Date:
June 25th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4305 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 1161)
---------------------------------------
Vector Time (GMT): 2007/173/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1656716
37 A = 6714048
44 meter
Y = -5332541
93 meter E =
0009893
Z = -3738989
43 I = 51
94539
XDOT = 4600
702831 Wp = 22
26301
YDOT = 4439
459274 meter/sec RA = 75
64646 deg
ZDOT = -4287
730684 TA = 202
69483
MA = 202
73860
Ha = 184
772 n
mi
Hp = 177
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5435421
16 X = 1734385
79
Y = -17495216
29 feet Y = -5313580
83 meter
Z = -12267025
70 Z = -3730753
17
XDOT = 15094
169393 XDOT = 4571
547173
YDOT = 14565
155099 feet/sec YDOT = 4490
744461 meter/sec
ZDOT = -14067
357886 ZDOT = -4265
450765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18227069
84 X = -5555610
89
Y = -2036832
81 feet Y = -620826
64 meter
Z = -12236484
50 Z = -3729680
47
XDOT = 11227
044764 XDOT = 3422
003244
YDOT = -16361
273241 feet/sec YDOT = -4986
916084 meter/sec
ZDOT = -13982
628796 ZDOT = -4261
905257
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 07173
55569111
00020000 00000-0 20000-3 0 9000
2 25544 51
6348 76
1711 0008078 345
4358 14
6574 15
78247670 11621
Satellite: ISS
Catalog Number: 25544
Epoch time: 07173
55569111 = yrday
fracday
Element set: 900
Inclination: 51
6348 deg
RA of node: 76
1711 deg
Eccentricity:
0008078
Arg of perigee: 345
4358 deg
Mean anomaly: 14
6574 deg
Mean motion: 15
78247670 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1162
Checksum: 293
Coasting Arc #2 (Orbit 1177)
---------------------------------------
Vector Time (GMT): 2007/174/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3870684
86 A = 6717203
07 meter
Y = -4837885
06 meter E =
0012961
Z = 2591800
70 I = 51
94746
XDOT = 2631
823100 Wp = 68
47007
YDOT = -4950
524285 meter/sec RA = 70
45123 deg
ZDOT = -5284
619528 TA = 82
18388
MA = 82
03677
Ha = 184
911 n
mi
Hp = 177
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12699097
31 X = -3828889
76
Y = -15872326
32 feet Y = -4880935
90 meter
Z = 8503283
15 Z = 2573097
75
XDOT = 8634
590224 XDOT = 2712
656736
YDOT = -16241
877574 feet/sec YDOT = -4920
641075 meter/sec
ZDOT = -17337
990576 ZDOT = -5271
638447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12855279
58 X = -3918289
22
Y = 15784365
30 feet Y = 4811074
54 meter
Z = 8432036
43 Z = 2570084
70
XDOT = -16557
813771 XDOT = -5046
821637
YDOT = -4203
837701 feet/sec YDOT = -1281
329731 meter/sec
ZDOT = -17289
462665 ZDOT = -5269
828220
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 07174
56878114
00020000 00000-0 20000-3 0 9019
2 25544 51
6347 70
9345 0008028 350
2782 9
8227 15
78259265 11786
Satellite: ISS
Catalog Number: 25544
Epoch time: 07174
56878114 = yrday
fracday
Element set: 901
Inclination: 51
6347 deg
RA of node: 70
9345 deg
Eccentricity:
0008028
Arg of perigee: 350
2782 deg
Mean anomaly: 9
8227 deg
Mean motion: 15
78259265 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1178
Checksum: 307
Coasting Arc #3 (Orbit 1193)
---------------------------------------
Vector Time (GMT): 2007/175/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2985150
32 A = 6708544
79 meter
Y = 3127838
97 meter E =
0006060
Z = 5125900
38 I = 51
90830
XDOT = -4156
261185 Wp = 26
42080
YDOT = -6331
856266 meter/sec RA = 65
33712 deg
ZDOT = 1447
919414 TA = 49
80305
MA = 49
75002
Ha = 185
067 n
mi
Hp = 176
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9793800
26 X = -3044805
21
Y = 10261938
87 feet Y = 3094123
