Date:
July 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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
205/16:18:03
319 -11
1 11
8 11
8
N/A 1
6 -0
0 191
9
000/00:22:06
638 -3
9 -0
1 186
9
Coasting Arc #1 (Orbit 3282)
---------------------------------------
Vector Time (GMT): 2008/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3883700
47 A = 6729263
43 meter
Y = -5480264
35 meter E =
0020912
Z = -51721
38 I = 51
39117
XDOT = 3903
410805 Wp = 29
48542
YDOT = -2813
213386 meter/sec RA = 235
02824 deg
ZDOT = 6024
789706 TA = 329
94999
MA = 330
06982
Ha = 190
957 n
mi
Hp = 180
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12741799
43 X = -3821879
38
Y = -17979869
93 feet Y = -5523348
45 meter
Z = -169689
58 Z = -70439
15
XDOT = 12806
465897 XDOT = 3905
311309
YDOT = -9229
702710 feet/sec YDOT = -2769
553690 meter/sec
ZDOT = 19766
370427 ZDOT = 6043
756481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11906529
15 X = -3629110
09
Y = 18542756
15 feet Y = 5651832
07 meter
Z = -242338
53 Z = -73864
78
XDOT = -11956
541023 XDOT = -3644
353704
YDOT = -7449
583442 feet/sec YDOT = -2270
633033 meter/sec
ZDOT = 19839
222024 ZDOT = 6046
994873
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 08196
50014429
00020000 00000-0 20000-3 0 9008
2 25544 51
6394 235
9268 0009767 9
9943 350
1413 15
75025317 32837
Satellite: ISS
Catalog Number: 25544
Epoch time: 08196
50014429 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 235
9268 deg
Eccentricity:
0009767
Arg of perigee: 9
9943 deg
Mean anomaly: 350
1413 deg
Mean motion: 15
75025317 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3283
Checksum: 297
Coasting Arc #2 (Orbit 3298)
---------------------------------------
Vector Time (GMT): 2008/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3475315
91 A = 6717111
95 meter
Y = 2381981
06 meter E =
0019290
Z = -5245850
64 I = 51
36893
XDOT = -4715
222583 Wp = 63
71756
YDOT = -6063
431569 meter/sec RA = 229
86341 deg
ZDOT = 380
048590 TA = 209
85434
MA = 209
96451
Ha = 190
961 n
mi
Hp = 180
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11401955
08 X = -3476210
14
Y = 7814898
50 feet Y = 2343114
08 meter
Z = -17210796
06 Z = -5262735
30
XDOT = -15469
890365 XDOT = -4648
916074
YDOT = -19893
148192 feet/sec YDOT = -6115
789225 meter/sec
ZDOT = 1246
878577 ZDOT = 357
302142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11604928
35 X = 3537182
16
Y = 7359732
86 feet Y = 2243246
57 meter
Z = -17275667
55 Z = -5265623
47
XDOT = -11743
544013 XDOT = -3579
432215
YDOT = 21164
280467 feet/sec YDOT = 6450
872686 meter/sec
ZDOT = 1158
633974 ZDOT = 353
151635
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 08197
51528476
00020000 00000-0 20000-3 0 9013
2 25544 51
6399 230
7050 0009603 13
7426 346
3997 15
75064603 32994
Satellite: ISS
Catalog Number: 25544
Epoch time: 08197
51528476 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 230
7050 deg
Eccentricity:
0009603
Arg of perigee: 13
7426 deg
Mean anomaly: 346
3997 deg
Mean motion: 15
75064603 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3299
Checksum: 309
Coasting Arc #3 (Orbit 3314)
---------------------------------------
Vector Time (GMT): 2008/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4326247
33 A = 6728813
01 meter
Y = 5103605
31 meter E =
0009890
Z = -731240
81 I = 51
42787
XDOT = -4097
828585 Wp = 84
37936
YDOT = 2629
703362 meter/sec RA = 224
71221 deg
ZDOT = -5958
430116 TA = 103
60873
MA = 103
49856
Ha = 191
072 n
mi
Hp = 180
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14193724
85 X = 4272408
66
Y = 16744111
93 feet Y = 5151683
00 meter
Z = -2399084
04 Z = -710353
98
XDOT = -13444
319504 XDOT = -4097
985185
YDOT = 8627
635703 feet/sec YDOT = 2583
879338 meter/sec
ZDOT = -19548
655235 ZDOT = -5978
337003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9537024
61 X = 2906885
10
Y = -19780150
