Date:
September 4th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12109 4 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 5)
---------------------------------------
Vector Time (GMT): 2008/242/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6706127
21 A = 6738359
14 meter
Y = 370629
75 meter E =
0019406
Z = 421612
40 I = 51
66167
XDOT = -652
570011 Wp = 52
49807
YDOT = 4757
713122 meter/sec RA =
31780 deg
ZDOT = 6020
514558 TA = 312
08329
MA = 312
24817
Ha = 195
688 n
mi
Hp = 185
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22001729
70 X = 6699436
28
Y = 1215976
88 feet Y = 445584
12 meter
Z = 1383242
78 Z = 454173
89
XDOT = -2140
977727 XDOT = -734
969044
YDOT = 15609
295020 feet/sec YDOT = 4749
955065 meter/sec
ZDOT = 19752
344350 ZDOT = 6017
144231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7719323
52 X = -2352849
81
Y = -20630137
75 feet Y = -6288065
99 meter
Z = 1509149
11 Z = 459988
65
XDOT = 13696
039836 XDOT = 4174
552942
YDOT = -3641
836853 feet/sec YDOT = -1110
031873 meter/sec
ZDOT = 19739
721198 ZDOT = 6016
667021
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 08242
44182882
00020000 00000-0 20000-3 0 9002
2 25544 51
6404
4844 0006412 59
4199 300
7595 15
71802014 66
Satellite: ISS
Catalog Number: 25544
Epoch time: 08242
44182882 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node:
4844 deg
Eccentricity:
0006412
Arg of perigee: 59
4199 deg
Mean anomaly: 300
7595 deg
Mean motion: 15
71802014 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 6
Checksum: 260
Coasting Arc #2 (Orbit 20)
---------------------------------------
Vector Time (GMT): 2008/243/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -698207
03 A = 6726328
96 meter
Y = -4137910
44 meter E =
0021130
Z = -5274814
63 I = 51
59284
XDOT = 7624
149279 Wp = 80
01716
YDOT = -887
540544 meter/sec RA = 355
19720 deg
ZDOT = -310
396885 TA = 187
01233
MA = 187
04194
Ha = 195
721 n
mi
Hp = 184
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2290705
48 X = -626260
67
Y = -13575821
66 feet Y = -4145316
12 meter
Z = -17305822
29 Z = -5278031
56
XDOT = 25013
613120 XDOT = 7635
015086
YDOT = -2911
878424 feet/sec YDOT = -802
222171 meter/sec
ZDOT = -1018
362484 ZDOT = -273
332932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11422680
97 X = -3481633
16
Y = 7657002
74 feet Y = 2333854
44 meter
Z = -17318614
81 Z = -5278713
79
XDOT = -12528
547925 XDOT = -3818
701407
YDOT = -20688
288822 feet/sec YDOT = -6305
790433 meter/sec
ZDOT = -875
162369 ZDOT = -266
749490
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 08243
39550282
00020000 00000-0 20000-3 0 9011
2 25544 51
6411 355
6036 0006559 63
1947 296
9885 15
71829062 214
Satellite: ISS
Catalog Number: 25544
Epoch time: 08243
39550282 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 355
6036 deg
Eccentricity:
0006559
Arg of perigee: 63
1947 deg
Mean anomaly: 296
9885 deg
Mean motion: 15
71829062 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 21
Checksum: 297
Coasting Arc #3 (Orbit 36)
---------------------------------------
Vector Time (GMT): 2008/244/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6393600
55 A = 6737917
15 meter
Y = 1883659
01 meter E =
0017744
Z = 948948
54 I = 51
60244
XDOT = -2186
803561 Wp = 106
39306
YDOT = -4390
241951 meter/sec RA = 350
06277 deg
ZDOT = -5932
654230 TA = 63
24606
MA = 63
06461
Ha = 195
660 n
mi
Hp = 184
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20976379
77 X = -6418798
52
Y = 6179983
63 feet Y = 1812021
25 meter
Z = 3113348
