Date:
February 1st 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
There are no maneuvers
Coasting Arc #1 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2010/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5500562
76 A = 6727197
30 meter
Y = 3680562
04 meter E =
0009351
Z = 1170198
28 I = 51
43280
XDOT = -1850
721342 Wp = 177
96925
YDOT = 4630
688458 meter/sec RA = 221
89205 deg
ZDOT = -5873
040705 TA = 349
16412
MA = 349
18425
Ha = 186
113 n
mi
Hp = 183
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18046465
75 X = 5453312
82
Y = 12075334
77 feet Y = 3741808
32 meter
Z = 3839233
19 Z = 1196804
66
XDOT = -6071
920415 XDOT = -1873
835695
YDOT = 15192
547436 feet/sec YDOT = 4609
863761 meter/sec
ZDOT = -19268
506249 ZDOT = -5882
087053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1527527
32 X = 465590
33
Y = 21641012
02 feet Y = 6596180
46 meter
Z = 3944820
19 Z = 1202381
20
XDOT = -14073
398130 XDOT = -4289
571750
YDOT = 4507
700191 feet/sec YDOT = 1373
947018 meter/sec
ZDOT = -19304
197985 ZDOT = -5883
919546
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
53402907
00016717 00000-0 10270-3 0 9009
2 25544 51
6407 222
6960 0011599 260
2015 99
7839 15
75529921 1634
Satellite: ISS
Catalog Number: 25544
Epoch time: 10029
53402907 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 222
6960 deg
Eccentricity:
0011599
Arg of perigee: 260
2015 deg
Mean anomaly: 99
7839 deg
Mean motion: 15
75529921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 307
Coasting Arc #2 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2010/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1812818
16 A = 6716153
43 meter
Y = -3837013
50 meter E =
0009052
Z = 5213223
78 I = 51
41704
XDOT = 6478
633647 Wp = 250
99418
YDOT = 4087
061785 meter/sec RA = 216
74668 deg
ZDOT = 753
456863 TA = 191
80145
MA = 191
82268
Ha = 186
019 n
mi
Hp = 183
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5947566
13 X = 1830265
53
Y = -12588626
97 feet Y = -3816644
12 meter
Z = 17103752
55 Z = 5222072
40
XDOT = 21255
359733 XDOT = 6428
789860
YDOT = 13408
995359 feet/sec YDOT = 4159
230987 meter/sec
ZDOT = 2471
971334 ZDOT = 784
808090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13471663
71 X = 4106163
10
Y = -3341430
33 feet Y = -1018467
96 meter
Z = 17138685
57 Z = 5223871
36
XDOT = 2634
836366 XDOT = 803
098124
YDOT = 23971
088893 feet/sec YDOT = 7306
387895 meter/sec
ZDOT = 2596
400799 ZDOT = 791
382964
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
54889778
00016717 00000-0 10270-3 0 9018
2 25544 51
6396 217
4713 0011417 263
0162 96
9703 15
75458967 1799
Satellite: ISS
Catalog Number: 25544
Epoch time: 10030
54889778 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 217
4713 deg
Eccentricity:
0011417
Arg of perigee: 263
0162 deg
Mean anomaly: 96
9703 deg
Mean motion: 15
75458967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 179
Checksum: 331
Coasting Arc #3 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2010/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5780192
98 A = 6727828
92 meter
Y = -3429807
54 meter E =
0008506
Z = -131612
92 I = 51
48193
XDOT = 2345
108726 Wp = 338
15287
YDOT = -4187
853586 meter/sec RA = 211
57679 deg
ZDOT = 6025
234136 TA = 20
41329
MA = 20
37931
Ha = 185
709 n
mi
Hp = 183
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18963887
73 X = -5740771
34
Y = -11252649
41 feet Y = -3494224
66 meter
Z = -431800
93 Z = -159596
47
XDOT = 7693
926266 XDOT = 2362
495174
YDOT = -13739
677119 feet/sec YDOT = -4161
531984 meter/sec
ZDOT = 19767
828531 ZDOT = 6036
668542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3503289
