Date:
January 7th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 3799)
---------------------------------------
Vector Time (GMT): 2010/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6467086
70 A = 6722898
20 meter
Y = 1681225
78 meter E =
0017913
Z = -653965
63 I = 51
55453
XDOT = -653
329899 Wp = 144
91946
YDOT = -4807
152056 meter/sec RA = 340
97140 deg
ZDOT = -5992
672691 TA = 42
22470
MA = 42
08689
Ha = 187
199 n
mi
Hp = 177
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21217476
05 X = -6482228
99
Y = 5515832
62 feet Y = 1608822
37 meter
Z = -2145556
54 Z = -685419
18
XDOT = -2143
470797 XDOT = -570
415829
YDOT = -15771
496246 feet/sec YDOT = -4813
994023 meter/sec
ZDOT = -19660
999643 ZDOT = -5995
645433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10878983
44 X = -3315914
15
Y = -19018508
77 feet Y = -5796841
47 meter
Z = -2270056
32 Z = -691913
17
XDOT = 13302
711460 XDOT = 4054
666453
YDOT = -5296
494288 feet/sec YDOT = -1614
371459 meter/sec
ZDOT = -19672
836966 ZDOT = -5996
280707
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 10006
53040419
00016717 00000-0 10270-3 0 9000
2 25544 51
6437 341
3247 0007323 153
0297 207
1250 15
77193338 38009
Satellite: ISS
Catalog Number: 25544
Epoch time: 10006
53040419 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 341
3247 deg
Eccentricity:
0007323
Arg of perigee: 153
0297 deg
Mean anomaly: 207
1250 deg
Mean motion: 15
77193338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 273
Coasting Arc #2 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2010/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -345579
45 A = 6712248
05 meter
Y = 4490945
12 meter E =
0008373
Z = 4969014
33 I = 51
49027
XDOT = -7293
537285 Wp = 113
54012
YDOT = 1586
483020 meter/sec RA = 335
78115 deg
ZDOT = -1941
815110 TA = 355
22496
MA = 355
23295
Ha = 187
106 n
mi
Hp = 177
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1133790
84 X = -419910
77
Y = 14734071
90 feet Y = 4486664
68 meter
Z = 16302540
45 Z = 4967155
28
XDOT = -23928
928099 XDOT = -7301
302600
YDOT = 5204
996786 feet/sec YDOT = 1504
879093 meter/sec
ZDOT = -6370
784480 ZDOT = -1977
265708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14493669
78 X = -4417670
55
Y = 2923990
87 feet Y = 891232
42 meter
Z = 16295244
57 Z = 4966790
54
XDOT = -11441
096670 XDOT = -3487
246265
YDOT = -20438
566408 feet/sec YDOT = -6229
675041 meter/sec
ZDOT = -6511
106372 ZDOT = -1984
585222
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 10007
54417082
00016717 00000-0 10270-3 0 9017
2 25544 51
6435 336
0947 0007272 157
4992 202
6493 15
77211638 38168
Satellite: ISS
Catalog Number: 25544
Epoch time: 10007
54417082 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 336
0947 deg
Eccentricity:
0007272
Arg of perigee: 157
4992 deg
Mean anomaly: 202
6493 deg
Mean motion: 15
77211638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3816
Checksum: 309
Coasting Arc #3 (Orbit 3831)
---------------------------------------
Vector Time (GMT): 2010/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6084851
19 A = 6719702
44 meter
Y = -986199
35 meter E =
0016305
Z = 2667762
76 I = 51
48950
XDOT = -1393
858243 Wp = 105
05387
YDOT = 5521
849274 meter/sec RA = 330
65004 deg
ZDOT = 5190
027227 TA = 285
44901
MA = 285
62904
Ha = 186
935 n
mi
Hp = 177
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19963422
53 X = 6082467
33
Y = -3235562
16 feet Y = -918168
51 meter
Z = 8752502
48 Z = 2697317
01
XDOT = -4573
025730 XDOT = -1480
713081
YDOT = 18116
303394 feet/sec YDOT = 5505
776243 meter/sec
ZDOT = 17027
648383 ZDOT = 5183
