Date:
March 7th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11732 66 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 1217)
---------------------------------------
Vector Time (GMT): 2008/065/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6371781
74 A = 6726253
26 meter
Y = -1894849
00 meter E =
0011706
Z = 993025
95 I = 51
60123
XDOT = 2234
713361 Wp = 62
13227
YDOT = -4382
952749 meter/sec RA = 189
76210 deg
ZDOT = 5928
168507 TA = 308
73403
MA = 308
83861
Ha = 186
976 n
mi
Hp = 181
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20904795
75 X = -6354943
51
Y = -6216696
20 feet Y = -1966007
70 meter
Z = 3257959
14 Z = 962113
60
XDOT = 7331
736750 XDOT = 2254
760863
YDOT = -14379
766238 feet/sec YDOT = -4357
850472 meter/sec
ZDOT = 19449
371741 ZDOT = 5939
073427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19589612
85 X = -5970914
00
Y = -9626207
34 feet Y = -2934068
00 meter
Z = 3139314
51 Z = 956863
06
XDOT = 8821
135167 XDOT = 2688
681999
YDOT = -11542
127743 feet/sec YDOT = -3518
040536 meter/sec
ZDOT = 19490
607041 ZDOT = 5940
737026
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 08065
58240397
00020000 00000-0 20000-3 0 9006
2 25544 51
6379 190
4344 0002458 203
0024 157
1031 15
75946483 12180
Satellite: ISS
Catalog Number: 25544
Epoch time: 08065
58240397 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 190
4344 deg
Eccentricity:
0002458
Arg of perigee: 203
0024 deg
Mean anomaly: 157
1031 deg
Mean motion: 15
75946483 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1218
Checksum: 278
Coasting Arc #2 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2008/066/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2419337
48 A = 6715503
25 meter
Y = 3785066
70 meter E =
0012924
Z = -5003398
77 I = 51
59511
XDOT = -7163
251230 Wp = 114
56893
YDOT = -2077
796006 meter/sec RA = 184
58470 deg
ZDOT = 1890
393226 TA = 173
71060
MA = 173
69436
Ha = 186
787 n
mi
Hp = 180
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7937458
91 X = -2437177
80
Y = 12418197
85 feet Y = 3757912
13 meter
Z = -16415350
29 Z = -5015195
29
XDOT = -23501
480414 XDOT = -7148
667592
YDOT = -6816
916031 feet/sec YDOT = -2157
817872 meter/sec
ZDOT = 6202
077513 ZDOT = 1855
630530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9619894
83 X = -2932143
95
Y = 11099649
45 feet Y = 3383173
15 meter
Z = -16460073
58 Z = -5017030
43
XDOT = -21436
490422 XDOT = -6533
842281
YDOT = -9572
141030 feet/sec YDOT = -2917
588586 meter/sec
ZDOT = 6068
649981 ZDOT = 1849
724514
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 08066
53355740
00020000 00000-0 20000-3 0 9012
2 25544 51
6382 185
5363 0002377 207
5041 152
5998 15
76013692 12334
Satellite: ISS
Catalog Number: 25544
Epoch time: 08066
53355740 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 185
5363 deg
Eccentricity:
0002377
Arg of perigee: 207
5041 deg
Mean anomaly: 152
5998 deg
Mean motion: 15
76013692 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1233
Checksum: 288
Coasting Arc #3 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2008/067/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6066777
33 A = 6724170
76 meter
Y = 1759950
13 meter E =
0006884
Z = -2295858
53 I = 51
65396
XDOT = -3311
149048 Wp = 156
13748
YDOT = 4333
748734 meter/sec RA = 179
46844 deg
ZDOT = -5439
352677 TA = 49
68230
MA = 49
62218
Ha = 186
731 n
mi
Hp = 181
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19904125
11 X = 6057799
07
Y = 5774114
59 feet Y = 1827741
86 meter
Z = -7532344
26 Z = -2266408
64
