Date:
October 15th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 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 709)
---------------------------------------
Vector Time (GMT): 2008/287/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1037655
15 A = 6727397
75 meter
Y = 4598772
73 meter E =
0010902
Z = -4809247
48 I = 51
87505
XDOT = -6045
108777 Wp = 127
20561
YDOT = 4018
682566 meter/sec RA = 130
47184 deg
ZDOT = 2535
974590 TA = 167
59497
MA = 167
56811
Ha = 192
450 n
mi
Hp = 187
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3404380
40 X = 1009516
76
Y = 15087837
03 feet Y = 4610218
62 meter
Z = -15778371
00 Z = -4804275
21
XDOT = -19833
034046 XDOT = -6101
916617
YDOT = 13184
654087 feet/sec YDOT = 3950
765265 meter/sec
ZDOT = 8320
126608 ZDOT = 2506
468478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15268487
51 X = 4653834
99
Y = -2593813
98 feet Y = -790594
50 meter
Z = -15758649
74 Z = -4803236
44
XDOT = 11793
287381 XDOT = 3594
593994
YDOT = 19513
956503 feet/sec YDOT = 5947
853942 meter/sec
ZDOT = 8206
249551 ZDOT = 2501
264863
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 08287
19282729
00020000 00000-0 20000-3 0 9004
2 25544 51
6389 131
3538 0003844 220
1644 139
9234 15
72170365 7102
Satellite: ISS
Catalog Number: 25544
Epoch time: 08287
19282729 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 131
3538 deg
Eccentricity:
0003844
Arg of perigee: 220
1644 deg
Mean anomaly: 139
9234 deg
Mean motion: 15
72170365 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 710
Checksum: 288
Coasting Arc #2 (Orbit 725)
---------------------------------------
Vector Time (GMT): 2008/288/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4773535
86 A = 6736075
54 meter
Y = -4435415
68 meter E =
0009119
Z = -1686569
55 I = 51
92302
XDOT = 2251
537151 Wp = 167
17499
YDOT = 4602
471542 meter/sec RA = 125
40308 deg
ZDOT = -5745
788239 TA = 31
38619
MA = 31
33180
Ha = 192
315 n
mi
Hp = 187
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15661206
88 X = 4830971
88
Y = -14551888
72 feet Y = -4381714
24 meter
Z = -5533364
68 Z = -1663239
22
XDOT = 7386
932911 XDOT = 2227
816993
YDOT = 15099
972252 feet/sec YDOT = 4627
516451 meter/sec
ZDOT = -18851
011282 ZDOT = -5734
907957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13877905
12 X = -4229985
48
Y = -16291767
64 feet Y = -4965730
78 meter
Z = -5443440
77 Z = -1659160
75
XDOT = 14214
219826 XDOT = 4332
494203
YDOT = -5840
115635 feet/sec YDOT = -1780
067246 meter/sec
ZDOT = -18808
411815 ZDOT = -5732
803921
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 08288
20982365
00020000 00000-0 20000-3 0 9011
2 25544 51
6393 126
1446 0003808 225
5264 134
5587 15
72212162 7265
Satellite: ISS
Catalog Number: 25544
Epoch time: 08288
20982365 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 126
1446 deg
Eccentricity:
0003808
Arg of perigee: 225
5264 deg
Mean anomaly: 134
5587 deg
Mean motion: 15
72212162 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 726
Checksum: 288
Coasting Arc #3 (Orbit 741)
---------------------------------------
Vector Time (GMT): 2008/289/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2781268
12 A = 6725676
27 meter
Y = -3278189
05 meter E =
0000509
Z = 5171862
38 I = 51
90422
XDOT = 4664
285577 Wp = 97
12052
YDOT = -5988
225985 meter/sec RA = 120
27478 deg
ZDOT = -1287
287100 TA = 5
14662
MA = 5
14609
Ha = 192
219 n
mi
Hp = 187
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9124895
41 X = -2769528
95
Y = -10755213
42 feet Y = -3309224
