Date:
January 20th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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
022/09:06:27
018 1
5 3
3 3
3
N/A 2
7 0
0 185
6
000/00:00:54
036 1
2 0
0 179
8
024/09:02:55
202 -4
6 8
5 8
5
N/A -6
9 0
0 188
0
000/00:02:20
404 -2
2 0
1 183
7
Coasting Arc #1 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2010/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -779371
38 A = 6719978
80 meter
Y = -6313267
94 meter E =
0002439
Z = -2171336
29 I = 51
32674
XDOT = 4816
926899 Wp = 141
34976
YDOT = -2476
448439 meter/sec RA = 278
81749 deg
ZDOT = 5472
854168 TA = 194
20830
MA = 194
21516
Ha = 185
281 n
mi
Hp = 178
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2556992
72 X = -698169
66
Y = -20712821
34 feet Y = -6321529
22 meter
Z = -7123806
72 Z = -2174925
43
XDOT = 15803
565940 XDOT = 4817
675445
YDOT = -8124
830838 feet/sec YDOT = -2422
578769 meter/sec
ZDOT = 17955
558295 ZDOT = 5496
255979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17310103
23 X = 5276119
46
Y = -11649659
93 feet Y = -3550816
35 meter
Z = -7138175
63 Z = -2175715
93
XDOT = 13519
147247 XDOT = 4120
636081
YDOT = 9032
035952 feet/sec YDOT = 2752
964558 meter/sec
ZDOT = 18048
175604 ZDOT = 5501
083924
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 10018
50429993
00016717 00000-0 10270-3 0 9008
2 25544 51
6454 279
5422 0007034 202
0697 158
0167 15
77564762 39895
Satellite: ISS
Catalog Number: 25544
Epoch time: 10018
50429993 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 279
5422 deg
Eccentricity:
0007034
Arg of perigee: 202
0697 deg
Mean anomaly: 158
0167 deg
Mean motion: 15
77564762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 327
Coasting Arc #2 (Orbit 4004)
---------------------------------------
Vector Time (GMT): 2010/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4195036
00 A = 6710390
32 meter
Y = 1048086
53 meter E =
0011774
Z = -5140384
88 I = 51
29099
XDOT = -460
606242 Wp = 109
58272
YDOT = -7594
679682 meter/sec RA = 273
66099 deg
ZDOT = -1178
683807 TA = 149
13808
MA = 149
06882
Ha = 185
020 n
mi
Hp = 178
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13763241
46 X = -4181473
53
Y = 3438604
09 feet Y = 1001251
14 meter
Z = -16864779
80 Z = -5160730
99
XDOT = -1511
175335 XDOT = -369
921240
YDOT = -24916
928090 feet/sec YDOT = -7599
323371 meter/sec
ZDOT = -3867
072856 ZDOT = -1180
701348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9451101
35 X = -2880695
69
Y = -10450074
99 feet Y = -3185182
86 meter
Z = -16945330
55 Z = -5164936
75
XDOT = 20539
008848 XDOT = 6260
289897
YDOT = -12323
855808 feet/sec YDOT = -3756
311250 meter/sec
ZDOT = -3875
261639 ZDOT = -1181
179747
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 10019
51784393
00016717 00000-0 10270-3 0 9019
2 25544 51
6454 274
3100 0006941 206
5622 153
5188 15
77572536 40055
Satellite: ISS
Catalog Number: 25544
Epoch time: 10019
51784393 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 274
3100 deg
Eccentricity:
0006941
Arg of perigee: 206
5622 deg
Mean anomaly: 153
5188 deg
Mean motion: 15
77572536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 298
Coasting Arc #3 (Orbit 4020)
---------------------------------------
Vector Time (GMT): 2010/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 50461
11 A = 6722196
21 meter
Y = 6710227
72 meter E =
0015520
Z = -161382
34 I = 51
32938
XDOT = -4820
