Date:
September 29th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3982 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2707)
---------------------------------------
Vector Time (GMT): 2007/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4472335
81 A = 6717639
24 meter
Y = 571205
27 meter E =
0015419
Z = -4993781
99 I = 51
31548
XDOT = 1133
652776 Wp = 70
96364
YDOT = -7376
558425 meter/sec RA = 290
24020 deg
ZDOT = -1858
753728 TA = 180
99962
MA = 181
00271
Ha = 188
866 n
mi
Hp = 181
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14673017
76 X = -4454131
31
Y = 1874033
04 feet Y = 521294
53 meter
Z = -16383799
19 Z = -5015464
88
XDOT = 3719
333253 XDOT = 1225
083982
YDOT = -24201
307170 feet/sec YDOT = -7363
370189 meter/sec
ZDOT = -6098
273386 ZDOT = -1853
023728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14296215
65 X = 4357486
53
Y = -3424376
79 feet Y = -1043750
04 meter
Z = -16466031
33 Z = -5018846
35
XDOT = -1390
717015 XDOT = -423
890546
YDOT = 23421
530358 feet/sec YDOT = 7138
882453 meter/sec
ZDOT = -6077
428592 ZDOT = -1852
400235
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 07271
51903879
00020000 00000-0 20000-3 0 9008
2 25544 51
6346 290
7784 0002493 43
5728 316
5632 15
75265513 27084
Satellite: ISS
Catalog Number: 25544
Epoch time: 07271
51903879 = yrday
fracday
Element set: 900
Inclination: 51
6346 deg
RA of node: 290
7784 deg
Eccentricity:
0002493
Arg of perigee: 43
5728 deg
Mean anomaly: 316
5632 deg
Mean motion: 15
75265513 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2708
Checksum: 304
Coasting Arc #2 (Orbit 2723)
---------------------------------------
Vector Time (GMT): 2007/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -786080
14 A = 6727883
44 meter
Y = 6570365
88 meter E =
0014836
Z = 1182952
08 I = 51
34036
XDOT = -4979
696822 Wp = 112
11972
YDOT = 468
696029 meter/sec RA = 285
04475 deg
ZDOT = -5859
220340 TA = 54
85609
MA = 54
71717
Ha = 188
899 n
mi
Hp = 181
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2579003
08 X = -865239
23
Y = 21556318
51 feet Y = 6561132
93 meter
Z = 3881076
39 Z = 1178940
69
XDOT = -16337
587998 XDOT = -4956
104065
YDOT = 1537
716631 feet/sec YDOT = 413
141941 meter/sec
ZDOT = -19223
163844 ZDOT = -5883
354964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -95471
55 X = -29099
73
Y = -21712410
19 feet Y = -6617942
63 meter
Z = 3866653
24 Z = 1178555
91
XDOT = 14329
475054 XDOT = 4367
623997
YDOT = -3533
785493 feet/sec YDOT = -1077
097818 meter/sec
ZDOT = -19314
716479 ZDOT = -5887
125583
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 07272
53404218
00020000 00000-0 20000-3 0 9015
2 25544 51
6334 285
5544 0002660 48
0822 312
0568 15
75298946 27241
Satellite: ISS
Catalog Number: 25544
Epoch time: 07272
53404218 = yrday
fracday
Element set: 901
Inclination: 51
6334 deg
RA of node: 285
5544 deg
Eccentricity:
0002660
Arg of perigee: 48
0822 deg
Mean anomaly: 312
0568 deg
Mean motion: 15
75298946 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2724
Checksum: 288
Coasting Arc #3 (Orbit 2739)
---------------------------------------
Vector Time (GMT): 2007/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4257488
06 A = 6716584
52 meter
Y = -227255
19 meter E =
0004882
Z = 5185656
79 I = 51
29582
XDOT = -635
504153 Wp = 89
73972
YDOT = 7633
297700 meter/sec RA = 279
89420 deg
ZDOT = 855
605755 TA = 352
07821
MA = 352
08592
Ha = 188
758 n
mi
Hp = 180
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13968136
69 X = 4234521
33
Y = -745587
90 feet Y = -179773
93 meter
Z = 17013309
67 Z = 5206284
31
XDOT = -2084
987380 XDOT = -724
970064
YDOT = 25043
627624 feet/sec YDOT = 7625
690911 meter/sec
ZDOT = 2807
