Date:
February 10th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4305 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
044/07:19:00
000 0
0 0
0 0
0
N/A 0
0 0
0 197
2
000/00:00:00
000 0
0 0
0 186
8
Coasting Arc #1 (Orbit 2587)
---------------------------------------
Vector Time (GMT): 2009/040/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 624260
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 626373
65 A = 6734055
37 meter
Y = -5337462
87 meter E =
0012711
Z = 4043916
52 I = 51
34674
XDOT = 5643
657664 Wp = 60
56500
YDOT = 3572
187596 meter/sec RA = 239
69105 deg
ZDOT = 3837
792713 TA = 349
78263
MA = 349
80844
Ha = 196
880 n
mi
Hp = 187
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2055031
66 X = 666367
54
Y = -17511361
11 feet Y = -5330234
77 meter
Z = 13267442
66 Z = 4047056
50
XDOT = 18515
937219 XDOT = 5584
650755
YDOT = 11719
775579 feet/sec YDOT = 3634
968340 meter/sec
ZDOT = 12591
183442 ZDOT = 3865
065340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9456412
18 X = 2882314
43
Y = -14870566
45 feet Y = -4532548
65 meter
Z = 13279249
98 Z = 4047515
39
XDOT = 10352
121059 XDOT = 3155
326499
YDOT = 17930
444548 feet/sec YDOT = 5465
199498 meter/sec
ZDOT = 12697
732395 ZDOT = 3870
268834
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 09040
59644537
00010596 00000-0 82463-4 0 9006
2 25544 51
6363 240
2749 0008689 4
2508 355
8726 15
70845073 25883
Satellite: ISS
Catalog Number: 25544
Epoch time: 09040
59644537 = yrday
fracday
Element set: 900
Inclination: 51
6363 deg
RA of node: 240
2749 deg
Eccentricity:
0008689
Arg of perigee: 4
2508 deg
Mean anomaly: 355
8726 deg
Mean motion: 15
70845073 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2588
Checksum: 329
Coasting Arc #2 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2009/041/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 624260
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5123610
23 A = 6733839
39 meter
Y = -1561822
10 meter E =
0010477
Z = -4084222
73 I = 51
36214
XDOT = -995
579801 Wp = 55
61437
YDOT = -6617
183361 meter/sec RA = 234
50752 deg
ZDOT = 3792
123784 TA = 253
46633
MA = 253
58146
Ha = 196
966 n
mi
Hp = 187
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16809744
84 X = -5085925
07
Y = -5124088
24 feet Y = -1618906
70 meter
Z = -13399680
87 Z = -4109020
87
XDOT = -3266
337930 XDOT = -939
932253
YDOT = -21709
919165 feet/sec YDOT = -6628
005254 meter/sec
ZDOT = 12441
350996 ZDOT = 3787
422776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12994505
49 X = -3960725
27
Y = -11720251
38 feet Y = -3572332
62 meter
Z = -13496435
97 Z = -4113713
68
XDOT = 5302
810825 XDOT = 1616
296739
YDOT = -20136
640031 feet/sec YDOT = -6137
647881 meter/sec
ZDOT = 12422
491630 ZDOT = 3786
375449
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 09041
55070713
00010596 00000-0 82463-4 0 9013
2 25544 51
6363 235
3960 0008626 9
2747 350
8572 15
70844543 26037
Satellite: ISS
Catalog Number: 25544
Epoch time: 09041
55070713 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 235
3960 deg
Eccentricity:
0008626
Arg of perigee: 9
2747 deg
Mean anomaly: 350
8572 deg
Mean motion: 15
70844543 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2603
Checksum: 300
Coasting Arc #3 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2009/042/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 624260
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2357895
03 A = 6738415
07 meter
Y = 5807145
20 meter E =
0007879
Z = -2487944
76 I = 51
39626
XDOT = -5570
073951 Wp = 50
43020
YDOT = -4
408049 meter/sec RA = 229
42402 deg
ZDOT = -5295
425619 TA = 157
74154
MA = 157
70732
Ha = 197
168 n
mi
Hp = 187
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7735876
08 X = 2304869
00
Y = 19052313
65 feet Y = 5833215
95 meter
Z = -8162548
43 Z = -2476619
49
XDOT = -18274
520837 XDOT = -5543