89 feet Y = -6028989
99 meter
Z = -2318082
38 Z = -706551
51
XDOT = 11853
663207 XDOT = 3612
996545
YDOT = 7988
079945 feet/sec YDOT = 2434
766767 meter/sec
ZDOT = -19625
161712 ZDOT = -5981
749290
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 08198
53041407
00020000 00000-0 20000-3 0 9021
2 25544 51
6391 225
4830 0009682 18
3100 341
8410 15
75104151 33152
Satellite: ISS
Catalog Number: 25544
Epoch time: 08198
53041407 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 225
4830 deg
Eccentricity:
0009682
Arg of perigee: 18
3100 deg
Mean anomaly: 341
8410 deg
Mean motion: 15
75104151 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3315
Checksum: 255
Coasting Arc #4 (Orbit 3330)
---------------------------------------
Vector Time (GMT): 2008/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3704009
30 A = 6717396
35 meter
Y = -2249424
38 meter E =
0013397
Z = 5128615
40 I = 51
41028
XDOT = 5164
355374 Wp = 32
06866
YDOT = 5577
366554 meter/sec RA = 219
53465 deg
ZDOT = -1270
862949 TA = 70
18299
MA = 70
03861
Ha = 191
045 n
mi
Hp = 180
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12152261
49 X = 3703973
97
Y = -7380001
24 feet Y = -2208005
14 meter
Z = 16826166
00 Z = 5146608
69
XDOT = 16943
423144 XDOT = 5107
778070
YDOT = 18298
446700 feet/sec YDOT = 5634
801226 meter/sec
ZDOT = -4169
497865 ZDOT = -1245
911347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11774027
17 X = -3588723
48
Y = -7821869
56 feet Y = -2384105
84 meter
Z = 16895336
07 Z = 5149698
43
XDOT = 8871
202871 XDOT = 2703
942635
YDOT = -22240
484365 feet/sec YDOT = -6778
899634 meter/sec
ZDOT = -4072
762907 ZDOT = -1241
378134
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 08199
54553241
00020000 00000-0 20000-3 0 9038
2 25544 51
6379 220
2610 0009751 22
2645 337
8941 15
75128912 33315
Satellite: ISS
Catalog Number: 25544
Epoch time: 08199
54553241 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 220
2610 deg
Eccentricity:
0009751
Arg of perigee: 22
2645 deg
Mean anomaly: 337
8941 deg
Mean motion: 15
75128912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3331
Checksum: 285
Coasting Arc #5 (Orbit 3346)
---------------------------------------
Vector Time (GMT): 2008/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4654719
86 A = 6728065
53 meter
Y = -4609834
39 meter E =
0022771
Z = 1473961
22 I = 51
46968
XDOT = 4396
944253 Wp = 46
94098
YDOT = -2575
846565 meter/sec RA = 214
40140 deg
ZDOT = 5788
705366 TA = 329
35500
MA = 329
48781
Ha = 191
243 n
mi
Hp = 179
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15271390
60 X = -4609986
10
Y = -15124128
57 feet Y = -4661636
26 meter
Z = 4835830
76 Z = 1451456
93
XDOT = 14425
670122 XDOT = 4397
301058
YDOT = -8450
940173 feet/sec YDOT = -2526
676359 meter/sec
ZDOT = 18991
815504 ZDOT = 5810
065755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6916837
40 X = -2108252
04
Y = 20370272
09 feet Y = 6208858
93 meter
Z = 4748607
22 Z = 1447375
48
XDOT = -12372
812326 XDOT = -3771
233197
YDOT = -8679
370257 feet/sec YDOT = -2645
472054 meter/sec
ZDOT = 19073
944561 ZDOT = 5813
738302
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 08200
56064058
00020000 00000-0 20000-3 0 9047
2 25544 51
6380 215
0394 0009829 25
7471 334
4181 15
75130446 33470
Satellite: ISS
Catalog Number: 25544
Epoch time: 08200
56064058 = yrday
fracday
Element set: 904
Inclination: 51
6380 deg
RA of node: 215
0394 deg
Eccentricity:
0009829
Arg of perigee: 25
7471 deg
Mean anomaly: 334
4181 deg
Mean motion: 15
75130446 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3347
Checksum: 279
Coasting Arc #6 (Orbit 3361)
---------------------------------------
Vector Time (GMT): 2008/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3984327
28 A = 6718336
99 meter
Y = 2266278
78 meter E =
0017790
Z = -4924737
29 I = 51
46207
XDOT = -5453
168605 Wp = 73
42003
YDOT = -4990
