Date:
November 25th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 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 3562)
---------------------------------------
Vector Time (GMT): 2007/325/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2421537
09 A = 6715603
79 meter
Y = 4217576
45 meter E =
0008065
Z = 4627603
15 I = 51
69046
XDOT = -7090
092707 Wp = 124
67138
YDOT = 896
128488 meter/sec RA = 11
39682 deg
ZDOT = 2885
337273 TA = 296
79023
MA = 296
87271
Ha = 185
987 n
mi
Hp = 180
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7944675
49 X = 2351714
80
Y = 13837193
06 feet Y = 4244264
87 meter
Z = 15182425
03 Z = 4639197
89
XDOT = -23261
459014 XDOT = -7113
603263
YDOT = 2940
054093 feet/sec YDOT = 816
711487 meter/sec
ZDOT = 9466
329636 ZDOT = 2850
835492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6307510
77 X = -1922529
28
Y = 14609782
30 feet Y = 4453061
65 meter
Z = 15226995
08 Z = 4641188
10
XDOT = -15329
433504 XDOT = -4672
411332
YDOT = -16375
075568 feet/sec YDOT = -4991
123033 meter/sec
ZDOT = 9335
060150 ZDOT = 2845
326334
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 07325
74000277
00020000 00000-0 20000-3 0 9003
2 25544 51
6387 11
5954 0001191 212
2976 147
8116 15
76522917 35638
Satellite: ISS
Catalog Number: 25544
Epoch time: 07325
74000277 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 11
5954 deg
Eccentricity:
0001191
Arg of perigee: 212
2976 deg
Mean anomaly: 147
8116 deg
Mean motion: 15
76522917 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3563
Checksum: 283
Coasting Arc #2 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2007/326/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6458342
97 A = 6723647
64 meter
Y = -675953
18 meter E =
0006707
Z = -1734495
32 I = 51
68880
XDOT = 2026
461281 Wp = 39
13385
YDOT = 4757
195989 meter/sec RA = 6
20791 deg
ZDOT = 5708
566496 TA = 301
66512
MA = 301
73051
Ha = 186
072 n
mi
Hp = 180
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21188789
26 X = 6473847
72
Y = -2217694
17 feet Y = -603645
52 meter
Z = -5690601
43 Z = -1703082
02
XDOT = 6648
495018 XDOT = 1945
382872
YDOT = 15607
598389 feet/sec YDOT = 4779
403306 meter/sec
ZDOT = 18728
892705 ZDOT = 5718
214753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14822762
31 X = 4517977
95
Y = 15346491
96 feet Y = 4677610
75 meter
Z = -5571068
52 Z = -1698061
68
XDOT = -7141
553498 XDOT = -2176
745506
YDOT = 13689
564577 feet/sec YDOT = 4172
579283 meter/sec
ZDOT = 18766
099538 ZDOT = 5719
907139
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 07326
69081434
00020000 00000-0 20000-3 0 9013
2 25544 51
6384 6
6943 0001045 205
2497 154
8616 15
76556564 35780
Satellite: ISS
Catalog Number: 25544
Epoch time: 07326
69081434 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 6
6943 deg
Eccentricity:
0001045
Arg of perigee: 205
2497 deg
Mean anomaly: 154
8616 deg
Mean motion: 15
76556564 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3578
Checksum: 305
Coasting Arc #3 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2007/327/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1042284
24 A = 6713047
84 meter
Y = -4135321
22 meter E =
0013917
Z = -5196428
52 I = 51
62477
XDOT = 7600
929000 Wp = 85
09544
YDOT = -653
489566 meter/sec RA = 1
07794 deg
ZDOT = -1005
657533 TA = 175
31480
MA = 175
30176
Ha = 185
936 n
mi
Hp = 179
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3419567
73 X = -970720
84
Y = -13567326
82 feet Y = -4146575
95 meter
Z = -17048650
01 Z = -5201318
71