02 X = -1067802
49
Y = -21768552
19 feet Y = -6635054
71 meter
Z = -542872
06 Z = -165467
41
XDOT = 13817
229574 XDOT = 4211
491574
YDOT = -2725
349799 feet/sec YDOT = -830
686619 meter/sec
ZDOT = 19812
995336 ZDOT = 6039
000978
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
50031992
00016717 00000-0 10270-3 0 9023
2 25544 51
6395 212
5731 0011503 266
3429 93
6420 15
75523902 1941
Satellite: ISS
Catalog Number: 25544
Epoch time: 10031
50031992 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 212
5731 deg
Eccentricity:
0011503
Arg of perigee: 266
3429 deg
Mean anomaly: 93
6420 deg
Mean motion: 15
75523902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 278
Coasting Arc #4 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2010/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2311542
23 A = 6715718
31 meter
Y = 3511373
96 meter E =
0003730
Z = -5240334
92 I = 51
46814
XDOT = -6716
196946 Wp = 103
58013
YDOT = -3741
011229 meter/sec RA = 206
41557 deg
ZDOT = 455
234783 TA = 170
75698
MA = 170
75012
Ha = 185
407 n
mi
Hp = 183
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7583799
97 X = -2325179
32
Y = 11520255
77 feet Y = 3485448
57 meter
Z = -17192699
88 Z = -5251597
29
XDOT = -22034
766884 XDOT = -6676
076525
YDOT = -12273
658889 feet/sec YDOT = -3815
891389 meter/sec
ZDOT = 1493
552437 ZDOT = 422
705902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13609318
65 X = -4148120
32
Y = 1866625
53 feet Y = 568947
46 meter
Z = -17237209
73 Z = -5253901
52
XDOT = -4982
982013 XDOT = -1518
812918
YDOT = -23712
602401 feet/sec YDOT = -7227
601212 meter/sec
ZDOT = 1364
435736 ZDOT = 415
880012
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
51515845
00016717 00000-0 10270-3 0 9030
2 25544 51
6399 207
3494 0011328 270
0121 89
9745 15
75556268 2107
Satellite: ISS
Catalog Number: 25544
Epoch time: 10032
51515845 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 207
3494 deg
Eccentricity:
0011328
Arg of perigee: 270
0121 deg
Mean anomaly: 89
9745 deg
Mean motion: 15
75556268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 301
Coasting Arc #5 (Orbit 225)
---------------------------------------
Vector Time (GMT): 2010/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5897585
89 A = 6727235
82 meter
Y = 3088730
67 meter E =
0008517
Z = -929973
38 I = 51
53553
XDOT = -2981
915527 Wp = 216
50837
YDOT = 3899
935298 meter/sec RA = 201
27095 deg
ZDOT = -5936
412796 TA = 333
66853
MA = 333
71180
Ha = 185
626 n
mi
Hp = 183
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19349035
08 X = 5867126
39
Y = 10133630
82 feet Y = 3154510
64 meter
Z = -3051093
78 Z = -901397
59
XDOT = -9783
187425 XDOT = -2996
466270
YDOT = 12795
063313 feet/sec YDOT = 3866
508239 meter/sec
ZDOT = -19476
419936 ZDOT = -5950
934074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5354595
56 X = 1632080
73
Y = 21191583
87 feet Y = 6459194
76 meter
Z = -2937666
59 Z = -895400
78
XDOT = -14437
195578 XDOT = -4400
457212
YDOT = 930
135438 feet/sec YDOT = 283
505281 meter/sec
ZDOT = -19533
835242 ZDOT = -5953
912982
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
52998087
00016717 00000-0 10270-3 0 9046
2 25544 51
6403 202
1255 0011404 275
3033 84
6830 15
75614944 2266
Satellite: ISS
Catalog Number: 25544
Epoch time: 10033
52998087 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 202
1255 deg
Eccentricity:
0011404
Arg of perigee: 275
3033 deg
Mean anomaly: 84
6830 deg
Mean motion: 15
75614944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 226
Checksum: 286
Coasting Arc #6 (Orbit 241)
---------------------------------------
