Date:
February 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7104 18 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3139)
---------------------------------------
Vector Time (GMT): 2007/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6438841
56 A = 6720065
87 meter
Y = -1843786
37 meter E =
0027435
Z = 231946
18 I = 51
74772
XDOT = 1116
138125 Wp = 179
74703
YDOT = -4656
899281 meter/sec RA = 17
54381 deg
ZDOT = -6058
763712 TA = 357
72694
MA = 357
73938
Ha = 188
294 n
mi
Hp = 174
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21124808
27 X = -6418872
26
Y = -6049167
87 feet Y = -1915677
44 meter
Z = 760978
29 Z = 200715
53
XDOT = 3661
870490 XDOT = 1197
560880
YDOT = -15278
540947 feet/sec YDOT = -4643
962441 meter/sec
ZDOT = -19877
833700 ZDOT = -6053
144119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13355064
05 X = -4070623
52
Y = -17454433
88 feet Y = -5320111
45 meter
Z = 643464
47 Z = 196127
97
XDOT = 10865
489331 XDOT = 3311
801148
YDOT = -9042
190366 feet/sec YDOT = -2756
059624 meter/sec
ZDOT = -19857
290305 ZDOT = -6052
502085
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 07045
53203413
00020000 00000-0 20000-3 0 9006
2 25544 51
6324 17
8717 0021000 206
5229 153
4863 15
78266123 31402
Satellite: ISS
Catalog Number: 25544
Epoch time: 07045
53203413 = yrday
fracday
Element set: 900
Inclination: 51
6324 deg
RA of node: 17
8717 deg
Eccentricity:
0021000
Arg of perigee: 206
5229 deg
Mean anomaly: 153
4863 deg
Mean motion: 15
78266123 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3140
Checksum: 250
Coasting Arc #2 (Orbit 3155)
---------------------------------------
Vector Time (GMT): 2007/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2337306
43 A = 6708539
17 meter
Y = 3638812
34 meter E =
0017032
Z = 5131193
74 I = 51
68134
XDOT = -7101
691699 Wp = 203
79524
YDOT = -2661
541994 meter/sec RA = 12
37166 deg
ZDOT = -1364
303304 TA = 259
15074
MA = 259
34247
Ha = 188
065 n
mi
Hp = 174
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7668328
19 X = -2402748
08
Y = 11938360
71 feet Y = 3612309
21 meter
Z = 16834625
13 Z = 5119680
62
XDOT = -23299
513447 XDOT = -7064
774816
YDOT = -8732
093155 feet/sec YDOT = -2740
750617 meter/sec
ZDOT = -4476
060709 ZDOT = -1398
712670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13262182
53 X = -4042313
24
Y = 5184730
41 feet Y = 1580305
83 meter
Z = 16791825
45 Z = 5118148
40
XDOT = -13457
021415 XDOT = -4101
700127
YDOT = -19685
514801 feet/sec YDOT = -6000
144911 meter/sec
ZDOT = -4605
619172 ZDOT = -1403
792724
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 07046
54510433
00020000 00000-0 20000-3 0 9012
2 25544 51
6325 12
6355 0021008 210
5004 149
4941 15
78290762 31563
Satellite: ISS
Catalog Number: 25544
Epoch time: 07046
54510433 = yrday
fracday
Element set: 901
Inclination: 51
6325 deg
RA of node: 12
6355 deg
Eccentricity:
0021008
Arg of perigee: 210
5004 deg
Mean anomaly: 149
4941 deg
Mean motion: 15
78290762 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3156
Checksum: 257
Coasting Arc #3 (Orbit 3171)
---------------------------------------
Vector Time (GMT): 2007/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5588824
52 A = 6716875
90 meter
Y = 2738775
60 meter E =
0014424
Z = 2546858
77 I = 51
68271
XDOT = -4216
443764 Wp = 173
33283
YDOT = 3674
051498 meter/sec RA = 7
23968 deg
ZDOT = 5284
603426 TA = 215
52970
MA = 215
62583
Ha = 187
729 n
mi
Hp = 174
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18336038
45 X = 5545412
01
Y = 8985484
24 feet Y = 2801030