899332 Wp = 162
30582
YDOT = -104
501824 meter/sec RA = 268
46630 deg
ZDOT = -6018
141318 TA = 19
45883
MA = 19
39965
Ha = 185
054 n
mi
Hp = 179
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 165554
81 X = -23793
64
Y = 22015182
81 feet Y = 6710376
83 meter
Z = -529469
61 Z = -161317
41
XDOT = -15816
598859 XDOT = -4790
137903
YDOT = -342
853753 feet/sec YDOT = -158
239840 meter/sec
ZDOT = -19744
558129 ZDOT = -6041
486154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19175355
14 X = -5844648
25
Y = 10816741
90 feet Y = 3296942
93 meter
Z = -529027
79 Z = -161247
67
XDOT = -6519
825638 XDOT = -1987
242854
YDOT = -12501
607708 feet/sec YDOT = -3810
490029 meter/sec
ZDOT = -19837
016823 ZDOT = -6046
322728
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 10020
53138921
00016717 00000-0 10270-3 0 9024
2 25544 51
6452 269
0780 0007116 210
1764 149
8992 15
77511552 40211
Satellite: ISS
Catalog Number: 25544
Epoch time: 10020
53138921 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 269
0780 deg
Eccentricity:
0007116
Arg of perigee: 210
1764 deg
Mean anomaly: 149
8992 deg
Mean motion: 15
77511552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4021
Checksum: 289
Coasting Arc #4 (Orbit 4036)
---------------------------------------
Vector Time (GMT): 2010/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4230390
04 A = 6710651
46 meter
Y = 1217829
20 meter E =
0002854
Z = 5064466
19 I = 51
29325
XDOT = -343
738177 Wp = 184
16685
YDOT = 7546
149408 meter/sec RA = 263
26531 deg
ZDOT = -1530
326486 TA = 280
55734
MA = 280
58950
Ha = 184
604 n
mi
Hp = 179
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13879232
43 X = 4191855
69
Y = 3995502
61 feet Y = 1264920
35 meter
Z = 16615702
73 Z = 5084923
60
XDOT = -1127
749924 XDOT = -420
661047
YDOT = 24757
708030 feet/sec YDOT = 7541
875460 meter/sec
ZDOT = -5020
756187 ZDOT = -1532
183015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3423827
41 X = 1043582
59
Y = 13934644
88 feet Y = 4247279
76 meter
Z = 16696759
83 Z = 5089172
40
XDOT = -20978
915418 XDOT = -6394
373419
YDOT = 11167
956042 feet/sec YDOT = 3403
993002 meter/sec
ZDOT = -5027
893152 ZDOT = -1532
501833
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 10021
54493109
00016717 00000-0 10270-3 0 9039
2 25544 51
6452 263
8456 0006960 216
0676 144
0021 15
77590112 40372
Satellite: ISS
Catalog Number: 25544
Epoch time: 10021
54493109 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 263
8456 deg
Eccentricity:
0006960
Arg of perigee: 216
0676 deg
Mean anomaly: 144
0021 deg
Mean motion: 15
77590112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4037
Checksum: 285
Coasting Arc #5 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/022/09:06:54
036
Vector Time (MET): N/A
Weight (LBS) : 751544
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3155640
71 A = 6713953
13 meter
Y = -3565867
60 meter E =
0009145
Z = 4732574
08 I = 51
30064
XDOT = 3383
836320 Wp = 150
16913
YDOT = 6426
014012 meter/sec RA = 258
73514 deg
ZDOT = 2575
549975 TA = 274
42060
MA = 274
52508
Ha = 185
580 n
mi
Hp = 179
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10353151
94 X = 3172290
57
Y = -11699040
68 feet Y = -3530486
40 meter
Z = 15526817
84 Z = 4747944
37
XDOT = 11101
825198 XDOT = 3299
216566
YDOT = 21082
723136 feet/sec YDOT = 6463
380864 meter/sec
ZDOT = 8449
967111 ZDOT = 2591
783142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9214760
