Date:
November 13th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2935)
---------------------------------------
Vector Time (GMT): 2009/316/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4240326
45 A = 6714383
56 meter
Y = 1167803
89 meter E =
0007830
Z = 5075202
10 I = 51
29531
XDOT = -281
061193 Wp = 358
90541
YDOT = 7551
559329 meter/sec RA = 263
00976 deg
ZDOT = -1495
095822 TA = 105
53884
MA = 105
45238
Ha = 186
476 n
mi
Hp = 181
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13911832
18 X = 4202297
68
Y = 3831377
60 feet Y = 1215009
12 meter
Z = 16650925
52 Z = 5095709
73
XDOT = -922
116775 XDOT = -358
220072
YDOT = 24775
457116 feet/sec YDOT = 7547
984911 meter/sec
ZDOT = -4905
170021 ZDOT = -1496
648715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6061715
63 X = 1847610
92
Y = 12991237
90 feet Y = 3959729
31 meter
Z = 16731861
56 Z = 5099871
40
XDOT = -18467
819584 XDOT = -5628
991409
YDOT = 14974
463751 feet/sec YDOT = 4564
216551 meter/sec
ZDOT = -4910
988127 ZDOT = -1496
869181
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 09316
76536809
00016717 00000-0 10270-3 0 9000
2 25544 51
6458 263
5885 0006456 322
1269 37
9440 15
76267884 29365
Satellite: ISS
Catalog Number: 25544
Epoch time: 09316
76536809 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 263
5885 deg
Eccentricity:
0006456
Arg of perigee: 322
1269 deg
Mean anomaly: 37
9440 deg
Mean motion: 15
76267884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 349
Coasting Arc #2 (Orbit 2951)
---------------------------------------
Vector Time (GMT): 2009/317/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 283481
74 A = 6723867
79 meter
Y = -6395564
69 meter E =
0014108
Z = 2026496
31 I = 51
33175
XDOT = 4969
742478 Wp = 42
36063
YDOT = 1982
872588 meter/sec RA = 257
86416 deg
ZDOT = 5550
596581 TA = 340
37781
MA = 340
43204
Ha = 186
609 n
mi
Hp = 181
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 930058
22 X = 345132
36
Y = -20982823
80 feet Y = -6392049
94 meter
Z = 6648609
94 Z = 2028023
20
XDOT = 16304
929389 XDOT = 4920
235706
YDOT = 6505
487492 feet/sec YDOT = 2038
170325 meter/sec
ZDOT = 18210
618703 ZDOT = 5574
620052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16305155
05 X = 4969811
26
Y = -13236660
58 feet Y = -4034534
14 meter
Z = 6654370
93 Z = 2028252
26
XDOT = 4896
006647 XDOT = 1492
302826
YDOT = 15253
478687 feet/sec YDOT = 4649
260304 meter/sec
ZDOT = 18305
458197 ZDOT = 5579
503658
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 09317
77974325
00016717 00000-0 10270-3 0 9012
2 25544 51
6452 258
3613 0006485 325
6991 34
3754 15
76293718 29524
Satellite: ISS
Catalog Number: 25544
Epoch time: 09317
77974325 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 258
3613 deg
Eccentricity:
0006485
Arg of perigee: 325
6991 deg
Mean anomaly: 34
3754 deg
Mean motion: 15
76293718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2952
Checksum: 340
Coasting Arc #3 (Orbit 2966)
---------------------------------------
Vector Time (GMT): 2009/318/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4466742
50 A = 6716668
90 meter
Y = -2258164
05 meter E =
0006377
Z = -4483263
81 I = 51
31497
XDOT = 423
739109 Wp = 71
44815
YDOT = -7026
166815 meter/sec RA = 252
64575 deg
ZDOT = 3122
440029 TA = 229
82024
MA = 229
87609
Ha = 186
617 n
mi
Hp = 180
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14654666
99 X = -4419379
75
Y = -7408674
69 feet Y = -2307848
84 meter
Z = -14708870
75 Z = -4504848
95
XDOT = 1390
220173 XDOT = 487
106706
YDOT = -23051
728396 feet/sec YDOT = -7021
074099 meter/sec
ZDOT = 10244
225816 ZDOT = 3124