887122
YDOT = -14
462103 feet/sec YDOT = -66
549698 meter/sec
ZDOT = -17373
443631 ZDOT = -5322
420732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -652066
40 X = -198749
84
Y = 20570260
01 feet Y = 6269815
25 meter
Z = -8117933
45 Z = -2474346
12
XDOT = -15092
143349 XDOT = -4600
085293
YDOT = -7368
155596 feet/sec YDOT = -2245
813826 meter/sec
ZDOT = -17478
636353 ZDOT = -5327
488360
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 09042
56857864
00010596 00000-0 82463-4 0 9026
2 25544 51
6367 230
1926 0008835 13
3245 346
8148 15
70880454 26199
Satellite: ISS
Catalog Number: 25544
Epoch time: 09042
56857864 = yrday
fracday
Element set: 902
Inclination: 51
6367 deg
RA of node: 230
1926 deg
Eccentricity:
0008835
Arg of perigee: 13
3245 deg
Mean anomaly: 346
8148 deg
Mean motion: 15
70880454 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2619
Checksum: 325
Coasting Arc #4 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2009/043/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 624260
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4223249
88 A = 6730167
16 meter
Y = -1485059
39 meter E =
0013269
Z = 5022283
59 I = 51
38794
XDOT = 4282
731818 Wp = 31
85528
YDOT = 6147
348055 meter/sec RA = 224
25789 deg
ZDOT = -1770
391289 TA = 75
33418
MA = 75
18712
Ha = 197
188 n
mi
Hp = 187
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13855806
68 X = 4215145
33
Y = -4872242
10 feet Y = -1437877
60 meter
Z = 16477308
37 Z = 5042780
11
XDOT = 14050
957407 XDOT = 4222
272918
YDOT = 20168
464749 feet/sec YDOT = 6194
901913 meter/sec
ZDOT = -5808
370372 ZDOT = -1749
733392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14569468
78 X = 4440774
08
Y = 904597
20 feet Y = 275721
23 meter
Z = 16557055
79 Z = 5046590
60
XDOT = 5129
111530 XDOT = 1563
353194
YDOT = 23010
290858 feet/sec YDOT = 7013
536653 meter/sec
ZDOT = -5727
351491 ZDOT = -1745
696734
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 09043
58644534
00010596 00000-0 82463-4 0 9038
2 25544 51
6364 224
9884 0008656 17
6913 342
4548 15
70828863 26350
Satellite: ISS
Catalog Number: 25544
Epoch time: 09043
58644534 = yrday
fracday
Element set: 903
Inclination: 51
6364 deg
RA of node: 224
9884 deg
Eccentricity:
0008656
Arg of perigee: 17
6913 deg
Mean anomaly: 342
4548 deg
Mean motion: 15
70828863 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2635
Checksum: 338
Coasting Arc #5 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2009/044/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030693
65 A = 6729782
99 meter
Y = -1866425
55 meter E =
0013430
Z = 5052552
29 I = 51
40891
XDOT = 4782
462495 Wp = 31
09345
YDOT = 5800
501967 meter/sec RA = 220
35032 deg
ZDOT = -1659
216415 TA = 74
98653
MA = 74
83793
Ha = 197
197 n
mi
Hp = 186
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13224060
54 X = 4026720
79
Y = -6123443
39 feet Y = -1821373
94 meter
Z = 16576615
13 Z = 5072123
51
XDOT = 15690
493749 XDOT = 4725
304916
YDOT = 19030
518263 feet/sec YDOT = 5853
662575 meter/sec
ZDOT = -5443
623409 ZDOT = -1636
122735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1880171
66 X = 573076
32
Y = 14363431
27 feet Y = 4377973
85 meter
Z = 16652726
56 Z = 5075751
06
XDOT = -21837
616652 XDOT = -6656
105556
YDOT = 9115
208569 feet/sec YDOT = 2778
315572 meter/sec
ZDOT = -5353
136365 ZDOT = -1631
635964
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 09044
34983749
00010596 00000-0 82463-4 0 9048
2 25544 51
6412 221
0909 0009059 18
0034 342
1447 15
70917797 26470
Satellite: ISS
Catalog Number: 25544
Epoch time: 09044
34983749 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 221
0909 deg
Eccentricity:
0009059
Arg of perigee: 18
0034 deg
Mean anomaly: 342
1447 deg
Mean motion: 15
70917797 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2647
Checksum: 318