045394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8966383
84 X = 2732953
79
Y = 18070681
44 feet Y = 5507943
70 meter
Z = 8869488
97 Z = 2703420
24
XDOT = -17371
172948 XDOT = -5294
733515
YDOT = 226
853227 feet/sec YDOT = 69
144863 meter/sec
ZDOT = 17000
086091 ZDOT = 5181
626240
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 10008
55792057
00016717 00000-0 10270-3 0 9028
2 25544 51
6439 330
8643 0007375 162
0008 198
1419 15
77270093 38326
Satellite: ISS
Catalog Number: 25544
Epoch time: 10008
55792057 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 330
8643 deg
Eccentricity:
0007375
Arg of perigee: 162
0008 deg
Mean anomaly: 198
1419 deg
Mean motion: 15
77270093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3832
Checksum: 308
Coasting Arc #4 (Orbit 3846)
---------------------------------------
Vector Time (GMT): 2010/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1999049
37 A = 6716478
74 meter
Y = -5122750
74 meter E =
0011866
Z = -3870292
88 I = 51
45238
XDOT = 6505
067318 Wp = 136
67116
YDOT = -540
414310 meter/sec RA = 325
42832 deg
ZDOT = 4074
112955 TA = 175
94370
MA = 175
93408
Ha = 186
862 n
mi
Hp = 177
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6558560
94 X = 2074985
42
Y = -16806924
99 feet Y = -5099971
20 meter
Z = -12697811
28 Z = -3860397
62
XDOT = 21342
084375 XDOT = 6490
835612
YDOT = -1773
012829 feet/sec YDOT = -467
750805 meter/sec
ZDOT = 13366
512321 ZDOT = 4105
679852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18037112
20 X = 5497711
80
Y = 1068427
51 feet Y = 325656
71 meter
Z = -12658708
73 Z = -3858374
42
XDOT = 8384
834521 XDOT = 2555
697562
YDOT = 18338
388231 feet/sec YDOT = 5589
540733 meter/sec
ZDOT = 13491
473710 ZDOT = 4112
201187
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 10009
50829931
00016717 00000-0 10270-3 0 9037
2 25544 51
6439 325
9603 0007147 165
0719 195
0658 15
77242381 38472
Satellite: ISS
Catalog Number: 25544
Epoch time: 10009
50829931 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 325
9603 deg
Eccentricity:
0007147
Arg of perigee: 165
0719 deg
Mean anomaly: 195
0658 deg
Mean motion: 15
77242381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3847
Checksum: 323
Coasting Arc #5 (Orbit 3862)
---------------------------------------
Vector Time (GMT): 2010/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5166406
62 A = 6714665
76 meter
Y = -160528
20 meter E =
0010438
Z = -4291992
63 I = 51
42356
XDOT = 3068
616649 Wp = 111
23186
YDOT = -6148
746959 meter/sec RA = 320
30414 deg
ZDOT = -3474
305857 TA = 123
56859
MA = 123
46888
Ha = 186
616 n
mi
Hp = 177
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16950152
96 X = -5143377
98
Y = -526667
33 feet Y = -218172
74 meter
Z = -14081340
66 Z = -4317034
99
XDOT = 10067
639923 XDOT = 3154
022410
YDOT = -20173
054328 feet/sec YDOT = -6113
953925 meter/sec
ZDOT = -11398
641263 ZDOT = -3459
191890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5030291
54 X = -1533232
86
Y = -16108359
43 feet Y = -4909827
95 meter
Z = -14180484
55 Z = -4322211
69
XDOT = 21205
931155 XDOT = 6463
567816
YDOT = 3329
597820 feet/sec YDOT = 1014
861416 meter/sec
ZDOT = -11338
891595 ZDOT = -3456
094158
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 10010
52202036
00016717 00000-0 10270-3 0 9043
2 25544 51
6446 320
7291 0007122 168
8356 191
2968 15
77293691 38637
Satellite: ISS
Catalog Number: 25544
Epoch time: 10010
52202036 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 320
7291 deg
Eccentricity:
0007122
Arg of perigee: 168
8356 deg
Mean anomaly: 191
2968 deg
Mean motion: 15