00 X = 2808658
85
Y = 12540041
01 feet Y = 3822204
50 meter
Z = 15587589
61 Z = 4751097
31
XDOT = -22053
646968 XDOT = -6721
951596
YDOT = 5581
454562 feet/sec YDOT = 1701
227351 meter/sec
ZDOT = 8514
449355 ZDOT = 2595
204163
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 10022
43180898
00016717 00000-0 10270-3 0 9047
2 25544 51
6436 259
2670 0004699 204
5300 155
5642 15
76944444 40516
Satellite: ISS
Catalog Number: 25544
Epoch time: 10022
43180898 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 259
2670 deg
Eccentricity:
0004699
Arg of perigee: 204
5300 deg
Mean anomaly: 155
5642 deg
Mean motion: 15
76944444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 307
Coasting Arc #6 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2010/023/09:06:54
036
Vector Time (MET): N/A
Weight (LBS) : 751544
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2857289
32 A = 6723076
97 meter
Y = -5939445
33 meter E =
0004369
Z = -1318798
64 I = 51
33874
XDOT = 3917
934039 Wp = 46
00932
YDOT = -3174
077659 meter/sec RA = 253
52080 deg
ZDOT = 5821
420001 TA = 299
43821
MA = 299
48180
Ha = 185
514 n
mi
Hp = 179
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9374308
80 X = -2784254
60
Y = -19486369
21 feet Y = -5970988
82 meter
Z = -4326767
19 Z = -1332502
09
XDOT = 12854
114301 XDOT = 3924
856754
YDOT = -10413
640615 feet/sec YDOT = -3130
226538 meter/sec
ZDOT = 19099
146986 ZDOT = 5840
469864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20954349
38 X = 6386885
69
Y = -5295026
04 feet Y = -1613923
94 meter
Z = -4381221
97 Z = -1335396
46
XDOT = 7290
839504 XDOT = 2222
247881
YDOT = 13027
129035 feet/sec YDOT = 3970
668930 meter/sec
ZDOT = 19174
505386 ZDOT = 5844
389242
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 10023
38238128
00016717 00000-0 10270-3 0 9053
2 25544 51
6439 254
3642 0004591 209
0124 151
0786 15
76926337 40666
Satellite: ISS
Catalog Number: 25544
Epoch time: 10023
38238128 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 254
3642 deg
Eccentricity:
0004591
Arg of perigee: 209
0124 deg
Mean anomaly: 151
0786 deg
Mean motion: 15
76926337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 303
Coasting Arc #7 (Orbit 4081)
---------------------------------------
Vector Time (GMT): 2010/024/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3148188
24 A = 6717032
91 meter
Y = 3082533
28 meter E =
0005737
Z = -5073394
48 I = 51
31362
XDOT = -3881
997165 Wp = 124
37158
YDOT = -6472
420849 meter/sec RA = 248
37620 deg
ZDOT = -1528
095563 TA = 130
92565
MA = 130
87597
Ha = 188
046 n
mi
Hp = 183
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10328701
58 X = -3157778
24
Y = 10113298
15 feet Y = 3047275
05 meter
Z = -16644995
02 Z = -5088711
38
XDOT = -12736
211170 XDOT = -3801
909734
YDOT = -21234
976539 feet/sec YDOT = -6515
383756 meter/sec
ZDOT = -5013
436885 ZDOT = -1546
760023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7939972
35 X = -2420103
57
Y = -11995723
88 feet Y = -3656296
64 meter
Z = -16705573
40 Z = -5091858
77
XDOT = 22419
215878 XDOT = 6833
376999
YDOT = -7774
334378 feet/sec YDOT = -2369
617119 meter/sec
ZDOT = -5087
565145 ZDOT = -1550
689856
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 10024
39633086
00016717 00000-0 10270-3 0 9068
2 25544 51
6446 249
1349 0010662 235
5625 124
4532 15
75352391 40829
Satellite: ISS
Catalog Number: 25544
Epoch time: 10024
