Date:
November 16th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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 2947)
---------------------------------------
Vector Time (GMT): 2009/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1071666
50 A = 6722398
40 meter
Y = 6040567
92 meter E =
0002964
Z = -2752970
72 I = 51
32411
XDOT = -4790
515497 Wp = 11
39164
YDOT = -3182
770433 meter/sec RA = 259
00928 deg
ZDOT = -5116
871475 TA = 200
23731
MA = 200
24906
Ha = 186
725 n
mi
Hp = 181
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3515966
19 X = -1125759
72
Y = 19818136
23 feet Y = 6028281
48 meter
Z = -9032056
17 Z = -2758308
39
XDOT = -15716
914359 XDOT = -4729
711619
YDOT = -10442
160212 feet/sec YDOT = -3236
000806 meter/sec
ZDOT = -16787
636072 ZDOT = -5139
996773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13475939
06 X = -4107466
23
Y = -14937982
41 feet Y = -4553097
04 meter
Z = -9052862
99 Z = -2759312
64
XDOT = 16758
673619 XDOT = 5108
043719
YDOT = -4885
440079 feet/sec YDOT = -1489
082136 meter/sec
ZDOT = -16878
981230 ZDOT = -5144
713479
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
52615796
00016717 00000-0 10270-3 0 9008
2 25544 51
6440 259
6680 0006402 327
0337 33
0428 15
76272234 29487
Satellite: ISS
Catalog Number: 25544
Epoch time: 09317
52615796 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 259
6680 deg
Eccentricity:
0006402
Arg of perigee: 327
0337 deg
Mean anomaly: 33
0428 deg
Mean motion: 15
76272234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 309
Coasting Arc #2 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2009/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4290355
85 A = 6718570
29 meter
Y = 3268179
88 meter E =
0010805
Z = 4005756
64 I = 51
31885
XDOT = -1335
435188 Wp = 43
04468
YDOT = 6521
216695 meter/sec RA = 253
78473 deg
ZDOT = -3876
214989 TA = 87
15446
MA = 87
03080
Ha = 186
770 n
mi
Hp = 181
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14075970
64 X = 4234031
77
Y = 10722374
92 feet Y = 3315842
14 meter
Z = 13142246
18 Z = 4026463
10
XDOT = -4381
349043 XDOT = -1389
426775
YDOT = 21395
067896 feet/sec YDOT = 6505
981283 meter/sec
ZDOT = -12717
240779 ZDOT = -3882
833727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16992192
67 X = -5179220
33
Y = 4712813
43 feet Y = 1436465
53 meter
Z = 13224057
10 Z = 4030692
60
XDOT = -14137
380534 XDOT = -4309
073587
YDOT = -15088
389204 feet/sec YDOT = -4598
941029 meter/sec
ZDOT = -12743
081762 ZDOT = -3884
091321
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
54052138
00016717 00000-0 10270-3 0 9017
2 25544 51
6444 254
4418 0006395 330
5538 29
5265 15
76295311 29644
Satellite: ISS
Catalog Number: 25544
Epoch time: 09318
54052138 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 254
4418 deg
Eccentricity:
0006395
Arg of perigee: 330
5538 deg
Mean anomaly: 29
5265 deg
Mean motion: 15
76295311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 315
Coasting Arc #3 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2009/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1320315
82 A = 6718770
28 meter
Y = -5275811
83 meter E =
0008855
Z = 3935499
12 I = 51
32961
XDOT = 5069
074607 Wp = 65
99305
YDOT = 4235
497805 meter/sec RA = 248
66099 deg
ZDOT = 3973
898144 TA = 342
67255
MA = 342
70275
Ha = 186
807 n
mi
Hp = 180
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4331744
83 X = 1360094
18
Y = -17309093
93 feet Y = -5260825
05 meter
Z = 12911742
50 Z = 3942009
79
XDOT = 16630
822203 XDOT = 5002
030676
YDOT = 13895
990174 feet/sec YDOT = 4291