XDOT = -10863
349895 XDOT = -3332
940682
YDOT = 14218
335742 feet/sec YDOT = 4296
599180 meter/sec
ZDOT = -17845
645267 ZDOT = -5455
491321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19000336
20 X = 5791302
48
Y = 8378066
36 feet Y = 2553634
63 meter
Z = -7419301
43 Z = -2261403
08
XDOT = -11948
004247 XDOT = -3641
751694
YDOT = 11273
665407 feet/sec YDOT = 3436
213216 meter/sec
ZDOT = -17906
935070 ZDOT = -5458
033809
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 08067
54809406
00020000 00000-0 20000-3 0 9028
2 25544 51
6386 180
3102 0002342 213
0104 147
0914 15
76031761 12497
Satellite: ISS
Catalog Number: 25544
Epoch time: 08067
54809406 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 180
3102 deg
Eccentricity:
0002342
Arg of perigee: 213
0104 deg
Mean anomaly: 147
0914 deg
Mean motion: 15
76031761 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1249
Checksum: 257
Coasting Arc #4 (Orbit 1264)
---------------------------------------
Vector Time (GMT): 2008/068/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3330863
26 A = 6717777
90 meter
Y = -3828312
10 meter E =
0007513
Z = 4396648
49 I = 51
66246
XDOT = 6666
580457 Wp = 77
72976
YDOT = 1974
351885 meter/sec RA = 174
27489 deg
ZDOT = -3325
086491 TA = 45
67106
MA = 45
60950
Ha = 186
512 n
mi
Hp = 181
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10928029
07 X = 3352066
61
Y = -12560079
06 feet Y = -3790945
45 meter
Z = 14424699
77 Z = 4412881
55
XDOT = 21871
983128 XDOT = 6660
159958
YDOT = 6477
532432 feet/sec YDOT = 2048
865134 meter/sec
ZDOT = -10909
076414 ZDOT = -3292
716436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12230395
63 X = 3727824
59
Y = -11216529
86 feet Y = -3418798
30 meter
Z = 14486416
03 Z = 4415459
61
XDOT = 20215
635332 XDOT = 6161
725649
YDOT = 8087
414024 feet/sec YDOT = 2465
043795 meter/sec
ZDOT = -10784
813918 ZDOT = -3287
211282
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 08068
56260286
00020000 00000-0 20000-3 0 9039
2 25544 51
6389 175
0846 0002113 217
3231 142
7786 15
76072148 12651
Satellite: ISS
Catalog Number: 25544
Epoch time: 08068
56260286 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 175
0846 deg
Eccentricity:
0002113
Arg of perigee: 217
3231 deg
Mean anomaly: 142
7786 deg
Mean motion: 15
76072148 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1265
Checksum: 292
Coasting Arc #5 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2008/069/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5489131
26 A = 6720976
15 meter
Y = -1733622
94 meter E =
0011138
Z = 3461623
75 I = 51
70240
XDOT = 4299
553220 Wp = 99
52765
YDOT = -4485
876483 meter/sec RA = 169
17609 deg
ZDOT = 4557
074100 TA = 301
51799
MA = 301
62675
Ha = 186
469 n
mi
Hp = 181
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18008960
84 X = -5486153
51
Y = -5687739
32 feet Y = -1794988
54 meter
Z = 11357033
31 Z = 3434965
11
XDOT = 14106
145736 XDOT = 4327
258111
YDOT = -14717
442530 feet/sec YDOT = -4437
641052 meter/sec
ZDOT = 14951
030512 ZDOT = 4578
028965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17421579
36 X = -5310097
39
Y = -7448223
45 feet Y = -2270218
51 meter
Z = 11254678
79 Z = 3430426
10
XDOT = 14865
485896 XDOT = 4531
000101
YDOT = -11987
444473 feet/sec YDOT = -3653
773075 meter/sec
ZDOT = 15030
760297 ZDOT = 4581
375738
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 08069
57708181
00020000 00000-0 20000-3 0 9043
2 25544 51
6388 169
8583 0002136 223
2973 136
8024 15
76137409 12812
Satellite: ISS
Catalog Number: 25544
Epoch time: 08069