39633086 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 249
1349 deg
Eccentricity:
0010662
Arg of perigee: 235
5625 deg
Mean anomaly: 124
4532 deg
Mean motion: 15
75352391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 301
Coasting Arc #8 (Orbit 4097)
---------------------------------------
Vector Time (GMT): 2010/025/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3619188
45 A = 6728109
86 meter
Y = 5591214
81 meter E =
0013566
Z = 885765
84 I = 51
36262
XDOT = -3646
865965 Wp = 172
07364
YDOT = 3300
304156 meter/sec RA = 243
18755 deg
ZDOT = -5934
080509 TA = 358
20991
MA = 358
21477
Ha = 187
965 n
mi
Hp = 183
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11873977
86 X = 3552094
66
Y = 18343880
62 feet Y = 5631311
51 meter
Z = 2906055
91 Z = 903185
18
XDOT = -11964
783350 XDOT = -3654
673077
YDOT = 10827
769540 feet/sec YDOT = 3259
479562 meter/sec
ZDOT = -19468
768073 ZDOT = -5951
815526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20150976
54 X = -6142017
65
Y = 8427371
75 feet Y = 2568662
91 meter
Z = 2975234
03 Z = 906851
33
XDOT = -7947
482228 XDOT = -2422
392583
YDOT = -12108
193484 feet/sec YDOT = -3690
577374 meter/sec
ZDOT = -19538
923287 ZDOT = -5955
463818
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 10025
41130443
00016717 00000-0 10270-3 0 9072
2 25544 51
6444 243
9128 0010751 239
1244 120
8863 15
75305552 40981
Satellite: ISS
Catalog Number: 25544
Epoch time: 10025
41130443 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 243
9128 deg
Eccentricity:
0010751
Arg of perigee: 239
1244 deg
Mean anomaly: 120
8863 deg
Mean motion: 15
75305552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 287
Coasting Arc #9 (Orbit 4113)
---------------------------------------
Vector Time (GMT): 2010/026/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3258825
28 A = 6716329
67 meter
Y = -2682693
45 meter E =
0009184
Z = 5230747
19 I = 51
33803
XDOT = 4393
967120 Wp = 230
95897
YDOT = 6301
720277 meter/sec RA = 238
03439 deg
ZDOT = 489
334340 TA = 214
34183
MA = 214
40123
Ha = 187
609 n
mi
Hp = 184
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10691683
98 X = 3263171
73
Y = -8801487
71 feet Y = -2646227
54 meter
Z = 17161244
05 Z = 5246588
65
XDOT = 14415
902626 XDOT = 4320
796535
YDOT = 20674
935291 feet/sec YDOT = 6350
447051 meter/sec
ZDOT = 1605
427626 ZDOT = 510
502839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6995408
62 X = 2132200
55
Y = 11861169
11 feet Y = 3615284
35 meter
Z = 17223922
75 Z = 5249851
65
XDOT = -21846
608620 XDOT = -6658
846307
YDOT = 10406
855999 feet/sec YDOT = 3172
009709 meter/sec
ZDOT = 1689
493002 ZDOT = 514
957467
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 10026
42627553
00016717 00000-0 10270-3 0 9088
2 25544 51
6444 238
6905 0010772 243
9165 116
0891 15
75354315 41141
Satellite: ISS
Catalog Number: 25544
Epoch time: 10026
42627553 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 238
6905 deg
Eccentricity:
0010772
Arg of perigee: 243
9165 deg
Mean anomaly: 116
0891 deg
Mean motion: 15
75354315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4114
Checksum: 303
Coasting Arc #10 (Orbit 4129)
---------------------------------------
Vector Time (GMT): 2010/027/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4034810
46 A = 6728358
10 meter
Y = -5380319
09 meter E =
0004769
Z = 39430
84 I = 51
39542
XDOT = 3864
508860 Wp = 345
52079