22 Z = 917827
47
XDOT = -7174
552367 XDOT = -2108
729198
YDOT = -14403
680941 feet/sec YDOT = -4414
259833 meter/sec
ZDOT = -19464
088682 ZDOT = -5943
087726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14658787
08 X = 4467998
30
Y = 16249746
98 feet Y = 4952922
88 meter
Z = 2993213
56 Z = 912331
49
XDOT = -8741
869311 XDOT = -2664
521766
YDOT = 11533
125662 feet/sec YDOT = 3515
296702 meter/sec
ZDOT = -19504
801431 ZDOT = -5945
063476
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 08244
41273816
00020000 00000-0 20000-3 0 9021
2 25544 51
6405 350
3953 0006467 65
1321 295
0513 15
71860102 378
Satellite: ISS
Catalog Number: 25544
Epoch time: 08244
41273816 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 350
3953 deg
Eccentricity:
0006467
Arg of perigee: 65
1321 deg
Mean anomaly: 295
0513 deg
Mean motion: 15
71860102 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 37
Checksum: 261
Coasting Arc #4 (Orbit 52)
---------------------------------------
Vector Time (GMT): 2008/245/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3044719
02 A = 6727230
62 meter
Y = 3296805
53 meter E =
0010548
Z = 5002809
79 I = 51
53913
XDOT = -6689
645960 Wp = 94
24807
YDOT = 3334
793523 meter/sec RA = 344
96324 deg
ZDOT = 1869
589575 TA = 337
67709
MA = 337
72296
Ha = 195
555 n
mi
Hp = 184
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9989235
64 X = 2983324
71
Y = 10816291
12 feet Y = 3330510
37 meter
Z = 16413417
95 Z = 5017451
62
XDOT = -21947
657350 XDOT = -6735
521045
YDOT = 10940
923633 feet/sec YDOT = 3259
729660 meter/sec
ZDOT = 6133
824065 ZDOT = 1836
979827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5232210
64 X = 1594777
80
Y = -13694174
12 feet Y = -4173984
27 meter
Z = 16470301
70 Z = 5020147
96
XDOT = 18636
407117 XDOT = 5680
376889
YDOT = 14362
852435 feet/sec YDOT = 4377
797422 meter/sec
ZDOT = 6008
068839 ZDOT = 1831
259382
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 08245
42995876
00020000 00000-0 20000-3 0 9031
2 25544 51
6414 345
1884 0006431 69
2791 290
9060 15
71887941 539
Satellite: ISS
Catalog Number: 25544
Epoch time: 08245
42995876 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 345
1884 deg
Eccentricity:
0006431
Arg of perigee: 69
2791 deg
Mean anomaly: 290
9060 deg
Mean motion: 15
71887941 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 53
Checksum: 312
Coasting Arc #5 (Orbit 67)
---------------------------------------
Vector Time (GMT): 2008/246/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5074828
42 A = 6735986
96 meter
Y = -3796227
48 meter E =
0012140
Z = -2279713
23 I = 51
54151
XDOT = 4603
750039 Wp = 58
62251
YDOT = 2906
570986 meter/sec RA = 339
80252 deg
ZDOT = 5435
690919 TA = 275
76685
MA = 275
90525
Ha = 195
728 n
mi
Hp = 184
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16649699
53 X = 5127975
70
Y = -12454814
57 feet Y = -3739180
80 meter
Z = -7479374
12 Z = -2254930
42
XDOT = 15104
166796 XDOT = 4544
500548
YDOT = 9535
994049 feet/sec YDOT = 2957
721811 meter/sec
ZDOT = 17833
631624 ZDOT = 5457
911831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18774382
55 X = -5722431
80
Y = -9015334
37 feet Y = -2747873
92 meter
Z = -7383917
91 Z = -2250618
18
XDOT = 836
457958 XDOT = 254
952386
YDOT = -16344
209515 feet/sec YDOT = -4981
715060 meter/sec
ZDOT = 17919
773118 ZDOT = 5461
946846
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 08246
38358920
00020000 00000-0 20000-3 0 9041
2 25544 51
6423 340
3073 0006569 73
1959 286
9924 15
71889052 683
Satellite: ISS