Vector Time (GMT): 2010/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2913365
31 A = 6716566
22 meter
Y = -3339557
22 meter E =
0008321
Z = 5054098
71 I = 51
52748
XDOT = 6733
597945 Wp = 302
71886
YDOT = 3330
662595 meter/sec RA = 196
09264 deg
ZDOT = -1678
287270 TA = 163
46474
MA = 163
43759
Ha = 185
865 n
mi
Hp = 183
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9558285
14 X = 2925940
82
Y = -10956552
57 feet Y = -3306907
84 meter
Z = 16581688
67 Z = 5068282
20
XDOT = 22091
856774 XDOT = 6704
006109
YDOT = 10927
370718 feet/sec YDOT = 3405
796191 meter/sec
ZDOT = -5506
191830 ZDOT = -1645
647945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14466999
50 X = 4409541
45
Y = -499097
38 feet Y = -152124
88 meter
Z = 16637790
88 Z = 5071198
66
XDOT = 6972
343759 XDOT = 2125
170378
YDOT = 22603
982684 feet/sec YDOT = 6889
693922 meter/sec
ZDOT = -5376
633826 ZDOT = -1638
797990
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 10034
54479220
00016717 00000-0 10270-3 0 9053
2 25544 51
6402 196
9013 0011237 277
9219 82
0669 15
75553607 2423
Satellite: ISS
Catalog Number: 25544
Epoch time: 10034
54479220 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 196
9013 deg
Eccentricity:
0011237
Arg of perigee: 277
9219 deg
Mean anomaly: 82
0669 deg
Mean motion: 15
75553607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 242
Checksum: 300
Coasting Arc #7 (Orbit 257)
---------------------------------------
Vector Time (GMT): 2010/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5806909
89 A = 6725857
90 meter
Y = -2734636
11 meter E =
0007817
Z = 1992126
64 I = 51
58970
XDOT = 3703
783778 Wp = 15
16576
YDOT = -3795
545921 meter/sec RA = 190
97108 deg
ZDOT = 5588
537147 TA = 7
06189
MA = 7
05088
Ha = 186
185 n
mi
Hp = 183
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19051541
63 X = -5785576
38
Y = -8971903
23 feet Y = -2799453
13 meter
Z = 6535848
56 Z = 1963968
90
XDOT = 12151
521583 XDOT = 3718
803254
YDOT = -12452
578481 feet/sec YDOT = -3754
044024 meter/sec
ZDOT = 18335
095625 ZDOT = 5606
566363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6727658
08 X = -2050590
18
Y = -19991084
32 feet Y = -6093282
50 meter
Z = 6424077
14 Z = 1958058
71
XDOT = 15865
573218 XDOT = 4835
826717
YDOT = 572
889588 feet/sec YDOT = 174
616746 meter/sec
ZDOT = 18406
434348 ZDOT = 5610
281189
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 10035
55958460
00016717 00000-0 10270-3 0 9064
2 25544 51
6411 191
6773 0011315 281
6117 78
3777 15
75635446 2581
Satellite: ISS
Catalog Number: 25544
Epoch time: 10035
55958460 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 191
6773 deg
Eccentricity:
0011315
Arg of perigee: 281
6117 deg
Mean anomaly: 78
3777 deg
Mean motion: 15
75635446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 258
Checksum: 319
Coasting Arc #8 (Orbit 272)
---------------------------------------
Vector Time (GMT): 2010/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3539346
97 A = 6718060
37 meter
Y = 3334821
83 meter E =
0000807
Z = -4634909
41 I = 51
59412
XDOT = -6519
190672 Wp = 223
71412
YDOT = -2940
311358 meter/sec RA = 185
78084 deg
ZDOT = 2861
811433 TA = 74
59138
MA = 74
58246
Ha = 186
439 n
mi
Hp = 183
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11612030
73 X = -3553859
24
Y = 10941016
51 feet Y = 3295161
69 meter
Z = -15206395
69 Z = -4652138
52
XDOT = -21388
420840 XDOT = -6499
729044
YDOT = -9646
690807 feet/sec YDOT = -3013
104040 meter/sec
ZDOT = 9389
145120 ZDOT = 2830
188859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15881987
37 X = -4840829
75
Y = -478530