03 meter
Z = 16817258
48 Z = 5111254
03
XDOT = -13636
027509 XDOT = -4092
182297
YDOT = -20773
806647 feet/sec YDOT = -6377
975845 meter/sec
ZDOT = 4750
391778 ZDOT = 1427
882910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12230611
13 X = 3727890
27
Y = 7313410
18 feet Y = 2229127
42 meter
Z = 16762227
73 Z = 5109127
01
XDOT = -16616
327225 XDOT = -5064
656538
YDOT = 17110
989702 feet/sec YDOT = 5215
429661 meter/sec
ZDOT = 4673
943945 ZDOT = 1424
618114
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 07175
58185454
00020000 00000-0 20000-3 0 9021
2 25544 51
6352 65
6977 0008116 353
3882 6
7175 15
78296589 11943
Satellite: ISS
Catalog Number: 25544
Epoch time: 07175
58185454 = yrday
fracday
Element set: 902
Inclination: 51
6352 deg
RA of node: 65
6977 deg
Eccentricity:
0008116
Arg of perigee: 353
3882 deg
Mean anomaly: 6
7175 deg
Mean motion: 15
78296589 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1194
Checksum: 326
Coasting Arc #4 (Orbit 1209)
---------------------------------------
Vector Time (GMT): 2007/176/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3222756
77 A = 6719867
75 meter
Y = 5881263
85 meter E =
0018891
Z = 164506
98 I = 51
93354
XDOT = -4247
377655 Wp = 27
11492
YDOT = 2150
527051 meter/sec RA = 60
17781 deg
ZDOT = 6070
810702 TA = 334
67001
MA = 334
76251
Ha = 185
034 n
mi
Hp = 176
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10573348
97 X = 3155952
94
Y = 19295485
07 feet Y = 5916928
98 meter
Z = 539721
06 Z = 180001
95
XDOT = -13934
966061 XDOT = -4300
600566
YDOT = 7055
534945 feet/sec YDOT = 2102
731891 meter/sec
ZDOT = 19917
357946 ZDOT = 6050
047892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16153660
27 X = 4923635
65
Y = -14936642
16 feet Y = -4552688
53 meter
Z = 598942
47 Z = 182557
66
XDOT = 9163
968411 XDOT = 2793
177572
YDOT = 10736
253607 feet/sec YDOT = 3272
410099 meter/sec
ZDOT = 19839
090282 ZDOT = 6046
954718
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 07176
59491318
00020000 00000-0 20000-3 0 9033
2 25544 51
6352 60
4608 0008177 356
1998 3
9104 15
78336174 12108
Satellite: ISS
Catalog Number: 25544
Epoch time: 07176
59491318 = yrday
fracday
Element set: 903
Inclination: 51
6352 deg
RA of node: 60
4608 deg
Eccentricity:
0008177
Arg of perigee: 356
1998 deg
Mean anomaly: 3
9104 deg
Mean motion: 15
78336174 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1210
Checksum: 293
Coasting Arc #5 (Orbit 1224)
---------------------------------------
Vector Time (GMT): 2007/177/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4400137
23 A = 6708845
12 meter
Y = -606443
07 meter E =
0013767
Z = -5037411
97 I = 51
88052
XDOT = 3030
222197 Wp = 68
26957
YDOT = 6837
154916 meter/sec RA = 55
01072 deg
ZDOT = 1832
723018 TA = 219
29099
MA = 219
39098
Ha = 185
144 n
mi
Hp = 176
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14436145
78 X = 4431062
53
Y = -1989642
61 feet Y = -557064
41 meter
Z = -16526942
15 Z = -5015960
96
XDOT = 9941
673874 XDOT = 2944
639823
YDOT = 22431
610616 feet/sec YDOT = 6870
561703 meter/sec
ZDOT = 6012
870794 ZDOT = 1847
237332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5689054
42 X = -1734023
79
Y = -13515464
66 feet Y = -4119513
63 meter
Z = -16445901
44 Z = -5012710
76
XDOT = 18109
350247 XDOT = 5519
729955
YDOT = -14971
065606 feet/sec YDOT = -4563
180797 meter/sec
ZDOT = 6068
480474 ZDOT = 1849
672849
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 07177
54464368
00020000 00000-0 20000-3 0 9045
2 25544 51
6347 55
5512 0008226 359
2830
8322 15
78353378 12254