808136 meter/sec
ZDOT = 13037
723571 ZDOT = 3998
361857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11486605
56 X = 3501117
38
Y = 13629685
01 feet Y = 4154327
99 meter
Z = 12937210
66 Z = 3943261
81
XDOT = -19984
482828 XDOT = -6091
270366
YDOT = 4364
340848 feet/sec YDOT = 1330
251090 meter/sec
ZDOT = 13134
399173 ZDOT = 4003
364868
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
55486646
00016717 00000-0 10270-3 0 9025
2 25544 51
6447 249
2152 0006350 334
2337 25
8510 15
76327315 29803
Satellite: ISS
Catalog Number: 25544
Epoch time: 09319
55486646 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 249
2152 deg
Eccentricity:
0006350
Arg of perigee: 334
2337 deg
Mean anomaly: 25
8510 deg
Mean motion: 15
76327315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 312
Coasting Arc #4 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2009/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4556544
77 A = 6721939
01 meter
Y = -4039463
36 meter E =
0008194
Z = -2837718
43 I = 51
35274
XDOT = 1759
695898 Wp = 12
17568
YDOT = -5534
624442 meter/sec RA = 243
43658 deg
ZDOT = 5063
473344 TA = 315
08314
MA = 315
14941
Ha = 186
910 n
mi
Hp = 180
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14949293
85 X = -4497250
57
Y = -13252832
55 feet Y = -4090085
60 meter
Z = -9310099
83 Z = -2859711
08
XDOT = 5773
280506 XDOT = 1796
856034
YDOT = -18158
216674 feet/sec YDOT = -5514
739066 meter/sec
ZDOT = 16612
445355 ZDOT = 5072
112096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19405586
74 X = 5914822
84
Y = -4573404
53 feet Y = -1393973
70 meter
Z = -9397025
60 Z = -2864213
40
XDOT = 11264
734454 XDOT = 3433
491062
YDOT = 13664
928671 feet/sec YDOT = 4165
070259 meter/sec
ZDOT = 16646
301508 ZDOT = 5073
792700
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
50579931
00016717 00000-0 10270-3 0 9033
2 25544 51
6448 244
3154 0006457 337
7684 22
3199 15
76340766 29959
Satellite: ISS
Catalog Number: 25544
Epoch time: 09320
50579931 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 244
3154 deg
Eccentricity:
0006457
Arg of perigee: 337
7684 deg
Mean anomaly: 22
3199 deg
Mean motion: 15
76340766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 336
Coasting Arc #5 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2009/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1833758
32 A = 6715312
30 meter
Y = 4337033
77 meter E =
0013534
Z = -4799595
85 I = 51
34594
XDOT = -5352
697524 Wp = 44
08092
YDOT = -4963
030539 meter/sec RA = 238
30595 deg
ZDOT = -2434
167605 TA = 201
99352
MA = 202
05166
Ha = 187
069 n
mi
Hp = 180
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6016267
45 X = -1858803
25
Y = 14229113
42 feet Y = 4316388
00 meter
Z = -15746705
53 Z = -4808564
95
XDOT = -17561
343583 XDOT = -5284
977134
YDOT = -16282
908593 feet/sec YDOT = -5022
508698 meter/sec
ZDOT = -7986
114189 ZDOT = -2460
007706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8463015
25 X = -2579527
05
Y = -12881394
80 feet Y = -3926249
13 meter
Z = -15781917
46 Z = -4810328
44
XDOT = 22362
439110 XDOT = 6816
071441
YDOT = -4760
564180 feet/sec YDOT = -1451
019962 meter/sec
ZDOT = -8088
265062 ZDOT = -2465
303191
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
52010990
00016717 00000-0 10270-3 0 9042
2 25544 51
6455 239
0888 0006441 342
5179 17
5756 15
76390967 30111
Satellite: ISS
Catalog Number: 25544
Epoch time: 09321
52010990 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 239
0888 deg
Eccentricity:
0006441
Arg of perigee: 342
5179 deg
Mean anomaly: 17
5756 deg
Mean motion: 15