XDOT = 24937
431102 XDOT = 7612
556961
YDOT = -2143
994639 feet/sec YDOT = -568
426551 meter/sec
ZDOT = -3299
401355 ZDOT = -968
702802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8447450
90 X = 2574783
03
Y = -11124628
05 feet Y = -3390786
63 meter
Z = -17067673
88 Z = -5202227
00
XDOT = 16567
917982 XDOT = 5049
901401
YDOT = 17421
351671 feet/sec YDOT = 5310
027989 meter/sec
ZDOT = -3158
764599 ZDOT = -962
791450
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 07327
70498508
00020000 00000-0 20000-3 0 9021
2 25544 51
6388 1
4653 0000995 216
9986 143
1110 15
76586236 35947
Satellite: ISS
Catalog Number: 25544
Epoch time: 07327
70498508 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 1
4653 deg
Eccentricity:
0000995
Arg of perigee: 216
9986 deg
Mean anomaly: 143
1110 deg
Mean motion: 15
76586236 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3594
Checksum: 310
Coasting Arc #4 (Orbit 3609)
---------------------------------------
Vector Time (GMT): 2007/328/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6702190
70 A = 6724660
22 meter
Y = 467293
08 meter E =
0012190
Z = -14493
20 I = 51
63573
XDOT = -325
813621 Wp = 139
07829
YDOT = -4771
747218 meter/sec RA = 355
91381 deg
ZDOT = -6042
172118 TA = 41
07935
MA = 40
98762
Ha = 185
793 n
mi
Hp = 179
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21988814
62 X = -6706847
51
Y = 1533113
78 feet Y = 392319
35 meter
Z = -47549
86 Z = -47064
66
XDOT = -1068
942325 XDOT = -243
078360
YDOT = -15655
338643 feet/sec YDOT = -4774
927207 meter/sec
ZDOT = -19823
399336 ZDOT = -6043
554666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15311095
85 X = -4666822
02
Y = -15855648
56 feet Y = -4832801
68 meter
Z = -171522
49 Z = -52280
06
XDOT = 10219
220184 XDOT = 3114
818312
YDOT = -9681
866846 feet/sec YDOT = -2951
033015 meter/sec
ZDOT = -19829
124551 ZDOT = -6043
917163
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 07328
71912677
00020000 00000-0 20000-3 0 9032
2 25544 51
6391 356
2368 0000913 226
9198 133
1891 15
76645921 36102
Satellite: ISS
Catalog Number: 25544
Epoch time: 07328
71912677 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 356
2368 deg
Eccentricity:
0000913
Arg of perigee: 226
9198 deg
Mean anomaly: 133
1891 deg
Mean motion: 15
76645921 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3610
Checksum: 306
Coasting Arc #5 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2007/329/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -479923
34 A = 6712854
02 meter
Y = 4241823
25 meter E =
0002878
Z = 5178784
34 I = 51
56744
XDOT = -7626
226379 Wp = 57
69585
YDOT = 407
507166 meter/sec RA = 350
74640 deg
ZDOT = -1038
578675 TA = 42
22057
MA = 42
19841
Ha = 185
756 n
mi
Hp = 179
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1574551
62 X = -552478
54
Y = 13916742
94 feet Y = 4236049
96 meter
Z = 16990762
28 Z = 5176277
26
XDOT = -25020
427751 XDOT = -7625
171042
YDOT = 1336
965768 feet/sec YDOT = 322
232453 meter/sec
ZDOT = -3407
410350 ZDOT = -1075
625104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11599454
05 X = -3535513
60
Y = 7868807
26 feet Y = 2398412
45 meter
Z = 16981622
06 Z = 5175998
40
XDOT = -16836
028723 XDOT = -5131
621555
YDOT = -17146
544418 feet/sec YDOT = -5226
266738 meter/sec
ZDOT = -3548
437442 ZDOT = -1081
563732
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 07329
73324030
00020000 00000-0 20000-3 0 9046
2 25544 51
6392 351
0085 0000892 230
6117 129
4969 15
76680439 36265
Satellite: ISS
Catalog Number: 25544
