Date:
March 1st 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 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
064/20:15:11
644 0
3 1
6 1
6
N/A -1
5 0
0 198
7
000/00:00:23
287 0
4 0
0 184
5
Coasting Arc #1 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2009/056/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -490262
43 A = 6729456
52 meter
Y = 4469454
99 meter E =
0021062
Z = -5024772
89 I = 51
74776
XDOT = -7320
450371 Wp = 88
17452
YDOT = 1332
069651 meter/sec RA = 158
03175 deg
ZDOT = 1906
618732 TA = 200
21037
MA = 200
29387
Ha = 197
743 n
mi
Hp = 185
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1608472
55 X = -515795
28
Y = 14663566
24 feet Y = 4463829
41 meter
Z = -16485475
35 Z = -5027216
92
XDOT = -24017
225627 XDOT = -7344
063532
YDOT = 4370
307253 feet/sec YDOT = 1250
076244 meter/sec
ZDOT = 6255
310800 ZDOT = 1870
999306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8640297
06 X = -2633562
54
Y = 11943669
12 feet Y = 3640430
35 meter
Z = -16494614
00 Z = -5027558
35
XDOT = -22146
023464 XDOT = -6750
107952
YDOT = -7607
878299 feet/sec YDOT = -2318
881305 meter/sec
ZDOT = 6116
461655 ZDOT = 1864
297512
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 09056
49968765
00010596 00000-0 82463-4 0 9004
2 25544 51
6415 158
9825 0009143 64
1039 296
1064 15
71126325 28384
Satellite: ISS
Catalog Number: 25544
Epoch time: 09056
49968765 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 158
9825 deg
Eccentricity:
0009143
Arg of perigee: 64
1039 deg
Mean anomaly: 296
1064 deg
Mean motion: 15
71126325 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2838
Checksum: 328
Coasting Arc #2 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2009/057/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6214915
72 A = 6740131
23 meter
Y = -2484641
29 meter E =
0015846
Z = -779826
08 I = 51
81014
XDOT = 1141
551841 Wp = 107
41808
YDOT = 4700
004703 meter/sec RA = 152
95050 deg
ZDOT = -5981
194052 TA = 81
04909
MA = 80
86975
Ha = 197
789 n
mi
Hp = 185
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20390143
42 X = 6246025
67
Y = -8151710
26 feet Y = -2414968
61 meter
Z = -2558484
51 Z = -749558
74
XDOT = 3745
248822 XDOT = 1117
965831
YDOT = 15419
962935 feet/sec YDOT = 4712
637769 meter/sec
ZDOT = -19623
340067 ZDOT = -5975
706214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21798034
59 X = 6644040
94
Y = 2764646
34 feet Y = 842664
21 meter
Z = -2440612
74 Z = -743898
76
XDOT = -3900
719997 XDOT = -1188
939455
YDOT = 13767
197656 feet/sec YDOT = 4196
241846 meter/sec
ZDOT = -19601
511640 ZDOT = -5974
540748
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 09057
51738901
00010596 00000-0 82463-4 0 9016
2 25544 51
6412 153
7783 0009113 67
7978 292
4149 15
71122745 28548
Satellite: ISS
Catalog Number: 25544
Epoch time: 09057
51738901 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 153
7783 deg
Eccentricity:
0009113
Arg of perigee: 67
7978 deg
Mean anomaly: 292
4149 deg
Mean motion: 15
71122745 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2854
Checksum: 324
Coasting Arc #3 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2009/058/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2390375
64 A = 6728125
81 meter
Y = -3404390
60 meter E =
0011279
Z = 5278607
73 I = 51
79641
XDOT = 6439
712281 Wp = 77
24002
YDOT = -4227
117966 meter/sec RA = 147
84274 deg
ZDOT = 192
031473 TA = 10
95488
MA = 10
93033
Ha = 197
760 n
mi
Hp = 184
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7842439
77 X = -2377771
74
Y = -11169260
49 feet Y = -3431050
21 meter
Z = 17318266
82 Z = 5267026
35
XDOT = 21127
664963 XDOT = 6485
569160
YDOT = -13868
497265 feet/sec YDOT = -4154
848937 meter/sec
ZDOT = 630
024519 ZDOT = 223
426996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1764434
39 X = -537799
60
Y = -13591045
13 feet Y = -4142550
56 meter