77293691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3863
Checksum: 304
Coasting Arc #6 (Orbit 3878)
---------------------------------------
Vector Time (GMT): 2010/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3211448
85 A = 6720975
54 meter
Y = 5520143
77 meter E =
0018594
Z = 2058133
47 I = 51
42275
XDOT = -5270
309147 Wp = 130
34866
YDOT = -990
937984 meter/sec RA = 315
08497 deg
ZDOT = -5544
957219 TA = 26
54982
MA = 26
45470
Ha = 186
571 n
mi
Hp = 177
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10536249
50 X = -3282935
33
Y = 18110707
92 feet Y = 5483831
48 meter
Z = 6752406
40 Z = 2042359
48
XDOT = -17291
040509 XDOT = -5231
900451
YDOT = -3251
108870 feet/sec YDOT = -1049
658215 meter/sec
ZDOT = -18192
116859 ZDOT = -5570
466987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20643400
03 X = -6292108
33
Y = -3701184
06 feet Y = -1128120
90 meter
Z = 6690034
31 Z = 2039122
46
XDOT = -3127
161006 XDOT = -953
158675
YDOT = -15748
657261 feet/sec YDOT = -4800
190733 meter/sec
ZDOT = -18293
127030 ZDOT = -5575
745119
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 10011
53572648
00016717 00000-0 10270-3 0 9055
2 25544 51
6451 315
4985 0007112 172
6830 187
4440 15
77305275 38794
Satellite: ISS
Catalog Number: 25544
Epoch time: 10011
53572648 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 315
4985 deg
Eccentricity:
0007112
Arg of perigee: 172
6830 deg
Mean anomaly: 187
4440 deg
Mean motion: 15
77305275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3879
Checksum: 313
Coasting Arc #7 (Orbit 3894)
---------------------------------------
Vector Time (GMT): 2010/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3978267
44 A = 6710926
70 meter
Y = 1652509
49 meter E =
0009906
Z = 5144337
77 I = 51
36936
XDOT = -4153
179934 Wp = 159
36862
YDOT = 6391
125282 meter/sec RA = 309
93624 deg
ZDOT = 1148
943877 TA = 279
57555
MA = 279
68746
Ha = 186
230 n
mi
Hp = 178
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13052058
52 X = 3934503
19
Y = 5421619
08 feet Y = 1696751
45 meter
Z = 16877748
58 Z = 5163557
85
XDOT = -13625
918419 XDOT = -4229
919236
YDOT = 20968
258798 feet/sec YDOT = 6344
252743 meter/sec
ZDOT = 3769
500910 ZDOT = 1128
582453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -394724
61 X = -120312
06
Y = 14036346
16 feet Y = 4278278
31 meter
Z = 16953871
57 Z = 5167540
05
XDOT = -23452
416913 XDOT = -7148
296675
YDOT = -5154
006135 feet/sec YDOT = -1570
941070 meter/sec
ZDOT = 3688
979463 ZDOT = 1124
400940
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 10012
54941510
00016717 00000-0 10270-3 0 9066
2 25544 51
6454 310
2683 0007119 178
1997 181
9194 15
77369408 38958
Satellite: ISS
Catalog Number: 25544
Epoch time: 10012
54941510 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 310
2683 deg
Eccentricity:
0007119
Arg of perigee: 178
1997 deg
Mean anomaly: 181
9194 deg
Mean motion: 15
77369408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3895
Checksum: 328
Coasting Arc #8 (Orbit 3910)
---------------------------------------
Vector Time (GMT): 2010/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3905937
33 A = 6722637
09 meter
Y = -5468776
74 meter E =
0009137
Z = 115665
81 I = 51
39005
XDOT = 3847
215808 Wp = 79
71262
YDOT = 2883
500378 meter/sec RA = 304
74786 deg
ZDOT = 6016
514886 TA = 281
54927
MA = 281
65184
Ha = 186
257 n
mi
Hp = 178
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12814755
01 X = 3966237
98
Y = -17942180
90 feet Y = -5424761
09 meter
Z = 379481
00 Z = 134786
28
XDOT = 12622
099107 XDOT = 3785
459443
YDOT = 9460