Catalog Number: 25544
Epoch time: 08246
38358920 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 340
3073 deg
Eccentricity:
0006569
Arg of perigee: 73
1959 deg
Mean anomaly: 286
9924 deg
Mean motion: 15
71889052 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 68
Checksum: 316
Coasting Arc #6 (Orbit 83)
---------------------------------------
Vector Time (GMT): 2008/247/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4801512
76 A = 6729510
76 meter
Y = -1637021
08 meter E =
0016117
Z = -4437726
09 I = 51
49299
XDOT = 4739
733138 Wp = 71
72897
YDOT = -5099
853044 meter/sec RA = 334
71814 deg
ZDOT = -3251
704226 TA = 165
55829
MA = 165
51217
Ha = 195
655 n
mi
Hp = 184
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15752994
63 X = -4761292
73
Y = -5370804
06 feet Y = -1690489
69 meter
Z = -14559468
81 Z = -4460954
13
XDOT = 15550
305570 XDOT = 4812
204484
YDOT = -16731
801326 feet/sec YDOT = -5046
445565 meter/sec
ZDOT = -10668
320952 ZDOT = -3228
502258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2787391
97 X = 849597
07
Y = 16328085
51 feet Y = 4976800
46 meter
Z = -14649388
30 Z = -4465133
55
XDOT = -20973
240148 XDOT = -6392
643597
YDOT = -5897
332823 feet/sec YDOT = -1797
507044 meter/sec
ZDOT = -10579
092112 ZDOT = -3224
507276
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 08247
40077870
00020000 00000-0 20000-3 0 9058
2 25544 51
6422 335
1002 0006525 76
2139 283
9749 15
71910197 847
Satellite: ISS
Catalog Number: 25544
Epoch time: 08247
40077870 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 335
1002 deg
Eccentricity:
0006525
Arg of perigee: 76
2139 deg
Mean anomaly: 283
9749 deg
Mean motion: 15
71910197 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 84
Checksum: 287
Coasting Arc #7 (Orbit 99)
---------------------------------------
Vector Time (GMT): 2008/248/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3089070
65 A = 6733216
33 meter
Y = 4931245
76 meter E =
0019120
Z = 3372448
39 I = 51
47936
XDOT = -6127
722385 Wp = 86
62924
YDOT = -662
738757 meter/sec RA = 329
53847 deg
ZDOT = -4620
172523 TA = 53
51095
MA = 53
33495
Ha = 195
720 n
mi
Hp = 184
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10134746
22 X = -3160365
87
Y = 16178627
83 feet Y = 4896303
47 meter
Z = 11064463
23 Z = 3357268
28
XDOT = -20104
076065 XDOT = -6097
412030
YDOT = -2174
339754 feet/sec YDOT = -731
093156 meter/sec
ZDOT = -15158
046336 ZDOT = -4649
867499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19104330
18 X = 5822999
84
Y = 878075
55 feet Y = 267637
43 meter
Z = 11006224
50 Z = 3354697
23
XDOT = 8058
361763 XDOT = 2456
188665
YDOT = 17086
555609 feet/sec YDOT = 5207
982150 meter/sec
ZDOT = -15272
872314 ZDOT = -4655
171481
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 08248
41795300
00020000 00000-0 20000-3 0 9066
2 25544 51
6422 329
8924 0006590 80
3983 279
7924 15
71922005 1003
Satellite: ISS
Catalog Number: 25544
Epoch time: 08248
41795300 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 329
8924 deg
Eccentricity:
0006590
Arg of perigee: 80
3983 deg
Mean anomaly: 279
7924 deg
Mean motion: 15
71922005 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 100
Checksum: 291
Coasting Arc #8 (Orbit 115)
---------------------------------------
Vector Time (GMT): 2008/249/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5672229
75 A = 6732260
41 meter
Y = -559665
91 meter E =
0018503
Z = 3566783
05 I = 51
45339
XDOT = -2210
067677 Wp = 89
94620
YDOT = 5909
057799 meter/sec RA = 324
45780 deg