Z = 17272778
32 Z = 5264742
83
XDOT = 24171
678557 XDOT = 7367
527624
YDOT = -2190
924452 feet/sec YDOT = -667
793773 meter/sec
ZDOT = 752
151093 ZDOT = 229
255653
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 09058
53507231
00010596 00000-0 82463-4 0 9020
2 25544 51
6415 148
5741 0009095 70
7598 289
4547 15
71189206 28709
Satellite: ISS
Catalog Number: 25544
Epoch time: 09058
53507231 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 148
5741 deg
Eccentricity:
0009095
Arg of perigee: 70
7598 deg
Mean anomaly: 289
4547 deg
Mean motion: 15
71189206 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2870
Checksum: 329
Coasting Arc #4 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2009/059/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4715462
68 A = 6739764
21 meter
Y = 4680043
08 meter E =
0017800
Z = -1106448
41 I = 51
85905
XDOT = -4084
943245 Wp = 55
56106
YDOT = -2734
216565 meter/sec RA = 142
73053 deg
ZDOT = 5921
104232 TA = 292
38250
MA = 292
57100
Ha = 197
795 n
mi
Hp = 184
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15470678
08 X = -4762070
35
Y = 15354472
06 feet Y = 4627051
35 meter
Z = -3630080
09 Z = -1129469
55
XDOT = -13402
044767 XDOT = -4082
828628
YDOT = -8970
526789 feet/sec YDOT = -2779
884474 meter/sec
ZDOT = 19426
194987 ZDOT = 5901
265082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20740283
51 X = -6321638
41
Y = 6654707
50 feet Y = 2028354
84 meter
Z = -3719500
23 Z = -1133703
67
XDOT = -7474
972279 XDOT = -2278
371551
YDOT = -12620
202545 feet/sec YDOT = -3846
637736 meter/sec
ZDOT = 19348
544138 ZDOT = 5897
436253
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 09059
48913815
00010596 00000-0 82463-4 0 9035
2 25544 51
6411 143
6961 0009228 73
0485 287
1688 15
71140405 28859
Satellite: ISS
Catalog Number: 25544
Epoch time: 09059
48913815 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 143
6961 deg
Eccentricity:
0009228
Arg of perigee: 73
0485 deg
Mean anomaly: 287
1688 deg
Mean motion: 15
71140405 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2885
Checksum: 324
Coasting Arc #5 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2009/060/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4453785
14 A = 6729859
32 meter
Y = 1176775
05 meter E =
0021486
Z = -4925776
15 I = 51
84759
XDOT = -4086
652039 Wp = 75
50797
YDOT = 6104
095179 meter/sec RA = 137
65991 deg
ZDOT = -2239
650858 TA = 172
73881
MA = 172
70764
Ha = 197
754 n
mi
Hp = 184
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14612155
98 X = 4464223
66
Y = 3860810
53 feet Y = 1226637
93 meter
Z = -16160682
91 Z = -4904114
47
XDOT = -13407
651046 XDOT = -4143
725543
YDOT = 20026
558986 feet/sec YDOT = 6058
076604 meter/sec
ZDOT = -7347
935887 ZDOT = -2259
642735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11516211
57 X = 3510141
29
Y = 9926027
49 feet Y = 3025453
18 meter
Z = -16076053
05 Z = -4899980
97
XDOT = -20077
830706 XDOT = -6119
722799
YDOT = 11283
542941 feet/sec YDOT = 3439
223888 meter/sec
ZDOT = -7425
424120 ZDOT = -2263
269272
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 09060
50679150
00010596 00000-0 82463-4 0 9042
2 25544 51
6401 138
4917 0009156 77
6112 282
6074 15
71178600 29014
Satellite: ISS
Catalog Number: 25544
Epoch time: 09060
50679150 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 138
4917 deg
Eccentricity:
0009156
Arg of perigee: 77
6112 deg
Mean anomaly: 282
6074 deg
Mean motion: 15
71178600 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2901
Checksum: 296
Coasting Arc #6 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2009/061/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2281486
53 A = 6736710
66 meter
Y = -5694611
78 meter E =
0022547
Z = 2763212
98 I = 51
89231
XDOT = 5709
887367 Wp = 92
35382
YDOT = -234
816932 meter/sec RA = 132
52095 deg
ZDOT = -5163
291207 TA = 56
18375