303077 feet/sec YDOT = 2926
176149 meter/sec
ZDOT = 19739
222068 ZDOT = 6035
054700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21443247
01 X = 6535901
69
Y = 5124826
59 feet Y = 1562047
14 meter
Z = 455101
28 Z = 138714
87
XDOT = -3689
826998 XDOT = -1124
659269
YDOT = 13582
195249 feet/sec YDOT = 4139
853112 meter/sec
ZDOT = 19812
676960 ZDOT = 6038
903937
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 10013
56309152
00016717 00000-0 10270-3 0 9070
2 25544 51
6452 305
0368 0007035 181
2536 178
8613 15
77354677 39111
Satellite: ISS
Catalog Number: 25544
Epoch time: 10013
56309152 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 305
0368 deg
Eccentricity:
0007035
Arg of perigee: 181
2536 deg
Mean anomaly: 178
8613 deg
Mean motion: 15
77354677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3911
Checksum: 305
Coasting Arc #9 (Orbit 3925)
---------------------------------------
Vector Time (GMT): 2010/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2754756
17 A = 6711200
68 meter
Y = -3408373
55 meter E =
0016282
Z = -5096098
24 I = 51
33609
XDOT = 4682
951701 Wp = 126
19935
YDOT = -5935
777217 meter/sec RA = 299
55332 deg
ZDOT = 1432
243371 TA = 157
62647
MA = 157
55537
Ha = 186
082 n
mi
Hp = 178
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9037913
94 X = -2691683
00
Y = -11182327
92 feet Y = -3438825
61 meter
Z = -16719482
42 Z = -5109327
76
XDOT = 15364
014767 XDOT = 4742
021131
YDOT = -19474
334703 feet/sec YDOT = -5883
079576 meter/sec
ZDOT = 4698
961191 ZDOT = 1455
135452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6784368
59 X = 2067875
55
Y = -12607309
12 feet Y = -3842707
82 meter
Z = -16771927
09 Z = -5112083
38
XDOT = 23007
541736 XDOT = 7012
698721
YDOT = 5981
995973 feet/sec YDOT = 1823
312372 meter/sec
ZDOT = 4789
504291 ZDOT = 1459
840908
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 10014
51339773
00016717 00000-0 10270-3 0 9089
2 25544 51
6459 300
1326 0006995 184
9625 175
1471 15
77377312 39260
Satellite: ISS
Catalog Number: 25544
Epoch time: 10014
51339773 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 300
1326 deg
Eccentricity:
0006995
Arg of perigee: 184
9625 deg
Mean anomaly: 175
1471 deg
Mean motion: 15
77377312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3926
Checksum: 323
Coasting Arc #10 (Orbit 3941)
---------------------------------------
Vector Time (GMT): 2010/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4181207
16 A = 6720091
94 meter
Y = 4709623
90 meter E =
0011297
Z = -2328207
11 I = 51
35308
XDOT = -2517
651973 Wp = 164
52133
YDOT = -4894
545498 meter/sec RA = 294
40460 deg
ZDOT = -5396
258826 TA = 41
83629
MA = 41
75001
Ha = 185
860 n
mi
Hp = 178
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13717871
25 X = -4222250
51
Y = 15451521
97 feet Y = 4662637
92 meter
Z = -7638474
78 Z = -2348618
15
XDOT = -8260
013034 XDOT = -2436
519762
YDOT = -16058
220138 feet/sec YDOT = -4922
245193 meter/sec
ZDOT = -17704
261240 ZDOT = -5408
292718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19683234
80 X = -5999449
97
Y = -6185456
16 feet Y = -1885327
04 meter
Z = -7719211
10 Z = -2352815
54
XDOT = 10887
235191 XDOT = 3318
429286
YDOT = -12559
125247 feet/sec YDOT = -3828
021375 meter/sec
ZDOT = -17752
007695 ZDOT = -5410
811946
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 10015
52704310
00016717 00000-0 10270-3 0 9095
2 25544 51
6464 294
9019 0007001 188
9852 171
1189 15
77401769 39424
Satellite: ISS
Catalog Number: 25544
Epoch time: 10015
52704310 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 294
9019 deg
Eccentricity:
0007001
