Date:
October 27th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4574 66 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 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 3148)
---------------------------------------
Vector Time (GMT): 2007/299/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 106959
75 A = 6716244
31 meter
Y = -4656370
87 meter E =
0007679
Z = 4833322
93 I = 51
80305
XDOT = 6925
436434 Wp = 74
41987
YDOT = -2362
526715 meter/sec RA = 146
05405 deg
ZDOT = -2424
097904 TA = 39
19555
MA = 39
13996
Ha = 187
625 n
mi
Hp = 180
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 350917
80 X = 135539
78
Y = -15276807
33 feet Y = -4655014
95 meter
Z = 15857358
70 Z = 4833912
02
XDOT = 22721
248142 XDOT = 6963
116097
YDOT = -7751
071900 feet/sec YDOT = -2284
871905 meter/sec
ZDOT = -7953
077114 ZDOT = -2390
361379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3508911
70 X = 1069516
29
Y = 14870745
74 feet Y = 4532603
30 meter
Z = 15859012
27 Z = 4833826
94
XDOT = -19071
030791 XDOT = -5812
850185
YDOT = 12863
296841 feet/sec YDOT = 3920
732877 meter/sec
ZDOT = -7825
085551 ZDOT = -2385
086076
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 07299
48950989
00020000 00000-0 20000-3 0 9008
2 25544 51
6372 146
8010 0002098 134
7911 225
3424 15
76014798 31498
Satellite: ISS
Catalog Number: 25544
Epoch time: 07299
48950989 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 146
8010 deg
Eccentricity:
0002098
Arg of perigee: 134
7911 deg
Mean anomaly: 225
3424 deg
Mean motion: 15
76014798 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3149
Checksum: 308
Coasting Arc #2 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2007/300/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5819828
91 A = 6723383
15 meter
Y = 1982663
62 meter E =
0014836
Z = 2706419
61 I = 51
84898
XDOT = 499
330335 Wp = 85
41112
YDOT = -5664
953636 meter/sec RA = 140
95749 deg
ZDOT = 5200
661060 TA = 305
40773
MA = 305
54621
Ha = 187
648 n
mi
Hp = 180
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19093926
87 X = -5854714
57
Y = 6504801
90 feet Y = 1917387
86 meter
Z = 8879329
41 Z = 2678061
20
XDOT = 1638
222885 XDOT = 537
374825
YDOT = -18585
805893 feet/sec YDOT = -5659
157279 meter/sec
ZDOT = 17062
536285 ZDOT = 5203
179137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16759833
14 X = 5108397
14
Y = -11309189
55 feet Y = -3447040
98 meter
Z = 8771727
69 Z = 2673622
60
XDOT = 2574
075513 XDOT = 784
578216
YDOT = 17115
288978 feet/sec YDOT = 5216
740080 meter/sec
ZDOT = 17071
409801 ZDOT = 5203
365707
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 07300
50406180
00020000 00000-0 20000-3 0 9014
2 25544 51
6361 141
5741 0002041 138
0283 222
1038 15
76000474 31656
Satellite: ISS
Catalog Number: 25544
Epoch time: 07300
50406180 = yrday
fracday
Element set: 901
Inclination: 51
6361 deg
RA of node: 141
5741 deg
Eccentricity:
0002041
Arg of perigee: 138
0283 deg
Mean anomaly: 222
1038 deg
Mean motion: 15
76000474 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3165
Checksum: 232
Coasting Arc #3 (Orbit 3179)
---------------------------------------
Vector Time (GMT): 2007/301/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -717999
92 A = 6718888
11 meter
Y = 5244894
55 meter E =
0009678
Z = -4147852
23 I = 51
85538
XDOT = -6381
051828 Wp = 116
85588
YDOT = 2094
856422 meter/sec RA = 135
77246 deg
ZDOT = 3755
892267 TA = 191
49505
MA = 191
51717
Ha = 187
486 n
mi
Hp = 180
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2355642
79 X = -756445
62
Y = 17207659
28 feet Y = 5236650
