Date:
April 9th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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 1738)
---------------------------------------
Vector Time (GMT): 2008/098/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5850544
02 A = 6718781
57 meter
Y = 597418
03 meter E =
0012595
Z = 3238954
90 I = 51
75752
XDOT = -3177
663211 Wp = 87
18245
YDOT = -5150
742554 meter/sec RA = 19
89509 deg
ZDOT = -4773
333178 TA = 54
92069
MA = 54
80265
Ha = 185
294 n
mi
Hp = 179
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19194698
24 X = -5872524
15
Y = 1960032
92 feet Y = 531871
13 meter
Z = 10626492
45 Z = 3210479
06
XDOT = -10425
404237 XDOT = -3096
642246
YDOT = -16898
761659 feet/sec YDOT = -5185
824167 meter/sec
ZDOT = -15660
541922 ZDOT = -4788
573533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13335505
88 X = -4064662
19
Y = 14026779
89 feet Y = 4275362
51 meter
Z = 10517330
46 Z = 3205682
33
XDOT = -17826
185991 XDOT = -5433
421490
YDOT = -5120
214901 feet/sec YDOT = -1560
641502 meter/sec
ZDOT = -15719
516703 ZDOT = -4791
308691
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 08098
60827130
00020000 00000-0 20000-3 0 9001
2 25544 51
6422 20
2271 0001253 345
4714 14
6414 15
77137005 17391
Satellite: ISS
Catalog Number: 25544
Epoch time: 08098
60827130 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 20
2271 deg
Eccentricity:
0001253
Arg of perigee: 345
4714 deg
Mean anomaly: 14
6414 deg
Mean motion: 15
77137005 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1739
Checksum: 254
Coasting Arc #2 (Orbit 1754)
---------------------------------------
Vector Time (GMT): 2008/099/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1932389
41 A = 6713323
90 meter
Y = 4362370
85 meter E =
0006735
Z = 4718334
67 I = 51
71252
XDOT = -7220
196401 Wp = 110
34269
YDOT = 287
088872 meter/sec RA = 14
78808 deg
ZDOT = 2686
220580 TA = 313
27396
MA = 313
33014
Ha = 185
101 n
mi
Hp = 178
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6339860
28 X = 1860543
89
Y = 14312240
32 feet Y = 4383578
24 meter
Z = 15480100
62 Z = 4727547
84
XDOT = -23688
308402 XDOT = -7235
919438
YDOT = 941
892625 feet/sec YDOT = 206
260607 meter/sec
ZDOT = 8813
059646 ZDOT = 2651
106099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14179720
86 X = 4321978
92
Y = 6546817
20 feet Y = 1995469
88 meter
Z = 15515871
47 Z = 4729237
62
XDOT = -16642
586915 XDOT = -5072
660492
YDOT = 15436
714093 feet/sec YDOT = 4705
110455 meter/sec
ZDOT = 8678
401977 ZDOT = 2645
176923
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 08099
62205802
00020000 00000-0 20000-3 0 9011
2 25544 51
6428 14
9962 0001308 345
5024 14
6103 15
77195041 17557
Satellite: ISS
Catalog Number: 25544
Epoch time: 08099
62205802 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 14
9962 deg
Eccentricity:
0001308
Arg of perigee: 345
5024 deg
Mean anomaly: 14
6103 deg
Mean motion: 15
77195041 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1755
Checksum: 270
Coasting Arc #3 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2008/100/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6584416
48 A = 6722181
28 meter
Y = 49224
36 meter E =
0009846
Z = -1329603
17 I = 51
71434
XDOT = 1140
180192 Wp = 30
42227
YDOT = 4879
385429 meter/sec RA = 9
59980 deg
ZDOT = 5854
105686 TA = 314
97214
MA = 315
05192
Ha = 185
051 n
mi
Hp = 178
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21602416
28 X = 6589835
73
Y = 161497
24 feet Y = 122885
40 meter
Z = -4362215
13 Z = -1297602