105497 ZDOT = 852
301035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13627977
72 X = -4153807
61
Y = 2696933
05 feet Y = 822025
19 meter
Z = 17091583
46 Z = 5209514
64
XDOT = -1259
709036 XDOT = -383
959314
YDOT = -24095
562686 feet/sec YDOT = -7344
327507 meter/sec
ZDOT = 2795
491323 ZDOT = 852
065755
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 07273
54903113
00020000 00000-0 20000-3 0 9026
2 25544 51
6330 280
3305 0002651 50
3062 309
8335 15
75317248 27408
Satellite: ISS
Catalog Number: 25544
Epoch time: 07273
54903113 = yrday
fracday
Element set: 902
Inclination: 51
6330 deg
RA of node: 280
3305 deg
Eccentricity:
0002651
Arg of perigee: 50
3062 deg
Mean anomaly: 309
8335 deg
Mean motion: 15
75317248 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2740
Checksum: 256
Coasting Arc #4 (Orbit 2754)
---------------------------------------
Vector Time (GMT): 2007/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 314231
58 A = 6728195
10 meter
Y = -6707902
75 meter E =
0014161
Z = -297769
36 I = 51
33241
XDOT = 4825
135660 Wp = 45
11155
YDOT = -32
414939 meter/sec RA = 274
71555 deg
ZDOT = 6006
001438 TA = 311
63596
MA = 311
75715
Ha = 188
781 n
mi
Hp = 180
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1030943
51 X = 390663
53
Y = -22007554
95 feet Y = -6703961
48 meter
Z = -976933
61 Z = -296057
22
XDOT = 15830
497572 XDOT = 4795
962954
YDOT = -106
348225 feet/sec YDOT = 21
379279 meter/sec
ZDOT = 19704
729127 ZDOT = 6029
371477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2458323
35 X = 749296
96
Y = 21894360
83 feet Y = 6673401
18 meter
Z = -971251
11 Z = -296037
34
XDOT = -13908
063042 XDOT = -4239
177615
YDOT = 2412
745519 feet/sec YDOT = 735
404834 meter/sec
ZDOT = 19793
443444 ZDOT = 6033
041562
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 07274
50057022
00020000 00000-0 20000-3 0 9033
2 25544 51
6334 275
4345 0002566 56
0519 304
0889 15
75386015 27551
Satellite: ISS
Catalog Number: 25544
Epoch time: 07274
50057022 = yrday
fracday
Element set: 903
Inclination: 51
6334 deg
RA of node: 275
4345 deg
Eccentricity:
0002566
Arg of perigee: 56
0519 deg
Mean anomaly: 304
0889 deg
Mean motion: 15
75386015 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2755
Checksum: 286
Coasting Arc #5 (Orbit 2770)
---------------------------------------
Vector Time (GMT): 2007/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206634
62 A = 6716304
26 meter
Y = -199533
91 meter E =
0017229
Z = -5246710
32 I = 51
28992
XDOT = 106
407459 Wp = 86
36482
YDOT = -7687
013294 meter/sec RA = 269
54645 deg
ZDOT = 208
691664 TA = 185
61839
MA = 185
63774
Ha = 188
881 n
mi
Hp = 180
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13801294
68 X = -4178602
88
Y = -654638
81 feet Y = -246418
06 meter
Z = -17213616
54 Z = -5267078
31
XDOT = 349
105838 XDOT = 191
343087
YDOT = -25219
859890 feet/sec YDOT = -7685
348490 meter/sec
ZDOT = 684
683938 ZDOT = 209
414790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13607034
16 X = 4147424
01
Y = -1756099
18 feet Y = -535259
03 meter
Z = -17290969
27 Z = -5270287
43
XDOT = 3949
687987 XDOT = 1203
864898
YDOT = 23898
173803 feet/sec YDOT = 7284
163375 meter/sec
ZDOT = 686
489915 ZDOT = 209
242126
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 07275
51553125
00020000 00000-0 20000-3 0 9041
2 25544 51
6325 270
2103 0002641 55
0083 305
1328 15
75340408 27719
Satellite: ISS
Catalog Number: 25544
Epoch time: 07275
51553125 = yrday
fracday
Element set: 904
Inclination: 51
6325 deg
RA of node: 270
2103 deg
Eccentricity:
0002641
Arg of perigee: 55
0083 deg
Mean anomaly: 305
1328 deg
Mean motion: 15
75340408 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2771