75 meter
Z = -13608439
08 Z = -4151433
46
XDOT = -20935
209409 XDOT = -6422
248581
YDOT = 6872
888523 feet/sec YDOT = 2023
269324 meter/sec
ZDOT = 12322
481190 ZDOT = 3724
792206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2621025
72 X = -798888
64
Y = -17158944
46 feet Y = -5230046
27 meter
Z = -13621418
96 Z = -4151808
50
XDOT = 16995
198757 XDOT = 5180
136581
YDOT = -12278
100055 feet/sec YDOT = -3742
364897 meter/sec
ZDOT = 12204
449472 ZDOT = 3719
916199
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 07301
45518671
00020000 00000-0 20000-3 0 9029
2 25544 51
6354 136
6737 0002030 143
5037 216
6266 15
76035209 31806
Satellite: ISS
Catalog Number: 25544
Epoch time: 07301
45518671 = yrday
fracday
Element set: 902
Inclination: 51
6354 deg
RA of node: 136
6737 deg
Eccentricity:
0002030
Arg of perigee: 143
5037 deg
Mean anomaly: 216
6266 deg
Mean motion: 15
76035209 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3180
Checksum: 267
Coasting Arc #4 (Orbit 3195)
---------------------------------------
Vector Time (GMT): 2007/302/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5308374
56 A = 6720144
11 meter
Y = -1592300
40 meter E =
0007003
Z = -3806601
55 I = 51
87869
XDOT = -1106
844056 Wp = 91
75773
YDOT = 6350
850685 meter/sec RA = 130
68872 deg
ZDOT = -4206
894371 TA = 134
26966
MA = 134
21218
Ha = 187
455 n
mi
Hp = 180
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17415927
03 X = 5344277
61
Y = -5224082
67 feet Y = -1532738
13 meter
Z = -12488850
22 Z = -3780725
73
XDOT = -3631
378135 XDOT = -1157
341120
YDOT = 20836
124294 feet/sec YDOT = 6338
191292 meter/sec
ZDOT = -13802
146888 ZDOT = -4212
393751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15156559
76 X = -4619719
42
Y = 10165055
63 feet Y = 3098308
96 meter
Z = -12390612
34 Z = -3776658
64
XDOT = -2030
887870 XDOT = -619
014623
YDOT = -19849
230136 feet/sec YDOT = -6050
045345 meter/sec
ZDOT = -13822
298948 ZDOT = -4213
036719
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 07302
46970316
00020000 00000-0 20000-3 0 9030
2 25544 51
6347 131
4474 0001974 148
1611 211
9673 15
76047159 31968
Satellite: ISS
Catalog Number: 25544
Epoch time: 07302
46970316 = yrday
fracday
Element set: 903
Inclination: 51
6347 deg
RA of node: 131
4474 deg
Eccentricity:
0001974
Arg of perigee: 148
1611 deg
Mean anomaly: 211
9673 deg
Mean motion: 15
76047159 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3196
Checksum: 290
Coasting Arc #5 (Orbit 3211)
---------------------------------------
Vector Time (GMT): 2007/303/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1144851
78 A = 6721846
50 meter
Y = -5829658
92 meter E =
0014056
Z = 3129675
43 I = 51
90412
XDOT = 5772
276185 Wp = 100
55968
YDOT = -1497
300076 meter/sec RA = 125
50378 deg
ZDOT = -4884
680462 TA = 43
12461
MA = 43
01458
Ha = 187
213 n
mi
Hp = 180
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3756075
38 X = 1194751
13
Y = -19126177
56 feet Y = -5816577
76 meter
Z = 10267964
01 Z = 3135358
02
XDOT = 18937
913992 XDOT = 5812
319550
YDOT = -4912
401824 feet/sec YDOT = -1432
526979 meter/sec
ZDOT = -16025
854535 ZDOT = -4856
541052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2460724
21 X = 750028
74
Y = 19324428
77 feet Y = 5890085
89 meter
Z = 10288884
50 Z = 3136051
99
XDOT = -15132
404992 XDOT = -4612
357041
YDOT = 10430
322235 feet/sec YDOT = 3179
162217 meter/sec
ZDOT = -15918
979315 ZDOT = -4852
104895
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 07303
48420029
00020000 00000-0 20000-3 0 9045
2 25544 51
6356 126
2204 0001765 152