51
XDOT = 3740
748663 XDOT = 1057
094856
YDOT = 16008
482379 feet/sec YDOT = 4891
670880 meter/sec
ZDOT = 19206
383484 ZDOT = 5859
443053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16027230
50 X = 4885099
86
Y = -14521508
78 feet Y = -4426155
88 meter
Z = -4239464
19 Z = -1292188
69
XDOT = 12451
029449 XDOT = 3795
073776
YDOT = 8155
472644 feet/sec YDOT = 2485
788062 meter/sec
ZDOT = 19227
333595 ZDOT = 5860
491280
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 08100
57245363
00020000 00000-0 20000-3 0 9025
2 25544 51
6429 10
0921 0001360 342
7068 17
4051 15
77260254 17704
Satellite: ISS
Catalog Number: 25544
Epoch time: 08100
57245363 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 10
0921 deg
Eccentricity:
0001360
Arg of perigee: 342
7068 deg
Mean anomaly: 17
4051 deg
Mean motion: 15
77260254 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1770
Checksum: 251
Coasting Arc #4 (Orbit 1785)
---------------------------------------
Vector Time (GMT): 2008/101/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 29543
88 A = 6710679
51 meter
Y = -4176472
12 meter E =
0014746
Z = -5265152
28 I = 51
64660
XDOT = 7681
313686 Wp = 82
47283
YDOT = 389
002672 meter/sec RA = 4
45668 deg
ZDOT = -264
199778 TA = 185
01066
MA = 185
02544
Ha = 184
922 n
mi
Hp = 178
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 96928
74 X = 101820
99
Y = -13702336
34 feet Y = -4175737
41 meter
Z = -17274121
65 Z = -5264833
35
XDOT = 25201
160388 XDOT = 7677
676348
YDOT = 1276
255487 feet/sec YDOT = 474
879183 meter/sec
ZDOT = -866
797173 ZDOT = -226
892507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9306691
77 X = -2836679
65
Y = -10058686
29 feet Y = -3065887
58 meter
Z = -17273303
49 Z = -5264902
90
XDOT = 18402
268518 XDOT = 5609
011444
YDOT = -15776
669247 feet/sec YDOT = -4808
728787 meter/sec
ZDOT = -723
652485 ZDOT = -220
569277
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 08101
58617774
00020000 00000-0 20000-3 0 9037
2 25544 51
6425 4
8606 0001434 343
0052 17
1065 15
77317149 17865
Satellite: ISS
Catalog Number: 25544
Epoch time: 08101
58617774 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 4
8606 deg
Eccentricity:
0001434
Arg of perigee: 343
0052 deg
Mean anomaly: 17
1065 deg
Mean motion: 15
77317149 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1786
Checksum: 274
Coasting Arc #5 (Orbit 1801)
---------------------------------------
Vector Time (GMT): 2008/102/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6629237
21 A = 6722398
44 meter
Y = -627184
84 meter E =
0008837
Z = -894692
34 I = 51
65682
XDOT = 1245
566643 Wp = 138
52587
YDOT = -4726
316930 meter/sec RA = 359
30386 deg
ZDOT = -5955
718732 TA = 51
24953
MA = 51
17059
Ha = 184
890 n
mi
Hp = 178
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21749465
92 X = -6617384
97
Y = -2057693
03 feet Y = -701250
45 meter
Z = -2935342
31 Z = -926868
46
XDOT = 4086
504735 XDOT = 1327
256332
YDOT = -15506
289141 feet/sec YDOT = -4711
931315 meter/sec
ZDOT = -19539
759621 ZDOT = -5949
469516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16924341
88 X = -5158539
41
Y = 13787668
25 feet Y = 4202481
28 meter
Z = -3058832
91 Z = -932332
27
XDOT = -6888
148686 XDOT = -2099
507719
YDOT = -12757
091333 feet/sec YDOT = -3888
361438 meter/sec
ZDOT = -19516
244396 ZDOT = -5948
551292
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 08102
59987102
00020000 00000-0 20000-3 0 9045
2 25544 51
6424 359
6294 0001279 339
5756 20
5358 15
77308526 18027
Satellite: ISS