YDOT = -2855
153655 meter/sec RA = 232
86481 deg
ZDOT = 6017
490255 TA = 14
90908
MA = 14
89502
Ha = 187
390 n
mi
Hp = 184
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13237567
14 X = -3974538
45
Y = -17651965
51 feet Y = -5425101
73 meter
Z = 129366
26 Z = 19975
93
XDOT = 12678
834843 XDOT = 3866
917147
YDOT = -9367
302018 feet/sec YDOT = -2811
925593 meter/sec
ZDOT = 19742
422096 ZDOT = 6036
269240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19361544
51 X = 5901398
77
Y = -10581572
91 feet Y = -3225263
42 meter
Z = 52103
86 Z = 15881
26
XDOT = 6705
120623 XDOT = 2043
720766
YDOT = 12359
755338 feet/sec YDOT = 3767
253427 meter/sec
ZDOT = 19816
740781 ZDOT = 6040
142590
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 10027
44124820
00016717 00000-0 10270-3 0 9091
2 25544 51
6443 233
4677 0010759 248
3109 111
6910 15
75342856 41309
Satellite: ISS
Catalog Number: 25544
Epoch time: 10027
44124820 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 233
4677 deg
Eccentricity:
0010759
Arg of perigee: 248
3109 deg
Mean anomaly: 111
6910 deg
Mean motion: 15
75342856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4130
Checksum: 294
Coasting Arc #11 (Orbit 4144)
---------------------------------------
Vector Time (GMT): 2010/028/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3522705
68 A = 6716336
74 meter
Y = 2332495
17 meter E =
0006364
Z = -5225346
57 I = 51
37380
XDOT = -4818
438311 Wp = 133
80970
YDOT = -5978
267962 meter/sec RA = 227
69567 deg
ZDOT = 575
893802 TA = 141
70658
MA = 141
66137
Ha = 186
991 n
mi
Hp = 184
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11557433
32 X = -3523143
09
Y = 7652543
22 feet Y = 2293100
25 meter
Z = -17143525
50 Z = -5242460
28
XDOT = -15808
524644 XDOT = -4754
027664
YDOT = -19613
740034 feet/sec YDOT = -6031
790508 meter/sec
ZDOT = 1889
415361 ZDOT = 552
642293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6150557
45 X = -1874689
91
Y = -12327976
98 feet Y = -3757567
38 meter
Z = -17211268
87 Z = -5245994
75
XDOT = 20548
470240 XDOT = 6263
173729
YDOT = -12778
586823 feet/sec YDOT = -3894
913264 meter/sec
ZDOT = 1797
069225 ZDOT = 547
746700
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 10028
39278472
00016717 00000-0 10270-3 0 9101
2 25544 51
6439 228
5717 0010771 252
3479 107
6509 15
75354045 41451
Satellite: ISS
Catalog Number: 25544
Epoch time: 10028
39278472 = yrday
fracday
Element set: 910
Inclination: 51
6439 deg
RA of node: 228
5717 deg
Eccentricity:
0010771
Arg of perigee: 252
3479 deg
Mean anomaly: 107
6509 deg
Mean motion: 15
75354045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4145
Checksum: 316
Coasting Arc #12 (Orbit 4160)
---------------------------------------
Vector Time (GMT): 2010/029/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4351153
32 A = 6728119
01 meter
Y = 5031374
40 meter E =
0011423
Z = -958733
45 I = 51
43391
XDOT = -4230
749221 Wp = 202
39443
YDOT = 2527
611300 meter/sec RA = 222
54772 deg
ZDOT = -5923
558125 TA = 348
11808
MA = 348
14501
Ha = 186
881 n
mi
Hp = 184
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14275437
40 X = 4299225
43
Y = 16507133
86 feet Y = 5079741
30 meter
Z = -3145450
96 Z = -937721
97
XDOT = -13880
410829 XDOT = -4229
924294
YDOT = 8292
687993 feet/sec YDOT = 2480
305600 meter/sec
ZDOT = -19434
245816 ZDOT = -5944
108285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17962698