22 feet Y = -145856
01 meter
Z = -15274588
57 Z = -4655694
60
XDOT = -8283
523460 XDOT = -2524
817951
YDOT = -20860
604798 feet/sec YDOT = -6358
312342 meter/sec
ZDOT = 9263
614740 ZDOT = 2823
549773
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 10036
51094122
00016717 00000-0 10270-3 0 9078
2 25544 51
6416 186
7807 0011259 285
7054 74
2868 15
75639767 2734
Satellite: ISS
Catalog Number: 25544
Epoch time: 10036
51094122 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 186
7807 deg
Eccentricity:
0011259
Arg of perigee: 285
7054 deg
Mean anomaly: 74
2868 deg
Mean motion: 15
75639767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 273
Checksum: 326
Coasting Arc #9 (Orbit 288)
---------------------------------------
Vector Time (GMT): 2010/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5514741
78 A = 6723630
81 meter
Y = 2425588
69 meter E =
0006758
Z = -2982467
28 I = 51
64293
XDOT = -4407
419787 Wp = 289
07674
YDOT = 3886
906210 meter/sec RA = 180
67722 deg
ZDOT = -4977
093293 TA = 285
37958
MA = 285
45424
Ha = 186
816 n
mi
Hp = 183
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18092984
84 X = 5501696
62
Y = 7957968
15 feet Y = 2487184
96 meter
Z = -9784997
63 Z = -2955708
67
XDOT = -14460
038671 XDOT = -4426
378830
YDOT = 12752
316962 feet/sec YDOT = 3837
513982 meter/sec
ZDOT = -16329
046236 ZDOT = -4998
550151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7446112
00 X = 2269574
94
Y = 18365958
04 feet Y = 5597944
01 meter
Z = -9678767
35 Z = -2950088
29
XDOT = -17847
685783 XDOT = -5439
974627
YDOT = -1433
871150 feet/sec YDOT = -437
043926 meter/sec
ZDOT = -16413
994602 ZDOT = -5002
985555
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 10037
52570600
00016717 00000-0 10270-3 0 9081
2 25544 51
6415 181
5566 0011299 290
1157 69
8791 15
75672281 2896
Satellite: ISS
Catalog Number: 25544
Epoch time: 10037
52570600 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 181
5566 deg
Eccentricity:
0011299
Arg of perigee: 290
1157 deg
Mean anomaly: 69
8791 deg
Mean motion: 15
75672281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 289
Checksum: 321
Coasting Arc #10 (Orbit 304)
---------------------------------------
Vector Time (GMT): 2010/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4132859
91 A = 6720423
89 meter
Y = -3492354
78 meter E =
0006795
Z = 3990576
73 I = 51
66265
XDOT = 6055
825081 Wp = 2
93527
YDOT = 2650
741636 meter/sec RA = 175
47998 deg
ZDOT = -3944
988126 TA = 127
88877
MA = 127
82729
Ha = 187
055 n
mi
Hp = 183
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13559251
66 X = 4152219
71
Y = -11457856
89 feet Y = -3446030
61 meter
Z = 13092443
35 Z = 4010700
69
XDOT = 19868
192523 XDOT = 6044
897637
YDOT = 8696
658912 feet/sec YDOT = 2718
400528 meter/sec
ZDOT = -12942
874429 ZDOT = -3915
595877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17670172
21 X = 5385868
49
Y = 898783
33 feet Y = 273949
16 meter
Z = 13172132
15 Z = 4014865
88
XDOT = 8626
243629 XDOT = 2629
279058
YDOT = 18713
933568 feet/sec YDOT = 5704
006952 meter/sec
ZDOT = -12826
175839 ZDOT = -3909
418396
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 10038
54045675
00016717 00000-0 10270-3 0 9094
2 25544 51
6416 176
3325 0011235 293
7482 66
2503 15
75665958 3056
Satellite: ISS
Catalog Number: 25544
Epoch time: 10038
54045675 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 176
3325 deg
Eccentricity:
0011235
Arg of perigee: 293
7482 deg
Mean anomaly: 66
2503 deg
Mean motion: 15
75665958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 305
Checksum: 314
Coasting Arc #11 (Orbit 320)
---------------------------------------