21 meter
Z = 8355835
85 Z = 2573902
93
XDOT = -13833
476916 XDOT = -4282
884949
YDOT = 12053
974730 feet/sec YDOT = 3626
529363 meter/sec
ZDOT = 17337
937749 ZDOT = 5263
959259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9942555
72 X = 3030490
98
Y = 17787111
19 feet Y = 5421511
49 meter
Z = 8457747
16 Z = 2577921
33
XDOT = -17014
751394 XDOT = -5186
096225
YDOT = 1277
037738 feet/sec YDOT = 389
241102 meter/sec
ZDOT = 17260
849256 ZDOT = 5261
106853
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 07047
55814958
00020000 00000-0 20000-3 0 9024
2 25544 51
6331 7
3984 0021145 214
3854 145
5944 15
78370177 31723
Satellite: ISS
Catalog Number: 25544
Epoch time: 07047
55814958 = yrday
fracday
Element set: 902
Inclination: 51
6331 deg
RA of node: 7
3984 deg
Eccentricity:
0021145
Arg of perigee: 214
3854 deg
Mean anomaly: 145
5944 deg
Mean motion: 15
78370177 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3172
Checksum: 299
Coasting Arc #4 (Orbit 3186)
---------------------------------------
Vector Time (GMT): 2007/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4855362
65 A = 6713855
55 meter
Y = -2776399
70 meter E =
0019087
Z = -3722892
39 I = 51
64367
XDOT = 5327
490414 Wp = 202
02878
YDOT = 3565
272125 meter/sec RA = 2
02353 deg
ZDOT = 4264
782711 TA = 113
01176
MA = 112
81033
Ha = 187
454 n
mi
Hp = 175
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15929667
50 X = 4904132
44
Y = -9108922
90 feet Y = -2721831
75 meter
Z = -12214213
88 Z = -3699187
28
XDOT = 17478
643092 XDOT = 5266
510224
YDOT = 11697
087024 feet/sec YDOT = 3624
506265 meter/sec
ZDOT = 13992
069262 ZDOT = 4290
514586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18364253
66 X = 5597424
52
Y = 1280514
35 feet Y = 390300
77 meter
Z = -12125521
60 Z = -3695858
98
XDOT = 8098
226800 XDOT = 2468
339529
YDOT = 18039
217097 feet/sec YDOT = 5498
353371 meter/sec
ZDOT = 14089
157634 ZDOT = 4294
375247
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 07048
50786147
00020000 00000-0 20000-3 0 9039
2 25544 51
6333 2
4887 0020949 218
3497 141
6180 15
78354273 31875
Satellite: ISS
Catalog Number: 25544
Epoch time: 07048
50786147 = yrday
fracday
Element set: 903
Inclination: 51
6333 deg
RA of node: 2
4887 deg
Eccentricity:
0020949
Arg of perigee: 218
3497 deg
Mean anomaly: 141
6180 deg
Mean motion: 15
78354273 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3187
Checksum: 306
Coasting Arc #5 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2007/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3439135
18 A = 6710289
95 meter
Y = -3462076
81 meter E =
0012518
Z = -4596960
34 I = 51
60470
XDOT = 6610
465367 Wp = 197
91838
YDOT = -2685
290063 meter/sec RA = 356
90183 deg
ZDOT = -2932
765780 TA = 43
11332
MA = 43
01535
Ha = 187
014 n
mi
Hp = 175
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11283251
91 X = -3377835
59
Y = -11358519
72 feet Y = -3500192
66 meter
Z = -15081890
88 Z = -4613518
08
XDOT = 21687
878501 XDOT = 6654
247797
YDOT = -8810
006769 feet/sec YDOT = -2611
123515 meter/sec
ZDOT = -9621
934974 ZDOT = -2900
546578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3298872
96 X = -1005496
48
Y = -15606165
01 feet Y = -4756759
09 meter
Z = -15144511
46 Z = -4616047
09
XDOT = 21919
796726 XDOT = 6681
154042
YDOT = 4556
242414 feet/sec YDOT = 1388
742688 meter/sec
ZDOT = -9501
257831 ZDOT = -2895
983387
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 07049
52086381
00020000 00000-0 20000-3 0 9046
2 25544 51
6343 357
2518 0020916 222
2417 137
7138 15
78416746 32030