ZDOT = 4422
143603 TA = 312
76202
MA = 312
91754
Ha = 195
463 n
mi
Hp = 184
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18609677
67 X = 5660739
57
Y = -1836174
26 feet Y = -496299
96 meter
Z = 11702044
14 Z = 3594310
99
XDOT = -7250
878205 XDOT = -2297
461544
YDOT = 19386
672569 feet/sec YDOT = 5883
854970 meter/sec
ZDOT = 14508
345153 ZDOT = 4411
194667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11013658
17 X = -3356963
01
Y = -15029663
95 feet Y = -4581041
57 meter
Z = 11808387
32 Z = 3599196
46
XDOT = 19325
523242 XDOT = 5890
419484
YDOT = -2745
346087 feet/sec YDOT = -836
781487 meter/sec
ZDOT = 14466
544273 ZDOT = 4409
402694
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 08249
43510901
00020000 00000-0 20000-3 0 9072
2 25544 51
6430 324
6850 0006536 83
6897 276
5010 15
71997626 1162
Satellite: ISS
Catalog Number: 25544
Epoch time: 08249
43510901 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 324
6850 deg
Eccentricity:
0006536
Arg of perigee: 83
6897 deg
Mean anomaly: 276
5010 deg
Mean motion: 15
71997626 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 116
Checksum: 296
Coasting Arc #9 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2008/250/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 752510
52 A = 6730013
56 meter
Y = -5151511
55 meter E =
0014727
Z = -4278845
05 I = 51
42234
XDOT = 6554
326742 Wp = 99
51982
YDOT = -1950
110402 meter/sec RA = 319
27375 deg
ZDOT = 3508
400227 TA = 206
16899
MA = 206
24349
Ha = 195
581 n
mi
Hp = 184
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2468866
52 X = 830845
57
Y = -16901284
60 feet Y = -5142658
54 meter
Z = -14038205
53 Z = -4274999
06
XDOT = 21503
696659 XDOT = 6558
602805
YDOT = -6398
000005 feet/sec YDOT = -1876
792237 meter/sec
ZDOT = 11510
499434 ZDOT = 3540
251674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15735234
19 X = -4796099
38
Y = 6675001
43 feet Y = 2034540
44 meter
Z = -14023790
45 Z = -4274451
33
XDOT = -16186
163802 XDOT = -4933
542727
YDOT = -13769
411849 feet/sec YDOT = -4196
916732 meter/sec
ZDOT = 11633
432194 ZDOT = 3545
870133
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 08250
38868143
00020000 00000-0 20000-3 0 9083
2 25544 51
6429 319
8037 0006541 85
8884 274
3025 15
71983768 1310
Satellite: ISS
Catalog Number: 25544
Epoch time: 08250
38868143 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 319
8037 deg
Eccentricity:
0006541
Arg of perigee: 85
8884 deg
Mean anomaly: 274
3025 deg
Mean motion: 15
71983768 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 131
Checksum: 315
Coasting Arc #10 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2008/251/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5566825
87 A = 6734945
94 meter
Y = 2809012
85 meter E =
0011088
Z = -2549880
70 I = 51
41833
XDOT = -420
764985 Wp = 105
97545
YDOT = -5592
049248 meter/sec RA = 314
18409 deg
ZDOT = -5263
700054 TA = 102
98478
MA = 102
86094
Ha = 195
535 n
mi
Hp = 184
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18263864
41 X = -5585436
07
Y = 9215921
44 feet Y = 2746657
37 meter
Z = -8365750
34 Z = -2576969
58
XDOT = -1380
462548 XDOT = -332
632351
YDOT = -18346
618268 feet/sec YDOT = -5596
261648 meter/sec
ZDOT = -17269
357134 ZDOT = -5265
530126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17568917
02 X = 5355005
91
Y = 10395987
00 feet Y = 3168696
84 meter
Z = -8470203
02 Z = -2581717
88
XDOT = -14017
243486 XDOT = -4272
455814
YDOT = 9670
221021 feet/sec YDOT = 2947
483367 meter/sec
ZDOT = -17276