87 meter
Z = 16968052
43 Z = 5158379
25
XDOT = 15302
774204 XDOT = 4737
153834
YDOT = -19646
410712 feet/sec YDOT = -5935
659893 meter/sec
ZDOT = -4223
382874 ZDOT = -1264
449945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10981750
22 X = -3347237
47
Y = 8950973
20 feet Y = 2728256
63 meter
Z = 16915506
97 Z = 5155846
53
XDOT = -18605
435464 XDOT = -5670
936729
YDOT = -15011
045188 feet/sec YDOT = -4575
366573 meter/sec
ZDOT = -4135
509389 ZDOT = -1260
503262
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 08289
22680550
00020000 00000-0 20000-3 0 9026
2 25544 51
6394 120
9360 0003789 230
1220 129
9609 15
72229048 7427
Satellite: ISS
Catalog Number: 25544
Epoch time: 08289
22680550 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 120
9360 deg
Eccentricity:
0003789
Arg of perigee: 230
1220 deg
Mean anomaly: 129
9609 deg
Mean motion: 15
72229048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 742
Checksum: 285
Coasting Arc #4 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2008/290/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3246361
00 A = 6737007
36 meter
Y = 5871269
09 meter E =
0009363
Z = 560864
45 I = 51
95610
XDOT = -3919
473227 Wp = 49
20835
YDOT = -2748
594990 meter/sec RA = 115
18838 deg
ZDOT = 6027
415846 TA = 316
86393
MA = 316
93726
Ha = 191
944 n
mi
Hp = 187
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10650790
68 X = -3314497
87
Y = 19262693
86 feet Y = 5834585
45 meter
Z = 1840106
45 Z = 544927
44
XDOT = -12859
164131 XDOT = -3917
727773
YDOT = -9017
700100 feet/sec YDOT = -2792
414901 meter/sec
ZDOT = 19774
986373 ZDOT = 6008
378708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19179660
54 X = 5845960
53
Y = 10809844
02 feet Y = 3294840
46 meter
Z = 1778932
97 Z = 542218
77
XDOT = -8329
419847 XDOT = -2538
807169
YDOT = 11503
576624 feet/sec YDOT = 3506
290155 meter/sec
ZDOT = 19700
981342 ZDOT = 6004
859113
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 08290
24377139
00020000 00000-0 20000-3 0 9037
2 25544 51
6392 115
7262 0003821 234
9918 125
0885 15
72261688 7587
Satellite: ISS
Catalog Number: 25544
Epoch time: 08290
24377139 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 115
7262 deg
Eccentricity:
0003821
Arg of perigee: 234
9918 deg
Mean anomaly: 125
0885 deg
Mean motion: 15
72261688 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 758
Checksum: 306
Coasting Arc #5 (Orbit 772)
---------------------------------------
Vector Time (GMT): 2008/291/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3895049
74 A = 6725022
08 meter
Y = 1437574
86 meter E =
0011893
Z = -5300392
94 I = 51
92804
XDOT = -2647
947089 Wp = 99
21474
YDOT = 7219
453396 meter/sec RA = 110
08159 deg
ZDOT = 10
350693 TA = 170
89403
MA = 170
87244
Ha = 191
800 n
mi
Hp = 187
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12779034
57 X = 3904434
23
Y = 4716452
97 feet Y = 1481184
07 meter
Z = -17389740
62 Z = -5281447
37
XDOT = -8687
490451 XDOT = -2728
529666
YDOT = 23685
870723 feet/sec YDOT = 7189
391962 meter/sec
ZDOT = 33
958966 ZDOT = -2
709134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4594240
17 X = 1400324
40
Y = -12922594
73 feet Y = -3938806
87 meter
Z = -17316213
06 Z = -5277981
74
XDOT = 22824
722793 XDOT = 6956
975507
YDOT = 8127
904145 feet/sec YDOT = 2477
385183 meter/sec
ZDOT = -15
960180 ZDOT = -4
864663
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 08291
19716375
00020000 00000-0 20000-3 0 9042
2 25544 51
6400 110
8424 0003797 240
2882 119
7902 15
72275686 7735