57708181 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 169
8583 deg
Eccentricity:
0002136
Arg of perigee: 223
2973 deg
Mean anomaly: 136
8024 deg
Mean motion: 15
76137409 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1281
Checksum: 307
Coasting Arc #6 (Orbit 1295)
---------------------------------------
Vector Time (GMT): 2008/070/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4124216
56 A = 6720734
85 meter
Y = 4025740
10 meter E =
0003920
Z = -3461964
89 I = 51
73006
XDOT = -5845
799932 Wp = 116
30555
YDOT = -2066
701186 meter/sec RA = 163
97906 deg
ZDOT = 4563
067065 TA = 202
70819
MA = 202
72553
Ha = 186
269 n
mi
Hp = 180
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13530894
22 X = -4152108
90
Y = 13207808
73 feet Y = 3979464
52 meter
Z = -11358152
52 Z = -3482068
40
XDOT = -19179
133635 XDOT = -5844
421823
YDOT = -6780
515703 feet/sec YDOT = -2132
064176 meter/sec
ZDOT = 14970
692470 ZDOT = 4534
671716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14501764
55 X = -4420137
83
Y = 12061746
88 feet Y = 3676420
45 meter
Z = -11434685
22 Z = -3485292
05
XDOT = -17764
813933 XDOT = -5414
715287
YDOT = -7276
501923 feet/sec YDOT = -2217
877786 meter/sec
ZDOT = 14861
638579 ZDOT = 4529
827439
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 08070
52813220
00020000 00000-0 20000-3 0 9052
2 25544 51
6383 164
9595 0002060 230
5873 129
5109 15
76162432 12965
Satellite: ISS
Catalog Number: 25544
Epoch time: 08070
52813220 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 164
9595 deg
Eccentricity:
0002060
Arg of perigee: 230
5873 deg
Mean anomaly: 129
5109 deg
Mean motion: 15
76162432 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1296
Checksum: 279
Coasting Arc #7 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2008/071/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4659590
36 A = 6717493
76 meter
Y = 1949676
83 meter E =
0007450
Z = -4435796
53 I = 51
74577
XDOT = -5102
008092 Wp = 73
35854
YDOT = 4740
986800 meter/sec RA = 158
88371 deg
ZDOT = -3278
020081 TA = 163
81322
MA = 163
78941
Ha = 186
227 n
mi
Hp = 181
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15287369
94 X = 4658990
78
Y = 6396577
52 feet Y = 2001779
43 meter
Z = -14553138
22 Z = -4413161
78
XDOT = -16738
871693 XDOT = -5138
719303
YDOT = 15554
418635 feet/sec YDOT = 4683
727791 meter/sec
ZDOT = -10754
659059 ZDOT = -3302
895089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14923877
93 X = 4548797
99
Y = 7377099
25 feet Y = 2248539
85 meter
Z = -14466167
08 Z = -4409287
72
XDOT = -17110
562244 XDOT = -5215
299372
YDOT = 13355
179865 feet/sec YDOT = 4070
658823 meter/sec
ZDOT = -10849
398773 ZDOT = -3306
896746
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 08071
54255834
00020000 00000-0 20000-3 0 9067
2 25544 51
6373 159
7329 0002001 235
4511 124
6465 15
76186774 13124
Satellite: ISS
Catalog Number: 25544
Epoch time: 08071
54255834 = yrday
fracday
Element set: 906
Inclination: 51
6373 deg
RA of node: 159
7329 deg
Eccentricity:
0002001
Arg of perigee: 235
4511 deg
Mean anomaly: 124
6465 deg
Mean motion: 15
76186774 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1312
Checksum: 283
Coasting Arc #8 (Orbit 1327)
---------------------------------------
Vector Time (GMT): 2008/072/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4710937
12 A = 6723618
54 meter
Y = -4255537
43 meter E =
0012863
Z = 2194687
95 I = 51
79392
XDOT = 4798
352910 Wp = 114
48354
YDOT = 2462
177314 meter/sec RA = 153
69696 deg
ZDOT = -5505
681790 TA = 40
94673
