
69703
Ha = 186
962 n
mi
Hp = 180
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6097113
36 X = -1883132
39
Y = 14153595
10 feet Y = 4293096
20 meter
Z = -15782821
66 Z = -4819692
11
XDOT = -17524
600094 XDOT = -5273
625789
YDOT = -16368
837616 feet/sec YDOT = -5048
573779 meter/sec
ZDOT = -7891
488474 ZDOT = -2431
111013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8355278
47 X = -2546688
88
Y = -12905842
19 feet Y = -3933700
70 meter
Z = -15818503
86 Z = -4821479
98
XDOT = 22411
532004 XDOT = 6831
034955
YDOT = -4690
287215 feet/sec YDOT = -1429
599543 meter/sec
ZDOT = -7993
424290 ZDOT = -2436
395724
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 09321
52005649
00016717 00000-0 10270-3 0 9014
2 25544 51
6458 239
0911 0006342 342
5699 17
5247 15
76445153 30111
Satellite: ISS
Catalog Number: 25544
Epoch time: 09321
52005649 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 239
0911 deg
Eccentricity:
0006342
Arg of perigee: 342
5699 deg
Mean anomaly: 17
5247 deg
Mean motion: 15
76445153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 299
Coasting Arc #3 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2009/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4742711
47 A = 6724402
76 meter
Y = 4581222
38 meter E =
0010574
Z = 1305401
37 I = 51
39432
XDOT = -2568
047951 Wp = 95
49585
YDOT = 4330
593521 meter/sec RA = 233
10251 deg
ZDOT = -5828
429946 TA = 70
11489
MA = 70
00097
Ha = 187
020 n
mi
Hp = 180
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15560077
00 X = 4684789
39
Y = 15030257
15 feet Y = 4633934
18 meter
Z = 4282812
90 Z = 1328301
81
XDOT = -8425
354171 XDOT = -2587
968370
YDOT = 14207
983994 feet/sec YDOT = 4301
765306 meter/sec
ZDOT = -19122
145492 ZDOT = -5840
953786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21075228
75 X = -6423729
72
Y = 4803702
93 feet Y = 1464168
65 meter
Z = 4373360
66 Z = 1333000
33
XDOT = -7010
290910 XDOT = -2136
736669
YDOT = -13186
945742 feet/sec YDOT = -4019
381062 meter/sec
ZDOT = -19171
387680 ZDOT = -5843
438965
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 09322
53430932
00016717 00000-0 10270-3 0 9024
2 25544 51
6455 233
8642 0006290 345
7512 14
3474 15
76462580 30279
Satellite: ISS
Catalog Number: 25544
Epoch time: 09322
53430932 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 233
8642 deg
Eccentricity:
0006290
Arg of perigee: 345
7512 deg
Mean anomaly: 14
3474 deg
Mean motion: 15
76462580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 297
Coasting Arc #4 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2009/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2691824
15 A = 6712945
70 meter
Y = -3245228
86 meter E =
0005187
Z = 5222103
99 I = 51
37520
XDOT = 5465
533026 Wp = 14
59658
YDOT = 5406
230050 meter/sec RA = 227
94766 deg
ZDOT = 547
182309 TA = 70
21733
MA = 70
16140
Ha = 186
878 n
mi
Hp = 179
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8831444
06 X = 2702544
24
Y = -10647076
32 feet Y = -3215067
92 meter
Z = 17132887
12 Z = 5235206
84
XDOT = 17931
538800 XDOT = 5402
015236
YDOT = 17736
975231 feet/sec YDOT = 5466
993657 meter/sec
ZDOT = 1795
217550 ZDOT = 573
580717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4374837
49 X = 1333450
47
Y = 13055477
21 feet Y = 3979309
45 meter
Z = 17184463
08 Z = 5237824
35
XDOT = -23598
430787 XDOT = -7192
801704
YDOT = 5428
153789 feet/sec YDOT = 1654
501275 meter/sec
ZDOT = 1899
615602 ZDOT = 579
002836
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 09323
54853202
00016717 00000-0 10270-3 0 9036
2 25544 51
6452 228
6371 0006325 348
3018 11
7998 15
76548165 30430
Satellite: ISS
Catalog Number: 25544
Epoch time: 09323
54853202 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 228
6371 deg
Eccentricity:
0006325
Arg of perigee: 348
3018 deg
Mean anomaly: 11
7998 deg
Mean motion: 15
76548165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 310