76390967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 317
Coasting Arc #6 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2009/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4763395
05 A = 6724547
28 meter
Y = 4546438
03 meter E =
0010624
Z = 1351982
93 I = 51
39388
XDOT = -2517
934487 Wp = 94
26208
YDOT = 4378
511435 meter/sec RA = 233
10061 deg
ZDOT = -5814
259238 TA = 70
82389
MA = 70
70893
Ha = 187
159 n
mi
Hp = 180
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15627936
52 X = 4705634
10
Y = 14916135
28 feet Y = 4599382
03 meter
Z = 4435639
55 Z = 1374984
25
XDOT = -8260
939918 XDOT = -2538
463298
YDOT = 14365
194997 feet/sec YDOT = 4350
240215 meter/sec
ZDOT = -19075
653667 ZDOT = -5826
541093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21016210
35 X = -6405740
92
Y = 4922126
57 feet Y = 1500264
18 meter
Z = 4526583
93 Z = 1379702
78
XDOT = -7222
996619 XDOT = -2201
569369
YDOT = -13139
620990 feet/sec YDOT = -4004
956478 meter/sec
ZDOT = -19123
939075 ZDOT = -5828
976630
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
53440332
00016717 00000-0 10270-3 0 9052
2 25544 51
6452 233
8622 0006406 345
8000 14
2983 15
76392259 30275
Satellite: ISS
Catalog Number: 25544
Epoch time: 09322
53440332 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 233
8622 deg
Eccentricity:
0006406
Arg of perigee: 345
8000 deg
Mean anomaly: 14
2983 deg
Mean motion: 15
76392259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 291
Coasting Arc #7 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2009/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2624438
50 A = 6713229
75 meter
Y = -3311523
32 meter E =
0005168
Z = 5215035
62 I = 51
37507
XDOT = 5508
549907 Wp = 15
37622
YDOT = 5352
994797 meter/sec RA = 227
94747 deg
ZDOT = 631
751326 TA = 68
62861
MA = 68
57347
Ha = 187
053 n
mi
Hp = 180
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8610362
52 X = 2635939
24
Y = -10864577
83 feet Y = -3282111
56 meter
Z = 17109696
92 Z = 5227812
99
XDOT = 18072
670297 XDOT = 5445
213375
YDOT = 17562
318889 feet/sec YDOT = 5414
240449 meter/sec
ZDOT = 2072
674953 ZDOT = 658
359149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4676521
25 X = 1425403
68
Y = 12983996
37 feet Y = 3957522
09 meter
Z = 17159985
72 Z = 5230363
65
XDOT = -23529
899840 XDOT = -7171
913471
YDOT = 5617
168352 feet/sec YDOT = 1712
112914 meter/sec
ZDOT = 2177
897258 ZDOT = 663
823084
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
54867714
00016717 00000-0 10270-3 0 9062
2 25544 51
6450 228
6353 0006451 348
4848 11
6168 15
76460464 30433
Satellite: ISS
Catalog Number: 25544
Epoch time: 09323
54867714 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 228
6353 deg
Eccentricity:
0006451
Arg of perigee: 348
4848 deg
Mean anomaly: 11
6168 deg
Mean motion: 15
76460464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 319
Coasting Arc #8 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2009/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4778136
17 A = 6725211
01 meter
Y = -4710279
75 meter E =
0017368
Z = 266782
66 I = 51
43649
XDOT = 3551
903751 Wp = 29
88126
YDOT = -3253
406780 meter/sec RA = 222
77367 deg
ZDOT = 6021
028556 TA = 333
03129
MA = 333
12144
Ha = 187
301 n
mi
Hp = 179
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15676299
76 X = -4726405
88
Y = -15453673
72 feet Y = -4763422
47 meter
Z = 875271
18 Z = 243695
24
XDOT = 11653
227531 XDOT = 3558
770364
YDOT = -10673
906760 feet/sec YDOT = -3213
649537 meter/sec
ZDOT = 19754
030696 ZDOT = 6038
300337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21335531