652337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4376425
27 X = -1333934
42
Y = -15747377
55 feet Y = -4799800
68 meter
Z = -14794107
15 Z = -4509243
86
XDOT = 16748
946374 XDOT = 5105
078855
YDOT = -14269
556199 feet/sec YDOT = -4349
360730 meter/sec
ZDOT = 10252
665168 ZDOT = 3125
012343
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 09318
73069364
00016717 00000-0 10270-3 0 9028
2 25544 51
6447 253
4607 0006452 329
0230 31
0553 15
76336070 29671
Satellite: ISS
Catalog Number: 25544
Epoch time: 09318
73069364 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 253
4607 deg
Eccentricity:
0006452
Arg of perigee: 329
0230 deg
Mean anomaly: 31
0553 deg
Mean motion: 15
76336070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2967
Checksum: 303
Coasting Arc #4 (Orbit 2982)
---------------------------------------
Vector Time (GMT): 2009/319/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -530640
38 A = 6720473
89 meter
Y = 5789016
85 meter E =
0006013
Z = -3379491
66 I = 51
33748
XDOT = -5294
687319 Wp = 18
41625
YDOT = -3172
028282 meter/sec RA = 247
51951 deg
ZDOT = -4598
876254 TA = 201
64800
MA = 201
67343
Ha = 186
783 n
mi
Hp = 180
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1740946
14 X = -578917
25
Y = 18992837
42 feet Y = 5782813
16 meter
Z = -11087571
06 Z = -3382186
56
XDOT = -17371
021387 XDOT = -5236
482392
YDOT = -10406
916936 feet/sec YDOT = -3230
910915 meter/sec
ZDOT = -15088
176687 ZDOT = -4624
457465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14936042
39 X = -4552505
72
Y = 11850855
50 feet Y = 3612140
76 meter
Z = -11097966
50 Z = -3382660
19
XDOT = -3473
988676 XDOT = -1058
871748
YDOT = -18613
062907 feet/sec YDOT = -5673
261574 meter/sec
ZDOT = -15189
218602 ZDOT = -4629
673830
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 09319
74501291
00016717 00000-0 10270-3 0 9031
2 25544 51
6440 248
2344 0006443 332
3909 27
6912 15
76363523 29835
Satellite: ISS
Catalog Number: 25544
Epoch time: 09319
74501291 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 248
2344 deg
Eccentricity:
0006443
Arg of perigee: 332
3909 deg
Mean anomaly: 27
6912 deg
Mean motion: 15
76363523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2983
Checksum: 310
Coasting Arc #5 (Orbit 2998)
---------------------------------------
Vector Time (GMT): 2009/320/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4794337
35 A = 6719956
47 meter
Y = 3214651
05 meter E =
0011538
Z = 3438556
70 I = 51
34994
XDOT = -864
029705 Wp = 56
98619
YDOT = 6162
818460 meter/sec RA = 242
29226 deg
ZDOT = -4539
616245 TA = 82
07117
MA = 81
94024
Ha = 186
748 n
mi
Hp = 180
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15729453
23 X = 4741329
82
Y = 10546755
41 feet Y = 3267967
52 meter
Z = 11281354
01 Z = 3461719
80
XDOT = -2834
743126 XDOT = -910
825877
YDOT = 20219
220670 feet/sec YDOT = 6152
895057 meter/sec
ZDOT = -14893
754084 ZDOT = -4543
927045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3442525
85 X = 1049281
88
Y = 18566788
67 feet Y = 5659157
19 meter
Z = 11372865
56 Z = 3466449
42
XDOT = -15001
838614 XDOT = -4572
560410
YDOT = 11949
075610 feet/sec YDOT = 3642
078246 meter/sec
ZDOT = -14910
511380 ZDOT = -4544
723868
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 09320
75930202
00016717 00000-0 10270-3 0 9043
2 25544 51
6446 243
0069 0006571 335
6635 24
4219 15
76456952 29993
Satellite: ISS
Catalog Number: 25544
Epoch time: 09320
75930202 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 243
0069 deg
Eccentricity:
0006571
Arg of perigee: 335
6635 deg
Mean anomaly: 24
4219 deg
Mean motion: 15
76456952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2999
