Date:
February 17th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12852 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 877)
---------------------------------------
Vector Time (GMT): 2008/043/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4550094
14 A = 6718557
89 meter
Y = -4542887
06 meter E =
0018850
Z = 1914014
87 I = 51
37710
XDOT = 2361
607208 Wp = 59
27180
YDOT = 4741
245212 meter/sec RA = 301
28679 deg
ZDOT = 5607
917248 TA = 322
14727
MA = 322
27967
Ha = 185
094 n
mi
Hp = 175
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14928130
37 X = 4591257
38
Y = -14904485
10 feet Y = -4491775
15 meter
Z = 6279576
33 Z = 1936219
02
XDOT = 7748
055144 XDOT = 2281
172360
YDOT = 15555
266445 feet/sec YDOT = 4767
204336 meter/sec
ZDOT = 18398
678635 ZDOT = 5619
194436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21065433
97 X = -6420744
27
Y = -415167
89 feet Y = -126543
17 meter
Z = 6364036
35 Z = 1939758
28
XDOT = 5892
853059 XDOT = 1796
141612
YDOT = -14752
156178 feet/sec YDOT = -4496
457203 meter/sec
ZDOT = 18442
310242 ZDOT = 5621
216162
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 08044
03785776
00020000 00000-0 20000-3 0 9008
2 25544 51
6400 301
5720 0005238 37
1976 322
9551 15
78221715 8786
Satellite: ISS
Catalog Number: 25544
Epoch time: 08044
03785776 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 301
5720 deg
Eccentricity:
0005238
Arg of perigee: 37
1976 deg
Mean anomaly: 322
9551 deg
Mean motion: 15
78221715 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 878
Checksum: 286
Coasting Arc #2 (Orbit 892)
---------------------------------------
Vector Time (GMT): 2008/044/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1236273
59 A = 6712285
84 meter
Y = -5103013
00 meter E =
0011169
Z = -4190382
29 I = 51
34182
XDOT = 5302
202525 Wp = 84
02889
YDOT = -4250
074285 meter/sec RA = 296
05587 deg
ZDOT = 3620
817679 TA = 222
95499
MA = 223
04225
Ha = 185
062 n
mi
Hp = 175
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4056015
72 X = -1158763
12
Y = -16742168
63 feet Y = -5116404
23 meter
Z = -13747973
39 Z = -4196199
89
XDOT = 17395
677577 XDOT = 5331
744339
YDOT = -13943
813270 feet/sec YDOT = -4190
616945 meter/sec
ZDOT = 11879
323094 ZDOT = 3646
647178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9068219
19 X = -2763993
21
Y = 14625040
82 feet Y = 4457712
44 meter
Z = -13770759
89 Z = -4197327
61
XDOT = -21039
044326 XDOT = -6412
700710
YDOT = -1796
161627 feet/sec YDOT = -547
470064 meter/sec
ZDOT = 11977
684331 ZDOT = 3650
798184
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 08044
98763764
00020000 00000-0 20000-3 0 9016
2 25544 51
6393 296
6642 0005237 40
7920 319
3636 15
78295316 8931
Satellite: ISS
Catalog Number: 25544
Epoch time: 08044
98763764 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 296
6642 deg
Eccentricity:
0005237
Arg of perigee: 40
7920 deg
Mean anomaly: 319
3636 deg
Mean motion: 15
78295316 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 893
Checksum: 319
Coasting Arc #3 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2008/045/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4575913
47 A = 6712222
38 meter
Y = 2593561
77 meter E =
0013113
Z = -4183997
90 I = 51
32949
XDOT = -521
075894 Wp = 59
46343
YDOT = -6767
730248 meter/sec RA = 290
91606 deg
ZDOT = -3627
133290 TA = 173
41394
MA = 173
39668
Ha = 185
082 n
mi
Hp = 175
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15012839
45 X = -4584250
15
Y = 8509060
93 feet Y = 2542344
88 meter
Z = -13727027
22 Z = -4206247
52