MA = 55
96929
Ha = 197
724 n
mi
Hp = 184
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7485192
03 X = 2331571
92
Y = -18683109
50 feet Y = -5668818
72 meter
Z = 9065659
39 Z = 2774418
27
XDOT = 18733
226270 XDOT = 5737
171001
YDOT = -770
396757 feet/sec YDOT = -170
813290 meter/sec
ZDOT = -16939
931782 ZDOT = -5135
486398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14647201
06 X = 4464466
88
Y = -13775346
40 feet Y = -4198725
58 meter
Z = 9108907
35 Z = 2776394
96
XDOT = 16379
633234 XDOT = 4992
512210
YDOT = 6210
818556 feet/sec YDOT = 1893
057496 meter/sec
ZDOT = -16831
442785 ZDOT = -5130
223761
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 09061
52442829
00010596 00000-0 82463-4 0 9057
2 25544 51
6400 133
2870 0009334 80
4023 279
8193 15
71237985 29174
Satellite: ISS
Catalog Number: 25544
Epoch time: 09061
52442829 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 133
2870 deg
Eccentricity:
0009334
Arg of perigee: 80
4023 deg
Mean anomaly: 279
8193 deg
Mean motion: 15
71237985 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2917
Checksum: 311
Coasting Arc #7 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2009/062/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5177524
29 A = 6733269
80 meter
Y = 1651915
70 meter E =
0020166
Z = 3958751
06 I = 51
89969
XDOT = 1012
286933 Wp = 93
32654
YDOT = -6497
057052 meter/sec RA = 127
47293 deg
ZDOT = 4016
444340 TA = 315
10804
MA = 315
27096
Ha = 197
793 n
mi
Hp = 184
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16986628
24 X = -5214842
27
Y = 5419670
93 feet Y = 1593809
01 meter
Z = 12988028
41 Z = 3933508
12
XDOT = 3321
151355 XDOT = 1065
351822
YDOT = -21315
803977 feet/sec YDOT = -6485
440314 meter/sec
ZDOT = 13177
310828 ZDOT = 4021
490986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17788066
80 X = -5421802
76
Y = -2012206
63 feet Y = -613320
58 meter
Z = 12889645
38 Z = 3928763
91
XDOT = 11512
001659 XDOT = 3508
858106
YDOT = -16840
189195 feet/sec YDOT = -5132
889667 meter/sec
ZDOT = 13196
468159 ZDOT = 4022
283495
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 09062
54204842
00010596 00000-0 82463-4 0 9062
2 25544 51
6399 128
0823 0009269 84
4848 275
7370 15
71264310 29339
Satellite: ISS
Catalog Number: 25544
Epoch time: 09062
54204842 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 128
0823 deg
Eccentricity:
0009269
Arg of perigee: 84
4848 deg
Mean anomaly: 275
7370 deg
Mean motion: 15
71264310 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2933
Checksum: 321
Coasting Arc #8 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2009/063/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 482613
56 A = 6732494
81 meter
Y = 5301382
32 meter E =
0016916
Z = -4137652
54 I = 51
91391
XDOT = -5711
685669 Wp = 97
61146
YDOT = 3470
038787 meter/sec RA = 122
32674 deg
ZDOT = 3790
764413 TA = 211
15526
MA = 211
25565
Ha = 197
715 n
mi
Hp = 184
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1583377
84 X = 443396
52
Y = 17392986
61 feet Y = 5306559
92 meter
Z = -13574975
54 Z = -4135403
28
XDOT = -18739
126212 XDOT = -5768
478378
YDOT = 11384
641689 feet/sec YDOT = 3405
849842 meter/sec
ZDOT = 12436
891118 ZDOT = 3762
879384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5292869
56 X = -1613266
64
Y = 16651085
24 feet Y = 5075250
78 meter
Z = -13565762
84 Z = -4134844
51
XDOT = -20554
433329 XDOT = -6264
991279
YDOT = 3481
009949 feet/sec YDOT = 1061
011832 meter/sec
ZDOT = 12328
331204 ZDOT = 3757
675351
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 09063
49605431
00010596 00000-0 82463-4 0 9077
2 25544 51
6393 123
2032 0009474 87
3881 272
8365 15
71294467 29483
Satellite: ISS
Catalog Number: 25544
Epoch time: 09063
49605431 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 123
2032 deg
Eccentricity:
0009474
Arg of perigee: 87
3881 deg
Mean anomaly: 272