27 X = -5475030
43
Y = 12415035
43 feet Y = 3784102
80 meter
Z = -3061994
30 Z = -933295
86
XDOT = -5841
696363 XDOT = -1780
549052
YDOT = -13275
859543 feet/sec YDOT = -4046
481989 meter/sec
ZDOT = -19515
607704 ZDOT = -5948
357228
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 10029
40775784
00016717 00000-0 10270-3 0 9113
2 25544 51
6437 223
3497 0010890 255
5570 104
4386 15
75294316 41616
Satellite: ISS
Catalog Number: 25544
Epoch time: 10029
40775784 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 223
3497 deg
Eccentricity:
0010890
Arg of perigee: 255
5570 deg
Mean anomaly: 104
4386 deg
Mean motion: 15
75294316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4161
Checksum: 313
Coasting Arc #13 (Orbit 4176)
---------------------------------------
Vector Time (GMT): 2010/030/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3884272
79 A = 6717047
48 meter
Y = -2114452
42 meter E =
0006830
Z = 5061772
39 I = 51
42033
XDOT = 5111
745581 Wp = 279
38218
YDOT = 5524
583952 meter/sec RA = 217
36360 deg
ZDOT = -1615
591341 TA = 186
18638
MA = 186
19482
Ha = 186
218 n
mi
Hp = 184
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12743677
15 X = 3883039
93
Y = -6937179
86 feet Y = -2071023
27 meter
Z = 16606864
78 Z = 5080638
48
XDOT = 16770
818835 XDOT = 5057
436782
YDOT = 18125
275434 feet/sec YDOT = 5581
442924 meter/sec
ZDOT = -5300
496524 ZDOT = -1590
891006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5749732
96 X = 1752518
60
Y = 13227981
19 feet Y = 4031888
67 meter
Z = 16681571
09 Z = 5084542
87
XDOT = -18622
818007 XDOT = -5676
234928
YDOT = 14652
204155 feet/sec YDOT = 4465
991826 meter/sec
ZDOT = -5202
380168 ZDOT = -1585
685475
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 10030
42272820
00016717 00000-0 10270-3 0 9121
2 25544 51
6436 218
1265 0010883 260
7176 99
2757 15
75362930 41770
Satellite: ISS
Catalog Number: 25544
Epoch time: 10030
42272820 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 218
1265 deg
Eccentricity:
0010883
Arg of perigee: 260
7176 deg
Mean anomaly: 99
2757 deg
Mean motion: 15
75362930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4177
Checksum: 305
Coasting Arc #14 (Orbit 4192)
---------------------------------------
Vector Time (GMT): 2010/031/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4533915
25 A = 6726881
75 meter
Y = -4605001
75 meter E =
0005118
Z = 1855336
99 I = 51
47736
XDOT = 4692
008605 Wp = 23
77308
YDOT = -2347
668708 meter/sec RA = 212
23376 deg
ZDOT = 5638
172213 TA = 356
88034
MA = 356
88353
Ha = 185
932 n
mi
Hp = 184
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14875050
04 X = -4491096
94
Y = -15108273
45 feet Y = -4655463
27 meter
Z = 6087063
63 Z = 1833415
92
XDOT = 15393
729019 XDOT = 4690
523584
YDOT = -7702
325157 feet/sec YDOT = -2295
208217 meter/sec
ZDOT = 18497
940333 ZDOT = 5660
961647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16175879
26 X = 4930408
00
Y = -13744836
37 feet Y = -4189426
13 meter
Z = 5999982
28 Z = 1828794
60
XDOT = 5540
726864 XDOT = 1688
813548
YDOT = 14636
076676 feet/sec YDOT = 4461
076171 meter/sec
ZDOT = 18588
194109 ZDOT = 5665
681564
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 10031
43770043
00016717 00000-0 10270-3 0 9134
2 25544 51
6430 212
9029 0010936 264
8196 95
1720 15
75350207 41937
Satellite: ISS
Catalog Number: 25544
Epoch time: 10031
43770043 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 212