Satellite: ISS
Catalog Number: 25544
Epoch time: 07049
52086381 = yrday
fracday
Element set: 904
Inclination: 51
6343 deg
RA of node: 357
2518 deg
Eccentricity:
0020916
Arg of perigee: 222
2417 deg
Mean anomaly: 137
7138 deg
Mean motion: 15
78416746 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3203
Checksum: 288
Coasting Arc #6 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2007/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6329406
09 A = 6719035
20 meter
Y = 1870469
48 meter E =
0022301
Z = 1182287
44 I = 51
60612
XDOT = -2386
825872 Wp = 188
20172
YDOT = -4372
668170 meter/sec RA = 351
69715 deg
ZDOT = -5895
269660 TA = 338
79677
MA = 338
88906
Ha = 186
838 n
mi
Hp = 175
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20765768
02 X = -6355594
74
Y = 6136710
89 feet Y = 1799544
18 meter
Z = 3878895
82 Z = 1151476
16
XDOT = -7830
793544 XDOT = -2309
115185
YDOT = -14346
024181 feet/sec YDOT = -4398
924914 meter/sec
ZDOT = -19341
435891 ZDOT = -5906
675520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20913014
56 X = -6374286
84
Y = -5692516
08 feet Y = -1735078
90 meter
Z = 3763410
33 Z = 1147087
47
XDOT = 545
070397 XDOT = 166
137457
YDOT = -14739
304437 feet/sec YDOT = -4492
539992 meter/sec
ZDOT = -19384
821601 ZDOT = -5908
493624
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 07050
53384363
00020000 00000-0 20000-3 0 9051
2 25544 51
6349 352
0155 0020945 226
0288 133
9151 15
78429734 32197
Satellite: ISS
Catalog Number: 25544
Epoch time: 07050
53384363 = yrday
fracday
Element set: 905
Inclination: 51
6349 deg
RA of node: 352
0155 deg
Eccentricity:
0020945
Arg of perigee: 226
0288 deg
Mean anomaly: 133
9151 deg
Mean motion: 15
78429734 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3219
Checksum: 290
Coasting Arc #7 (Orbit 3234)
---------------------------------------
Vector Time (GMT): 2007/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 599681
04 A = 6707366
72 meter
Y = 4144712
98 meter E =
0018605
Z = 5250288
52 I = 51
53925
XDOT = -7539
587353 Wp = 226
70778
YDOT = 1518
859693 meter/sec RA = 346
53158 deg
ZDOT = -351
184768 TA = 226
55426
MA = 226
70919
Ha = 186
410 n
mi
Hp = 175
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1967457
47 X = 527785
17
Y = 13598139
70 feet Y = 4151017
33 meter
Z = 17225356
03 Z = 5253026
79
XDOT = -24736
178979 XDOT = -7554
305140
YDOT = 4983
135476 feet/sec YDOT = 1434
465500 meter/sec
ZDOT = -1152
180997 ZDOT = -387
847317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5330561
79 X = -1624755
23
Y = 12648836
70 feet Y = 3855365
43 meter
Z = 17236160
36 Z = 5253581
68
XDOT = -22886
987116 XDOT = -6975
953673
YDOT = -7947
298830 feet/sec YDOT = -2422
336683 meter/sec
ZDOT = -1289
681059 ZDOT = -393
094787
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 07051
54679847
00020000 00000-0 20000-3 0 9068
2 25544 51
6349 346
7791 0020976 230
3025 129
6291 15
78497887 32353
Satellite: ISS
Catalog Number: 25544
Epoch time: 07051
54679847 = yrday
fracday
Element set: 906
Inclination: 51
6349 deg
RA of node: 346
7791 deg
Eccentricity:
0020976
Arg of perigee: 230
3025 deg
Mean anomaly: 129
6291 deg
Mean motion: 15
78497887 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3235
Checksum: 333
Coasting Arc #8 (Orbit 3250)
---------------------------------------
Vector Time (GMT): 2007/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6444862
54 A = 6717895
64 meter
Y = -670098
96 meter E =
0007700
Z = 1792515
40 I = 51
54724
XDOT = -1044
802423 Wp = 210
78585
YDOT = 5101
739095 meter/sec RA = 341