MA = 40
85020
Ha = 186
067 n
mi
Hp = 180
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15455830
45 X = 4747511
68
Y = -13961736
97 feet Y = -4202652
49 meter
Z = 7200419
79 Z = 2217662
63
XDOT = 15742
627659 XDOT = 4797
209439
YDOT = 8078
009560 feet/sec YDOT = 2515
828698 meter/sec
ZDOT = -18063
260467 ZDOT = -5482
374241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16060379
05 X = 4895203
53
Y = -13213963
74 feet Y = -4027616
15 meter
Z = 7287950
76 Z = 2221367
39
XDOT = 14479
769016 XDOT = 4413
433596
YDOT = 7650
260909 feet/sec YDOT = 2331
799525 meter/sec
ZDOT = -17973
643346 ZDOT = -5478
366492
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 08072
55695627
00020000 00000-0 20000-3 0 9078
2 25544 51
6372 154
5061 0001774 243
1233 116
9750 15
76255832 13282
Satellite: ISS
Catalog Number: 25544
Epoch time: 08072
55695627 = yrday
fracday
Element set: 907
Inclination: 51
6372 deg
RA of node: 154
5061 deg
Eccentricity:
0001774
Arg of perigee: 243
1233 deg
Mean anomaly: 116
9750 deg
Mean motion: 15
76255832 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1328
Checksum: 292
Coasting Arc #9 (Orbit 1343)
---------------------------------------
Vector Time (GMT): 2008/073/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3686209
57 A = 6714531
28 meter
Y = -2418985
61 meter E =
0004526
Z = 5062881
02 I = 51
78912
XDOT = 5616
154178 Wp = 145
83073
YDOT = -4995
679044 meter/sec RA = 148
58863 deg
ZDOT = 1697
760707 TA = 287
86057
MA = 287
90993
Ha = 186
067 n
mi
Hp = 180
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12093863
41 X = -3683480
59
Y = -7936304
49 feet Y = -2460191
62 meter
Z = 16610502
05 Z = 5044980
13
XDOT = 18425
702684 XDOT = 5663
351849
YDOT = -16390
023110 feet/sec YDOT = -4932
612100 meter/sec
ZDOT = 5570
081059 ZDOT = 1725
158538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11941834
02 X = -3639871
01
Y = -8301996
95 feet Y = -2530448
67 meter
Z = 16541604
71 Z = 5041881
12
XDOT = 18276
595354 XDOT = 5570
706264
YDOT = -14954
354965 feet/sec YDOT = -4558
087393 meter/sec
ZDOT = 5674
490818 ZDOT = 1729
584801
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 08073
57132567
00020000 00000-0 20000-3 0 9081
2 25544 51
6372 149
2786 0001853 248
5889 111
5078 15
76304374 13449
Satellite: ISS
Catalog Number: 25544
Epoch time: 08073
57132567 = yrday
fracday
Element set: 908
Inclination: 51
6372 deg
RA of node: 149
2786 deg
Eccentricity:
0001853
Arg of perigee: 248
5889 deg
Mean anomaly: 111
5078 deg
Mean motion: 15
76304374 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1344
Checksum: 312
Coasting Arc #10 (Orbit 1358)
---------------------------------------
Vector Time (GMT): 2008/074/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5010329
85 A = 6725440
62 meter
Y = 4421117
48 meter E =
0009378
Z = -719525
96 I = 51
84951
XDOT = -3648
028627 Wp = 33
05854
YDOT = -3164
507319 meter/sec RA = 143
42700 deg
ZDOT = 6002
458901 TA = 319
11674
MA = 319
18703
Ha = 185
985 n
mi
Hp = 180
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16438090
06 X = -5055899
80
Y = 14504978
61 feet Y = 4364834
32 meter
Z = -2360649
48 Z = -743976
59
XDOT = -11968
597856 XDOT = -3641
530075
YDOT = -10382
241860 feet/sec YDOT = -3205
265344 meter/sec
ZDOT = 19693
106630 ZDOT = 5984
752716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16613075
29 X = -5063665
35
Y = 14288535
19 feet Y = 4355145
53 meter
Z = -2453847
28 Z = -747932
65
XDOT = -10901
130992 XDOT = -3322
664726
YDOT = -9328
228975 feet/sec YDOT = -2843
244191 meter/sec
ZDOT = 19624