228971 meter/sec RA = 209
21355 deg
ZDOT = 2126
757308 TA = 217
21925
MA = 217
34269
Ha = 191
267 n
mi
Hp = 179
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13071939
91 X = -3985450
07
Y = 7435297
84 feet Y = 2221718
16 meter
Z = -16157274
58 Z = -4944095
16
XDOT = -17890
973113 XDOT = -5407
292968
YDOT = -16372
142293 feet/sec YDOT = -5050
953226 meter/sec
ZDOT = 6977
550222 ZDOT = 2100
377093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12503266
70 X = 3810995
69
Y = 8210756
56 feet Y = 2502638
60 meter
Z = -16231715
48 Z = -4947426
88
XDOT = -5888
865878 XDOT = -1794
926320
YDOT = 22486
133301 feet/sec YDOT = 6853
773430 meter/sec
ZDOT = 6875
325639 ZDOT = 2095
599255
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 08201
51229356
00020000 00000-0 20000-3 0 9058
2 25544 51
6381 210
1436 0009794 28
7657 331
4045 15
75126988 33623
Satellite: ISS
Catalog Number: 25544
Epoch time: 08201
51229356 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 210
1436 deg
Eccentricity:
0009794
Arg of perigee: 28
7657 deg
Mean anomaly: 331
4045 deg
Mean motion: 15
75126988 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3362
Checksum: 293
Coasting Arc #7 (Orbit 3377)
---------------------------------------
Vector Time (GMT): 2008/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4825485
20 A = 6726732
15 meter
Y = 4118567
44 meter E =
0010217
Z = -2251270
07 I = 51
51568
XDOT = -4762
964191 Wp = 68
66089
YDOT = 2612
541266 meter/sec RA = 204
09474 deg
ZDOT = -5445
834006 TA = 136
63104
MA = 136
55060
Ha = 191
362 n
mi
Hp = 179
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15831644
37 X = 4790008
13
Y = 13512360
36 feet Y = 4172330
68 meter
Z = -7386056
66 Z = -2227914
04
XDOT = -15626
522936 XDOT = -4765
369715
YDOT = 8571
329614 feet/sec YDOT = 2559
266244 meter/sec
ZDOT = -17866
909468 ZDOT = -5468
977559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4518593
57 X = 1377267
32
Y = -20350324
57 feet Y = -6202778
93 meter
Z = -7295565
85 Z = -2223688
47
XDOT = 13353
052897 XDOT = 4070
010523
YDOT = 9382
861969 feet/sec YDOT = 2859
896328 meter/sec
ZDOT = -17955
922345 ZDOT = -5472
965131
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 08202
52737994
00020000 00000-0 20000-3 0 9063
2 25544 51
6370 204
9205 0009823 33
2033 326
9745 15
75156385 33785
Satellite: ISS
Catalog Number: 25544
Epoch time: 08202
52737994 = yrday
fracday
Element set: 906
Inclination: 51
6370 deg
RA of node: 204
9205 deg
Eccentricity:
0009823
Arg of perigee: 33
2033 deg
Mean anomaly: 326
9745 deg
Mean motion: 15
75156385 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3378
Checksum: 300
Coasting Arc #8 (Orbit 3393)
---------------------------------------
Vector Time (GMT): 2008/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4335647
85 A = 6719614
47 meter
Y = -2346862
15 meter E =
0017683
Z = 4559973
78 I = 51
51936
XDOT = 5559
618827 Wp = 49
61421
YDOT = 4418
260787 meter/sec RA = 198
89877 deg
ZDOT = -2993
313088 TA = 70
22822
MA = 70
03761
Ha = 191
278 n
mi
Hp = 179
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14224566
44 X = 4339417
47
Y = -7699678
98 feet Y = -2298357
79 meter
Z = 14960543
91 Z = 4581044
92
XDOT = 18240
219250 XDOT = 5524
340643
YDOT = 14495
606255 feet/sec YDOT = 4480
234661 meter/sec
ZDOT = -9820
580997 ZDOT = -2966
390225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13569677
68 X = -4136037
76
Y = -8663460
65 feet Y = -2640622
81 meter
Z = 15041592
93 Z = 4584677
52
XDOT = 3227
423542 XDOT = 983
718696
YDOT = -22031
615302 feet/sec YDOT = -6715
236344 meter/sec
ZDOT = -9716
289566 ZDOT = -2961
525060
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 08203
54245405
00020000 00000-0 20000-3 0 9078
2 25544 51
6368 199
6978 0009861 36
1170 324
0658 15
75195208 33942
Satellite: ISS
Catalog Number: 25544
Epoch time: 08203
54245405 = yrday
fracday