8365 deg
Mean motion: 15
71294467 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2948
Checksum: 330
Coasting Arc #9 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2009/064/11:41:12
065
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4505451
49 A = 6736976
59 meter
Y = -4279052
60 meter E =
0013928
Z = -2609951
22 I = 51
94412
XDOT = 1941
652875 Wp = 103
60850
YDOT = 5245
916489 meter/sec RA = 117
27868 deg
ZDOT = -5275
571870 TA = 105
85147
MA = 105
69790
Ha = 197
753 n
mi
Hp = 184
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14781664
99 X = 4565644
19
Y = -14038886
49 feet Y = -4228333
46 meter
Z = -8562832
10 Z = -2587917
90
XDOT = 6370
252216 XDOT = 1908
475232
YDOT = 17211
012104 feet/sec YDOT = 5267
443702 meter/sec
ZDOT = -17308
306661 ZDOT = -5266
220029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19023804
74 X = 5798455
69
Y = -7425803
72 feet Y = -2263384
97 meter
Z = -8477165
78 Z = -2583840
13
XDOT = -1023
765796 XDOT = -312
043815
YDOT = 16993
282664 feet/sec YDOT = 5179
552556 meter/sec
ZDOT = -17271
375676 ZDOT = -5264
315306
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 09064
51364469
00010596 00000-0 82463-4 0 9085
2 25544 51
6398 117
9978 0009520 90
6403 269
5850 15
71298641 29644
Satellite: ISS
Catalog Number: 25544
Epoch time: 09064
51364469 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 117
9978 deg
Eccentricity:
0009520
Arg of perigee: 90
6403 deg
Mean anomaly: 269
5850 deg
Mean motion: 15
71298641 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2964
Checksum: 349
Coasting Arc #10 (Orbit 2969)
---------------------------------------
Vector Time (GMT): 2009/064/20:15:23
287
Vector Time (MET): N/A
Weight (LBS) : 638664
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4494365
53 A = 6729953
42 meter
Y = 356263
47 meter E =
0015887
Z = 4984197
76 I = 51
92256
XDOT = 1685
867444 Wp = 101
04598
YDOT = -7240
833121 meter/sec RA = 115
45505 deg
ZDOT = 2029
348725 TA = 329
36412
MA = 329
45680
Ha = 198
684 n
mi
Hp = 184
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14745293
74 X = -4522227
21
Y = 1168843
41 feet Y = 305849
07 meter
Z = 16352354
84 Z = 4962296
84
XDOT = 5531
061169 XDOT = 1756
852312
YDOT = -23756
014177 feet/sec YDOT = -7221
583878 meter/sec
ZDOT = 6657
968258 ZDOT = 2037
710927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5406447
86 X = 1647885
31
Y = 13868964
08 feet Y = 4227260
25 meter
Z = 16266885
02 Z = 4958146
55
XDOT = -23318
406352 XDOT = -7107
450256
YDOT = 1210
838818 feet/sec YDOT = 369
063672 meter/sec
ZDOT = 6690
029781 ZDOT = 2039
121077
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 09064
89524861
00010596 00000-0 82463-4 0 9091
2 25544 51
6398 116
0470 0010612 88
2832 271
9545 15
71027549 29706
Satellite: ISS
Catalog Number: 25544
Epoch time: 09064
89524861 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 116
0470 deg
Eccentricity:
0010612
Arg of perigee: 88
2832 deg
Mean anomaly: 271
9545 deg
Mean motion: 15
71027549 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2970
Checksum: 327
Coasting Arc #11 (Orbit 2984)
---------------------------------------
Vector Time (GMT): 2009/065/20:15:23
287
Vector Time (MET): N/A
Weight (LBS) : 638664
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -57118
85 A = 6737557
03 meter
Y = 6186148
23 meter E =
0014965
Z = -2677786
43 I = 51
96000
XDOT = -5182
495151 Wp = 80
27441
YDOT = 2205
317933 meter/sec RA = 110
32464 deg
ZDOT = 5232
340730 TA = 249
43591
MA = 249
59654
Ha = 198
586 n
mi
Hp = 184
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -187397
80 X = -113281
23
Y = 20295761
90 feet Y = 6185195
43 meter
Z = -8785388
54 Z = -2678200
41
XDOT = -17002
936847 XDOT = -5232
187407
YDOT = 7235
295057 feet/sec YDOT = 2147
086487 meter/sec
ZDOT = 17166
472211 ZDOT = 5207
044003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19368172