Coasting Arc #6 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2009/045/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5273545
86 A = 6740960
89 meter
Y = -4156088
89 meter E =
0021445
Z = 441273
39 I = 51
46965
XDOT = 3293
805844 Wp = 38
32588
YDOT = -3527
154967 meter/sec RA = 215
24185 deg
ZDOT = 6004
426800 TA = 326
48290
MA = 326
61841
Ha = 197
404 n
mi
Hp = 186
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17301659
63 X = -5228823
44
Y = -13635462
23 feet Y = -4214810
67 meter
Z = 1447747
33 Z = 415763
64
XDOT = 10806
449620 XDOT = 3303
834254
YDOT = -11572
030733 feet/sec YDOT = -3490
265419 meter/sec
ZDOT = 19699
562993 ZDOT = 6020
452377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18003985
52 X = 5487614
79
Y = -12704672
00 feet Y = -3872384
03 meter
Z = 1347977
47 Z = 410863
53
XDOT = 7117
308600 XDOT = 2169
355661
YDOT = 12234
696727 feet/sec YDOT = 3729
135562 meter/sec
ZDOT = 19761
719292 ZDOT = 6023
372040
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 09045
36769135
00010596 00000-0 82463-4 0 9053
2 25544 51
6414 215
8876 0009097 21
9177 338
2372 15
70896155 26634
Satellite: ISS
Catalog Number: 25544
Epoch time: 09045
36769135 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 215
8876 deg
Eccentricity:
0009097
Arg of perigee: 21
9177 deg
Mean anomaly: 338
2372 deg
Mean motion: 15
70896155 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2663
Checksum: 337
Coasting Arc #7 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2009/046/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1475788
76 A = 6729066
16 meter
Y = 3973425
71 meter E =
0020948
Z = -5243236
57 I = 51
45419
XDOT = -6860
913937 Wp = 62
92545
YDOT = -3395
512897 meter/sec RA = 210
11852 deg
ZDOT = -634
657942 TA = 200
96746
MA = 201
05348
Ha = 197
490 n
mi
Hp = 186
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4841826
64 X = -1494640
20
Y = 13036173
59 feet Y = 3956817
08 meter
Z = -17202219
73 Z = -5250451
73
XDOT = -22509
560162 XDOT = -6819
351817
YDOT = -11140
134175 feet/sec YDOT = -3472
003252 meter/sec
ZDOT = -2082
211097 ZDOT = -667
886827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11283749
89 X = -3439286
97
Y = -8068792
81 feet Y = -2459368
05 meter
Z = -17230004
11 Z = -5251705
25
XDOT = 16183
720100 XDOT = 4932
797886
YDOT = -17856
629253 feet/sec YDOT = -5442
700596 meter/sec
ZDOT = -2212
009122 ZDOT = -674
220380
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 09046
32192233
00010596 00000-0 82463-4 0 9060
2 25544 51
6410 211
0095 0009157 25
0538 335
1066 15
70916039 26780
Satellite: ISS
Catalog Number: 25544
Epoch time: 09046
32192233 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 211
0095 deg
Eccentricity:
0009157
Arg of perigee: 25
0538 deg
Mean anomaly: 335
1066 deg
Mean motion: 15
70916039 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2678
Checksum: 290
Coasting Arc #8 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2009/047/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6358515
74 A = 6739981
66 meter
Y = 1626262
63 meter E =
0017033
Z = 1522887
32 I = 51
51702
XDOT = 90
451367 Wp = 85
32810
YDOT = 5095
718488 meter/sec RA = 204
97593 deg
ZDOT = -5762
621439 TA = 77
88890
MA = 77
69811
Ha = 197
611 n
mi
Hp = 186
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20861272
10 X = 6332460
20
Y = 5335507
31 feet Y = 1697221
56 meter
Z = 4996349
48 Z = 1553713
30
XDOT = 296
756454 XDOT = 61
456888
YDOT = 16718
236508 feet/sec YDOT = 5096
567845 meter/sec
ZDOT = -18906
238317 ZDOT = -5762
252464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10411455
72 X = -3173411
70
Y = 18816093
56 feet Y = 5735145
32 meter
Z = 5116642
76 Z = 1559552
71
XDOT = -14909
036321 XDOT = -4544
274271
YDOT = -3059
564666 feet/sec YDOT = -932
555310 meter/sec
ZDOT = -18904
368523 ZDOT = -5762
051526
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 09047
