Date:
January 8th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 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 2507)
---------------------------------------
Vector Time (GMT): 2007/005/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5346921
66 A = 6723860
34 meter
Y = -3915990
09 meter E =
0032620
Z = -1073380
03 I = 51
43116
XDOT = 2124
264270 Wp = 51
41167
YDOT = -4480
611548 meter/sec RA = 223
63854 deg
ZDOT = 5904
973656 TA = 296
78933
MA = 297
12264
Ha = 194
129 n
mi
Hp = 171
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17542393
89 X = -5297520
94
Y = -12847736
51 feet Y = -3975505
98 meter
Z = -3521588
03 Z = -1099235
35
XDOT = 6969
370963 XDOT = 2145
524562
YDOT = -14700
169120 feet/sec YDOT = -4456
738782 meter/sec
ZDOT = 19373
273150 ZDOT = 5915
344131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9108011
14 X = 2776121
79
Y = -19726861
32 feet Y = -6012747
33 meter
Z = -3618918
99 Z = -1103046
51
XDOT = 14332
437382 XDOT = 4368
526914
YDOT = 3138
431132 feet/sec YDOT = 956
593809 meter/sec
ZDOT = 19411
554003 ZDOT = 5916
641660
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 07005
49518404
00020000 00000-0 20000-3 0 9006
2 25544 51
6321 224
5513 0023416 56
5103 303
8295 15
76738722 25081
Satellite: ISS
Catalog Number: 25544
Epoch time: 07005
49518404 = yrday
fracday
Element set: 900
Inclination: 51
6321 deg
RA of node: 224
5513 deg
Eccentricity:
0023416
Arg of perigee: 56
5103 deg
Mean anomaly: 303
8295 deg
Mean motion: 15
76738722 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2508
Checksum: 269
Coasting Arc #2 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2007/006/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2489198
73 A = 6712176
05 meter
Y = 3386836
91 meter E =
0037279
Z = -5263869
61 I = 51
41262
XDOT = -6076
764940 Wp = 71
70456
YDOT = -4692
290194 meter/sec RA = 218
47668 deg
ZDOT = -134
756447 TA = 196
94648
MA = 197
07133
Ha = 194
110 n
mi
Hp = 171
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8166662
51 X = -2501315
47
Y = 11111669
65 feet Y = 3358934
14 meter
Z = -17269913
42 Z = -5275990
92
XDOT = -19936
892848 XDOT = -6023
188846
YDOT = -15394
652868 feet/sec YDOT = -4759
944386 meter/sec
ZDOT = -442
114329 ZDOT = -164
147103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12590589
04 X = -3837611
54
Y = -5484996
75 feet Y = -1671827
01 meter
Z = -17314888
58 Z = -5277578
04
XDOT = 10334
416102 XDOT = 3149
930028
YDOT = -21866
475759 feet/sec YDOT = -6664
901811 meter/sec
ZDOT = -552
801260 ZDOT = -168
493824
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 07006
50923285
00020000 00000-0 20000-3 0 9017
2 25544 51
6309 219
3199 0023339 60
4219 299
9268 15
76795720 25249
Satellite: ISS
Catalog Number: 25544
Epoch time: 07006
50923285 = yrday
fracday
Element set: 901
Inclination: 51
6309 deg
RA of node: 219
3199 deg
Eccentricity:
0023339
Arg of perigee: 60
4219 deg
Mean anomaly: 299
9268 deg
Mean motion: 15
76795720 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2524
Checksum: 308
Coasting Arc #3 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2007/007/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5167965
76 A = 6723866
68 meter
Y = 4220390
70 meter E =
0027530
Z = -865010
90 I = 51
47560
XDOT = -3637
166878 Wp = 85
97117
YDOT = 3269
075749 meter/sec RA = 213
31243 deg
ZDOT = -5940
571627 TA = 103
48743
MA = 103
18051
Ha = 194
114 n
mi
Hp = 171
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16955268
25 X = 5124590
64
Y = 13846426
17 feet Y = 4277939
32 meter