2346 207
8913 15
76126158 32127
Satellite: ISS
Catalog Number: 25544
Epoch time: 07303
48420029 = yrday
fracday
Element set: 904
Inclination: 51
6356 deg
RA of node: 126
2204 deg
Eccentricity:
0001765
Arg of perigee: 152
2346 deg
Mean anomaly: 207
8913 deg
Mean motion: 15
76126158 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3212
Checksum: 264
Coasting Arc #6 (Orbit 3227)
---------------------------------------
Vector Time (GMT): 2007/304/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4766646
13 A = 6717013
31 meter
Y = 944760
54 meter E =
0009822
Z = 4632717
77 I = 51
90190
XDOT = 1454
393882 Wp = 122
49855
YDOT = -6986
123936 meter/sec RA = 120
41686 deg
ZDOT = 2911
522931 TA = 298
76368
MA = 298
86231
Ha = 187
415 n
mi
Hp = 180
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15638602
79 X = -4799361
54
Y = 3099608
08 feet Y = 891274
03 meter
Z = 15199205
28 Z = 4609481
66
XDOT = 4771
633472 XDOT = 1518
261826
YDOT = -22920
354122 feet/sec YDOT = -6969
503141 meter/sec
ZDOT = 9552
240587 ZDOT = 2918
743222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13831965
99 X = 4215983
23
Y = -8094844
29 feet Y = -2467308
54 meter
Z = 15110907
37 Z = 4605804
57
XDOT = 2486
443751 XDOT = 757
868055
YDOT = 22189
098815 feet/sec YDOT = 6763
237319 meter/sec
ZDOT = 9578
879745 ZDOT = 2919
642546
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 07304
49868326
00020000 00000-0 20000-3 0 9054
2 25544 51
6346 120
9930 0001851 153
2409 206
8851 15
76078021 32282
Satellite: ISS
Catalog Number: 25544
Epoch time: 07304
49868326 = yrday
fracday
Element set: 905
Inclination: 51
6346 deg
RA of node: 120
9930 deg
Eccentricity:
0001851
Arg of perigee: 153
2409 deg
Mean anomaly: 206
8851 deg
Mean motion: 15
76078021 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3228
Checksum: 288
Coasting Arc #7 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2007/305/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1341524
93 A = 6724536
26 meter
Y = 6311825
12 meter E =
0006301
Z = -1888371
51 I = 51
94089
XDOT = -5181
733014 Wp = 54
27371
YDOT = 588
673673 meter/sec RA = 115
24470 deg
ZDOT = 5665
494473 TA = 284
82810
MA = 284
89788
Ha = 187
162 n
mi
Hp = 180
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4401328
51 X = -1402831
53
Y = 20708087
67 feet Y = 6296480
72 meter
Z = -6195444
58 Z = -1895037
40
XDOT = -17000
436396 XDOT = -5215
452801
YDOT = 1931
344073 feet/sec YDOT = 530
539858 meter/sec
ZDOT = 18587
580292 ZDOT = 5640
239435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3042284
64 X = -927288
36
Y = -20943626
43 feet Y = -6383617
34 meter
Z = -6220059
24 Z = -1895874
06
XDOT = 13862
506665 XDOT = 4225
292032
YDOT = -7489
287704 feet/sec YDOT = -2282
734892 meter/sec
ZDOT = 18491
548716 ZDOT = 5636
224049
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 07305
44974091
00020000 00000-0 20000-3 0 9068
2 25544 51
6340 116
0921 0001949 160
1338 199
9903 15
76134424 32435
Satellite: ISS
Catalog Number: 25544
Epoch time: 07305
44974091 = yrday
fracday
Element set: 906
Inclination: 51
6340 deg
RA of node: 116
0921 deg
Eccentricity:
0001949
Arg of perigee: 160
1338 deg
Mean anomaly: 199
9903 deg
Mean motion: 15
76134424 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3243
Checksum: 285
Coasting Arc #8 (Orbit 3258)
---------------------------------------
Vector Time (GMT): 2007/306/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4310642
33 A = 6714545
81 meter
Y = -9129
69 meter E =
0014560
Z = -5160683
41 I = 51
91799
XDOT = -1592
725008 Wp = 87
49446
YDOT = 7405