Coasting Arc #5 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2009/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4714767
10 A = 6724894
51 meter
Y = -4766232
79 meter E =
0017342
Z = 372095
94 I = 51
43663
XDOT = 3661
529323 Wp = 31
03242
YDOT = -3143
977646 meter/sec RA = 222
77492 deg
ZDOT = 6013
700262 TA = 333
03170
MA = 333
12172
Ha = 187
103 n
mi
Hp = 179
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15468395
99 X = -4662927
44
Y = -15637246
67 feet Y = -4818666
28 meter
Z = 1220787
20 Z = 349316
63
XDOT = 12012
891481 XDOT = 3667
199733
YDOT = -10314
887290 feet/sec YDOT = -3103
001192 meter/sec
ZDOT = 19729
987737 ZDOT = 6031
501719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21386206
50 X = 6518515
74
Y = -5161085
66 feet Y = -1573098
91 meter
Z = 1130683
76 Z = 344632
41
XDOT = 2300
955386 XDOT = 701
331202
YDOT = 13957
138325 feet/sec YDOT = 4254
135762 meter/sec
ZDOT = 19800
116795 ZDOT = 6035
075599
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 09324
56272992
00016717 00000-0 10270-3 0 9041
2 25544 51
6453 223
4095 0006428 352
8632 7
2440 15
76547500 30594
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324
56272992 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 223
4095 deg
Eccentricity:
0006428
Arg of perigee: 352
8632 deg
Mean anomaly: 7
2440 deg
Mean motion: 15
76547500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 309
Coasting Arc #6 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2009/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3738501
20 A = 6713301
95 meter
Y = 2262978
02 meter E =
0013902
Z = -5106903
51 I = 51
42135
XDOT = -5235
192217 Wp = 74
50059
YDOT = -5459
585443 meter/sec RA = 217
58949 deg
ZDOT = 1420
015175 TA = 209
11240
MA = 209
18997
Ha = 187
079 n
mi
Hp = 179
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12265423
89 X = -3738719
60
Y = 7424468
58 feet Y = 2221171
17 meter
Z = -16754932
78 Z = -5125065
72
XDOT = -17175
827484 XDOT = -5180
651359
YDOT = -17912
025732 feet/sec YDOT = -5517
823631 meter/sec
ZDOT = 4658
842438 ZDOT = 1394
714210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -308892
11 X = -94150
31
Y = -14250039
97 feet Y = -4343412
18 meter
Z = -16826528
94 Z = -5128726
02
XDOT = 23089
757470 XDOT = 7037
758077
YDOT = -5857
035108 feet/sec YDOT = -1785
224301 meter/sec
ZDOT = 4558
741741 ZDOT = 1389
504483
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 09325
51351288
00016717 00000-0 10270-3 0 9054
2 25544 51
6455 218
5087 0006395 355
8954 4
2157 15
76610381 30742
Satellite: ISS
Catalog Number: 25544
Epoch time: 09325
51351288 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 218
5087 deg
Eccentricity:
0006395
Arg of perigee: 355
8954 deg
Mean anomaly: 4
2157 deg
Mean motion: 15
76610381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 320
Coasting Arc #7 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4311558
05 A = 6722873
16 meter
Y = 4716858
81 meter E =
0004279
Z = -2093811
87 I = 51
47815
XDOT = -4943
593974 Wp = 72
56020
YDOT = 2069
424074 meter/sec RA = 212
45136 deg
ZDOT = -5525
883666 TA = 130
89104
MA = 130
85396
Ha = 187
150 n
mi
Hp = 179
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14145531
66 X = 4268664
35
Y = 15475258
57 feet Y = 4764833
54 meter
Z = -6869461
51 Z = -2072969
86
XDOT = -16219
140335 XDOT = -4939
523137
YDOT = 6789
449062 feet/sec YDOT = 2014
165107 meter/sec
ZDOT = -18129
539586 ZDOT = -5549
889888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20425939
00 X = -6225826
21
Y = 4846350
79 feet Y = 1477167
72 meter
Z = -6786979
83 Z = -2068671
45
XDOT = 2276
655419 XDOT = 693
924572
YDOT = -15889
130796 feet/sec YDOT = -4843
007067 meter/sec
ZDOT = -18224
220545 ZDOT = -5554
742422
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 09326
52765597
00016717 00000-0 10270-3 0 9069
2 25544 51
6455 213
2806 0006283 358
4850 1
6294 15
76615465 30902
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