Z = -2837962
27 Z = -840010
43
XDOT = -11932
962198 XDOT = -3644
594207
YDOT = 10725
314136 feet/sec YDOT = 3228
361925 meter/sec
ZDOT = -19490
064392 ZDOT = -5958
258365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9523688
18 X = -2902820
16
Y = 19723837
73 feet Y = 6011825
74 meter
Z = -2743767
05 Z = -836300
20
XDOT = -11741
373249 XDOT = -3578
770566
YDOT = -8314
064364 feet/sec YDOT = -2534
126818 meter/sec
ZDOT = -19555
902654 ZDOT = -5960
639129
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 07007
52325624
00020000 00000-0 20000-3 0 9024
2 25544 51
6310 214
0896 0023264 64
3633 295
9931 15
76813357 25405
Satellite: ISS
Catalog Number: 25544
Epoch time: 07007
52325624 = yrday
fracday
Element set: 902
Inclination: 51
6310 deg
RA of node: 214
0896 deg
Eccentricity:
0023264
Arg of perigee: 64
3633 deg
Mean anomaly: 295
9931 deg
Mean motion: 15
76813357 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2540
Checksum: 281
Coasting Arc #4 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2007/008/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3858421
50 A = 6713260
37 meter
Y = -2388528
14 meter E =
0029024
Z = 4928211
85 I = 51
46485
XDOT = 5643
029314 Wp = 65
79734
YDOT = 4859
071147 meter/sec RA = 208
11682 deg
ZDOT = -2041
904295 TA = 44
07681
MA = 43
84582
Ha = 193
917 n
mi
Hp = 171
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12658863
17 X = 3860903
66
Y = -7836378
43 feet Y = -2345367
61 meter
Z = 16168674
06 Z = 4946961
59
XDOT = 18513
875703 XDOT = 5598
194118
YDOT = 15941
834472 feet/sec YDOT = 4921
924103 meter/sec
ZDOT = -6699
161073 ZDOT = -2014
599499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10720156
61 X = 3267503
73
Y = 10220932
78 feet Y = 3115340
31 meter
Z = 16238609
55 Z = 4949528
19
XDOT = -10073
527201 XDOT = -3070
411091
YDOT = 21155
150499 feet/sec YDOT = 6448
089872 meter/sec
ZDOT = -6596
239776 ZDOT = -2010
533884
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 07008
53725226
00020000 00000-0 20000-3 0 9039
2 25544 51
6308 208
8582 0023169 68
0336 292
3288 15
76873912 25566
Satellite: ISS
Catalog Number: 25544
Epoch time: 07008
53725226 = yrday
fracday
Element set: 903
Inclination: 51
6308 deg
RA of node: 208
8582 deg
Eccentricity:
0023169
Arg of perigee: 68
0336 deg
Mean anomaly: 292
3288 deg
Mean motion: 15
76873912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2556
Checksum: 307
Coasting Arc #5 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2007/009/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4526943
84 A = 6720910
64 meter
Y = -4188259
45 meter E =
0036831
Z = 2626221
02 I = 51
51590
XDOT = 5195
725417 Wp = 74
22282
YDOT = -2307
962385 meter/sec RA = 202
98711 deg
ZDOT = 5224
954829 TA = 315
81105
MA = 316
10465
Ha = 193
953 n
mi
Hp = 171
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14852177
96 X = -4492531
21
Y = -13741008
68 feet Y = -4238690
01 meter
Z = 8616210
70 Z = 2604312
76
XDOT = 17046
343231 XDOT = 5195
765699
YDOT = -7572
055068 feet/sec YDOT = -2249
861003 meter/sec
ZDOT = 17142
240253 ZDOT = 5250
195255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9288273
61 X = 2831065
80
Y = -18015201
62 feet Y = -5491033
46 meter
Z = 8533585
42 Z = 2601036
84
XDOT = 10490
182816 XDOT = 3197
407722
YDOT = 13652
436039 feet/sec YDOT = 4161
262505 meter/sec
ZDOT = 17236
506987 ZDOT = 5253
687330
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 07009
55122239
00020000 00000-0 20000-3 0 9048
2 25544 51
6299 203
6270 0023094 72
0547 288
3133 15
76929964 25729
Satellite: ISS