XDOT = -1709
566582 XDOT = -427
739644
YDOT = -22203
839395 feet/sec YDOT = -6773
035180 meter/sec
ZDOT = -11900
043601 ZDOT = -3629
438241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16640564
01 X = 5072043
91
Y = 4306340
70 feet Y = 1312572
65 meter
Z = -13811871
77 Z = -4209858
52
XDOT = -13982
889538 XDOT = -4261
984731
YDOT = 15854
198473 feet/sec YDOT = 4832
359694 meter/sec
ZDOT = -11909
568794 ZDOT = -3630
036568
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 08046
00070365
00020000 00000-0 20000-3 0 9020
2 25544 51
6386 291
4279 0005188 43
6126 316
5449 15
78306230 9094
Satellite: ISS
Catalog Number: 25544
Epoch time: 08046
00070365 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 291
4279 deg
Eccentricity:
0005188
Arg of perigee: 43
6126 deg
Mean anomaly: 316
5449 deg
Mean motion: 15
78306230 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 909
Checksum: 286
Coasting Arc #4 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2008/046/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -241951
80 A = 6718152
32 meter
Y = 6438484
75 meter E =
0016963
Z = 1884346
44 I = 51
34143
XDOT = -5075
750078 Wp = 96
13740
YDOT = 1464
407572 meter/sec RA = 285
68242 deg
ZDOT = -5613
958067 TA = 62
79492
MA = 62
62214
Ha = 185
030 n
mi
Hp = 175
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -793805
11 X = -323083
58
Y = 21123637
62 feet Y = 6435325
37 meter
Z = 6182238
97 Z = 1882974
35
XDOT = -16652
723352 XDOT = -5064
476991
YDOT = 4804
486784 feet/sec YDOT = 1407
710990 meter/sec
ZDOT = -18418
497594 ZDOT = -5638
588133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15063187
48 X = 4591259
55
Y = -14832231
43 feet Y = -4520864
14 meter
Z = 6177666
61 Z = 1882952
78
XDOT = 14270
947125 XDOT = 4349
784684
YDOT = 6726
010724 feet/sec YDOT = 2050
088069 meter/sec
ZDOT = -18512
572877 ZDOT = -5642
632213
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 08047
01373474
00020000 00000-0 20000-3 0 9030
2 25544 51
6390 286
1917 0005353 46
0643 314
0963 15
78396273 9252
Satellite: ISS
Catalog Number: 25544
Epoch time: 08047
01373474 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 286
1917 deg
Eccentricity:
0005353
Arg of perigee: 46
0643 deg
Mean anomaly: 314
0963 deg
Mean motion: 15
78396273 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 925
Checksum: 294
Coasting Arc #5 (Orbit 940)
---------------------------------------
Vector Time (GMT): 2008/047/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4212782
61 A = 6707537
62 meter
Y = 178778
14 meter E =
0006895
Z = 5210715
23 I = 51
29922
XDOT = -981
649457 Wp = 70
27974
YDOT = 7632
617924 meter/sec RA = 280
51273 deg
ZDOT = 533
504293 TA = 14
64602
MA = 14
62605
Ha = 184
813 n
mi
Hp = 175
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13821465
24 X = 4185158
30
Y = 586542
44 feet Y = 225733
15 meter
Z = 17095522
41 Z = 5231113
33
XDOT = -3220
634701 XDOT = -1069
517212
YDOT = 25041
397388 feet/sec YDOT = 7621
149240 meter/sec
ZDOT = 1750
342169 ZDOT = 528
522525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9771388
88 X = -2978319
33
Y = -9655138
36 feet Y = -2942886
17 meter
Z = 17173586
77 Z = 5234509
25
XDOT = 18512
801802 XDOT = 5642
701989
YDOT = -15664
873476 feet/sec YDOT = -4774
653435 meter/sec
ZDOT = 1732
091897 ZDOT = 527
941610
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 08048
02673167
00020000 00000-0 20000-3 0 9045
2 25544 51
6387 280
9555 0005201 49
5709 310
5910 15
78447029 9418
Satellite: ISS
Catalog Number: 25544
Epoch time: 08048