Satellite: ISS
Catalog Number: 25544
Epoch time: 07177
54464368 = yrday
fracday
Element set: 904
Inclination: 51
6347 deg
RA of node: 55
5512 deg
Eccentricity:
0008226
Arg of perigee: 359
2830 deg
Mean anomaly:
8322 deg
Mean motion: 15
78353378 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1225
Checksum: 291
Coasting Arc #6 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2007/178/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1852116
98 A = 6716075
69 meter
Y = -5761259
09 meter E =
0007840
Z = -2924715
91 I = 51
88697
XDOT = 5770
145745 Wp = 34
94068
YDOT = 706
540404 meter/sec RA = 49
89893 deg
ZDOT = -5046
135787 TA = 178
63600
MA = 178
63386
Ha = 185
174 n
mi
Hp = 176
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6076499
29 X = -1773348
28
Y = -18901768
66 feet Y = -5781529
48 meter
Z = -9595524
64 Z = -2933523
40
XDOT = 18930
924361 XDOT = 5786
329585
YDOT = 2318
045945 feet/sec YDOT = 771
156940 meter/sec
ZDOT = -16555
563606 ZDOT = -5018
064822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16506481
99 X = -5031175
71
Y = 11003854
39 feet Y = 3353974
82 meter
Z = -9629435
91 Z = -2935052
07
XDOT = -2217
905746 XDOT = -676
017671
YDOT = -17720
823833 feet/sec YDOT = -5401
307104 meter/sec
ZDOT = -16449
348332 ZDOT = -5013
761372
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 07178
55767534
00020000 00000-0 20000-3 0 9059
2 25544 51
6343 50
3149 0008179 2
3739 357
7464 15
78346222 12419
Satellite: ISS
Catalog Number: 25544
Epoch time: 07178
55767534 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 50
3149 deg
Eccentricity:
0008179
Arg of perigee: 2
3739 deg
Mean anomaly: 357
7464 deg
Mean motion: 15
78346222 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1241
Checksum: 300
Coasting Arc #7 (Orbit 1256)
---------------------------------------
Vector Time (GMT): 2007/179/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5524938
25 A = 6714590
12 meter
Y = -1692424
58 meter E =
0015801
Z = 3417084
08 I = 51
86323
XDOT = -1003
361908 Wp = 57
65812
YDOT = -6089
864936 meter/sec RA = 44
69599 deg
ZDOT = -4614
816476 TA = 82
01398
MA = 81
83470
Ha = 185
252 n
mi
Hp = 176
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18126437
82 X = -5522202
28
Y = -5552574
09 feet Y = -1754193
00 meter
Z = 11210905
79 Z = 3390250
16
XDOT = -3291
869776 XDOT = -912
771599
YDOT = -19979
871838 feet/sec YDOT = -6100
577556 meter/sec
ZDOT = -15140
474001 ZDOT = -4619
472119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8273
80 X = 2521
86
Y = 19017558
15 feet Y = 5796551
72 meter
Z = 11109259
61 Z = 3386102
33
XDOT = -16782
210221 XDOT = -5115
217675
YDOT = 8908
195343 feet/sec YDOT = 2715
217941 meter/sec
ZDOT = -15158
715559 ZDOT = -4620
376502
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 07179
57069094
00020000 00000-0 20000-3 0 9069
2 25544 51
6346 45
0775 0008391 5
8080 354
3182 15
78431693 12575
Satellite: ISS
Catalog Number: 25544
Epoch time: 07179
57069094 = yrday
fracday
Element set: 906
Inclination: 51
6346 deg
RA of node: 45
0775 deg
Eccentricity:
0008391
Arg of perigee: 5
8080 deg
Mean anomaly: 354
3182 deg
Mean motion: 15
78431693 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1257
Checksum: 306
Coasting Arc #8 (Orbit 1272)
---------------------------------------
Vector Time (GMT): 2007/180/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -269212
11 A = 6709677
53 meter
Y = 4673259
27 meter E =
0008886
Z = 4798807
11 I = 51
82357
XDOT = -6669
516945 Wp = 58
67635
YDOT = -2957
206275 meter/sec RA = 39
58588 deg
ZDOT = 2506