72 X = 5903419
04
Y = -6066899
85 feet Y = -1849191
07 meter
Z = -8786508
57 Z = -2678127
81
XDOT = 11669
324971 XDOT = 3556
810251
YDOT = 12663
532731 feet/sec YDOT = 3859
844776 meter/sec
ZDOT = 17067
883703 ZDOT = 5202
290953
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 09065
84940789
00010596 00000-0 82463-4 0 9100
2 25544 51
6401 111
1686 0010699 91
2030 269
0357 15
71020073 29855
Satellite: ISS
Catalog Number: 25544
Epoch time: 09065
84940789 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 111
1686 deg
Eccentricity:
0010699
Arg of perigee: 91
2030 deg
Mean anomaly: 269
0357 deg
Mean motion: 15
71020073 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2985
Checksum: 305
Coasting Arc #12 (Orbit 3000)
---------------------------------------
Vector Time (GMT): 2009/066/20:15:23
287
Vector Time (MET): N/A
Weight (LBS) : 638664
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4202801
88 A = 6733595
57 meter
Y = -3389669
24 meter E =
0017565
Z = -4039388
83 I = 51
95681
XDOT = 1429
703979 Wp = 85
58301
YDOT = 6443
407633 meter/sec RA = 105
28139 deg
ZDOT = -3932
749062 TA = 143
93727
MA = 143
81865
Ha = 198
560 n
mi
Hp = 184
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13788720
06 X = 4260015
49
Y = -11120962
07 feet Y = -3342351
33 meter
Z = -13252588
01 Z = -4018833
02
XDOT = 4690
629853 XDOT = 1376
650569
YDOT = 21139
788821 feet/sec YDOT = 6459
098618 meter/sec
ZDOT = -12902
720020 ZDOT = -3925
932861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14989999
62 X = -4568951
88
Y = -9550825
54 feet Y = -2911091
62 meter
Z = -13172597
70 Z = -4015007
78
XDOT = 17786
879104 XDOT = 5421
440751
YDOT = -10218
779579 feet/sec YDOT = -3114
684016 meter/sec
ZDOT = -12875
589078 ZDOT = -3924
479551
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 09066
86716093
00010596 00000-0 82463-4 0 9113
2 25544 51
6409 105
9645 0010751 94
6982 265
5408 15
71057259 30015
Satellite: ISS
Catalog Number: 25544
Epoch time: 09066
86716093 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 105
9645 deg
Eccentricity:
0010751
Arg of perigee: 94
6982 deg
Mean anomaly: 265
5408 deg
Mean motion: 15
71057259 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3001
Checksum: 318
Coasting Arc #13 (Orbit 3016)
---------------------------------------
Vector Time (GMT): 2009/067/20:15:23
287
Vector Time (MET): N/A
Weight (LBS) : 638664
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2418728
49 A = 6733250
92 meter
Y = -4738752
35 meter E =
0020880
Z = 4109651
53 I = 51
96157
XDOT = 3996
453505 Wp = 87
38552
YDOT = -5368
174021 meter/sec RA = 100
14037 deg
ZDOT = -3820
338775 TA = 41
70369
MA = 41
54470
Ha = 198
591 n
mi
Hp = 184
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7935460
94 X = -2385522
66
Y = -15547087
78 feet Y = -4765614
03 meter
Z = 13483108
68 Z = 4097982
62
XDOT = 13111
724098 XDOT = 4074
742351
YDOT = -17612
119492 feet/sec YDOT = -5323
045882 meter/sec
ZDOT = -12533
919865 ZDOT = -3800
733956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11924713
81 X = -3634652
77
Y = 12795370
98 feet Y = 3900029
08 meter
Z = 13437164
14 Z = 4095647
63
XDOT = -20098
180016 XDOT = -6125
925269
YDOT = -5587
504281 feet/sec YDOT = -1703
071305 meter/sec
ZDOT = -12457
797157 ZDOT = -3797
136574
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 09067
88489859
00010596 00000-0 82463-4 0 9124
2 25544 51
6401 100
7608 0010750 98
4284 261
8097 15
71065848 30178
Satellite: ISS
Catalog Number: 25544
Epoch time: 09067
88489859 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 100
7608 deg
Eccentricity:
0010750
Arg of perigee: 98
4284 deg
Mean anomaly: 261
8097 deg
Mean motion: 15
71065848 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3017
Checksum: 332
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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