52765597 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 213
2806 deg
Eccentricity:
0006283
Arg of perigee: 358
4850 deg
Mean anomaly: 1
6294 deg
Mean motion: 15
76615465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 325
Coasting Arc #8 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2009/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4882196
07 A = 6715925
31 meter
Y = -1414240
87 meter E =
0013246
Z = 4387376
16 I = 51
48190
XDOT = 4520
531077 Wp = 42
28485
YDOT = 5290
286729 meter/sec RA = 207
24109 deg
ZDOT = -3309
652022 TA = 81
08585
MA = 80
93592
Ha = 187
070 n
mi
Hp = 179
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16017703
65 X = 4876334
16
Y = -4639897
87 feet Y = -1359678
34 meter
Z = 14394278
74 Z = 4411079
83
XDOT = 14831
138703 XDOT = 4477
116077
YDOT = 17356
583755 feet/sec YDOT = 5340
595451 meter/sec
ZDOT = -10858
438391 ZDOT = -3287
796108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3433962
92 X = -1046671
90
Y = 16235831
99 feet Y = 4948681
59 meter
Z = 14487801
80 Z = 4415881
99
XDOT = -21148
664425 XDOT = -6446
112917
YDOT = 5183
983043 feet/sec YDOT = 1580
078031 meter/sec
ZDOT = -10771
916237 ZDOT = -3283
280069
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 09327
54177034
00016717 00000-0 10270-3 0 9076
2 25544 51
6453 208
0523 0006525 2
2263 357
8929 15
76723749 31063
Satellite: ISS
Catalog Number: 25544
Epoch time: 09327
54177034 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 208
0523 deg
Eccentricity:
0006525
Arg of perigee: 2
2263 deg
Mean anomaly: 357
8929 deg
Mean motion: 15
76723749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3106
Checksum: 313
Coasting Arc #9 (Orbit 3121)
---------------------------------------
Vector Time (GMT): 2009/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3455630
67 A = 6718901
43 meter
Y = -4489973
96 meter E =
0014035
Z = 3595261
08 I = 51
51874
XDOT = 6209
811877 Wp = 66
32335
YDOT = -1250
288050 meter/sec RA = 202
12480 deg
ZDOT = 4399
279559 TA = 336
86830
MA = 336
93142
Ha = 187
335 n
mi
Hp = 178
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11337370
97 X = -3422631
53
Y = -14730885
70 feet Y = -4528432
55 meter
Z = 11795475
98 Z = 3578553
31
XDOT = 20373
398545 XDOT = 6201
960090
YDOT = -4101
994914 feet/sec YDOT = -1180
890406 meter/sec
ZDOT = 14433
331887 ZDOT = 4429
428099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18314890
42 X = 5582378
60
Y = -3414148
79 feet Y = -1040632
55 meter
Z = 11729305
38 Z = 3575092
28
XDOT = -5871
872044 XDOT = -1789
746599
YDOT = 18585
194201 feet/sec YDOT = 5664
767193 meter/sec
ZDOT = 14552
317157 ZDOT = 4435
546269
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 09328
55586080
00016717 00000-0 10270-3 0 9084
2 25544 51
6452 202
8235 0006540 6
6127 353
5123 15
76705939 31226
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
55586080 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 202
8235 deg
Eccentricity:
0006540
Arg of perigee: 6
6127 deg
Mean anomaly: 353
5123 deg
Mean motion: 15
76705939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3122
Checksum: 304
Coasting Arc #10 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2009/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5876987
88 A = 6719904
32 meter
Y = 826172
10 meter E =
0009036
Z = -3148505
54 I = 51
55110
XDOT = -3288
442381 Wp = 37
30169
YDOT = -5013
647187 meter/sec RA = 196
90965 deg
ZDOT = 4836
883755 TA = 285
94235
MA = 286
04189
Ha = 187
156 n
mi
Hp = 178
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19281456
29 X = -5870494
37
Y = 2710538
40 feet Y = 760488
60 meter
Z = -10329742
60 Z = -3177040
61
XDOT = -10788
852955 XDOT = -3255
631581
YDOT = -16448
973711 feet/sec YDOT = -5050
237241 meter/sec
ZDOT = 15869
041190 ZDOT = 4820
987729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6056163
78 X = 1845918
72
Y = -18441926
02 feet Y = -5621099
05 meter
Z = -10442384