Catalog Number: 25544
Epoch time: 08102
59987102 = yrday
fracday
Element set: 904
Inclination: 51
6424 deg
RA of node: 359
6294 deg
Eccentricity:
0001279
Arg of perigee: 339
5756 deg
Mean anomaly: 20
5358 deg
Mean motion: 15
77308526 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1802
Checksum: 304
Coasting Arc #6 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2008/103/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2117516
31 A = 6712104
10 meter
Y = 4100486
34 meter E =
0007222
Z = 4871173
91 I = 51
59379
XDOT = -7289
872902 Wp = 45
77392
YDOT = -1058
349038 meter/sec RA = 354
11370 deg
ZDOT = -2271
007131 TA = 66
34775
MA = 66
27196
Ha = 184
788 n
mi
Hp = 178
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6947232
00 X = -2186874
43
Y = 13453039
17 feet Y = 4076419
14 meter
Z = 15981541
71 Z = 4860718
68
XDOT = -23916
905845 XDOT = -7266
464369
YDOT = -3472
273747 feet/sec YDOT = -1139
737622 meter/sec
ZDOT = -7450
810797 ZDOT = -2306
364396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4678310
61 X = 1425949
07
Y = 14444009
36 feet Y = 4402534
05 meter
Z = 15941830
95 Z = 4859070
07
XDOT = -18140
930483 XDOT = -5529
355611
YDOT = 14274
474414 feet/sec YDOT = 4350
859802 meter/sec
ZDOT = -7586
551342 ZDOT = -2312
380849
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 08103
61352940
00020000 00000-0 20000-3 0 9056
2 25544 51
6424 354
3972 0001527 341
6108 18
5002 15
77432637 18184
Satellite: ISS
Catalog Number: 25544
Epoch time: 08103
61352940 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 354
3972 deg
Eccentricity:
0001527
Arg of perigee: 341
6108 deg
Mean anomaly: 18
5002 deg
Mean motion: 15
77432637 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1818
Checksum: 272
Coasting Arc #7 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2008/104/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5878866
69 A = 6718441
54 meter
Y = 1264871
36 meter E =
0013076
Z = 2981397
99 I = 51
58555
XDOT = -3542
746993 Wp = 76
53537
YDOT = 4707
191673 meter/sec RA = 348
99090 deg
ZDOT = 4973
542880 TA = 317
99971
MA = 318
09990
Ha = 184
675 n
mi
Hp = 178
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19287620
39 X = 5849802
76
Y = 4149840
43 feet Y = 1330449
70 meter
Z = 9781489
48 Z = 3009886
78
XDOT = -11623
185672 XDOT = -3619
280681
YDOT = 15443
542235 feet/sec YDOT = 4667
146714 meter/sec
ZDOT = 16317
397901 ZDOT = 4956
146425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16239037
72 X = 4949658
70
Y = -11107415
69 feet Y = -3385540
30 meter
Z = 9890904
05 Z = 3014747
55
XDOT = 2344
023072 XDOT = 714
458232
YDOT = 17942
053206 feet/sec YDOT = 5468
737817 meter/sec
ZDOT = 16251
119456 ZDOT = 4953
341210
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 08104
62715916
00020000 00000-0 20000-3 0 9065
2 25544 51
6414 349
1646 0001581 344
2290 15
8826 15
77440206 18347
Satellite: ISS
Catalog Number: 25544
Epoch time: 08104
62715916 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 349
1646 deg
Eccentricity:
0001581
Arg of perigee: 344
2290 deg
Mean anomaly: 15
8826 deg
Mean motion: 15
77440206 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1834
Checksum: 284
Coasting Arc #8 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2008/105/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3946906
09 A = 6716748
28 meter
Y = -4100792
60 meter E =
0004920
Z = -3569906
75 I = 51
55096
XDOT = 5998
298479 Wp = 80
16877
YDOT = 1919
664427 meter/sec RA = 343
77258 deg
ZDOT = 4432
596287 TA = 237
10705
MA = 237