Vector Time (GMT): 2010/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5012380
94 A = 6720800
34 meter
Y = -2249232
83 meter E =
0003727
Z = 3867356
13 I = 51
69554
XDOT = 5028
530083 Wp = 19
11176
YDOT = -4144
037770 meter/sec RA = 170
38620 deg
ZDOT = 4109
545468 TA = 28
07123
MA = 28
05114
Ha = 187
338 n
mi
Hp = 183
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16444819
35 X = -5005643
60
Y = -7379372
82 feet Y = -2305246
75 meter
Z = 12688176
30 Z = 3843022
77
XDOT = 16497
802109 XDOT = 5054
532717
YDOT = -13595
924441 feet/sec YDOT = -4087
660566 meter/sec
ZDOT = 13482
760721 ZDOT = 4134
036513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7256108
92 X = -2211662
00
Y = -16573437
07 feet Y = -5051583
62 meter
Z = 12591549
20 Z = 3837904
19
XDOT = 20085
211768 XDOT = 6121
972547
YDOT = 1517
613575 feet/sec YDOT = 462
568618 meter/sec
ZDOT = 13579
760491 ZDOT = 4139
110998
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 10039
55518966
00016717 00000-0 10270-3 0 9106
2 25544 51
6427 171
1083 0011356 297
7311 62
2701 15
75742336 3211
Satellite: ISS
Catalog Number: 25544
Epoch time: 10039
55518966 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 171
1083 deg
Eccentricity:
0011356
Arg of perigee: 297
7311 deg
Mean anomaly: 62
2701 deg
Mean motion: 15
75742336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 321
Checksum: 291
Coasting Arc #12 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2010/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4592396
95 A = 6722933
71 meter
Y = 3770176
76 meter E =
0008692
Z = -3132883
79 I = 51
73271
XDOT = -5407
342409 Wp = 323
79859
YDOT = -2542
009252 meter/sec RA = 165
19272 deg
ZDOT = 4867
409894 TA = 359
75662
MA = 359
75704
Ha = 187
541 n
mi
Hp = 183
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15066919
12 X = -4618995
82
Y = 12369346
31 feet Y = 3718673
26 meter
Z = -10278490
11 Z = -3155257
54
XDOT = -17740
624701 XDOT = -5402
159723
YDOT = -8339
925369 feet/sec YDOT = -2602
448581 meter/sec
ZDOT = 15969
192566 ZDOT = 4841
154176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19437310
47 X = -5924492
23
Y = -611552
59 feet Y = -186401
23 meter
Z = -10367116
47 Z = -3159897
10
XDOT = -7938
772957 XDOT = -2419
737997
YDOT = -16618
287581 feet/sec YDOT = -5065
254055 meter/sec
ZDOT = 15864
913594 ZDOT = 4835
625663
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 10040
50649066
00016717 00000-0 10270-3 0 9110
2 25544 51
6431 166
2114 0011436 302
3273 57
6783 15
75717852 3364
Satellite: ISS
Catalog Number: 25544
Epoch time: 10040
50649066 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 166
2114 deg
Eccentricity:
0011436
Arg of perigee: 302
3273 deg
Mean anomaly: 57
6783 deg
Mean motion: 15
75717852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 288
Coasting Arc #13 (Orbit 351)
---------------------------------------
Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4385858
15 A = 6718203
55 meter
Y = 2245975
37 meter E =
0010243
Z = -4572008
07 I = 51
74621
XDOT = -5463
363101 Wp = 2
16914
YDOT = 4507
467811 meter/sec RA = 160
09914 deg
ZDOT = -3016
830237 TA = 237
84561
MA = 237
94503
Ha = 187
810 n
mi
Hp = 182
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14389298
38 X = 4382626
64
Y = 7368685
60 feet Y = 2295002
70 meter
Z = -15000026
47 Z = -4550709
96
XDOT = -17924
419622 XDOT = -5498
705562
YDOT = 14788
280220 feet/sec YDOT = 4446
175725 meter/sec
ZDOT = -9897
736999 ZDOT = -3043
456206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6271882
46 X = 1911669
77
Y = 14984791
91 feet Y = 4567364
57 meter
Z = -14915419