Checksum: 320
Coasting Arc #6 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2009/321/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1057868
59 A = 6716610
90 meter
Y = -4916674
38 meter E =
0006744
Z = 4445224
06 I = 51
35190
XDOT = 5688
267604 Wp = 67
03864
YDOT = 4109
592869 meter/sec RA = 237
16656 deg
ZDOT = 3190
526993 TA = 350
95360
MA = 350
96574
Ha = 186
878 n
mi
Hp = 180
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3470697
47 X = 1091174
37
Y = -16130821
46 feet Y = -4904658
86 meter
Z = 14584068
45 Z = 4450443
78
XDOT = 18662
295288 XDOT = 5626
391210
YDOT = 13482
916238 feet/sec YDOT = 4172
856168 meter/sec
ZDOT = 10467
608245 ZDOT = 3218
011455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13729492
14 X = 4184749
20
Y = -9118928
51 feet Y = -2779449
41 meter
Z = 14604464
48 Z = 4451440
77
XDOT = 3129
633771 XDOT = 953
912373
YDOT = 21656
848800 feet/sec YDOT = 6601
007514 meter/sec
ZDOT = 10576
214928 ZDOT = 3223
630310
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 09321
77356649
00016717 00000-0 10270-3 0 9054
2 25544 51
6431 237
7790 0006448 340
2705 19
8209 15
76430112 30158
Satellite: ISS
Catalog Number: 25544
Epoch time: 09321
77356649 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 237
7790 deg
Eccentricity:
0006448
Arg of perigee: 340
2705 deg
Mean anomaly: 19
8209 deg
Mean motion: 15
76430112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 306
Coasting Arc #7 (Orbit 3029)
---------------------------------------
Vector Time (GMT): 2009/322/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5098518
14 A = 6723201
57 meter
Y = -3866130
63 meter E =
0011217
Z = -2043806
47 I = 51
39131
XDOT = 1642
350484 Wp = 12
69863
YDOT = -5090
352428 meter/sec RA = 231
94996 deg
ZDOT = 5548
567619 TA = 324
38552
MA = 324
46032
Ha = 186
800 n
mi
Hp = 180
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16727421
72 X = -5044978
77
Y = -12684155
59 feet Y = -3922845
69 meter
Z = -6705401
80 Z = -2068446
02
XDOT = 5388
288989 XDOT = 1672
195040
YDOT = -16700
631326 feet/sec YDOT = -5071
820401 meter/sec
ZDOT = 18203
962004 ZDOT = 5556
618319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3348450
82 X = -1020607
81
Y = -20692192
68 feet Y = -6306980
33 meter
Z = -6802785
68 Z = -2073489
08
XDOT = 13828
381286 XDOT = 4214
890616
YDOT = -8215
289701 feet/sec YDOT = -2504
020301 meter/sec
ZDOT = 18235
523532 ZDOT = 5558
187573
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 09322
72441039
00016717 00000-0 10270-3 0 9069
2 25544 51
6421 232
8777 0006276 343
0311 17
0642 15
76496420 30303
Satellite: ISS
Catalog Number: 25544
Epoch time: 09322
72441039 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 232
8777 deg
Eccentricity:
0006276
Arg of perigee: 343
0311 deg
Mean anomaly: 17
0642 deg
Mean motion: 15
76496420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3030
Checksum: 286
Coasting Arc #8 (Orbit 3045)
---------------------------------------
Vector Time (GMT): 2009/323/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1897707
01 A = 6713549
21 meter
Y = 3939485
37 meter E =
0015183
Z = -5106718
22 I = 51
37762
XDOT = -5938
396718 Wp = 55
26591
YDOT = -4687
242111 meter/sec RA = 226
80820 deg
ZDOT = -1403
551254 TA = 201
20069
MA = 201
26368
Ha = 186
930 n
mi
Hp = 179
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6226072
87 X = -1916809
97
Y = 12924820
76 feet Y = 3918157
83 meter
Z = -16754324
86 Z = -5115983
44
XDOT = -19482
928865 XDOT = -5878
723466
YDOT = -15378
090916 feet/sec YDOT = -4753
314963 meter/sec
ZDOT = -4604
826949 ZDOT = -1432
256118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13257591