Arg of perigee: 188
9852 deg
Mean anomaly: 171
1189 deg
Mean motion: 15
77401769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 313
Coasting Arc #11 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2010/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1703057
05 A = 6715138
56 meter
Y = 5045803
76 meter E =
0009719
Z = 4080098
11 I = 51
32434
XDOT = -4826
828229 Wp = 115
76079
YDOT = 4683
007215 meter/sec RA = 289
17558 deg
ZDOT = -3773
882830 TA = 13
06885
MA = 13
04368
Ha = 185
720 n
mi
Hp = 178
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5587457
51 X = 1626687
52
Y = 16554474
27 feet Y = 5064421
01 meter
Z = 13386148
67 Z = 4088186
28
XDOT = -15836
050620 XDOT = -4860
503320
YDOT = 15364
196899 feet/sec YDOT = 4628
842789 meter/sec
ZDOT = -12381
505348 ZDOT = -3797
412389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12666038
58 X = -3860608
56
Y = 11999183
46 feet Y = 3657351
12 meter
Z = 13418283
74 Z = 4089892
89
XDOT = -19717
424137 XDOT = -6009
870877
YDOT = -6853
119924 feet/sec YDOT = -2088
830953 meter/sec
ZDOT = -12474
586464 ZDOT = -3802
253954
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 10016
54067365
00016717 00000-0 10270-3 0 9102
2 25544 51
6456 289
6712 0006959 192
5680 167
5313 15
77420863 39588
Satellite: ISS
Catalog Number: 25544
Epoch time: 10016
54067365 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 289
6712 deg
Eccentricity:
0006959
Arg of perigee: 192
5680 deg
Mean anomaly: 167
5313 deg
Mean motion: 15
77420863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 334
Coasting Arc #12 (Orbit 3973)
---------------------------------------
Vector Time (GMT): 2010/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197565
26 A = 6714983
18 meter
Y = -3271386
43 meter E =
0012339
Z = 4094365
57 I = 51
31554
XDOT = 1450
531095 Wp = 138
52893
YDOT = 6573
149716 meter/sec RA = 284
04207 deg
ZDOT = 3749
264303 TA = 272
83804
MA = 272
97925
Ha = 185
571 n
mi
Hp = 178
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13771539
57 X = 4213945
31
Y = -10732895
12 feet Y = -3224355
45 meter
Z = 13432957
90 Z = 4114796
42
XDOT = 4758
960284 XDOT = 1358
708367
YDOT = 21565
451825 feet/sec YDOT = 6588
856771 meter/sec
ZDOT = 12300
735902 ZDOT = 3756
088190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15652915
86 X = 4771008
75
Y = 7593306
15 feet Y = 2314439
71 meter
Z = 13513793
87 Z = 4119004
37
XDOT = -16767
453161 XDOT = -5110
719724
YDOT = 12534
257381 feet/sec YDOT = 3820
441650 meter/sec
ZDOT = 12327
909250 ZDOT = 3757
546740
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 10017
55428842
00016717 00000-0 10270-3 0 9116
2 25544 51
6459 284
4395 0006921 196
7799 163
3138 15
77445680 39748
Satellite: ISS
Catalog Number: 25544
Epoch time: 10017
55428842 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 284
4395 deg
Eccentricity:
0006921
Arg of perigee: 196
7799 deg
Mean anomaly: 163
3138 deg
Mean motion: 15
77445680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 348
Coasting Arc #13 (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 = -879002
15 A = 6719975
02 meter
Y = -6260676
08 meter E =
0002766
Z = -2283413
41 I = 51
32688
XDOT = 4794
051447 Wp = 144
43956
YDOT = -2646
763865 meter/sec RA = 278
81090 deg
ZDOT = 5412
501756 TA = 189
76801
MA = 189
77339
Ha = 185
406 n
mi
Hp = 178
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2883865
31 X = -797836
67
Y = -20540275
84 feet Y = -6270051
68 meter
Z = -7491513
81 Z = -2287486
64
XDOT = 15728
515247 XDOT = 4796
999365
YDOT = -8683
608480 feet/sec YDOT = -2593
137701 meter/sec
ZDOT = 17757