860538 ZDOT = 5981
657492
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 08074
52227358
00020000 00000-0 20000-3 0 9091
2 25544 51
6366 144
3781 0001660 261
5196 98
5780 15
76282718 13592
Satellite: ISS
Catalog Number: 25544
Epoch time: 08074
52227358 = yrday
fracday
Element set: 909
Inclination: 51
6366 deg
RA of node: 144
3781 deg
Eccentricity:
0001660
Arg of perigee: 261
5196 deg
Mean anomaly: 98
5780 deg
Mean motion: 15
76282718 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1359
Checksum: 315
Coasting Arc #11 (Orbit 1374)
---------------------------------------
Vector Time (GMT): 2008/075/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2682411
69 A = 6713422
48 meter
Y = 3173282
84 meter E =
0013447
Z = -5284530
42 I = 51
83223
XDOT = -5795
209304 Wp = 91
79554
YDOT = 5061
646268 meter/sec RA = 138
29408 deg
ZDOT = 97
613327 TA = 179
13012
MA = 179
12778
Ha = 185
905 n
mi
Hp = 180
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8800563
29 X = 2672399
11
Y = 10411032
94 feet Y = 3203223
10 meter
Z = -17337698
22 Z = -5271523
78
XDOT = -19013
153885 XDOT = -5851
852887
YDOT = 16606
451009 feet/sec YDOT = 4996
524220 meter/sec
ZDOT = 320
253698 ZDOT = 69
323017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8941401
66 X = 2725339
23
Y = 10374504
75 feet Y = 3162149
05 meter
Z = -17287460
44 Z = -5269217
94
XDOT = -18189
912028 XDOT = -5544
285186
YDOT = 16032
237753 feet/sec YDOT = 4886
626067 meter/sec
ZDOT = 212
398732 ZDOT = 64
739134
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 08075
53659110
00020000 00000-0 20000-3 0 9100
2 25544 51
6367 139
1504 0001643 262
4147 97
6831 15
76347183 13758
Satellite: ISS
Catalog Number: 25544
Epoch time: 08075
53659110 = yrday
fracday
Element set: 910
Inclination: 51
6367 deg
RA of node: 139
1504 deg
Eccentricity:
0001643
Arg of perigee: 262
4147 deg
Mean anomaly: 97
6831 deg
Mean motion: 15
76347183 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1375
Checksum: 290
Coasting Arc #12 (Orbit 1390)
---------------------------------------
Vector Time (GMT): 2008/076/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5046041
50 A = 6724953
45 meter
Y = -4345707
49 meter E =
0009356
Z = -902165
73 I = 51
89356
XDOT = 2521
359192 Wp = 148
31618
YDOT = 4160
495271 meter/sec RA = 133
16550 deg
ZDOT = -5973
949362 TA = 41
50703
MA = 41
43601
Ha = 185
881 n
mi
Hp = 180
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16555254
25 X = 5098643
32
Y = -14257570
50 feet Y = -4288985
68 meter
Z = -2959861
30 Z = -877524
66
XDOT = 8272
175828 XDOT = 2503
668319
YDOT = 13649
918867 feet/sec YDOT = 4188
591506 meter/sec
ZDOT = -19599
571396 ZDOT = -5961
743888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16264341
98 X = 4957371
43
Y = -14607304
05 feet Y = -4452306
27 meter
Z = -2865900
83 Z = -873526
57
XDOT = 7606
920423 XDOT = 2318
589345
YDOT = 12282
290636 feet/sec YDOT = 3743
642186 meter/sec
ZDOT = -19552
283291 ZDOT = -5959
535947
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 08076
55088080
00020000 00000-0 20000-3 0 9116
2 25544 51
6375 133
9227 0001440 270
6841 89
4159 15
76424822 13914
Satellite: ISS
Catalog Number: 25544
Epoch time: 08076
55088080 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 133
9227 deg
Eccentricity:
0001440
Arg of perigee: 270
6841 deg
Mean anomaly: 89
4159 deg
Mean motion: 15
76424822 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1391
Checksum: 292
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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