20 X = -4040913
80
Y = 5369365
99 feet Y = 1636582
75 meter
Z = -16790728
43 Z = -5117814
02
XDOT = -3527
298561 XDOT = -1075
120601
YDOT = -23521
094563 feet/sec YDOT = -7169
229623 meter/sec
ZDOT = -4718
301296 ZDOT = -1438
138235
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 09323
73861806
00016717 00000-0 10270-3 0 9070
2 25544 51
6412 227
6501 0006187 347
9529 12
1487 15
76543870 30467
Satellite: ISS
Catalog Number: 25544
Epoch time: 09323
73861806 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 227
6501 deg
Eccentricity:
0006187
Arg of perigee: 347
9529 deg
Mean anomaly: 12
1487 deg
Mean motion: 15
76543870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3046
Checksum: 321
Coasting Arc #9 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2009/324/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5202786
14 A = 6724619
13 meter
Y = 4242549
19 meter E =
0009032
Z = 356398
97 I = 51
43764
XDOT = -2785
795863 Wp = 104
08887
YDOT = 3931
470896 meter/sec RA = 221
62076 deg
ZDOT = -6007
566045 TA = 72
02356
MA = 71
92513
Ha = 186
953 n
mi
Hp = 179
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17069508
34 X = 5153227
18
Y = 13919124
64 feet Y = 4300452
68 meter
Z = 1169287
94 Z = 381554
57
XDOT = -9139
750208 XDOT = -2800
367068
YDOT = 12898
526561 feet/sec YDOT = 3900
237633 meter/sec
ZDOT = -19709
862353 ZDOT = -6021
134650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3518417
91 X = 1072413
78
Y = 21736797
93 feet Y = 6625376
01 meter
Z = 1268751
84 Z = 386715
56
XDOT = -13726
616277 XDOT = -4183
872641
YDOT = 3397
431798 feet/sec YDOT = 1035
537212 meter/sec
ZDOT = -19763
253258 ZDOT = -6023
839593
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 09324
75279587
00016717 00000-0 10270-3 0 9083
2 25544 51
6414 222
4220 0006436 350
9825 9
1223 15
76635301 30623
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324
75279587 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 222
4220 deg
Eccentricity:
0006436
Arg of perigee: 350
9825 deg
Mean anomaly: 9
1223 deg
Mean motion: 15
76635301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 300
Coasting Arc #10 (Orbit 3077)
---------------------------------------
Vector Time (GMT): 2009/325/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3014526
01 A = 6712844
73 meter
Y = -2950842
83 meter E =
0007520
Z = 5220550
43 I = 51
41978
XDOT = 5885
017484 Wp = 17
01742
YDOT = 4940
100083 meter/sec RA = 216
44835 deg
ZDOT = -598
583569 TA = 78
72680
MA = 78
64230
Ha = 186
980 n
mi
Hp = 179
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9890177
20 X = 3021937
97
Y = -9681242
88 feet Y = -2917091
67 meter
Z = 17127790
12 Z = 5235212
93
XDOT = 19307
800143 XDOT = 5832
246881
YDOT = 16207
677438 feet/sec YDOT = 5005
614819 meter/sec
ZDOT = -1963
856855 ZDOT = -570
121485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13733435
40 X = 4185951
11
Y = -976268
65 feet Y = -297566
69 meter
Z = 17185543
77 Z = 5238153
74
XDOT = 4043
941689 XDOT = 1232
593427
YDOT = 23877
751779 feet/sec YDOT = 7277
938742 meter/sec
ZDOT = -1851
296463 ZDOT = -564
275162
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 09325
76695035
00016717 00000-0 10270-3 0 9096
2 25544 51
6404 217
1931 0006078 356
1850 3
9268 15
76583611 30784
Satellite: ISS
Catalog Number: 25544
Epoch time: 09325
76695035 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 217
1931 deg
Eccentricity:
0006078
Arg of perigee: 356
1850 deg
Mean anomaly: 3
9268 deg
Mean motion: 15
76583611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3078
Checksum: 324