Catalog Number: 25544
Epoch time: 07009
55122239 = yrday
fracday
Element set: 904
Inclination: 51
6299 deg
RA of node: 203
6270 deg
Eccentricity:
0023094
Arg of perigee: 72
0547 deg
Mean anomaly: 288
3133 deg
Mean motion: 15
76929964 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2572
Checksum: 299
Coasting Arc #6 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2007/010/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5157429
49 A = 6716789
84 meter
Y = 1673801
35 meter E =
0029515
Z = -3986898
79 I = 51
52881
XDOT = -4572
254222 Wp = 83
65523
YDOT = -4757
620513 meter/sec RA = 197
77099 deg
ZDOT = 3945
423626 TA = 227
17624
MA = 227
42468
Ha = 193
921 n
mi
Hp = 170
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16920700
44 X = -5156395
44
Y = 5491474
25 feet Y = 1616134
14 meter
Z = -13080376
59 Z = -4011950
70
XDOT = -15000
834063 XDOT = -4537
879973
YDOT = -15608
991184 feet/sec YDOT = -4808
558064 meter/sec
ZDOT = 12944
303234 ZDOT = 3923
295030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10023500
93 X = -3055163
08
Y = -14612910
37 feet Y = -4454015
08 meter
Z = -13174024
60 Z = -4015442
70
XDOT = 9654
750510 XDOT = 2942
767956
YDOT = -18134
266449 feet/sec YDOT = -5527
324414 meter/sec
ZDOT = 12860
771808 ZDOT = 3919
963247
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 07010
50179685
00020000 00000-0 20000-3 0 9053
2 25544 51
6294 198
7221 0023197 75
6930 284
6808 15
76945319 25879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07010
50179685 = yrday
fracday
Element set: 905
Inclination: 51
6294 deg
RA of node: 198
7221 deg
Eccentricity:
0023197
Arg of perigee: 75
6930 deg
Mean anomaly: 284
6808 deg
Mean motion: 15
76945319 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2587
Checksum: 324
Coasting Arc #7 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2007/011/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3301322
14 A = 6716177
68 meter
Y = 4133283
61 meter E =
0031090
Z = -4168725
23 I = 51
55440
XDOT = -6559
971408 Wp = 77
41082
YDOT = 1531
611023 meter/sec RA = 192
65671 deg
ZDOT = -3692
897583 TA = 154
80236
MA = 154
65036
Ha = 193
925 n
mi
Hp = 170
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10831109
38 X = 3275108
59
Y = 13560641
77 feet Y = 4170054
57 meter
Z = -13676920
04 Z = -4152750
89
XDOT = -21522
215905 XDOT = -6558
671249
YDOT = 5024
970548 feet/sec YDOT = 1458
261310 meter/sec
ZDOT = -12115
805719 ZDOT = -3724
762430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9683700
75 X = -2951591
99
Y = 14459538
95 feet Y = 4407267
47 meter
Z = -13616524
91 Z = -4150316
79
XDOT = -10149
831784 XDOT = -3093
668728
YDOT = -18268
006937 feet/sec YDOT = -5568
088514 meter/sec
ZDOT = -12235
007251 ZDOT = -3729
230210
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 07011
51571606
00020000 00000-0 20000-3 0 9065
2 25544 51
6292 193
4907 0023288 79
4412 280
9374 15
76999283 26033
Satellite: ISS
Catalog Number: 25544
Epoch time: 07011
51571606 = yrday
fracday
Element set: 906
Inclination: 51
6292 deg
RA of node: 193
4907 deg
Eccentricity:
0023288
Arg of perigee: 79
4412 deg
Mean anomaly: 280
9374 deg
Mean motion: 15
76999283 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2603
Checksum: 310
Coasting Arc #8 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2007/012/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6193491
81 A = 6721026
40 meter
Y = -1067780
85 meter E =
0036259
Z = 2348504
71 I = 51
59970
XDOT = 2883
648422 Wp = 91
99867
YDOT = 4693
789982 meter/sec RA = 187
44619 deg