919323 ZDOT = -5266
005010
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 08251
40580879
00020000 00000-0 20000-3 0 9095
2 25544 51
6432 314
5955 0006619 89
7503 270
4417 15
72012250 1471
Satellite: ISS
Catalog Number: 25544
Epoch time: 08251
40580879 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 314
5955 deg
Eccentricity:
0006619
Arg of perigee: 89
7503 deg
Mean anomaly: 270
4417 deg
Mean motion: 15
72012250 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 147
Checksum: 288
Coasting Arc #11 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2008/252/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1437111
56 A = 6727402
77 meter
Y = 4405283
25 meter E =
0012735
Z = 4867698
96 I = 51
37388
XDOT = -5895
762270 Wp = 74
66247
YDOT = 4420
450656 meter/sec RA = 309
00653 deg
ZDOT = -2251
680554 TA = 37
34788
MA = 37
25941
Ha = 195
495 n
mi
Hp = 184
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4714932
93 X = 1364097
76
Y = 14453029
02 feet Y = 4420945
54 meter
Z = 15970140
96 Z = 4874503
17
XDOT = -19343
052068 XDOT = -5933
816018
YDOT = 14502
790866 feet/sec YDOT = 4354
308113 meter/sec
ZDOT = -7387
403392 ZDOT = -2280
414523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9493072
53 X = 2893488
51
Y = -11838459
39 feet Y = -3608362
42 meter
Z = 15996827
68 Z = 4875833
08
XDOT = 21887
995548 XDOT = 6671
461043
YDOT = 7383
455027 feet/sec YDOT = 2250
477092 meter/sec
ZDOT = -7498
074512 ZDOT = -2285
413111
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 08252
42292028
00020000 00000-0 20000-3 0 9106
2 25544 51
6434 309
3879 0006679 91
9707 268
2220 15
72045282 1633
Satellite: ISS
Catalog Number: 25544
Epoch time: 08252
42292028 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 309
3879 deg
Eccentricity:
0006679
Arg of perigee: 91
9707 deg
Mean anomaly: 268
2220 deg
Mean motion: 15
72045282 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 163
Checksum: 291
Coasting Arc #12 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2008/253/09:05:56
834
Vector Time (MET): N/A
Weight (LBS) : 661688
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4526251
02 A = 6736886
12 meter
Y = -4790968
75 meter E =
0019847
Z = 1358368
64 I = 51
38866
XDOT = 2735
180622 Wp = 71
27458
YDOT = 4249
281020 meter/sec RA = 303
89906 deg
ZDOT = 5810
340494 TA = 303
69611
MA = 303
88518
Ha = 195
500 n
mi
Hp = 184
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14849904
91 X = 4572889
31
Y = -15718401
42 feet Y = -4740092
86 meter
Z = 4456590
01 Z = 1380470
31
XDOT = 8973
689706 XDOT = 2659
235698
YDOT = 13941
210697 feet/sec YDOT = 4279
442678 meter/sec
ZDOT = 19062
796896 ZDOT = 5823
443548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21351635
19 X = -6507978
41
Y = -3306149
14 feet Y = -1007714
26 meter
Z = 4541592
91 Z = 1384277
52
XDOT = 6221
859018 XDOT = 1896
422629
YDOT = -13647
185901 feet/sec YDOT = -4159
662263 meter/sec
ZDOT = 19113
821269 ZDOT = 5825
892723
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 08253
44001602
00020000 00000-0 20000-3 0 9116
2 25544 51
6435 304
1804 0006685 95
5707 264
6217 15
72059177 1793
Satellite: ISS
Catalog Number: 25544
Epoch time: 08253
44001602 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 304
1804 deg
Eccentricity:
0006685
Arg of perigee: 95
5707 deg
Mean anomaly: 264
6217 deg
Mean motion: 15
72059177 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 179
Checksum: 281
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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