Coasting Arc #11 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2009/326/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4955361
70 A = 6723793
12 meter
Y = -4309645
67 meter E =
0017746
Z = 1392478
98 I = 51
48244
XDOT = 4157
092525 Wp = 43
28572
YDOT = -2890
647522 meter/sec RA = 211
29721 deg
ZDOT = 5816
454935 TA = 332
08746
MA = 332
18255
Ha = 187
014 n
mi
Hp = 179
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16257748
36 X = -4913566
69
Y = -14139257
44 feet Y = -4364825
87 meter
Z = 4568500
60 Z = 1368506
72
XDOT = 13638
755004 XDOT = 4160
851651
YDOT = -9483
751713 feet/sec YDOT = -2844
139904 meter/sec
ZDOT = 19082
857398 ZDOT = 5836
659243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3524339
65 X = -1074218
72
Y = -21276029
55 feet Y = -6484933
81 meter
Z = 4473676
03 Z = 1363576
46
XDOT = 14915
475108 XDOT = 4546
236813
YDOT = 1580
266201 feet/sec YDOT = 481
665138 meter/sec
ZDOT = 19162
495370 ZDOT = 5840
728589
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 09326
78107368
00016717 00000-0 10270-3 0 9108
2 25544 51
6405 211
9642 0006008 359
5297
5861 15
76667747 30944
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
78107368 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 211
9642 deg
Eccentricity:
0006008
Arg of perigee: 359
5297 deg
Mean anomaly:
5861 deg
Mean motion: 15
76667747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 326
Coasting Arc #12 (Orbit 3108)
---------------------------------------
Vector Time (GMT): 2009/327/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4244188
36 A = 6714530
05 meter
Y = 2134966
78 meter E =
0011753
Z = -4753864
63 I = 51
47875
XDOT = -5344
995400 Wp = 79
11987
YDOT = -4902
899848 meter/sec RA = 206
09661 deg
ZDOT = 2577
601039 TA = 216
18143
MA = 216
26099
Ha = 187
003 n
mi
Hp = 179
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13924502
48 X = -4244652
78
Y = 7004484
20 feet Y = 2087503
47 meter
Z = -15596668
75 Z = -4774484
15
XDOT = -17536
074147 XDOT = -5302
294739
YDOT = -16085
629422 feet/sec YDOT = -4962
432153 meter/sec
ZDOT = 8456
696322 ZDOT = 2551
738131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15178245
06 X = -4626329
09
Y = -3167382
30 feet Y = -965418
12 meter
Z = -15677984
90 Z = -4778649
80
XDOT = -3921
602403 XDOT = -1195
304413
YDOT = -22438
053621 feet/sec YDOT = -6839
118744 meter/sec
ZDOT = 8354
368075 ZDOT = 2546
411389
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 09327
73179085
00016717 00000-0 10270-3 0 9110
2 25544 51
6411 207
0625 0005947 4
0218 356
0993 15
76707551 31094
Satellite: ISS
Catalog Number: 25544
Epoch time: 09327
73179085 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 207
0625 deg
Eccentricity:
0005947
Arg of perigee: 4
0218 deg
Mean anomaly: 356
0993 deg
Mean motion: 15
76707551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3109
Checksum: 308
Coasting Arc #13 (Orbit 3124)
---------------------------------------
Vector Time (GMT): 2009/328/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4240252
75 A = 6720295
54 meter
Y = 4229127
10 meter E =
0006907
Z = -3059082
97 I = 51
52634
XDOT = -5569
825019 Wp = 48
22037
YDOT = 2038
774233 meter/sec RA = 200
97541 deg
ZDOT = -4904
441094 TA = 167
30347
MA = 167
28606
Ha = 187
085 n
mi
Hp = 178
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13911590
40 X = 4207507
45
Y = 13875088
93 feet Y = 4276361
18 meter
Z = -10036361
45 Z = -3038562
86
XDOT = -18273
704130 XDOT = -5568
383760
YDOT = 6688
891840 feet/sec YDOT = 1976
497470 meter/sec
ZDOT = -16090
686005 ZDOT = -4931
496082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2583476
85 X = 787443
74
Y = 19519213
06 feet Y = 5949456
14 meter