02673167 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 280
9555 deg
Eccentricity:
0005201
Arg of perigee: 49
5709 deg
Mean anomaly: 310
5910 deg
Mean motion: 15
78447029 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 941
Checksum: 295
Coasting Arc #6 (Orbit 956)
---------------------------------------
Vector Time (GMT): 2008/048/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1412796
12 A = 6719139
90 meter
Y = -6481706
48 meter E =
0019304
Z = 1006161
19 I = 51
33343
XDOT = 4569
159662 Wp = 54
83030
YDOT = 1923
759239 meter/sec RA = 275
32535 deg
ZDOT = 5908
550209 TA = 316
24239
MA = 316
39522
Ha = 185
077 n
mi
Hp = 175
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4635157
88 X = 1480282
96
Y = -21265441
19 feet Y = -6465530
48 meter
Z = 3301053
78 Z = 1013188
05
XDOT = 14990
681306 XDOT = 4518
606489
YDOT = 6311
546061 feet/sec YDOT = 1974
571329 meter/sec
ZDOT = 19385
007247 ZDOT = 5930
623801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17486278
12 X = -5329817
57
Y = 12952226
15 feet Y = 3947838
53 meter
Z = 3327243
48 Z = 1014143
81
XDOT = -6088
326798 XDOT = -1855
722008
YDOT = -13278
429211 feet/sec YDOT = -4047
265223 meter/sec
ZDOT = 19469
677320 ZDOT = 5934
357647
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 08049
03969783
00020000 00000-0 20000-3 0 9050
2 25544 51
6379 275
7189 0005527 52
5084 307
6583 15
78438864 9572
Satellite: ISS
Catalog Number: 25544
Epoch time: 08049
03969783 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 275
7189 deg
Eccentricity:
0005527
Arg of perigee: 52
5084 deg
Mean anomaly: 307
6583 deg
Mean motion: 15
78438864 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 957
Checksum: 344
Coasting Arc #7 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2008/049/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3716280
33 A = 6709827
85 meter
Y = -3122403
10 meter E =
0014878
Z = -4645722
59 I = 51
30136
XDOT = 2246
446802 Wp = 92
25334
YDOT = -6813
189906 meter/sec RA = 270
10037 deg
ZDOT = 2789
258100 TA = 205
37624
MA = 205
44938
Ha = 184
946 n
mi
Hp = 175
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12192520
76 X = -3658521
59
Y = -10244104
66 feet Y = -3163637
68 meter
Z = -15241872
01 Z = -4663635
42
XDOT = 7370
232291 XDOT = 2308
916714
YDOT = -22352
985256 feet/sec YDOT = -6787
719592 meter/sec
ZDOT = 9151
109251 ZDOT = 2800
322664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2623739
01 X = 799715
65
Y = 15640028
69 feet Y = 4767080
74 meter
Z = -15310760
97 Z = -4666719
94
XDOT = -18885
432835 XDOT = -5756
279928
YDOT = 12144
626730 feet/sec YDOT = 3701
682227 meter/sec
ZDOT = 9192
703714 ZDOT = 2801
936092
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 08049
98931838
00020000 00000-0 20000-3 0 9065
2 25544 51
6378 270
8092 0005441 55
8671 304
3010 15
78524853 9723
Satellite: ISS
Catalog Number: 25544
Epoch time: 08049
98931838 = yrday
fracday
Element set: 906
Inclination: 51
6378 deg
RA of node: 270
8092 deg
Eccentricity:
0005441
Arg of perigee: 55
8671 deg
Mean anomaly: 304
3010 deg
Mean motion: 15
78524853 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 972
Checksum: 310
Coasting Arc #8 (Orbit 987)
---------------------------------------
Vector Time (GMT): 2008/050/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2510575
22 A = 6713196
02 meter
Y = 5033961
51 meter E =
0011149
Z = -3676196
19 I = 51
31486
XDOT = -3894
733513 Wp = 69
38948
YDOT = -5069
243196 meter/sec RA = 264
95384 deg
ZDOT = -4288
306631 TA = 155
10330
MA = 155
04947
Ha = 184
912 n
mi
Hp = 174