753025 meter/sec RA = 110
14167 deg
ZDOT = -1346
100084 TA = 169
67775
MA = 169
64782
Ha = 187
131 n
mi
Hp = 180
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14142527
33 X = 4335493
99
Y = -29953
06 feet Y = 39213
39 meter
Z = -16931376
01 Z = -5139681
71
XDOT = -5225
475747 XDOT = -1668
879695
YDOT = 24297
089976 feet/sec YDOT = 7387
516491 meter/sec
ZDOT = -4416
338858 ZDOT = -1354
022491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13267165
77 X = -4043832
13
Y = 5166648
13 feet Y = 1574794
35 meter
Z = -16851454
82 Z = -5136323
43
XDOT = -3542
779240 XDOT = -1079
839112
YDOT = -23568
883731 feet/sec YDOT = -7183
795761 meter/sec
ZDOT = -4445
608916 ZDOT = -1355
021597
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 07306
46418608
00020000 00000-0 20000-3 0 9079
2 25544 51
6334 110
8650 0001980 160
3998 199
7243 15
76165796 32596
Satellite: ISS
Catalog Number: 25544
Epoch time: 07306
46418608 = yrday
fracday
Element set: 907
Inclination: 51
6334 deg
RA of node: 110
8650 deg
Eccentricity:
0001980
Arg of perigee: 160
3998 deg
Mean anomaly: 199
7243 deg
Mean motion: 15
76165796 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3259
Checksum: 317
Coasting Arc #9 (Orbit 3274)
---------------------------------------
Vector Time (GMT): 2007/307/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1403864
60 A = 6725724
37 meter
Y = -6555670
14 meter E =
0014446
Z = 434767
08 I = 51
96566
XDOT = 4736
567162 Wp = 134
31179
YDOT = 605
661402 meter/sec RA = 104
99481 deg
ZDOT = -6049
191297 TA = 40
97545
MA = 40
86699
Ha = 186
905 n
mi
Hp = 180
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4605855
00 X = 1474954
71
Y = -21508104
13 feet Y = -6539573
84 meter
Z = 1426401
19 Z = 441759
83
XDOT = 15539
918512 XDOT = 4758
828792
YDOT = 1987
078089 feet/sec YDOT = 658
752842 meter/sec
ZDOT = -19846
428139 ZDOT = -6026
126682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3848111
29 X = 1172904
32
Y = 21654794
11 feet Y = 6600381
24 meter
Z = 1452238
08 Z = 442642
17
XDOT = -13667
014473 XDOT = -4165
706011
YDOT = 3778
087841 feet/sec YDOT = 1151
561174 meter/sec
ZDOT = -19758
579413 ZDOT = -6022
415005
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 07307
47861058
00020000 00000-0 20000-3 0 9083
2 25544 51
6339 105
6376 0001662 165
7420 194
3791 15
76242092 32756
Satellite: ISS
Catalog Number: 25544
Epoch time: 07307
47861058 = yrday
fracday
Element set: 908
Inclination: 51
6339 deg
RA of node: 105
6376 deg
Eccentricity:
0001662
Arg of perigee: 165
7420 deg
Mean anomaly: 194
3791 deg
Mean motion: 15
76242092 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3275
Checksum: 301
Coasting Arc #10 (Orbit 3290)
---------------------------------------
Vector Time (GMT): 2007/308/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4004027
67 A = 6713934
65 meter
Y = -1090835
72 meter E =
0003185
Z = 5275186
02 I = 51
93070
XDOT = 1589
889046 Wp = 112
15203
YDOT = -7533
476670 meter/sec RA = 99
86464 deg
ZDOT = -352
052423 TA = 341
16823
MA = 341
18000
Ha = 187
185 n
mi
Hp = 180
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13136573
73 X = -4017158
52
Y = -3578857
35 feet Y = -1135684
38 meter
Z = 17307040
73 Z = 5255702
25
XDOT = 5216
171411 XDOT = 1675
721589
YDOT = -24716
130806 feet/sec YDOT = -7515
217720 meter/sec
ZDOT = -1155
027635 ZDOT = -344
120027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13575977
27 X = 4137957
87
Y = -1906894
59 feet Y = -581221
47 meter
Z = 17232760
73 Z = 5252545
47
XDOT = 4766
442883 XDOT = 1452
811791
YDOT = 23791
035163 feet/sec YDOT = 7251
507518 meter/sec