Z = -9955147
43 Z = -3034328
94
XDOT = -17055
181579 XDOT = -5198
419345
YDOT = -5999
291275 feet/sec YDOT = -1828
583981 meter/sec
ZDOT = -16197
423019 ZDOT = -4936
974536
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 09328
74586259
00016717 00000-0 10270-3 0 9128
2 25544 51
6413 201
8337 0006069 7
8198 352
3060 15
76768219 31252
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
74586259 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 201
8337 deg
Eccentricity:
0006069
Arg of perigee: 7
8198 deg
Mean anomaly: 352
3060 deg
Mean motion: 15
76768219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3125
Checksum: 324
Coasting Arc #14 (Orbit 3140)
---------------------------------------
Vector Time (GMT): 2009/329/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5427769
67 A = 6718344
85 meter
Y = -1490405
11 meter E =
0014677
Z = 3662967
49 I = 51
54822
XDOT = 4240
035227 Wp = 61
91917
YDOT = 4764
548550 meter/sec RA = 195
76024 deg
ZDOT = -4324
327936 TA = 73
93498
MA = 73
77342
Ha = 187
049 n
mi
Hp = 178
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17807643
28 X = 5426237
90
Y = -4889780
54 feet Y = -1429717
30 meter
Z = 12017609
86 Z = 3689332
25
XDOT = 13910
876730 XDOT = 4207
449238
YDOT = 15631
720965 feet/sec YDOT = 4811
781104 meter/sec
ZDOT = -14187
427610 ZDOT = -4303
808456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17146656
48 X = 5226300
89
Y = 6671037
32 feet Y = 2033332
18 meter
Z = 12121653
86 Z = 3694680
10
XDOT = 2375
180760 XDOT = 723
955096
YDOT = 19644
492528 feet/sec YDOT = 5987
641323 meter/sec
ZDOT = -14106
183682 ZDOT = -4299
564786
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 09329
75990892
00016717 00000-0 10270-3 0 9133
2 25544 51
6409 196
6042 0005907 11
4190 348
7108 15
76771923 31410
Satellite: ISS
Catalog Number: 25544
Epoch time: 09329
75990892 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 196
6042 deg
Eccentricity:
0005907
Arg of perigee: 11
4190 deg
Mean anomaly: 348
7108 deg
Mean motion: 15
76771923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3141
Checksum: 327
Coasting Arc #15 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2009/330/17:17:16
381
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3041823
66 A = 6715806
74 meter
Y = -4092197
92 meter E =
0010714
Z = 4360394
30 I = 51
57056
XDOT = 6783
691501 Wp = 76
97184
YDOT = -1445
900937 meter/sec RA = 190
64840 deg
ZDOT = 3370
822916 TA = 339
09064
MA = 339
13442
Ha = 187
085 n
mi
Hp = 178
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9979736
41 X = -3017020
35
Y = -13425846
21 feet Y = -4126074
87 meter
Z = 14305755
58 Z = 4345676
92
XDOT = 22256
205712 XDOT = 6782
980451
YDOT = -4743
769478 feet/sec YDOT = -1370
045794 meter/sec
ZDOT = 11059
130302 ZDOT = 3403
776983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -342218
44 X = -104308
18
Y = -16774868
27 feet Y = -5112979
85 meter
Z = 14247449
21 Z = 4342622
52
XDOT = 19568
239072 XDOT = 5964
399269
YDOT = 9116
838750 feet/sec YDOT = 2778
812451 meter/sec
ZDOT = 11189
206366 ZDOT = 3410
470100
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 09330
77392693
00016717 00000-0 10270-3 0 9143
2 25544 51
6419 191
3753 0005869 14
2610 345
8719 15
76857779 31574
Satellite: ISS
Catalog Number: 25544
Epoch time: 09330
77392693 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 191
3753 deg
Eccentricity:
0005869
Arg of perigee: 14
2610 deg
Mean anomaly: 345
8719 deg
Mean motion: 15
76857779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3157
Checksum: 351
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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