832023 TA = 6
91300
MA = 6
90076
Ha = 185
448 n
mi
Hp = 175
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -883241
84 X = -344760
84
Y = 15332215
46 feet Y = 4669825
28 meter
Z = 15744117
80 Z = 4797316
84
XDOT = -21881
617273 XDOT = -6648
131036
YDOT = -9702
120325 feet/sec YDOT = -3031
669556 meter/sec
ZDOT = 8224
514511 ZDOT = 2474
482867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14882820
44 X = 4536283
67
Y = -3810611
14 feet Y = -1161474
28 meter
Z = 15738967
27 Z = 4797237
22
XDOT = -2734
816402 XDOT = -833
572039
YDOT = 22766
394422 feet/sec YDOT = 6939
197020 meter/sec
ZDOT = 8101
874884 ZDOT = 2469
451465
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 07180
58369597
00020000 00000-0 20000-3 0 9074
2 25544 51
6334 39
8397 0008335 10
5614 349
5725 15
78371589 12731
Satellite: ISS
Catalog Number: 25544
Epoch time: 07180
58369597 = yrday
fracday
Element set: 907
Inclination: 51
6334 deg
RA of node: 39
8397 deg
Eccentricity:
0008335
Arg of perigee: 10
5614 deg
Mean anomaly: 349
5725 deg
Mean motion: 15
78371589 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1273
Checksum: 327
Coasting Arc #9 (Orbit 1287)
---------------------------------------
Vector Time (GMT): 2007/181/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5819852
84 A = 6719413
62 meter
Y = 3247440
85 meter E =
0018360
Z = -774497
29 I = 51
83256
XDOT = -1736
713791 Wp = 27
56800
YDOT = 4526
124648 meter/sec RA = 34
40207 deg
ZDOT = 5999
613920 TA = 323
98909
MA = 324
11265
Ha = 185
432 n
mi
Hp = 175
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19094005
39 X = 5786869
28
Y = 10654333
50 feet Y = 3312337
47 meter
Z = -2541001
62 Z = -746304
04
XDOT = -5697
879893 XDOT = -1816
341303
YDOT = 14849
490316 feet/sec YDOT = 4506
257151 meter/sec
ZDOT = 19683
772702 ZDOT = 5990
984650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3863378
43 X = 1177557
74
Y = -21533747
96 feet Y = -6563486
38 meter
Z = -2434041
77 Z = -741895
93
XDOT = 14360
728368 XDOT = 4377
150007
YDOT = 383
051030 feet/sec YDOT = 116
753954 meter/sec
ZDOT = 19651
605803 ZDOT = 5989
809449
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 07181
53337131
00020000 00000-0 20000-3 0 9080
2 25544 51
6324 34
9293 0008280 13
0058 347
1319 15
78411000 12882
Satellite: ISS
Catalog Number: 25544
Epoch time: 07181
53337131 = yrday
fracday
Element set: 908
Inclination: 51
6324 deg
RA of node: 34
9293 deg
Eccentricity:
0008280
Arg of perigee: 13
0058 deg
Mean anomaly: 347
1319 deg
Mean motion: 15
78411000 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1288
Checksum: 264
Coasting Arc #10 (Orbit 1303)
---------------------------------------
Vector Time (GMT): 2007/182/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2807146
78 A = 6707678
63 meter
Y = -3149351
01 meter E =
0018146
Z = -5228653
11 I = 51
76771
XDOT = 6335
311027 Wp = 69
87895
YDOT = 4291
615052 meter/sec RA = 29
24309 deg
ZDOT = 824
751937 TA = 207
91318
MA = 208
01065
Ha = 185
423 n
mi
Hp = 175
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9209799
15 X = 2867554
18
Y = -10332516
44 feet Y = -3117621
03 meter
Z = -17154373
71 Z = -5214870
11
XDOT = 20785
141166 XDOT = 6282
844262
YDOT = 14080
101878 feet/sec YDOT = 4362
166520 meter/sec
ZDOT = 2705
879057 ZDOT = 855
401985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12888243
73 X = -3928336
69
Y = -5220066
25 feet Y = -1591076
19 meter
Z = -17102570
44 Z = -5212863
47
XDOT = 5764
563704 XDOT = 1757
039017
YDOT = -23388
437419 feet/sec YDOT = -7128
795725 meter/sec
ZDOT = 2822
245940 ZDOT = 860