25 Z = -4546219
79
XDOT = -22097
783158 XDOT = -6735
404307
YDOT = -740
138563 feet/sec YDOT = -225
594234 meter/sec
ZDOT = -10003
218855 ZDOT = -3048
981107
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 10041
52119605
00016717 00000-0 10270-3 0 9125
2 25544 51
6436 160
9875 0011433 306
0041 54
0063 15
75749588 3526
Satellite: ISS
Catalog Number: 25544
Epoch time: 10041
52119605 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 160
9875 deg
Eccentricity:
0011433
Arg of perigee: 306
0041 deg
Mean anomaly: 54
0063 deg
Mean motion: 15
75749588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 352
Checksum: 285
Coasting Arc #14 (Orbit 367)
---------------------------------------
Vector Time (GMT): 2010/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4899607
59 A = 6725185
70 meter
Y = -4107088
20 meter E =
0005200
Z = 2087562
16 I = 51
79857
XDOT = 4610
972992 Wp = 61
67896
YDOT = 2669
909112 meter/sec RA = 154
91848 deg
ZDOT = -5556
522941 TA = 95
05602
MA = 94
99666
Ha = 187
949 n
mi
Hp = 182
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16074828
06 X = 4935028
95
Y = -13474698
82 feet Y = -4052099
86 meter
Z = 6848957
21 Z = 2111449
70
XDOT = 15127
864146 XDOT = 4607
766649
YDOT = 8759
544332 feet/sec YDOT = 2721
453888 meter/sec
ZDOT = -18230
062141 ZDOT = -5534
131280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20942639
94 X = 6383316
65
Y = -260964
31 feet Y = -79541
92 meter
Z = 6943597
78 Z = 2116408
60
XDOT = 6214
228796 XDOT = 1894
096937
YDOT = 14903
434820 feet/sec YDOT = 4542
566933 meter/sec
ZDOT = -18141
087356 ZDOT = -5529
403426
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 10042
53588661
00016717 00000-0 10270-3 0 9130
2 25544 51
6440 155
7636 0011347 310
2442 49
7729 15
75772341 3684
Satellite: ISS
Catalog Number: 25544
Epoch time: 10042
53588661 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 155
7636 deg
Eccentricity:
0011347
Arg of perigee: 310
2442 deg
Mean anomaly: 49
7729 deg
Mean motion: 15
75772341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 368
Checksum: 308
Coasting Arc #15 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2010/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3656276
33 A = 6715877
32 meter
Y = -2480348
25 meter E =
0006258
Z = 5059933
65 I = 51
79548
XDOT = 5697
361605 Wp = 322
23169
YDOT = -4886
875229 meter/sec RA = 149
81380 deg
ZDOT = 1727
328389 TA = 111
21957
MA = 111
15271
Ha = 188
167 n
mi
Hp = 182
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11995657
24 X = -3652848
36
Y = -8137625
49 feet Y = -2521215
70 meter
Z = 16600832
17 Z = 5042180
36
XDOT = 18692
131250 XDOT = 5743
193289
YDOT = -16033
055213 feet/sec YDOT = -4822
907684 meter/sec
ZDOT = 5667
087890 ZDOT = 1755
116646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4436657
93 X = -1352293
34
Y = -13884190
58 feet Y = -4231901
29 meter
Z = 16530265
83 Z = 5038425
03
XDOT = 23567
927946 XDOT = 7183
504438
YDOT = -676
262380 feet/sec YDOT = -206
124773 meter/sec
ZDOT = 5777
187973 ZDOT = 1760
886894
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 10043
55056019
00016717 00000-0 10270-3 0 9141
2 25544 51
6450 150
5390 0011463 314
4654 45
5572 15
75839335 3840
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043
55056019 = yrday
fracday
Element set: 914
Inclination: 51
6450 deg
RA of node: 150
5390 deg
Eccentricity:
0011463
Arg of perigee: 314
4654 deg
Mean anomaly: 45
5572 deg
Mean motion: 15
75839335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 295
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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