33976308
00010596 00000-0 82463-4 0 9076
2 25544 51
6410 205
8067 0009154 29
5171 330
6506 15
70892795 26948
Satellite: ISS
Catalog Number: 25544
Epoch time: 09047
33976308 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 205
8067 deg
Eccentricity:
0009154
Arg of perigee: 29
5171 deg
Mean anomaly: 330
6506 deg
Mean motion: 15
70892795 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2694
Checksum: 324
Coasting Arc #9 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2009/048/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1696079
83 A = 6731667
83 meter
Y = -4547111
25 meter E =
0012934
Z = 4652611
76 I = 51
51539
XDOT = 7168
080097 Wp = 71
32931
YDOT = 211
473288 meter/sec RA = 199
89033 deg
ZDOT = 2817
458629 TA = 350
80928
MA = 350
83293
Ha = 197
750 n
mi
Hp = 186
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5564566
38 X = -1667708
44
Y = -14918344
00 feet Y = -4565919
23 meter
Z = 15264474
29 Z = 4644441
18
XDOT = 23517
323153 XDOT = 7151
496119
YDOT = 693
810000 feet/sec YDOT = 291
538165 meter/sec
ZDOT = 9243
630671 ZDOT = 2852
240366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15829258
46 X = 4824757
98
Y = -1984705
33 feet Y = -604938
18 meter
Z = 15232238
29 Z = 4642786
23
XDOT = -6338
591161 XDOT = -1932
002586
YDOT = 21487
631886 feet/sec YDOT = 6549
430199 meter/sec
ZDOT = 9379
237193 ZDOT = 2858
791497
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 09048
35759581
00010596 00000-0 82463-4 0 9082
2 25544 51
6403 200
6027 0009275 32
6181 327
5552 15
70891006 27108
Satellite: ISS
Catalog Number: 25544
Epoch time: 09048
35759581 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 200
6027 deg
Eccentricity:
0009275
Arg of perigee: 32
6181 deg
Mean anomaly: 327
5552 deg
Mean motion: 15
70891006 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2710
Checksum: 300
Coasting Arc #10 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2009/049/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5739693
44 A = 6736074
95 meter
Y = 1210071
81 meter E =
0012633
Z = -3312157
26 I = 51
55809
XDOT = -3715
788547 Wp = 53
20432
YDOT = -4829
408984 meter/sec RA = 194
72375 deg
ZDOT = 4694
516379 TA = 267
91096
MA = 268
05564
Ha = 197
603 n
mi
Hp = 186
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18831015
24 X = -5736708
51
Y = 3970051
86 feet Y = 1145903
97 meter
Z = -10866657
67 Z = -3340032
92
XDOT = -12190
907308 XDOT = -3684
313839
YDOT = -15844
517663 feet/sec YDOT = -4870
785200 meter/sec
ZDOT = 15401
956625 ZDOT = 4676
541753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 226403
89 X = 69007
91
Y = -19181909
84 feet Y = -5846646
12 meter
Z = -10975234
48 Z = -3345251
47
XDOT = 16745
685789 XDOT = 5104
085028
YDOT = -8537
783684 feet/sec YDOT = -2602
316467 meter/sec
ZDOT = 15331
469339 ZDOT = 4673
031855
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 09049
31180602
00010596 00000-0 82463-4 0 9092
2 25544 51
6394 195
7242 0009145 35
2219 324
9546 15
70929662 27257
Satellite: ISS
Catalog Number: 25544
Epoch time: 09049
31180602 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 195
7242 deg
Eccentricity:
0009145
Arg of perigee: 35
2219 deg
Mean anomaly: 324
9546 deg
Mean motion: 15
70929662 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2725
Checksum: 319
Coasting Arc #11 (Orbit 2740)
---------------------------------------
Vector Time (GMT): 2009/050/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597477
36 A = 6735898
25 meter
Y = 3544098
44 meter E =
0012865
Z = -3433250
70 I = 51
58517
XDOT = -5527
924163 Wp = 56
45007
YDOT = 2741
629786 meter/sec RA = 189
65750 deg
ZDOT = -4577
649944 TA = 164
06928
MA = 164
02877
Ha = 197
740 n
mi
Hp = 186
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15083587
14 X = 4574182
73
Y = 11627619
55 feet Y = 3595379
92 meter
Z = -11263945
86 Z = -3410973
13
XDOT = -18136