ZDOT = -5400
590801 TA = 61
47229
MA = 61
10772
Ha = 193
699 n
mi
Hp = 170
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20319855
02 X = 6193563
02
Y = -3503218
01 feet Y = -998521
58 meter
Z = 7705067
95 Z = 2378592
63
XDOT = 9460
788785 XDOT = 2857
182443
YDOT = 15399
573432 feet/sec YDOT = 4725
889033 meter/sec
ZDOT = -17718
473758 ZDOT = -5386
645984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9713570
27 X = 2960696
22
Y = 18140218
84 feet Y = 5529138
70 meter
Z = 7817680
58 Z = 2382829
04
XDOT = -10280
711756 XDOT = -3133
560943
YDOT = 13215
840789 feet/sec YDOT = 4028
188273 meter/sec
ZDOT = -17665
607749 ZDOT = -5384
477242
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 07012
52960664
00020000 00000-0 20000-3 0 9074
2 25544 51
6292 188
2586 0023009 83
0029 277
3752 15
77056758 26193
Satellite: ISS
Catalog Number: 25544
Epoch time: 07012
52960664 = yrday
fracday
Element set: 907
Inclination: 51
6292 deg
RA of node: 188
2586 deg
Eccentricity:
0023009
Arg of perigee: 83
0029 deg
Mean anomaly: 277
3752 deg
Mean motion: 15
77056758 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2619
Checksum: 309
Coasting Arc #9 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2007/013/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1653018
93 A = 6712335
36 meter
Y = -4073012
38 meter E =
0027384
Z = 5049900
38 I = 51
59800
XDOT = 7484
505156 Wp = 93
98832
YDOT = -995
797918 meter/sec RA = 182
31906 deg
ZDOT = 1637
345996 TA = 340
26902
MA = 340
37475
Ha = 193
887 n
mi
Hp = 170
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5423290
46 X = -1631882
47
Y = -13362901
50 feet Y = -4091379
70 meter
Z = 16567914
63 Z = 5041920
96
XDOT = 24555
463110 XDOT = 7487
130149
YDOT = -3267
053536 feet/sec YDOT = -912
087510 meter/sec
ZDOT = 5371
870066 ZDOT = 1673
711843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10780603
58 X = 3285927
97
Y = -9631471
85 feet Y = -2935672
62 meter
Z = 16537483
11 Z = 5040624
85
XDOT = 10506
751804 XDOT = 3202
457950
YDOT = 21271
048392 feet/sec YDOT = 6483
415550 meter/sec
ZDOT = 5508
030908 ZDOT = 1678
847821
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 07013
54347356
00020000 00000-0 20000-3 0 9085
2 25544 51
6285 183
0270 0023192 87
0532 273
3286 15
77051812 26356
Satellite: ISS
Catalog Number: 25544
Epoch time: 07013
54347356 = yrday
fracday
Element set: 908
Inclination: 51
6285 deg
RA of node: 183
0270 deg
Eccentricity:
0023192
Arg of perigee: 87
0532 deg
Mean anomaly: 273
3286 deg
Mean motion: 15
77051812 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2635
Checksum: 283
Coasting Arc #10 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2007/014/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6672477
97 A = 6723220
21 meter
Y = 670381
85 meter E =
0031725
Z = -425820
58 I = 51
66472
XDOT = -835
279031 Wp = 75
70693
YDOT = -4728
279063 meter/sec RA = 177
14085 deg
ZDOT = 6024
712368 TA = 279
65917
MA = 280
01742
Ha = 193
711 n
mi
Hp = 170
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21891331
91 X = -6677409
81
Y = 2199415
53 feet Y = 595738
97 meter
Z = -1397049
16 Z = -458247
21
XDOT = -2740
416767 XDOT = -811
611467
YDOT = -15512
726584 feet/sec YDOT = -4737
488031 meter/sec
ZDOT = 19766
116694 ZDOT = 6020
711508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9667531
95 X = -2946663
74
Y = -19754811
16 feet Y = -6021266
44 meter
Z = -1518502
49 Z = -462839
56
XDOT = 12114
835193 XDOT = 3692
601767
YDOT = -7358
711818 feet/sec YDOT = -2242
935362 meter/sec
ZDOT = 19750
511906 ZDOT = 6019