11 X = 6503069
88
Y = -5432221
80 feet Y = -1655741
20 meter
Z = 783954
00 Z = 238949
18
XDOT = 2774
520735 XDOT = 845
673920
YDOT = 13838
489096 feet/sec YDOT = 4217
971476 meter/sec
ZDOT = 19822
064682 ZDOT = 6041
765315
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
56293657
00016717 00000-0 10270-3 0 9075
2 25544 51
6450 223
4081 0006568 353
0393 7
0679 15
76445455 30596
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324
56293657 = yrday
fracday
Element set: 907
Inclination: 51
6450 deg
RA of node: 223
4081 deg
Eccentricity:
0006568
Arg of perigee: 353
0393 deg
Mean anomaly: 7
0679 deg
Mean motion: 15
76445455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 325
Coasting Arc #9 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2009/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3613746
64 A = 6713499
34 meter
Y = 2391180
95 meter E =
0014295
Z = -5138784
33 I = 51
42065
XDOT = -5348
645356 Wp = 73
25877
YDOT = -5387
533598 meter/sec RA = 217
59137 deg
ZDOT = 1261
340248 TA = 208
80416
MA = 208
88316
Ha = 187
315 n
mi
Hp = 179
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11856124
15 X = -3615253
02
Y = 7845081
86 feet Y = 2350761
98 meter
Z = -16859528
64 Z = -5156343
59
XDOT = -17548
049069 XDOT = -5294
130937
YDOT = -17675
635164 feet/sec YDOT = -5447
040619 meter/sec
ZDOT = 4138
255408 ZDOT = 1235
488063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -878477
13 X = -267759
83
Y = -14106833
68 feet Y = -4299762
91 meter
Z = -16928739
37 Z = -5159879
76
XDOT = 23081
210947 XDOT = 7035
153097
YDOT = -6253
452187 feet/sec YDOT = -1906
052227 meter/sec
ZDOT = 4035
981923 ZDOT = 1230
167290
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
51378681
00016717 00000-0 10270-3 0 9083
2 25544 51
6452 218
5077 0006549 356
2239 3
8875 15
76492625 30741
Satellite: ISS
Catalog Number: 25544
Epoch time: 09325
51378681 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 218
5077 deg
Eccentricity:
0006549
Arg of perigee: 356
2239 deg
Mean anomaly: 3
8875 deg
Mean motion: 15
76492625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 338
Coasting Arc #10 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4460120
18 A = 6723552
44 meter
Y = 4651159
55 meter E =
0004407
Z = -1924050
22 I = 51
47891
XDOT = -4767
779883 Wp = 78
31627
YDOT = 2256
904043 meter/sec RA = 212
45160 deg
ZDOT = -5606
277968 TA = 123
13289
MA = 123
09060
Ha = 187
417 n
mi
Hp = 179
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14632940
23 X = 4417125
42
Y = 15259709
82 feet Y = 4700795
01 meter
Z = -6312500
73 Z = -1902486
74
XDOT = -15642
322452 XDOT = -4765
428001
YDOT = 7404
540822 feet/sec YDOT = 2203
601528 meter/sec
ZDOT = -18393
300421 ZDOT = -5629
434235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20473644
98 X = -6240366
99
Y = 5374152
77 feet Y = 1638041
76 meter
Z = -6227173
70 Z = -1898042
54
XDOT = 1496
200321 XDOT = 456
041858
YDOT = -15680
342368 feet/sec YDOT = -4779
368354 meter/sec
ZDOT = -18484
617912 ZDOT = -5634
111540
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
52801169
00016717 00000-0 10270-3 0 9098
2 25544 51
6452 213
2802 0006441 358
9751 1
1399 15
76480002 30904
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
52801169 = yrday
fracday
Element set: 909
Inclination: 51
6452 deg
RA of node: 213
2802 deg
Eccentricity:
0006441
Arg of perigee: 358
9751 deg
Mean anomaly: 1
1399 deg
Mean motion: 15
76480002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 296
Coasting Arc #11 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2009/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4704800