Epoch time: 07329
73324030 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 351
0085 deg
Eccentricity:
0000892
Arg of perigee: 230
6117 deg
Mean anomaly: 129
4969 deg
Mean motion: 15
76680439 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3626
Checksum: 293
Coasting Arc #6 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2007/330/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6472749
42 A = 6722940
54 meter
Y = -200236
08 meter E =
0013243
Z = 1783053
72 I = 51
57390
XDOT = -1416
862696 Wp = 66
55825
YDOT = 5014
374913 meter/sec RA = 345
61095 deg
ZDOT = 5678
553999 TA = 313
24871
MA = 313
35918
Ha = 185
606 n
mi
Hp = 179
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21236054
51 X = 6465845
53
Y = -656942
50 feet Y = -127893
02 meter
Z = 5849913
78 Z = 1814482
02
XDOT = -4648
499660 XDOT = -1500
414694
YDOT = 16451
361262 feet/sec YDOT = 4998
062664 meter/sec
ZDOT = 18630
426506 ZDOT = 5671
468641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14670728
27 X = 4471637
98
Y = 15321780
49 feet Y = 4670078
69 meter
Z = 5969577
08 Z = 1819527
09
XDOT = -14291
536462 XDOT = -4356
060314
YDOT = 6400
867710 feet/sec YDOT = 1950
984478 meter/sec
ZDOT = 18603
923620 ZDOT = 5670
475919
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 07330
74732379
00020000 00000-0 20000-3 0 9059
2 25544 51
6394 345
7793 0000934 232
3014 127
8066 15
76745717 36424
Satellite: ISS
Catalog Number: 25544
Epoch time: 07330
74732379 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 345
7793 deg
Eccentricity:
0000934
Arg of perigee: 232
3014 deg
Mean anomaly: 127
8066 deg
Mean motion: 15
76745717 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3642
Checksum: 305
Coasting Arc #7 (Orbit 3656)
---------------------------------------
Vector Time (GMT): 2007/331/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1955199
59 A = 6715315
91 meter
Y = -4539375
53 meter E =
0009625
Z = -4555551
45 I = 51
52077
XDOT = 7081
339271 Wp = 113
69267
YDOT = 24
326144 meter/sec RA = 340
40812 deg
ZDOT = 3016
212200 TA = 186
33950
MA = 186
35169
Ha = 185
576 n
mi
Hp = 179
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6414696
81 X = 2027944
50
Y = -14892964
32 feet Y = -4517103
96 meter
Z = -14946034
94 Z = -4545876
98
XDOT = 23232
740391 XDOT = 7065
888608
YDOT = 79
810185 feet/sec YDOT = 103
426852 meter/sec
ZDOT = 9895
709318 ZDOT = 3050
576132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15327323
86 X = 4671768
31
Y = -5395264
29 feet Y = -1644476
55 meter
Z = -14909626
04 Z = -4544454
02
XDOT = 15344
901510 XDOT = 4677
125980
YDOT = 15895
963105 feet/sec YDOT = 4845
089554 meter/sec
ZDOT = 10026
582450 ZDOT = 3056
102331
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 07331
69800230
00020000 00000-0 20000-3 0 9067
2 25544 51
6397 340
8770 0000876 243
2538 116
8537 15
76767034 36578
Satellite: ISS
Catalog Number: 25544
Epoch time: 07331
69800230 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 340
8770 deg
Eccentricity:
0000876
Arg of perigee: 243
2538 deg
Mean anomaly: 116
8537 deg
Mean motion: 15
76767034 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3657
Checksum: 307
Coasting Arc #8 (Orbit 3672)
---------------------------------------
Vector Time (GMT): 2007/332/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5780671
67 A = 6718960
73 meter
Y = -327371
93 meter E =
0004284
Z = -3412636
07 I = 51
50776
XDOT = 3011
342246 Wp = 90
18596
YDOT = -5401
540961 meter/sec RA = 335
29097 deg
ZDOT = -4587
711269 TA = 130
26137
MA = 130