ZDOT = -1125
724922 ZDOT = -343
120956
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 07308
49302051
00020000 00000-0 20000-3 0 9090
2 25544 51
6330 100
4095 0001957 165
2770 194
8452 15
76178006 32918
Satellite: ISS
Catalog Number: 25544
Epoch time: 07308
49302051 = yrday
fracday
Element set: 909
Inclination: 51
6330 deg
RA of node: 100
4095 deg
Eccentricity:
0001957
Arg of perigee: 165
2770 deg
Mean anomaly: 194
8452 deg
Mean motion: 15
76178006 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3291
Checksum: 280
Coasting Arc #11 (Orbit 3306)
---------------------------------------
Vector Time (GMT): 2007/309/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1366011
44 A = 6725294
41 meter
Y = 6494754
15 meter E =
0013093
Z = 1053565
58 I = 51
97369
XDOT = -4506
869337 Wp = 64
22700
YDOT = -1920
848025 meter/sec RA = 94
74640 deg
ZDOT = 5946
553751 TA = 307
25325
MA = 307
37260
Ha = 186
884 n
mi
Hp = 180
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4481664
81 X = -1443653
37
Y = 21308248
53 feet Y = 6479044
54 meter
Z = 3456580
00 Z = 1046740
65
XDOT = -14786
316723 XDOT = -4513
943047
YDOT = -6301
994834 feet/sec YDOT = -1971
285841 meter/sec
ZDOT = 19509
690785 ZDOT = 5924
641776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4597294
43 X = -1401255
34
Y = -21287680
67 feet Y = -6488485
07 meter
Z = 3431363
53 Z = 1045879
60
XDOT = 14618
475821 XDOT = 4455
711430
YDOT = 1
542087 feet/sec YDOT =
470028 meter/sec
ZDOT = 19426
071994 ZDOT = 5921
066744
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 07309
50740702
00020000 00000-0 20000-3 0 9104
2 25544 51
6333 95
1814 0001982 171
0805 189
0395 15
76257010 33075
Satellite: ISS
Catalog Number: 25544
Epoch time: 07309
50740702 = yrday
fracday
Element set: 910
Inclination: 51
6333 deg
RA of node: 95
1814 deg
Eccentricity:
0001982
Arg of perigee: 171
0805 deg
Mean anomaly: 189
0395 deg
Mean motion: 15
76257010 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3307
Checksum: 271
Coasting Arc #12 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2007/310/10:42:16
349
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3912974
86 A = 6715016
74 meter
Y = 2266046
96 meter E =
0013769
Z = -4976867
69 I = 51
94100
XDOT = -1565
923549 Wp = 112
81802
YDOT = 7243
929613 meter/sec RA = 89
58888 deg
ZDOT = 2066
378653 TA = 177
12973
MA = 177
12182
Ha = 186
828 n
mi
Hp = 180
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12837844
03 X = 3911522
10
Y = 7434537
26 feet Y = 2309795
87 meter
Z = -16328306
06 Z = -4957861
53
XDOT = -5137
544452 XDOT = -1656
848228
YDOT = 23766
173272 feet/sec YDOT = 7225
910209 meter/sec
ZDOT = 6779
457523 ZDOT = 2058
550251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14862397
89 X = -4530058
88
Y = -1247895
38 feet Y = -380358
51 meter
Z = -16255708
19 Z = -4954739
86
XDOT = -5485
534510 XDOT = -1671
990919
YDOT = -22633
639164 feet/sec YDOT = -6898
733217 meter/sec
ZDOT = 6750
500185 ZDOT = 2057
552456
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 07310
45837846
00020000 00000-0 20000-3 0 9117
2 25544 51
6340 90
2806 0001986 171
4985 188
6213 15
76279884 33221
Satellite: ISS
Catalog Number: 25544
Epoch time: 07310
45837846 = yrday
fracday
Element set: 911
Inclination: 51
6340 deg
RA of node: 90
2806 deg
Eccentricity:
0001986
Arg of perigee: 171
4985 deg
Mean anomaly: 188
6213 deg
Mean motion: 15
76279884 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3322
Checksum: 310
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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