89 Z = -3182838
91
XDOT = 18218
352357 XDOT = 5552
953798
YDOT = -2940
885306 feet/sec YDOT = -896
381841 meter/sec
ZDOT = 15806
044854 ZDOT = 4817
682471
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 09329
50654378
00016717 00000-0 10270-3 0 9097
2 25544 51
6450 197
9217 0006515 8
0220 352
1048 15
76760685 31376
Satellite: ISS
Catalog Number: 25544
Epoch time: 09329
50654378 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 197
9217 deg
Eccentricity:
0006515
Arg of perigee: 8
0220 deg
Mean anomaly: 352
1048 deg
Mean motion: 15
76760685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 317
Coasting Arc #11 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2009/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2159677
07 A = 6714565
29 meter
Y = 4276811
02 meter E =
0015526
Z = -4718722
89 I = 51
56170
XDOT = -7181
663664 Wp = 50
20600
YDOT = 670
023949 meter/sec RA = 191
79297 deg
ZDOT = -2675
692010 TA = 193
41180
MA = 193
45312
Ha = 187
241 n
mi
Hp = 178
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7085554
69 X = 2134615
66
Y = 14031532
22 feet Y = 4300821
85 meter
Z = -15481374
31 Z = -4708291
69
XDOT = -23561
888660 XDOT = -7175
623944
YDOT = 2198
241302 feet/sec YDOT = 589
748216 meter/sec
ZDOT = -8778
517092 ZDOT = -2710
566521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15751360
29 X = -4801014
62
Y = 513205
70 feet Y = 156425
10 meter
Z = -15439987
08 Z = -4706108
06
XDOT = 8066
632179 XDOT = 2458
709488
YDOT = -21057
027791 feet/sec YDOT = -6418
182071 meter/sec
ZDOT = -8916
210075 ZDOT = -2717
660831
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 09330
52058117
00016717 00000-0 10270-3 0 9102
2 25544 51
6443 192
6927 0006499 11
3014 348
8296 15
76806756 31532
Satellite: ISS
Catalog Number: 25544
Epoch time: 09330
52058117 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 192
6927 deg
Eccentricity:
0006499
Arg of perigee: 11
3014 deg
Mean anomaly: 348
8296 deg
Mean motion: 15
76806756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 318
Coasting Arc #12 (Orbit 3168)
---------------------------------------
Vector Time (GMT): 2009/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6553901
79 A = 6723144
98 meter
Y = -385745
61 meter E =
0014165
Z = 1434699
82 I = 51
62122
XDOT = 1565
323490 Wp = 92
27204
YDOT = 4811
827203 meter/sec RA = 186
59812 deg
ZDOT = -5808
292165 TA = 71
92459
MA = 71
77033
Ha = 187
281 n
mi
Hp = 178
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21502302
47 X = 6550758
49
Y = -1265569
60 feet Y = -312473
65 meter
Z = 4707020
42 Z = 1466531
78
XDOT = 5135
575753 XDOT = 1539
616752
YDOT = 15786
834656 feet/sec YDOT = 4829
188070 meter/sec
ZDOT = -19056
076657 ZDOT = -5800
749898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7660821
70 X = -2335018
45
Y = 20101326
89 feet Y = 6126884
44 meter
Z = 4832720
48 Z = 1473013
20
XDOT = -15083
097098 XDOT = -4597
327995
YDOT = -1136
800684 feet/sec YDOT = -346
496849 meter/sec
ZDOT = -19026
072897 ZDOT = -5799
147019
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 09331
53459335
00016717 00000-0 10270-3 0 9112
2 25544 51
6446 187
4640 0006516 16
0878 344
0493 15
76845831 31690
Satellite: ISS
Catalog Number: 25544
Epoch time: 09331
53459335 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 187
4640 deg
Eccentricity:
0006516
Arg of perigee: 16
0878 deg
Mean anomaly: 344
0493 deg
Mean motion: 15
76845831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3169
Checksum: 326
Coasting Arc #13 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2009/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -517752
47 A = 6712043
77 meter
Y = -4162293
42 meter E =
0006824
Z = 5235635
05 I = 51
61302
XDOT = 7685
439414 Wp = 44
37729
YDOT = -251
641247 meter/sec RA = 181
45766 deg
ZDOT = 564
317839 TA = 40
29017
MA = 40
23962
Ha = 187
314 n
mi
Hp = 178
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1698662