Satellite: ISS
Catalog Number: 25544
Epoch time: 08291
19716375 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 110
8424 deg
Eccentricity:
0003797
Arg of perigee: 240
2882 deg
Mean anomaly: 119
7902 deg
Mean motion: 15
72275686 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 773
Checksum: 299
Coasting Arc #6 (Orbit 788)
---------------------------------------
Vector Time (GMT): 2008/292/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1323823
00 A = 6736920
09 meter
Y = -6576292
92 meter E =
0012102
Z = 537878
19 I = 51
97805
XDOT = 4761
035736 Wp = 145
81662
YDOT = 460
329940 meter/sec RA = 104
97615 deg
ZDOT = -6034
353438 TA = 28
36029
MA = 28
29447
Ha = 191
714 n
mi
Hp = 187
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4343251
32 X = 1394648
79
Y = -21575764
16 feet Y = -6561093
17 meter
Z = 1764692
23 Z = 544481
34
XDOT = 15620
195984 XDOT = 4784
849016
YDOT = 1510
268833 feet/sec YDOT = 513
703928 meter/sec
ZDOT = -19797
747499 ZDOT = -6011
165820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21683628
44 X = -6609169
95
Y = -3756180
84 feet Y = -1144883
92 meter
Z = 1789674
02 Z = 545492
64
XDOT = 816
178654 XDOT = 248
771254
YDOT = -14186
931253 feet/sec YDOT = -4324
176646 meter/sec
ZDOT = -19707
870198 ZDOT = -6006
958836
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 08292
21410108
00020000 00000-0 20000-3 0 9052
2 25544 51
6409 105
6334 0003760 244
0065 116
0710 15
72291150 7899
Satellite: ISS
Catalog Number: 25544
Epoch time: 08292
21410108 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 105
6334 deg
Eccentricity:
0003760
Arg of perigee: 244
0065 deg
Mean anomaly: 116
0710 deg
Mean motion: 15
72291150 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 789
Checksum: 253
Coasting Arc #7 (Orbit 804)
---------------------------------------
Vector Time (GMT): 2008/293/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4234262
59 A = 6725282
93 meter
Y = 658059
97 meter E =
0003734
Z = 5184271
05 I = 51
94607
XDOT = 340
139763 Wp = 184
12659
YDOT = -7590
081878 meter/sec RA = 99
89213 deg
ZDOT = 1237
662558 TA = 254
07113
MA = 254
11227
Ha = 191
563 n
mi
Hp = 187
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13891937
64 X = -4266491
23
Y = 2158989
41 feet Y = 610529
59 meter
Z = 17008763
29 Z = 5163622
29
XDOT = 1115
944103 XDOT = 418
975533
YDOT = -24901
843431 feet/sec YDOT = -7585
837497 meter/sec
ZDOT = 4060
572696 ZDOT = 1239
506173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2770530
79 X = 844457
79
Y = 13881086
77 feet Y = 4230955
25 meter
Z = 16928815
21 Z = 5159902
88
XDOT = -23913
557336 XDOT = -7288
852276
YDOT = -201
493893 feet/sec YDOT = -61
415339 meter/sec
ZDOT = 4067
034695 ZDOT = 1239
632175
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 08293
23102074
00020000 00000-0 20000-3 0 9066
2 25544 51
6411 100
4245 0003891 249
5267 110
5478 15
72362013 8051
Satellite: ISS
Catalog Number: 25544
Epoch time: 08293
23102074 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 100
4245 deg
Eccentricity:
0003891
Arg of perigee: 249
5267 deg
Mean anomaly: 110
5478 deg
Mean motion: 15
72362013 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 805
Checksum: 259
Coasting Arc #8 (Orbit 819)
---------------------------------------
Vector Time (GMT): 2008/294/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 717323
62 A = 6735778
52 meter
Y = 6498905
94 meter E =
0005530
Z = -1605340
56 I = 51
98535
XDOT = -4695
740506 Wp = 12
82051
YDOT = 1943
749541 meter/sec RA = 94
76668 deg