22391
Ha = 185
460 n
mi
Hp = 179
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18965458
22 X = -5760003
26
Y = -1074054
89 feet Y = -391898
68 meter
Z = -11196312
58 Z = -3440668
56
XDOT = 9879
731777 XDOT = 3093
805671
YDOT = -17721
591080 feet/sec YDOT = -5367
404770 meter/sec
ZDOT = -15051
546159 ZDOT = -4572
882468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12346061
85 X = -3763079
65
Y = -14353191
83 feet Y = -4374852
87 meter
Z = -11303108
25 Z = -3445187
40
XDOT = 18627
303156 XDOT = 5677
602002
YDOT = -4226
180719 feet/sec YDOT = -1288
139883 meter/sec
ZDOT = -14995
591251 ZDOT = -4570
656213
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 07332
71203094
00020000 00000-0 20000-3 0 9077
2 25544 51
6405 335
6477 0000796 248
2817 111
8263 15
76829224 36739
Satellite: ISS
Catalog Number: 25544
Epoch time: 07332
71203094 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 335
6477 deg
Eccentricity:
0000796
Arg of perigee: 248
2817 deg
Mean anomaly: 111
8263 deg
Mean motion: 15
76829224 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3673
Checksum: 298
Coasting Arc #9 (Orbit 3688)
---------------------------------------
Vector Time (GMT): 2007/333/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3205107
67 A = 6719298
32 meter
Y = 4884056
32 meter E =
0012001
Z = 3309125
38 I = 51
48342
XDOT = -6071
419318 Wp = 92
51822
YDOT = -803
468189 meter/sec RA = 330
07247 deg
ZDOT = -4680
673566 TA = 48
43694
MA = 48
33411
Ha = 185
456 n
mi
Hp = 179
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10515445
10 X = -3275558
91
Y = 16023806
84 feet Y = 4847820
74 meter
Z = 10856710
55 Z = 3293384
27
XDOT = -19919
354717 XDOT = -6039
245615
YDOT = -2636
050488 feet/sec YDOT = -871
181869 meter/sec
ZDOT = -15356
540571 ZDOT = -4710
090578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18813380
57 X = -5734318
40
Y = 3831656
22 feet Y = 1167888
81 meter
Z = 10797233
79 Z = 3290996
86
XDOT = -11863
237250 XDOT = -3615
914714
YDOT = -14528
719999 feet/sec YDOT = -4428
353856 meter/sec
ZDOT = -15468
659752 ZDOT = -4714
847492
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 07333
72603074
00020000 00000-0 20000-3 0 9082
2 25544 51
6407 330
4187 0000804 251
1868 108
9210 15
76869517 36896
Satellite: ISS
Catalog Number: 25544
Epoch time: 07333
72603074 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 330
4187 deg
Eccentricity:
0000804
Arg of perigee: 251
1868 deg
Mean anomaly: 108
9210 deg
Mean motion: 15
76869517 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3689
Checksum: 300
Coasting Arc #10 (Orbit 3704)
---------------------------------------
Vector Time (GMT): 2007/334/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4735152
58 A = 6714459
54 meter
Y = 1167855
45 meter E =
0007556
Z = 4611272
87 I = 51
44339
XDOT = -4229
524521 Wp = 121
00710
YDOT = 5766
564954 meter/sec RA = 324
95009 deg
ZDOT = 2875
398632 TA = 300
46258
MA = 300
53719
Ha = 185
206 n
mi
Hp = 179
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15535277
50 X = 4699340
67
Y = 3831546
75 feet Y = 1220606
00 meter
Z = 15128848
01 Z = 4634189
48
XDOT = -13876
392785 XDOT = -4307
661016
YDOT = 18919
176357 feet/sec YDOT = 5718
830894 meter/sec
ZDOT = 9433
722545 ZDOT = 2854
662169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8434122
89 X = 2570720
66
Y = 13499593
99 feet Y = 4114676
25 meter
Z = 15216247
00 Z = 4637912
09
XDOT = -22183
097408 XDOT = -6761
408090
YDOT = 3287
484589 feet/sec YDOT = 1002
025303 meter/sec
ZDOT = 9355