94 X = -496604
95
Y = -13655818
32 feet Y = -4167965
27 meter
Z = 17177280
34 Z = 5233170
89
XDOT = 25214
696240 XDOT = 7684
940677
YDOT = -825
594643 feet/sec YDOT = -165
700946 meter/sec
ZDOT = 1851
436480 ZDOT = 601
653489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13256718
97 X = 4040647
94
Y = 3737221
63 feet Y = 1139105
15 meter
Z = 17167363
41 Z = 5232612
37
XDOT = -8917
550067 XDOT = -2718
069260
YDOT = 22516
007590 feet/sec YDOT = 6862
879113 meter/sec
ZDOT = 1998
891015 ZDOT = 609
261981
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 09332
54857896
00016717 00000-0 10270-3 0 9129
2 25544 51
6436 182
2343 0006494 19
3226 340
8184 15
76868871 31858
Satellite: ISS
Catalog Number: 25544
Epoch time: 09332
54857896 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 182
2343 deg
Eccentricity:
0006494
Arg of perigee: 19
3226 deg
Mean anomaly: 340
8184 deg
Mean motion: 15
76868871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 341
Coasting Arc #14 (Orbit 3200)
---------------------------------------
Vector Time (GMT): 2009/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6696258
12 A = 6723786
12 meter
Y = 56180
65 meter E =
0019036
Z = 475934
13 I = 51
68196
XDOT = 396
547609 Wp = 40
89575
YDOT = -4796
829266 meter/sec RA = 176
29955 deg
ZDOT = 6024
868269 TA = 324
28846
MA = 324
41564
Ha = 187
269 n
mi
Hp = 178
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21969350
79 X = -6698700
73
Y = 184319
72 feet Y = -18714
55 meter
Z = 1561463
69 Z = 443396
82
XDOT = 1301
009217 XDOT = 420
888541
YDOT = -15737
628824 feet/sec YDOT = -4792
259194 meter/sec
ZDOT = 19766
628179 ZDOT = 6026
853517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8156199
41 X = 2486009
58
Y = -20409498
01 feet Y = -6220814
99 meter
Z = 1432940
62 Z = 436760
30
XDOT = 12626
588893 XDOT = 3848
584294
YDOT = 6464
565280 feet/sec YDOT = 1970
399497 meter/sec
ZDOT = 19774
262828 ZDOT = 6027
195310
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 09333
56253782
00016717 00000-0 10270-3 0 9137
2 25544 51
6423 177
0042 0006478 22
1497 337
9947 15
76927148 32012
Satellite: ISS
Catalog Number: 25544
Epoch time: 09333
56253782 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 177
0042 deg
Eccentricity:
0006478
Arg of perigee: 22
1497 deg
Mean anomaly: 337
9947 deg
Mean motion: 15
76927148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3201
Checksum: 323
Coasting Arc #15 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2009/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1218166
47 A = 6712519
90 meter
Y = 4245200
72 meter E =
0016472
Z = -5068141
64 I = 51
67310
XDOT = -7508
621595 Wp = 80
33427
YDOT = -166
079836 meter/sec RA = 171
12520 deg
ZDOT = 1672
947346 TA = 205
71493
MA = 205
79692
Ha = 187
278 n
mi
Hp = 177
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3996609
14 X = -1240925
66
Y = 13927823
89 feet Y = 4231451
74 meter
Z = -16627761
28 Z = -5074114
50
XDOT = -24634
585287 XDOT = -7514
333513
YDOT = -544
881352 feet/sec YDOT = -250
077785 meter/sec
ZDOT = 5488
672396 ZDOT = 1636
455485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11562986
09 X = -3524398
16
Y = -8687645
35 feet Y = -2647994
30 meter
Z = -16651179
51 Z = -5075279
52
XDOT = 8825
330228 XDOT = 2689
960654
YDOT = -21943
910592 feet/sec YDOT = -6688
503948 meter/sec
ZDOT = 5344
503020 ZDOT = 1629
004521
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 09334
51310148
00016717 00000-0 10270-3 0 9144
2 25544 51
6409 172
1004 0006461 26
0847 334
0642 15
76970754 32161
Satellite: ISS
Catalog Number: 25544
Epoch time: 09334
51310148 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 172
1004 deg
Eccentricity:
0006461
Arg of perigee: 26
0847 deg
Mean anomaly: 334
0642 deg
Mean motion: 15
76970754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 289
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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