956029
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 07014
49394599
00020000 00000-0 20000-3 0 9092
2 25544 51
6291 178
1224 0023220 90
9977 269
3848 15
77117151 26500
Satellite: ISS
Catalog Number: 25544
Epoch time: 07014
49394599 = yrday
fracday
Element set: 909
Inclination: 51
6291 deg
RA of node: 178
1224 deg
Eccentricity:
0023220
Arg of perigee: 90
9977 deg
Mean anomaly: 269
3848 deg
Mean motion: 15
77117151 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2650
Checksum: 314
Coasting Arc #11 (Orbit 2665)
---------------------------------------
Vector Time (GMT): 2007/015/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -262001
27 A = 6711315
87 meter
Y = 4224184
22 meter E =
0038053
Z = -5241436
24 I = 51
65365
XDOT = -7625
415790 Wp = 95
42380
YDOT = 467
711390 meter/sec RA = 171
98071 deg
ZDOT = 759
299716 TA = 181
81383
MA = 181
82767
Ha = 193
684 n
mi
Hp = 170
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -859584
23 X = -283755
50
Y = 13858872
11 feet Y = 4221133
48 meter
Z = -17196313
11 Z = -5242761
28
XDOT = -25017
768339 XDOT = -7633
767578
YDOT = 1534
486188 feet/sec YDOT = 382
392945 meter/sec
ZDOT = 2491
140802 ZDOT = 722
235536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13188173
74 X = -4019755
36
Y = 4327480
17 feet Y = 1319015
96 meter
Z = -17200738
19 Z = -5242785
00
XDOT = -10215
552293 XDOT = -3113
700339
YDOT = -21798
171393 feet/sec YDOT = -6644
082641 meter/sec
ZDOT = 2352
261499 ZDOT = 716
969305
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 07015
50775684
00020000 00000-0 20000-3 0 9105
2 25544 51
6295 172
8906 0023258 94
7388 265
6434 15
77155358 26669
Satellite: ISS
Catalog Number: 25544
Epoch time: 07015
50775684 = yrday
fracday
Element set: 910
Inclination: 51
6295 deg
RA of node: 172
8906 deg
Eccentricity:
0023258
Arg of perigee: 94
7388 deg
Mean anomaly: 265
6434 deg
Mean motion: 15
77155358 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2666
Checksum: 326
Coasting Arc #12 (Orbit 2681)
---------------------------------------
Vector Time (GMT): 2007/016/11:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6491058
10 A = 6721737
97 meter
Y = -104442
66 meter E =
0029190
Z = -1742855
78 I = 51
71745
XDOT = -1430
334130 Wp = 109
00581
YDOT = 4963
410622 meter/sec RA = 166
84509 deg
ZDOT = -5711
238096 TA = 90
28202
MA = 89
94753
Ha = 193
584 n
mi
Hp = 170
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21296122
36 X = 6500209
93
Y = -342659
63 feet Y = -31804
60 meter
Z = -5718030
77 Z = -1711300
42
XDOT = -4692
697278 XDOT = -1457
985595
YDOT = 16284
155585 feet/sec YDOT = 4947
262078 meter/sec
ZDOT = -18737
657795 ZDOT = -5718
252990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8412560
54 X = 2564148
45
Y = 19601272
12 feet Y = 5974467
74 meter
Z = -5599738
87 Z = -1706800
41
XDOT = -15377
926318 XDOT = -4687
191942
YDOT = 1322
585477 feet/sec YDOT = 403
124053 meter/sec
ZDOT = -18763
322084 ZDOT = -5719
060571
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 07016
52153832
00020000 00000-0 20000-3 0 9114
2 25544 51
6293 167
6572 0023183 98
0956 262
2840 15
77223919 26824
Satellite: ISS
Catalog Number: 25544
Epoch time: 07016
52153832 = yrday
fracday
Element set: 911
Inclination: 51
6293 deg
RA of node: 167
6572 deg
Eccentricity:
0023183
Arg of perigee: 98
0956 deg
Mean anomaly: 262
2840 deg
Mean motion: 15
77223919 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2682
Checksum: 300
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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