ZDOT = 5779
701645 TA = 329
56263
MA = 329
59472
Ha = 191
401 n
mi
Hp = 187
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2353423
96 X = 652397
07
Y = 21321869
87 feet Y = 6506564
50 meter
Z = -5266865
34 Z = -1602013
21
XDOT = -15405
972790 XDOT = -4745
204039
YDOT = 6377
131041 feet/sec YDOT = 1890
962282 meter/sec
ZDOT = 18962
275737 ZDOT = 5756
769282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21136605
71 X = 6442437
42
Y = -3680536
14 feet Y = -1121827
41 meter
Z = -5253395
33 Z = -1601234
90
XDOT = 7043
886423 XDOT = 2146
976582
YDOT = 13554
990532 feet/sec YDOT = 4131
561114 meter/sec
ZDOT = 18873
583933 ZDOT = 5752
668383
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 08294
18437158
00020000 00000-0 20000-3 0 9076
2 25544 51
6414 95
5405 0003778 255
0205 105
0539 15
72343346 8206
Satellite: ISS
Catalog Number: 25544
Epoch time: 08294
18437158 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 95
5405 deg
Eccentricity:
0003778
Arg of perigee: 255
0205 deg
Mean anomaly: 105
0539 deg
Mean motion: 15
72343346 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 820
Checksum: 284
Coasting Arc #9 (Orbit 835)
---------------------------------------
Vector Time (GMT): 2008/295/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3797519
25 A = 6726557
41 meter
Y = -2678781
54 meter E =
0008423
Z = -4870902
99 I = 51
95688
XDOT = 1909
129298 Wp = 69
78791
YDOT = 7056
117750 meter/sec RA = 89
70044 deg
ZDOT = -2392
608903 TA = 176
94921
MA = 176
94407
Ha = 191
304 n
mi
Hp = 187
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12459052
64 X = 3850853
83
Y = -8788653
35 feet Y = -2636017
18 meter
Z = -15980652
84 Z = -4852324
91
XDOT = 6263
547567 XDOT = 1841
707760
YDOT = 23149
992619 feet/sec YDOT = 7077
089811 meter/sec
ZDOT = -7849
766741 ZDOT = -2383
497867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9743222
13 X = -2969734
10
Y = -11824824
64 feet Y = -3604206
55 meter
Z = -15908891
56 Z = -4849030
15
XDOT = 21723
491658 XDOT = 6621
320257
YDOT = -7388
889584 feet/sec YDOT = -2252
133545 meter/sec
ZDOT = -7813
837082 ZDOT = -2381
657543
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 08295
20126209
00020000 00000-0 20000-3 0 9083
2 25544 51
6423 90
3310 0003689 259
6666 100
4080 15
72394973 8365
Satellite: ISS
Catalog Number: 25544
Epoch time: 08295
20126209 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 90
3310 deg
Eccentricity:
0003689
Arg of perigee: 259
6666 deg
Mean anomaly: 100
4080 deg
Mean motion: 15
72394973 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 836
Checksum: 290
Coasting Arc #10 (Orbit 851)
---------------------------------------
Vector Time (GMT): 2008/296/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2549526
19 A = 6733969
42 meter
Y = -5677322
14 meter E =
0010389
Z = 2557794
98 I = 51
97995
XDOT = 3781
023066 Wp = 110
93288
YDOT = -4096
816059 meter/sec RA = 84
55996 deg
ZDOT = -5310
981849 TA = 40
21622
MA = 40
13940
Ha = 191
301 n
mi
Hp = 187
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8364587
23 X = -2498277
40
Y = -18626384
99 feet Y = -5705545
86 meter
Z = 8391715
83 Z = 2545533
76
XDOT = 12404
931318 XDOT = 3852
353371
YDOT = -13440
997568 feet/sec YDOT = -4054
135667 meter/sec
ZDOT = -17424
481132 ZDOT = -5292
440169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17739511
84 X = -5407003
21
Y = 10149967
35 feet Y = 3093710
05 meter
Z = 8343699
08 Z = 2543159
48
XDOT = -13831
826818 XDOT = -4215
940814
YDOT = -9872
745614 feet/sec YDOT = -3009
212863 meter/sec