Element set: 907
Inclination: 51
6368 deg
RA of node: 199
6978 deg
Eccentricity:
0009861
Arg of perigee: 36
1170 deg
Mean anomaly: 324
0658 deg
Mean motion: 15
75195208 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3394
Checksum: 312
Coasting Arc #9 (Orbit 3409)
---------------------------------------
Vector Time (GMT): 2008/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4840201
64 A = 6724971
28 meter
Y = -3597197
72 meter E =
0021597
Z = 2947879
38 I = 51
56570
XDOT = 5152
376010 Wp = 64
83310
YDOT = -2820
043881 meter/sec RA = 193
79461 deg
ZDOT = 4999
271042 TA = 329
26720
MA = 329
39350
Ha = 191
392 n
mi
Hp = 179
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15879926
63 X = -4813937
53
Y = -11801829
79 feet Y = -3651177
01 meter
Z = 9671520
26 Z = 2924429
53
XDOT = 16904
120768 XDOT = 5159
242038
YDOT = -9252
112470 feet/sec YDOT = -2762
389040 meter/sec
ZDOT = 16401
807880 ZDOT = 5024
317404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2301899
48 X = -701618
96
Y = 19695305
18 feet Y = 6003129
02 meter
Z = 9580697
94 Z = 2920196
73
XDOT = -14956
760035 XDOT = -4558
820459
YDOT = -9804
705138 feet/sec YDOT = -2988
474126 meter/sec
ZDOT = 16498
148571 ZDOT = 5028
635685
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 08204
55751675
00020000 00000-0 20000-3 0 9082
2 25544 51
6369 194
4762 0009758 39
8766 320
3113 15
75228925 34100
Satellite: ISS
Catalog Number: 25544
Epoch time: 08204
55751675 = yrday
fracday
Element set: 908
Inclination: 51
6369 deg
RA of node: 194
4762 deg
Eccentricity:
0009758
Arg of perigee: 39
8766 deg
Mean anomaly: 320
3113 deg
Mean motion: 15
75228925 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3410
Checksum: 314
Coasting Arc #10 (Orbit 3424)
---------------------------------------
Vector Time (GMT): 2008/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4641177
24 A = 6721316
09 meter
Y = 2600556
65 meter E =
0014946
Z = -4116772
81 I = 51
58213
XDOT = -5489
817210 Wp = 72
50936
YDOT = -3853
932303 meter/sec RA = 188
59547 deg
ZDOT = 3770
217741 TA = 236
12987
MA = 236
27216
Ha = 191
479 n
mi
Hp = 178
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15226959
45 X = -4649913
78
Y = 8532010
01 feet Y = 2548607
78 meter
Z = -13506472
48 Z = -4139340
49
XDOT = -18011
211318 XDOT = -5464
628783
YDOT = -12644
134854 feet/sec YDOT = -3915
182019 meter/sec
ZDOT = 12369
480779 ZDOT = 3743
609360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15092446
28 X = 4600177
62
Y = 8632563
87 feet Y = 2631205
47 meter
Z = -13593277
53 Z = -4143230
99
XDOT = -955
845405 XDOT = -291
341679
YDOT = 20906
328449 feet/sec YDOT = 6372
248911 meter/sec
ZDOT = 12266
439959 ZDOT = 3738
810900
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 08205
50912919
00020000 00000-0 20000-3 0 9099
2 25544 51
6368 189
5800 0009963 43
2219 316
9725 15
75192152 34255
Satellite: ISS
Catalog Number: 25544
Epoch time: 08205
50912919 = yrday
fracday
Element set: 909
Inclination: 51
6368 deg
RA of node: 189
5800 deg
Eccentricity:
0009963
Arg of perigee: 43
2219 deg
Mean anomaly: 316
9725 deg
Mean motion: 15
75192152 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3425
Checksum: 306
Coasting Arc #11 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2008/205/16:29:06
638
Vector Time (MET): N/A
Weight (LBS) : 660953
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2715883
36 A = 6725621
05 meter
Y = 3622681
90 meter E =
0010008
Z = -4982063
17 I = 51
57893
XDOT = -6990
750377 Wp = 92
61513
YDOT = -2522
449811 meter/sec RA = 187
64318 deg
ZDOT = 1979
662246 TA = 196
54857
MA = 196
58125
Ha = 191
859 n
mi
Hp = 186
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8910378
49 X = -2731989
15
Y = 11885439
30 feet Y = 3592221
63 meter
Z = -16345351
62 Z = -4995295
70
XDOT = -22935
532732 XDOT = -6971
641138
YDOT = -8275
753972 feet/sec YDOT = -2600
517689 meter/sec
ZDOT = 6494