551692 ZDOT = 5435
797774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17008894
54 X = 5184311
06
Y = -11860558
90 feet Y = -3615098
35 meter
Z = -7507798
55 Z = -2288377
00
XDOT = 13968
007972 XDOT = 4257
448830
YDOT = 8734
346263 feet/sec YDOT = 2662
228741 meter/sec
ZDOT = 17849
745852 ZDOT = 5440
602536
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
50453825
00016717 00000-0 10270-3 0 9122
2 25544 51
6461 279
5347 0006932 201
0247 159
0634 15
77488886 39897
Satellite: ISS
Catalog Number: 25544
Epoch time: 10018
50453825 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 279
5347 deg
Eccentricity:
0006932
Arg of perigee: 201
0247 deg
Mean anomaly: 159
0634 deg
Mean motion: 15
77488886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 333
Coasting Arc #14 (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 = -4182283
84 A = 6710676
32 meter
Y = 1231105
16 meter E =
0011566
Z = -5110294
27 I = 51
29233
XDOT = -593
754274 Wp = 108
40586
YDOT = -7558
425989 meter/sec RA = 273
65710 deg
ZDOT = -1341
027874 TA = 148
73154
MA = 148
66269
Ha = 185
110 n
mi
Hp = 178
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13721403
66 X = -4170915
04
Y = 4039058
93 feet Y = 1184400
11 meter
Z = -16766057
30 Z = -5130583
75
XDOT = -1948
012710 XDOT = -502
676149
YDOT = -24797
985527 feet/sec YDOT = -7564
556415 meter/sec
ZDOT = -4399
697750 ZDOT = -1343
691280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9961889
70 X = -3036383
98
Y = -10131725
48 feet Y = -3088149
93 meter
Z = -16846379
00 Z = -5134776
32
XDOT = 20253
587826 XDOT = 6173
293569
YDOT = -12613
698884 feet/sec YDOT = -3844
655420 meter/sec
ZDOT = -4410
443453 ZDOT = -1344
303165
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
51812357
00016717 00000-0 10270-3 0 9134
2 25544 51
6460 274
3030 0006847 205
6091 154
4736 15
77519598 40057
Satellite: ISS
Catalog Number: 25544
Epoch time: 10019
51812357 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 274
3030 deg
Eccentricity:
0006847
Arg of perigee: 205
6091 deg
Mean anomaly: 154
4736 deg
Mean motion: 15
77519598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 305
Coasting Arc #15 (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 = 178217
74 A = 6722294
31 meter
Y = 6709984
06 meter E =
0015714
Z = -2732
48 I = 51
33027
XDOT = -4816
788251 Wp = 160
26818
YDOT = 129
575124 meter/sec RA = 268
45991 deg
ZDOT = -6021
026748 TA = 19
76169
MA = 19
70087
Ha = 185
114 n
mi
Hp = 179
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 584703
86 X = 103185
54
Y = 22014383
40 feet Y = 6711557
47 meter
Z = -8964
83 Z = -2048
81
XDOT = -15803
111061 XDOT = -4788
630601
YDOT = 425
115237 feet/sec YDOT = 75
868522 meter/sec
ZDOT = -19754
024765 ZDOT = -6044
357932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18973018
49 X = -5782976
04
Y = 11180320
57 feet Y = 3407761
71 meter
Z = -6072
51 Z = -1850
90
XDOT = -7158
506698 XDOT = -2181
912841
YDOT = -12132
335170 feet/sec YDOT = -3697
935760 meter/sec
ZDOT = -19846
422946 ZDOT = -6049
189714
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
53169543
00016717 00000-0 10270-3 0 9141
2 25544 51
6459 269
0712 0007029 209
2225 150
8548 15
77481063 40219
Satellite: ISS
Catalog Number: 25544
Epoch time: 10020
53169543 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 269
0712 deg
Eccentricity:
0007029
Arg of perigee: 209
2225 deg
Mean anomaly: 150
8548 deg
Mean motion: 15
77481063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4021
Checksum: 294
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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