ZDOT = -17352
979456 ZDOT = -5289
188138
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 08296
21813710
00020000 00000-0 20000-3 0 9096
2 25544 51
6420 85
1216 0003722 263
4556 96
6182 15
72386470 8528
Satellite: ISS
Catalog Number: 25544
Epoch time: 08296
21813710 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 85
1216 deg
Eccentricity:
0003722
Arg of perigee: 263
4556 deg
Mean anomaly: 96
6182 deg
Mean motion: 15
72386470 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 852
Checksum: 286
Coasting Arc #11 (Orbit 867)
---------------------------------------
Vector Time (GMT): 2008/297/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2665997
14 A = 6728452
09 meter
Y = 4367205
51 meter E =
0006170
Z = 4366834
17 I = 51
95813
XDOT = -3795
356005 Wp = 121
45429
YDOT = -5753
342486 meter/sec RA = 79
50494 deg
ZDOT = 3430
048554 TA = 294
06168
MA = 294
12623
Ha = 191
250 n
mi
Hp = 187
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8746709
79 X = -2735847
33
Y = 14328102
06 feet Y = 4337002
36 meter
Z = 14326883
76 Z = 4353712
82
XDOT = -12451
955396 XDOT = -3747
401858
YDOT = -18875
795557 feet/sec YDOT = -5795
516130 meter/sec
ZDOT = 11253
440139 ZDOT = 3411
727151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15230027
72 X = 4642112
45
Y = 7161663
96 feet Y = 2182875
18 meter
Z = 14276409
36 Z = 4351449
57
XDOT = -16826
444024 XDOT = -5128
700139
YDOT = 13448
752489 feet/sec YDOT = 4099
179759 meter/sec
ZDOT = 11181
929748 ZDOT = 3408
252187
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 08297
23499461
00020000 00000-0 20000-3 0 9104
2 25544 51
6424 79
9114 0003734 269
5659 90
5076 15
72422385 8682
Satellite: ISS
Catalog Number: 25544
Epoch time: 08297
23499461 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 79
9114 deg
Eccentricity:
0003734
Arg of perigee: 269
5659 deg
Mean anomaly: 90
5076 deg
Mean motion: 15
72422385 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 868
Checksum: 318
Coasting Arc #12 (Orbit 882)
---------------------------------------
Vector Time (GMT): 2008/298/04:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3955429
11 A = 6731609
66 meter
Y = 4254265
95 meter E =
0001089
Z = -3402059
61 I = 51
96291
XDOT = -2170
740612 Wp = 71
72077
YDOT = 5734
568741 meter/sec RA = 74
35410 deg
ZDOT = 4648
776666 TA = 248
36481
MA = 248
37641
Ha = 191
121 n
mi
Hp = 187
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12977129
61 X = 3924090
06
Y = 13957565
44 feet Y = 4298322
46 meter
Z = -11161612
88 Z = -3382920
18
XDOT = -7121
852402 XDOT = -2257
287394
YDOT = 18814
201906 feet/sec YDOT = 5709
810569 meter/sec
ZDOT = 15251
891948 ZDOT = 4638
020572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12150920
62 X = 3703600
61
Y = -14738835
13 feet Y = -4492396
95 meter
Z = -11087064
31 Z = -3379337
20
XDOT = 18514
752677 XDOT = 5643
296616
YDOT = 3825
657945 feet/sec YDOT = 1166
060542 meter/sec
ZDOT = 15210
700040 ZDOT = 4636
221372
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 08298
18828316
00020000 00000-0 20000-3 0 9115
2 25544 51
6429 75
0270 0003843 274
7197 85
3526 15
72458501 8831
Satellite: ISS
Catalog Number: 25544
Epoch time: 08298
18828316 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 75
0270 deg
Eccentricity:
0003843
Arg of perigee: 274
7197 deg
Mean anomaly: 85
3526 deg
Mean motion: 15
72458501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 883
Checksum: 308
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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