15440
Ha = 184
679 n
mi
Hp = 178
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12949166
97 X = 4009810
32
Y = -13454043
97 feet Y = -4056304
40 meter
Z = -11712292
49 Z = -3550579
91
XDOT = 19679
456952 XDOT = 5954
854051
YDOT = 6298
111638 feet/sec YDOT = 1986
498009 meter/sec
ZDOT = 14542
638737 ZDOT = 4461
630296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1137345
10 X = -346662
79
Y = -18684768
15 feet Y = -5695117
33 meter
Z = -11638552
54 Z = -3547430
81
XDOT = 16514
070639 XDOT = 5033
488731
YDOT = -10120
856533 feet/sec YDOT = -3084
837071 meter/sec
ZDOT = 14654
210240 ZDOT = 4466
603281
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 08105
57740672
00020000 00000-0 20000-3 0 9078
2 25544 51
6407 344
2589 0001521 343
5938 16
5178 15
77496390 18495
Satellite: ISS
Catalog Number: 25544
Epoch time: 08105
57740672 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 344
2589 deg
Eccentricity:
0001521
Arg of perigee: 343
5938 deg
Mean anomaly: 16
5178 deg
Mean motion: 15
77496390 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1849
Checksum: 315
Coasting Arc #9 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2008/106/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4425651
98 A = 6712938
11 meter
Y = -2169941
64 meter E =
0010772
Z = -4567889
18 I = 51
50985
XDOT = 5361
081136 Wp = 61
46224
YDOT = -4645
913751 meter/sec RA = 338
65115 deg
ZDOT = -2987
391312 TA = 178
81374
MA = 178
81119
Ha = 184
613 n
mi
Hp = 178
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14519855
58 X = -4378868
52
Y = -7119231
11 feet Y = -2219170
42 meter
Z = -14986513
05 Z = -4589275
20
XDOT = 17588
848873 XDOT = 5427
146185
YDOT = -15242
499182 feet/sec YDOT = -4585
593806 meter/sec
ZDOT = -9801
152598 ZDOT = -2961
186605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14894450
17 X = -4539828
41
Y = 6098587
66 feet Y = 1858849
52 meter
Z = -15068769
48 Z = -4592960
94
XDOT = 712
161522 XDOT = 217
066832
YDOT = -22228
711322 feet/sec YDOT = -6775
311211 meter/sec
ZDOT = -9701
086035 ZDOT = -2956
891024
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 08106
59097408
00020000 00000-0 20000-3 0 9084
2 25544 51
6396 339
0265 0001539 345
8344 14
2778 15
77535840 18653
Satellite: ISS
Catalog Number: 25544
Epoch time: 08106
59097408 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 339
0265 deg
Eccentricity:
0001539
Arg of perigee: 345
8344 deg
Mean anomaly: 14
2778 deg
Mean motion: 15
77535840 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1865
Checksum: 319
Coasting Arc #10 (Orbit 1880)
---------------------------------------
Vector Time (GMT): 2008/107/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5225352
05 A = 6720948
57 meter
Y = 3943232
90 meter E =
0013036
Z = 1497833
13 I = 51
51131
XDOT = -4026
321490 Wp = 112
49454
YDOT = -3126
272000 meter/sec RA = 333
44262 deg
ZDOT = -5781
001001 TA = 50
94925
MA = 50
83332
Ha = 184
523 n
mi
Hp = 178
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17143543
48 X = -5276333
75
Y = 12937115
82 feet Y = 3884515
05 meter
Z = 4914150
69 Z = 1472324
31
XDOT = -13209
716176 XDOT = -3962
980693
YDOT = -10256
797901 feet/sec YDOT = -3170
942771 meter/sec
ZDOT = -18966
538716 ZDOT = -5800
406874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1312327
80 X = -399997
51
Y = 21459175
77 feet Y = 6540756
77 meter
Z = 4816689
42 Z = 1468126
94
XDOT = -14743
081193 XDOT = -4493
691147
YDOT = 3398
628723 feet/sec YDOT = 1035
902035 meter/sec
ZDOT = -19041
292971 ZDOT = -5803
786098