310363 ZDOT = 2851
498599
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 07334
74000063
00020000 00000-0 20000-3 0 9095
2 25544 51
6408 325
1893 0000853 249
1414 110
9659 15
76928970 37058
Satellite: ISS
Catalog Number: 25544
Epoch time: 07334
74000063 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 325
1893 deg
Eccentricity:
0000853
Arg of perigee: 249
1414 deg
Mean anomaly: 110
9659 deg
Mean motion: 15
76928970 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3705
Checksum: 295
Coasting Arc #11 (Orbit 3719)
---------------------------------------
Vector Time (GMT): 2007/335/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4059471
11 A = 6722718
87 meter
Y = -5109668
39 meter E =
0007543
Z = -1601124
75 I = 51
44819
XDOT = 4743
753173 Wp = 32
82141
YDOT = 1976
234965 meter/sec RA = 319
74118 deg
ZDOT = 5739
318057 TA = 309
43913
MA = 309
50586
Ha = 185
309 n
mi
Hp = 179
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13318474
76 X = 4124084
52
Y = -16764003
92 feet Y = -5063911
71 meter
Z = -5253033
96 Z = -1581247
08
XDOT = 15563
494663 XDOT = 4693
421255
YDOT = 6483
710514 feet/sec YDOT = 2029
000490 meter/sec
ZDOT = 18829
783652 ZDOT = 5762
241275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21199995
39 X = 6461758
59
Y = -3123813
97 feet Y = -952138
50 meter
Z = -5177832
07 Z = -1578203
21
XDOT = 6630
832560 XDOT = 2021
077764
YDOT = 13748
419331 feet/sec YDOT = 4190
518212 meter/sec
ZDOT = 18917
289065 ZDOT = 5765
989707
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 07335
69057224
00020000 00000-0 20000-3 0 9103
2 25544 51
6407 320
2863 0000798 260
4832 99
6242 15
76944201 37201
Satellite: ISS
Catalog Number: 25544
Epoch time: 07335
69057224 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 320
2863 deg
Eccentricity:
0000798
Arg of perigee: 260
4832 deg
Mean anomaly: 99
6242 deg
Mean motion: 15
76944201 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3720
Checksum: 286
Coasting Arc #12 (Orbit 3735)
---------------------------------------
Vector Time (GMT): 2007/336/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514670
39 A = 6711681
41 meter
Y = -2368349
49 meter E =
0014136
Z = -5216520
75 I = 51
39094
XDOT = 4968
402167 Wp = 84
70107
YDOT = -5835
095811 meter/sec RA = 314
58804 deg
ZDOT = -698
646018 TA = 178
62917
MA = 178
62529
Ha = 185
220 n
mi
Hp = 179
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11531070
85 X = -3462584
72
Y = -7770175
49 feet Y = -2407360
97 meter
Z = -17114569
38 Z = -5233468
85
XDOT = 16300
532045 XDOT = 5036
675766
YDOT = -19144
015127 feet/sec YDOT = -5779
154540 meter/sec
ZDOT = -2292
145728 ZDOT = -674
343763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3273613
58 X = -997797
42
Y = -13431413
06 feet Y = -4093894
70 meter
Z = -17179356
93 Z = -5236267
99
XDOT = 23959
484052 XDOT = 7302
850739
YDOT = -3026
895466 feet/sec YDOT = -922
597738 meter/sec
ZDOT = -2200
167531 ZDOT = -670
611063
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 07336
70448581
00020000 00000-0 20000-3 0 9117
2 25544 51
6414 315
0562 0000712 261
1927 98
9158 15
77011236 37365
Satellite: ISS
Catalog Number: 25544
Epoch time: 07336
70448581 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 315
0562 deg
Eccentricity:
0000712
Arg of perigee: 261
1927 deg
Mean anomaly: 98
9158 deg
Mean motion: 15
77011236 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3736
Checksum: 284
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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