954874 ZDOT = 1945
747689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7007464
24 X = 2135875
10
Y = -13034352
72 feet Y = -3972870
71 meter
Z = -16396039
95 Z = -4997512
98
XDOT = 22976
310402 XDOT = 7003
179411
YDOT = 4359
449718 feet/sec YDOT = 1328
760274 meter/sec
ZDOT = 6363
858806 ZDOT = 1939
704164
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 08205
69946698
00020000 00000-0 20000-3 0 9102
2 25544 51
6396 188
6013 0003919 317
2749 42
8109 15
72500751 34288
Satellite: ISS
Catalog Number: 25544
Epoch time: 08205
69946698 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 188
6013 deg
Eccentricity:
0003919
Arg of perigee: 317
2749 deg
Mean anomaly: 42
8109 deg
Mean motion: 15
72500751 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3428
Checksum: 312
Coasting Arc #12 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2008/206/16:29:06
638
Vector Time (MET): N/A
Weight (LBS) : 660953
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6478409
14 A = 6735769
11 meter
Y = 1308148
76 meter E =
0005223
Z = -1287852
58 I = 51
64255
XDOT = -2077
807787 Wp = 144
93102
YDOT = 4543
869497 meter/sec RA = 182
54507 deg
ZDOT = -5852
615176 TA = 49
18628
MA = 49
14099
Ha = 191
958 n
mi
Hp = 186
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21254623
15 X = 6469555
85
Y = 4291826
65 feet Y = 1380544
66 meter
Z = -4225238
13 Z = -1256401
98
XDOT = -6816
954682 XDOT = -2100
032783
YDOT = 14907
708323 feet/sec YDOT = 4520
510451 meter/sec
ZDOT = -19201
493360 ZDOT = -5862
762760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21692178
04 X = -6611775
87
Y = -799981
34 feet Y = -243834
31 meter
Z = -4103761
75 Z = -1250826
58
XDOT = 4153
894235 XDOT = 1266
106963
YDOT = -14213
122325 feet/sec YDOT = -4332
159685 meter/sec
ZDOT = -19240
190934 ZDOT = -5864
410197
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 08206
71626427
00020000 00000-0 20000-3 0 9112
2 25544 51
6400 183
3911 0003883 320
0296 40
0580 15
72499758 34447
Satellite: ISS
Catalog Number: 25544
Epoch time: 08206
71626427 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 183
3911 deg
Eccentricity:
0003883
Arg of perigee: 320
0296 deg
Mean anomaly: 40
0580 deg
Mean motion: 15
72499758 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3444
Checksum: 281
Coasting Arc #13 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2008/207/16:29:06
638
Vector Time (MET): N/A
Weight (LBS) : 660953
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 865730
21 A = 6724444
69 meter
Y = -4165826
21 meter E =
0005045
Z = 5207382
38 I = 51
63405
XDOT = 7630
443184 Wp = 6
13250
YDOT = 400
826486 meter/sec RA = 177
40099 deg
ZDOT = -942
901109 TA = 92
88287
MA = 92
82513
Ha = 191
906 n
mi
Hp = 186
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2840322
20 X = 886952
29
Y = -13667408
82 feet Y = -4156026
97 meter
Z = 17084587
86 Z = 5211639
23
XDOT = 25034
262416 XDOT = 7629
974407
YDOT = 1315
047526 feet/sec YDOT = 486
151956 meter/sec
ZDOT = -3093
507575 ZDOT = -905
833528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -260315
75 X = -79344
24
Y = 13937373
78 feet Y = 4248111
53 meter
Z = 17100598
94 Z = 5212262
56
XDOT = -23867
901186 XDOT = -7274
936281
YDOT = 3194
422090 feet/sec YDOT = 973
659853 meter/sec
ZDOT = -2950
438662 ZDOT = -899
293704
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 08207
73304983
00020000 00000-0 20000-3 0 9126
2 25544 51
6396 178
1808 0004046 323
6962 36
3925 15
72570953 34605
Satellite: ISS
Catalog Number: 25544
Epoch time: 08207
73304983 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 178
1808 deg
Eccentricity:
0004046
Arg of perigee: 323
6962 deg
Mean anomaly: 36
3925 deg
Mean motion: 15
72570953 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3460
Checksum: 303
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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