37399 deg
ZDOT = 5667
903979 TA = 169
11936
MA = 169
10269
Ha = 186
133 n
mi
Hp = 175
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21144562
15 X = 6443169
08
Y = -2198487
41 feet Y = -598038
28 meter
Z = 5880956
04 Z = 1823820
08
XDOT = -3427
829473 XDOT = -1129
306466
YDOT = 16737
989158 feet/sec YDOT = 5089
583350 meter/sec
ZDOT = 18595
485496 ZDOT = 5662
622859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19426943
92 X = 5921332
51
Y = 8551262
89 feet Y = 2606424
93 meter
Z = 5998437
50 Z = 1828323
75
XDOT = -10737
355445 XDOT = -3272
745940
YDOT = 11372
156392 feet/sec YDOT = 3466
233268 meter/sec
ZDOT = 18576
291567 ZDOT = 5662
053670
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 07052
55973149
00020000 00000-0 20000-3 0 9073
2 25544 51
6346 341
5409 0020941 234
1617 125
7603 15
78516631 32511
Satellite: ISS
Catalog Number: 25544
Epoch time: 07052
55973149 = yrday
fracday
Element set: 907
Inclination: 51
6346 deg
RA of node: 341
5409 deg
Eccentricity:
0020941
Arg of perigee: 234
1617 deg
Mean anomaly: 125
7603 deg
Mean motion: 15
78516631 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3251
Checksum: 286
Coasting Arc #9 (Orbit 3265)
---------------------------------------
Vector Time (GMT): 2007/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2307663
55 A = 6711512
12 meter
Y = -4685850
85 meter E =
0017191
Z = -4214982
06 I = 51
49940
XDOT = 6817
754258 Wp = 214
98791
YDOT = 108
936679 meter/sec RA = 336
15282 deg
ZDOT = 3590
462977 TA = 91
64801
MA = 91
45109
Ha = 185
817 n
mi
Hp = 175
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7571074
65 X = 2380365
31
Y = -15373526
41 feet Y = -4659638
89 meter
Z = -13828681
31 Z = -4203594
82
XDOT = 22367
960165 XDOT = 6798
587758
YDOT = 357
403801 feet/sec YDOT = 185
069552 meter/sec
ZDOT = 11779
734177 ZDOT = 3623
536735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14093982
10 X = 4295845
74
Y = -9807698
44 feet Y = -2989386
48 meter
Z = -13786501
82 Z = -4202125
75
XDOT = 18672
040436 XDOT = 5691
237925
YDOT = 10001
606516 feet/sec YDOT = 3048
489666 meter/sec
ZDOT = 11903
956173 ZDOT = 3628
325841
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 07053
50933441
00020000 00000-0 20000-3 0 9081
2 25544 51
6349 336
6305 0020911 237
7728 122
1411 15
78559957 32665
Satellite: ISS
Catalog Number: 25544
Epoch time: 07053
50933441 = yrday
fracday
Element set: 908
Inclination: 51
6349 deg
RA of node: 336
6305 deg
Eccentricity:
0020911
Arg of perigee: 237
7728 deg
Mean anomaly: 122
1411 deg
Mean motion: 15
78559957 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3266
Checksum: 298
Coasting Arc #10 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2007/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5132428
05 A = 6711261
88 meter
Y = -978834
73 meter E =
0012566
Z = -4198586
59 I = 51
47406
XDOT = 4010
187040 Wp = 236
17295
YDOT = -5512
084269 meter/sec RA = 331
02208 deg
ZDOT = -3616
265617 TA = 357
02168
MA = 357
02915
Ha = 185
315 n
mi
Hp = 175
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16838674
72 X = -5100705
37
Y = -3211400
03 feet Y = -1036051
05 meter
Z = -13774890
39 Z = -4223442
60
XDOT = 13156
781628 XDOT = 4089
092887
YDOT = -18084
265975 feet/sec YDOT = -5466
798946 meter/sec
ZDOT = -11864
388506 ZDOT = -3596
592658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13342111
55 X = -4066675
60
Y = -10642288
22 feet Y = -3243769
45 meter
Z = -13868360
49 Z = -4227076
28
XDOT = 19342
914372 XDOT = 5895
720301
YDOT = -8881
034039 feet/sec YDOT = -2706