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8236795
33 X = -2548821
45
Y = 16515621
76 feet Y = 5005672
91 meter
Z = -12061011
11 Z = -3688485
16
XDOT = -12777
997090 XDOT = -3816
927855
YDOT = -16631
375316 feet/sec YDOT = -5112
361382 meter/sec
ZDOT = -14069
247478 ZDOT = -4307
037535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16775427
40 X = 5113150
27
Y = -7620534
48 feet Y = -2322738
91 meter
Z = -12107478
61 Z = -3690359
48
XDOT = -1246
349446 XDOT = -379
887311
YDOT = 19689
983378 feet/sec YDOT = 6001
506933 meter/sec
ZDOT = -14141
493881 ZDOT = -4310
327335
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 08051
00221536
00020000 00000-0 20000-3 0 9079
2 25544 51
6380 265
5716 0005480 60
0970 300
0739 15
78591843 9884
Satellite: ISS
Catalog Number: 25544
Epoch time: 08051
00221536 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 265
5716 deg
Eccentricity:
0005480
Arg of perigee: 60
0970 deg
Mean anomaly: 300
0739 deg
Mean motion: 15
78591843 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 988
Checksum: 285
Coasting Arc #9 (Orbit 1003)
---------------------------------------
Vector Time (GMT): 2008/051/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3023322
10 A = 6716181
82 meter
Y = 5442406
52 meter E =
0018316
Z = 2502258
58 I = 51
32843
XDOT = -3501
774224 Wp = 92
56830
YDOT = 4389
926322 meter/sec RA = 259
71129 deg
ZDOT = -5284
706140 TA = 58
89928
MA = 58
71969
Ha = 184
807 n
mi
Hp = 174
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9919035
76 X = 2950084
42
Y = 17855664
45 feet Y = 5475805
66 meter
Z = 8209509
76 Z = 2516767
28
XDOT = -11488
760579 XDOT = -3524
931435
YDOT = 14402
645415 feet/sec YDOT = 4350
637759 meter/sec
ZDOT = -17338
274739 ZDOT = -5301
773693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3307595
20 X = 1008155
02
Y = -20133228
36 feet Y = -6136608
00 meter
Z = 8265652
04 Z = 2519370
74
XDOT = 16394
765583 XDOT = 4997
124550
YDOT = -4494
724920 feet/sec YDOT = -1369
992156 meter/sec
ZDOT = -17403
095296 ZDOT = -5304
463446
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 08052
01507666
00020000 00000-0 20000-3 0 9083
2 25544 51
6369 260
3338 0005491 62
2370 297
9352 15
78659185 10043
Satellite: ISS
Catalog Number: 25544
Epoch time: 08052
01507666 = yrday
fracday
Element set: 908
Inclination: 51
6369 deg
RA of node: 260
3338 deg
Eccentricity:
0005491
Arg of perigee: 62
2370 deg
Mean anomaly: 297
9352 deg
Mean motion: 15
78659185 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1004
Checksum: 298
Coasting Arc #10 (Orbit 1019)
---------------------------------------
Vector Time (GMT): 2008/052/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3595876
66 A = 6707225
42 meter
Y = -2394627
40 meter E =
0008410
Z = 5123320
50 I = 51
30461
XDOT = 2949
169170 Wp = 90
71342
YDOT = 7025
641490 meter/sec RA = 254
54911 deg
ZDOT = 1212
038788 TA = 347
66449
MA = 347
68507
Ha = 184
704 n
mi
Hp = 174
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11797495
60 X = 3597498
99
Y = -7856389
12 feet Y = -2354406
85 meter
Z = 16808794
29 Z = 5140792
91
XDOT = 9675
751869 XDOT = 2864
500464
YDOT = 23050
004889 feet/sec YDOT = 7058
147456 meter/sec
ZDOT = 3976
505211 ZDOT = 1226
159349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14069810
17 X = -4288478
14
Y = -837277
46 feet Y = -255202
17 meter
Z = 16875388
18 Z = 5143618
32
XDOT = 6220
623823 XDOT = 1896
046141
YDOT = -23161
286473 feet/sec YDOT = -7059
560117 meter/sec
ZDOT = 4031
354007 ZDOT = 1228
756701
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 08053
02790391