9029 deg
Eccentricity:
0010936
Arg of perigee: 264
8196 deg
Mean anomaly: 95
1720 deg
Mean motion: 15
75350207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4193
Checksum: 285
Coasting Arc #15 (Orbit 4207)
---------------------------------------
Vector Time (GMT): 2010/032/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4311254
29 A = 6718467
00 meter
Y = 2033217
97 meter E =
0003919
Z = -4736309
60 I = 51
47490
XDOT = -5235
628409 Wp = 179
31905
YDOT = -5007
181640 meter/sec RA = 207
03813 deg
ZDOT = 2612
427566 TA = 116
39755
MA = 116
35732
Ha = 185
581 n
mi
Hp = 184
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14144535
08 X = -4310662
17
Y = 6670662
62 feet Y = 1985010
19 meter
Z = -15539073
50 Z = -4757251
70
XDOT = -17177
258559 XDOT = -5191
938448
YDOT = -16427
761286 feet/sec YDOT = -5065
485208 meter/sec
ZDOT = 8570
956582 ZDOT = 2587
099797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5854730
43 X = -1784521
84
Y = -14411906
90 feet Y = -4392749
22 meter
Z = -15622019
36 Z = -4761591
50
XDOT = 16336
036444 XDOT = 4979
223908
YDOT = -15831
525186 feet/sec YDOT = -4825
448877 meter/sec
ZDOT = 8470
340208 ZDOT = 2581
759695
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 10032
38923729
00016717 00000-0 10270-3 0 9141
2 25544 51
6426 208
0060 0010926 268
5681 91
4231 15
75346551 42082
Satellite: ISS
Catalog Number: 25544
Epoch time: 10032
38923729 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 208
0060 deg
Eccentricity:
0010926
Arg of perigee: 268
5681 deg
Mean anomaly: 91
4231 deg
Mean motion: 15
75346551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4208
Checksum: 297
Coasting Arc #16 (Orbit 4223)
---------------------------------------
Vector Time (GMT): 2010/033/09:04:05
404
Vector Time (MET): N/A
Weight (LBS) : 750857
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4563808
49 A = 6725338
19 meter
Y = 4139031
25 meter E =
0007348
Z = -2686977
96 I = 51
52477
XDOT = -5189
973650 Wp = 251
41427
YDOT = 2351
577030 meter/sec RA = 201
92653 deg
ZDOT = -5183
516325 TA = 319
29091
MA = 319
34581
Ha = 185
810 n
mi
Hp = 184
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14973124
97 X = 4530238
48
Y = 13579498
84 feet Y = 4189878
69 meter
Z = -8815544
49 Z = -2664889
12
XDOT = -17027
472606 XDOT = -5190
703642
YDOT = 7715
147736 feet/sec YDOT = 2293
535452 meter/sec
ZDOT = -17006
287156 ZDOT = -5208
730492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14170480
44 X = -4319162
44
Y = 14468384
79 feet Y = 4409963
68 meter
Z = -8727795
26 Z = -2660232
00
XDOT = -5975
145466 XDOT = -1821
224338
YDOT = -16189
555155 feet/sec YDOT = -4934
576411 meter/sec
ZDOT = -17106
161724 ZDOT = -5213
958093
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 10033
40420994
00016717 00000-0 10270-3 0 9152
2 25544 51
6424 202
7842 0010994 272
4271 87
5635 15
75320658 42245
Satellite: ISS
Catalog Number: 25544
Epoch time: 10033
40420994 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 202
7842 deg
Eccentricity:
0010994
Arg of perigee: 272
4271 deg
Mean anomaly: 87
5635 deg
Mean motion: 15
75320658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4224
Checksum: 301
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 normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! 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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