04 A = 6715869
59 meter
Y = -1615464
07 meter E =
0013087
Z = 4510103
57 I = 51
48007
XDOT = 4761
699816 Wp = 39
05829
YDOT = 5213
854321 meter/sec RA = 207
24468 deg
ZDOT = -3084
861458 TA = 81
79276
MA = 81
64434
Ha = 187
354 n
mi
Hp = 179
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15435695
68 X = 4700605
23
Y = -5300078
97 feet Y = -1562875
98 meter
Z = 14796927
71 Z = 4532949
47
XDOT = 15622
374725 XDOT = 4718
029567
YDOT = 17105
821264 feet/sec YDOT = 5266
858492 meter/sec
ZDOT = -10120
936543 ZDOT = -3061
834558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2576095
29 X = -785193
84
Y = 16032464
66 feet Y = 4886695
23 meter
Z = 14887055
38 Z = 4537574
48
XDOT = -21314
043854 XDOT = -6496
520567
YDOT = 5933
482650 feet/sec YDOT = 1808
525512 meter/sec
ZDOT = -10029
794543 ZDOT = -3057
081377
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
54221787
00016717 00000-0 10270-3 0 9105
2 25544 51
6451 208
0525 0006697 2
5819 357
5379 15
76575966 31065
Satellite: ISS
Catalog Number: 25544
Epoch time: 09327
54221787 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 208
0525 deg
Eccentricity:
0006697
Arg of perigee: 2
5819 deg
Mean anomaly: 357
5379 deg
Mean motion: 15
76575966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3106
Checksum: 334
Coasting Arc #12 (Orbit 3121)
---------------------------------------
Vector Time (GMT): 2009/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3742240
89 A = 6720020
50 meter
Y = -4425051
47 meter E =
0015004
Z = 3383654
15 I = 51
52067
XDOT = 5986
795389 Wp = 63
70933
YDOT = -1526
322146 meter/sec RA = 202
12821 deg
ZDOT = 4615
990638 TA = 336
38787
MA = 336
45667
Ha = 187
660 n
mi
Hp = 179
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12277693
20 X = -3708918
46
Y = -14517885
40 feet Y = -4466713
28 meter
Z = 11101227
54 Z = 3365554
80
XDOT = 19641
717157 XDOT = 5980
994082
YDOT = -5007
618588 feet/sec YDOT = -1459
406951 meter/sec
ZDOT = 15144
326239 ZDOT = 4645
060714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18553279
32 X = 5655039
54
Y = -4344251
11 feet Y = -1324127
74 meter
Z = 11029565
19 Z = 3361811
47
XDOT = -4797
923908 XDOT = -1462
407207
YDOT = 18327
139668 feet/sec YDOT = 5586
112171 meter/sec
ZDOT = 15259
040898 ZDOT = 4650
955666
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
55641060
00016717 00000-0 10270-3 0 9118
2 25544 51
6450 202
8243 0006734 7
0654 353
0605 15
76540337 31227
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
55641060 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 202
8243 deg
Eccentricity:
0006734
Arg of perigee: 7
0654 deg
Mean anomaly: 353
0605 deg
Mean motion: 15
76540337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3122
Checksum: 279
Coasting Arc #13 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2009/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5679365
89 A = 6719644
49 meter
Y = 1107522
91 meter E =
0008767
Z = -3415284
55 I = 51
54826
XDOT = -3717
301176 Wp = 44
03471
YDOT = -4941
811384 meter/sec RA = 196
91400 deg
ZDOT = 4592
268772 TA = 275
49481
MA = 275
59481
Ha = 187
505 n
mi
Hp = 178
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18633090
18 X = -5674737
19
Y = 3633605
34 feet Y = 1044038
91 meter
Z = -11205001
82 Z = -3442864
07
XDOT = -12195
870000 XDOT = -3684
073468
YDOT = -16213
291942 feet/sec YDOT = -4983
194849 meter/sec
ZDOT = 15066
498597 ZDOT = 4574
290332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4939420
47 X = 1505535
36
Y = -18263240
19 feet Y = -5566635
61 meter
Z = -11313858