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 08107
60450911
00020000 00000-0 20000-3 0 9090
2 25544 51
6402 333
7939 0001708 348
3406 11
7719 15
77623716 18810
Satellite: ISS
Catalog Number: 25544
Epoch time: 08107
60450911 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 333
7939 deg
Eccentricity:
0001708
Arg of perigee: 348
3406 deg
Mean anomaly: 11
7719 deg
Mean motion: 15
77623716 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1881
Checksum: 292
Coasting Arc #11 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2008/108/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2531087
01 A = 6709879
51 meter
Y = 3342088
45 meter E =
0002392
Z = 5236986
19 I = 51
44696
XDOT = -6397
165374 Wp = 68
74480
YDOT = 4287
340829 meter/sec RA = 328
28445 deg
ZDOT = 356
484749 TA = 17
86954
MA = 17
86113
Ha = 184
507 n
mi
Hp = 178
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8304091
24 X = 2468086
65
Y = 10964857
13 feet Y = 3370040
54 meter
Z = 17181713
22 Z = 5249129
08
XDOT = -20988
075373 XDOT = -6446
363385
YDOT = 14066
078836 feet/sec YDOT = 4215
529006 meter/sec
ZDOT = 1169
569385 ZDOT = 325
287402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13680512
27 X = 4169820
14
Y = 644433
07 feet Y = 196423
20 meter
Z = 17228626
83 Z = 5251285
46
XDOT = -2457
304583 XDOT = -748
986437
YDOT = 24148
913633 feet/sec YDOT = 7360
588875 meter/sec
ZDOT = 1050
326585 ZDOT = 320
139543
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 08108
61801535
00020000 00000-0 20000-3 0 9106
2 25544 51
6389 328
5602 0001520 352
6961 7
4181 15
77602751 18977
Satellite: ISS
Catalog Number: 25544
Epoch time: 08108
61801535 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 328
5602 deg
Eccentricity:
0001520
Arg of perigee: 352
6961 deg
Mean anomaly: 7
4181 deg
Mean motion: 15
77602751 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1897
Checksum: 285
Coasting Arc #12 (Orbit 1912)
---------------------------------------
Vector Time (GMT): 2008/109/13:40:43
799
Vector Time (MET): N/A
Weight (LBS) : 628879
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5722813
96 A = 6721354
89 meter
Y = -3391508
54 meter E =
0014472
Z = 906989
57 I = 51
46112
XDOT = 1768
834533 Wp = 49
35212
YDOT = 4586
907689 meter/sec RA = 323
11298 deg
ZDOT = 5938
685955 TA = 320
59341
MA = 320
69860
Ha = 184
450 n
mi
Hp = 178
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18775636
35 X = 5755906
96
Y = -11126996
53 feet Y = -3327327
69 meter
Z = 2975687
57 Z = 934871
84
XDOT = 5803
262904 XDOT = 1688
562169
YDOT = 15048
909741 feet/sec YDOT = 4606
239252 meter/sec
ZDOT = 19483
877806 ZDOT = 5947
083855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2978143
05 X = 907738
00
Y = -21606003
40 feet Y = -6585509
84 meter
Z = 3082299
42 Z = 939484
86
XDOT = 13743
489028 XDOT = 4189
015456
YDOT = 4702
267339 feet/sec YDOT = 1433
251085 meter/sec
ZDOT = 19516
549201 ZDOT = 5948
644197
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 08109
63148754
00020000 00000-0 20000-3 0 9117
2 25544 51
6379 323
3261 0001523 352
8081 7
3061 15
77678814 19136
Satellite: ISS
Catalog Number: 25544
Epoch time: 08109
63148754 = yrday
fracday
Element set: 911
Inclination: 51
6379 deg
RA of node: 323
3261 deg
Eccentricity:
0001523
Arg of perigee: 352
8081 deg
Mean anomaly: 7
3061 deg
Mean motion: 15
77678814 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1913
Checksum: 285
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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