939175 meter/sec
ZDOT = -11791
191526 ZDOT = -3593
955177
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 07054
52222153
00020000 00000-0 20000-3 0 9096
2 25544 51
6354 331
3932 0020854 241
8225 118
0834 15
78605992 32825
Satellite: ISS
Catalog Number: 25544
Epoch time: 07054
52222153 = yrday
fracday
Element set: 909
Inclination: 51
6354 deg
RA of node: 331
3932 deg
Eccentricity:
0020854
Arg of perigee: 241
8225 deg
Mean anomaly: 118
0834 deg
Mean motion: 15
78605992 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3282
Checksum: 283
Coasting Arc #11 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2007/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4403755
26 A = 6717708
53 meter
Y = 4730138
74 meter E =
0015832
Z = 1804193
86 I = 51
47093
XDOT = -4722
719166 Wp = 202
50136
YDOT = -2246
771879 meter/sec RA = 325
79716 deg
ZDOT = -5667
656845 TA = 317
39520
MA = 317
51791
Ha = 185
226 n
mi
Hp = 175
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14448015
94 X = -4465085
38
Y = 15518827
88 feet Y = 4680550
54 meter
Z = 5919271
18 Z = 1782651
81
XDOT = -15494
485452 XDOT = -4669
712362
YDOT = -7371
298816 feet/sec YDOT = -2299
287497 meter/sec
ZDOT = -18594
674689 ZDOT = -5690
470786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19915490
89 X = -6070241
62
Y = 7341443
98 feet Y = 2237672
12 meter
Z = 5838953
45 Z = 1779713
01
XDOT = -9891
442824 XDOT = -3014
911773
YDOT = -12056
734512 feet/sec YDOT = -3674
892679 meter/sec
ZDOT = -18680
636200 ZDOT = -5693
857914
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 07055
53508611
00020000 00000-0 20000-3 0 9106
2 25544 51
6352 326
1554 0020914 245
5297 114
3687 15
78609338 32982
Satellite: ISS
Catalog Number: 25544
Epoch time: 07055
53508611 = yrday
fracday
Element set: 910
Inclination: 51
6352 deg
RA of node: 326
1554 deg
Eccentricity:
0020914
Arg of perigee: 245
5297 deg
Mean anomaly: 114
3687 deg
Mean motion: 15
78609338 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3298
Checksum: 300
Coasting Arc #12 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2007/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2931513
75 A = 6706806
84 meter
Y = 3007505
72 meter E =
0018997
Z = 5244141
09 I = 51
41211
XDOT = -5780
744891 Wp = 245
00024
YDOT = 5070
095152 meter/sec RA = 320
63096 deg
ZDOT = 316
777806 TA = 201
94032
MA = 202
02177
Ha = 184
843 n
mi
Hp = 175
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9617827
26 X = 2872190
89
Y = 9867144
77 feet Y = 3039955
73 meter
Z = 17205187
29 Z = 5258238
10
XDOT = -18965
698462 XDOT = -5838
548606
YDOT = 16634
170445 feet/sec YDOT = 5005
128431 meter/sec
ZDOT = 1039
297264 ZDOT = 288
555173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4287302
46 X = 1306769
79
Y = 13024766
33 feet Y = 3969948
78 meter
Z = 17258508
52 Z = 5260393
40
XDOT = -23365
434618 XDOT = -7121
784472
YDOT = 6423
206053 feet/sec YDOT = 1957
793205 meter/sec
ZDOT = 933
927039 ZDOT = 284
660961
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 07056
54792524
00020000 00000-0 20000-3 0 9117
2 25544 51
6354 320
9170 0021013 249
7294 110
1613 15
78689441 33149
Satellite: ISS
Catalog Number: 25544
Epoch time: 07056
54792524 = yrday
fracday
Element set: 911
Inclination: 51
6354 deg
RA of node: 320
9170 deg
Eccentricity:
0021013
Arg of perigee: 249
7294 deg
Mean anomaly: 110
1613 deg
Mean motion: 15
78689441 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3314
Checksum: 278
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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