16 Z = -3448463
97
XDOT = 18639
198579 XDOT = 5681
227727
YDOT = -4221
680048 feet/sec YDOT = -1286
768079 meter/sec
ZDOT = 14995
282451 ZDOT = 4570
562091
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
50719856
00016717 00000-0 10270-3 0 9124
2 25544 51
6448 197
9232 0006694 8
7149 351
4130 15
76582075 31374
Satellite: ISS
Catalog Number: 25544
Epoch time: 09329
50719856 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 197
9232 deg
Eccentricity:
0006694
Arg of perigee: 8
7149 deg
Mean anomaly: 351
4130 deg
Mean motion: 15
76582075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 332
Coasting Arc #14 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2009/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2633062
44 A = 6715918
79 meter
Y = 4220139
53 meter E =
0014680
Z = -4526659
62 I = 51
56410
XDOT = -6971
673321 Wp = 47
36753
YDOT = 1041
285969 meter/sec RA = 191
80165 deg
ZDOT = -3081
044713 TA = 191
86473
MA = 191
89936
Ha = 187
621 n
mi
Hp = 178
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8638656
28 X = 2607666
53
Y = 13845602
12 feet Y = 4249442
15 meter
Z = -14851245
48 Z = -4513929
49
XDOT = -22872
943966 XDOT = -6967
831556
YDOT = 3416
292548 feet/sec YDOT = 963
346197 meter/sec
ZDOT = -10108
414414 ZDOT = -3114
904396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16243365
14 X = -4950977
70
Y = 1994119
29 feet Y = 607807
56 meter
Z = -14800782
06 Z = -4511278
37
XDOT = 6775
838679 XDOT = 2065
275629
YDOT = -20909
855135 feet/sec YDOT = -6373
323845 meter/sec
ZDOT = -10242
082938 ZDOT = -3121
786879
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
52135766
00016717 00000-0 10270-3 0 9131
2 25544 51
6441 192
6951 0006679 11
9890 348
1432 15
76605589 31531
Satellite: ISS
Catalog Number: 25544
Epoch time: 09330
52135766 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 192
6951 deg
Eccentricity:
0006679
Arg of perigee: 11
9890 deg
Mean anomaly: 348
1432 deg
Mean motion: 15
76605589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 326
Coasting Arc #15 (Orbit 3168)
---------------------------------------
Vector Time (GMT): 2009/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6406488
93 A = 6723052
69 meter
Y = -758666
80 meter E =
0015011
Z = 1881487
67 I = 51
61881
XDOT = 2229
998266 Wp = 86
47866
YDOT = 4752
949528 meter/sec RA = 186
60238 deg
ZDOT = -5637
262300 TA = 72
59501
MA = 72
43093
Ha = 187
672 n
mi
Hp = 178
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21018664
46 X = 6405356
18
Y = -2489064
31 feet Y = -687032
07 meter
Z = 6172859
80 Z = 1912608
34
XDOT = 7316
267276 XDOT = 2204
069656
YDOT = 15593
666431 feet/sec YDOT = 4777
741933 meter/sec
ZDOT = -18494
955054 ZDOT = -5626
491509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6343144
80 X = -1933390
53
Y = 20154705
23 feet Y = 6143154
16 meter
Z = 6295733
96 Z = 1918939
71
XDOT = -15796
834247 XDOT = -4814
875078
YDOT = 831
881140 feet/sec YDOT = 253
557371 meter/sec
ZDOT = -18452
203183 ZDOT = -5624
231530
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 09331
53550112
00016717 00000-0 10270-3 0 9140
2 25544 51
6444 187
4672 0006767 16
6790 343
4596 15
76646408 31696
Satellite: ISS
Catalog Number: 25544
Epoch time: 09331
53550112 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 187
4672 deg
Eccentricity:
0006767
Arg of perigee: 16
6790 deg
Mean anomaly: 343
4596 deg
Mean motion: 15
76646408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3169
Checksum: 330
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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