220563
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 07182
54634608
00020000 00000-0 20000-3 0 9092
2 25544 51
6313 29
6908 0008210 17
5725 342
5723 15
78454963 13049
Satellite: ISS
Catalog Number: 25544
Epoch time: 07182
54634608 = yrday
fracday
Element set: 909
Inclination: 51
6313 deg
RA of node: 29
6908 deg
Eccentricity:
0008210
Arg of perigee: 17
5725 deg
Mean anomaly: 342
5723 deg
Mean motion: 15
78454963 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1304
Checksum: 293
Coasting Arc #11 (Orbit 1319)
---------------------------------------
Vector Time (GMT): 2007/183/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4894890
16 A = 6717343
83 meter
Y = -4062959
17 meter E =
0007792
Z = -2169822
55 I = 51
77495
XDOT = 4658
787717 Wp = 65
32790
YDOT = -2673
971545 meter/sec RA = 24
10988 deg
ZDOT = -5514
975158 TA = 138
93595
MA = 138
87727
Ha = 185
472 n
mi
Hp = 175
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16059350
92 X = -4838553
32
Y = -13329918
53 feet Y = -4117381
16 meter
Z = -7118840
39 Z = -2193465
51
XDOT = 15284
736603 XDOT = 4715
132528
YDOT = -8772
872522 feet/sec YDOT = -2621
558240 meter/sec
ZDOT = -18093
750518 ZDOT = -5492
206792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6723218
26 X = -2049236
93
Y = 19725631
06 feet Y = 6012372
35 meter
Z = -7208688
11 Z = -2197208
14
XDOT = -12254
417457 XDOT = -3735
146441
YDOT = -10743
244961 feet/sec YDOT = -3274
541064 meter/sec
ZDOT = -18007
910775 ZDOT = -5488
811204
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 07183
55930617
00020000 00000-0 20000-3 0 9105
2 25544 51
6314 24
4535 0008294 21
0217 339
1288 15
78480467 13201
Satellite: ISS
Catalog Number: 25544
Epoch time: 07183
55930617 = yrday
fracday
Element set: 910
Inclination: 51
6314 deg
RA of node: 24
4535 deg
Eccentricity:
0008294
Arg of perigee: 21
0217 deg
Mean anomaly: 339
1288 deg
Mean motion: 15
78480467 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1320
Checksum: 278
Coasting Arc #12 (Orbit 1335)
---------------------------------------
Vector Time (GMT): 2007/184/12:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5162109
48 A = 6712548
59 meter
Y = 1560986
83 meter E =
0017066
Z = 3991875
16 I = 51
73170
XDOT = -4527
481923 Wp = 55
40180
YDOT = -4836
999299 meter/sec RA = 18
90110 deg
ZDOT = -3941
882642 TA = 75
32937
MA = 75
14024
Ha = 185
547 n
mi
Hp = 175
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16936054
73 X = -5198572
48
Y = 5121347
88 feet Y = 1503056
67 meter
Z = 13096703
29 Z = 3966709
76
XDOT = -14853
943317 XDOT = -4453
908776
YDOT = -15869
420273 feet/sec YDOT = -4887
216103 meter/sec
ZDOT = -12932
685832 ZDOT = -3963
698894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11102965
81 X = 3384183
98
Y = 13865867
14 feet Y = 4226316
30 meter
Z = 13001679
50 Z = 3962911
91
XDOT = -8189
864911 XDOT = -2496
270825
YDOT = 18828
733191 feet/sec YDOT = 5738
997877 meter/sec
ZDOT = -13015
710528 ZDOT = -3967
188569
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 07184
57225152
00020000 00000-0 20000-3 0 9110
2 25544 51
6314 19
2147 0008153 24
2515 335
9033 15
78495917 13367
Satellite: ISS
Catalog Number: 25544
Epoch time: 07184
57225152 = yrday
fracday
Element set: 911
Inclination: 51
6314 deg
RA of node: 19
2147 deg
Eccentricity:
0008153
Arg of perigee: 24
2515 deg
Mean anomaly: 335
9033 deg
Mean motion: 15
78495917 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1336
Checksum: 279
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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