00020000 00000-0 20000-3 0 9095
2 25544 51
6364 255
0957 0005541 66
2033 293
9713 15
78701173 10202
Satellite: ISS
Catalog Number: 25544
Epoch time: 08053
02790391 = yrday
fracday
Element set: 909
Inclination: 51
6364 deg
RA of node: 255
0957 deg
Eccentricity:
0005541
Arg of perigee: 66
2033 deg
Mean anomaly: 293
9713 deg
Mean motion: 15
78701173 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1020
Checksum: 279
Coasting Arc #11 (Orbit 1035)
---------------------------------------
Vector Time (GMT): 2008/053/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1979254
60 A = 6718620
38 meter
Y = -6392325
53 meter E =
0018496
Z = 503047
12 I = 51
35314
XDOT = 4750
068667 Wp = 55
47153
YDOT = -987
593318 meter/sec RA = 249
34969 deg
ZDOT = 5994
233717 TA = 310
03631
MA = 310
19844
Ha = 184
744 n
mi
Hp = 174
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6493617
46 X = -1910071
19
Y = -20972196
62 feet Y = -6414071
82 meter
Z = 1650417
08 Z = 493600
65
XDOT = 15584
214786 XDOT = 4731
640771
YDOT = -3240
135558 feet/sec YDOT = -934
577913 meter/sec
ZDOT = 19666
121119 ZDOT = 6017
264370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7173659
94 X = -2186531
55
Y = 20752328
28 feet Y = 6325309
66 meter
Z = 1613520
86 Z = 491801
16
XDOT = -12875
065292 XDOT = -3924
319901
YDOT = -6024
525888 feet/sec YDOT = -1836
275491 meter/sec
ZDOT = 19754
149106 ZDOT = 6021
064648
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 08054
04069598
00020000 00000-0 20000-3 0 9108
2 25544 51
6370 249
8577 0005523 68
0609 292
1143 15
78743215 10365
Satellite: ISS
Catalog Number: 25544
Epoch time: 08054
04069598 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 249
8577 deg
Eccentricity:
0005523
Arg of perigee: 68
0609 deg
Mean anomaly: 292
1143 deg
Mean motion: 15
78743215 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1036
Checksum: 295
Coasting Arc #12 (Orbit 1050)
---------------------------------------
Vector Time (GMT): 2008/054/23:28:48
314
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4624247
51 A = 6708333
61 meter
Y = -683798
07 meter E =
0016858
Z = -4826571
30 I = 51
33081
XDOT = -1391
235353 Wp = 96
20525
YDOT = -7192
738339 meter/sec RA = 244
13175 deg
ZDOT = 2357
186036 TA = 196
86399
MA = 196
92010
Ha = 184
658 n
mi
Hp = 174
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15171415
71 X = -4592811
26
Y = -2243431
98 feet Y = -735333
65 meter
Z = -15835207
69 Z = -4848959
11
XDOT = -4564
420450 XDOT = -1322
152238
YDOT = -23598
222898 feet/sec YDOT = -7207
909480 meter/sec
ZDOT = 7733
549987 ZDOT = 2350
595886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11010152
70 X = 3355894
54
Y = 10547883
00 feet Y = 3214994
74 meter
Z = -15920971
89 Z = -4852712
23
XDOT = -9110
460789 XDOT = -2776
868448
YDOT = 21117
563421 feet/sec YDOT = 6436
633331 meter/sec
ZDOT = 7707
485870 ZDOT = 2349
241693
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 08054
99015494
00020000 00000-0 20000-3 0 9119
2 25544 51
6374 244
9465 0005409 70
5383 289
6367 15
78781023 10516
Satellite: ISS
Catalog Number: 25544
Epoch time: 08054
99015494 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 244
9465 deg
Eccentricity:
0005409
Arg of perigee: 70
5383 deg
Mean anomaly: 289
6367 deg
Mean motion: 15
78781023 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1051
Checksum: 307
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 may contain past, current and future orbital data 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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