234132 XDOT = -5535
933746
YDOT = 8994
848379 feet/sec YDOT = 2679
768628 meter/sec
ZDOT = -15018
536561 ZDOT = -4604
523439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14443487
50 X = -4402374
99
Y = 12492312
34 feet Y = 3807656
80 meter
Z = -11176780
16 Z = -3406682
59
XDOT = -4259
097692 XDOT = -1298
172976
YDOT = -18439
057560 feet/sec YDOT = -5620
224744 meter/sec
ZDOT = -15123
088169 ZDOT = -4609
517274
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 09050
32962469
00010596 00000-0 82463-4 0 9106
2 25544 51
6385 190
5207 0009167 39
0542 321
1280 15
70933853 27415
Satellite: ISS
Catalog Number: 25544
Epoch time: 09050
32962469 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 190
5207 deg
Eccentricity:
0009167
Arg of perigee: 39
0542 deg
Mean anomaly: 321
1280 deg
Mean motion: 15
70933853 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2741
Checksum: 301
Coasting Arc #12 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2009/051/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3619854
82 A = 6731667
81 meter
Y = -3351465
82 meter E =
0017166
Z = 4573519
98 I = 51
60118
XDOT = 6479
661600 Wp = 53
47262
YDOT = 2889
135475 meter/sec RA = 184
49365 deg
ZDOT = -2993
579627 TA = 66
35675
MA = 66
17665
Ha = 197
656 n
mi
Hp = 185
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11876164
12 X = 3634845
64
Y = -10995622
76 feet Y = -3310902
73 meter
Z = 15004986
81 Z = 4591141
18
XDOT = 21258
732283 XDOT = 6461
415146
YDOT = 9478
790929 feet/sec YDOT = 2961
492833 meter/sec
ZDOT = -9821
455470 ZDOT = -2962
146475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8627635
21 X = 2629703
21
Y = 13618099
65 feet Y = 4150796
77 meter
Z = 15073416
87 Z = 4594377
46
XDOT = -12261
126817 XDOT = -3737
191454
YDOT = 18567
362698 feet/sec YDOT = 5659
332150 meter/sec
ZDOT = -9698
629904 ZDOT = -2956
142395
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 09051
34743521
00010596 00000-0 82463-4 0 9116
2 25544 51
6389 185
3164 0009131 42
4119 317
7747 15
70965127 27577
Satellite: ISS
Catalog Number: 25544
Epoch time: 09051
34743521 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 185
3164 deg
Eccentricity:
0009131
Arg of perigee: 42
4119 deg
Mean anomaly: 317
7747 deg
Mean motion: 15
70965127 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2757
Checksum: 313
Coasting Arc #13 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2009/052/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6383338
60 A = 6739623
76 meter
Y = -1277650
16 meter E =
0022963
Z = 1697197
87 I = 51
65625
XDOT = 2442
478265 Wp = 57
55168
YDOT = -4548
386925 meter/sec RA = 179
41757 deg
ZDOT = 5718
538646 TA = 321
21144
MA = 321
37606
Ha = 197
812 n
mi
Hp = 185
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20942711
93 X = -6376821
74
Y = -4191765
60 feet Y = -1348995
92 meter
Z = 5568234
50 Z = 1666204
27
XDOT = 8013
380134 XDOT = 2465
378666
YDOT = -14922
529280 feet/sec YDOT = -4520
945661 meter/sec
ZDOT = 18761
609732 ZDOT = 5730
459520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7652869
31 X = 2332594
57
Y = -19973342
70 feet Y = -6087874
85 meter
Z = 5447246
09 Z = 1660320
61
XDOT = 11927
298436 XDOT = 3635
440563
YDOT = 9739
451750 feet/sec YDOT = 2968
584893 meter/sec
ZDOT = 18807
710437 ZDOT = 5732
590141
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 09052
36523955
00010596 00000-0 82463-4 0 9127
2 25544 51
6379 180
1122 0009129 46
9069 313
2855 15
70971405 27738
Satellite: ISS
Catalog Number: 25544
Epoch time: 09052
36523955 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 180
1122 deg
Eccentricity:
0009129
Arg of perigee: 46
9069 deg
Mean anomaly: 313
2855 deg
Mean motion: 15
70971405 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2773
Checksum: 315
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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