Checksum: 252
Coasting Arc #6 (Orbit 2786)
---------------------------------------
Vector Time (GMT): 2007/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 118436
96 A = 6728039
17 meter
Y = 6689735
82 meter E =
0011456
Z = -670684
22 I = 51
33099
XDOT = -4845
742651 Wp = 126
17546
YDOT = -504
415228 meter/sec RA = 264
38461 deg
ZDOT = -5964
450260 TA = 61
16391
MA = 61
04895
Ha = 188
871 n
mi
Hp = 180
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 388572
72 X = 46880
62
Y = 21947952
15 feet Y = 6690660
16 meter
Z = -2200407
55 Z = -670282
61
XDOT = -15898
105810 XDOT = -4810
767636
YDOT = -1654
905603 feet/sec YDOT = -558
407460 meter/sec
ZDOT = -19568
406365 ZDOT = -5987
906089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4609137
66 X = -1404865
16
Y = -21462287
15 feet Y = -6541705
12 meter
Z = -2198059
57 Z = -669968
56
XDOT = 14246
613376 XDOT = 4342
367757
YDOT = -1072
359867 feet/sec YDOT = -326
855288 meter/sec
ZDOT = -19657
527618 ZDOT = -5991
614418
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 07276
53047727
00020000 00000-0 20000-3 0 9051
2 25544 51
6320 264
9862 0002769 58
0091 302
1341 15
75386148 27879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07276
53047727 = yrday
fracday
Element set: 905
Inclination: 51
6320 deg
RA of node: 264
9862 deg
Eccentricity:
0002769
Arg of perigee: 58
0091 deg
Mean anomaly: 302
1341 deg
Mean motion: 15
75386148 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2787
Checksum: 302
Coasting Arc #7 (Orbit 2802)
---------------------------------------
Vector Time (GMT): 2007/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4298461
11 A = 6716654
95 meter
Y = 666820
51 meter E =
0006903
Z = 5113580
45 I = 51
29625
XDOT = 382
448424 Wp = 56
63870
YDOT = 7586
234867 meter/sec RA = 259
19709 deg
ZDOT = -1305
728697 TA = 45
92789
MA = 45
87108
Ha = 188
687 n
mi
Hp = 180
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14102562
70 X = 4265844
22
Y = 2187731
34 feet Y = 714706
01 meter
Z = 16776838
74 Z = 5134383
21
XDOT = 1254
752046 XDOT = 303
932599
YDOT = 24889
222005 feet/sec YDOT = 7590
072606 meter/sec
ZDOT = -4283
886801 ZDOT = -1304
061537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14155885
42 X = -4314713
88
Y = 787301
83 feet Y = 239969
60 meter
Z = 16855913
65 Z = 5137682
48
XDOT = -6393
252560 XDOT = -1948
663380
YDOT = -23040
521481 feet/sec YDOT = -7022
750947 meter/sec
ZDOT = -4276
613846 ZDOT = -1303
511900
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 07277
54540749
00020000 00000-0 20000-3 0 9066
2 25544 51
6313 259
7623 0002653 59
5086 300
6340 15
75406720 28030
Satellite: ISS
Catalog Number: 25544
Epoch time: 07277
54540749 = yrday
fracday
Element set: 906
Inclination: 51
6313 deg
RA of node: 259
7623 deg
Eccentricity:
0002653
Arg of perigee: 59
5086 deg
Mean anomaly: 300
6340 deg
Mean motion: 15
75406720 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2803
Checksum: 288
Coasting Arc #8 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2007/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -525277
55 A = 6726866
68 meter
Y = -6504087
79 meter E =
0016680
Z = 1602109
14 I = 51
33796
XDOT = 5055
425538 Wp = 63
79209
YDOT = 1012
217699 meter/sec RA = 254
05419 deg
ZDOT = 5728
064626 TA = 313
98801
MA = 314
12541
Ha = 188
702 n
mi
Hp = 180
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1723351
55 X = -460291
60
Y = -21338870
69 feet Y = -6509598
33 meter
Z = 5256263
59 Z = 1599715
39
XDOT = 16586
041790 XDOT = 5015
905081
YDOT = 3320
924209 feet/sec YDOT = 1068
529527 meter/sec
ZDOT = 18792
862945 ZDOT = 5752
527901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6524243
02 X = 1988589
27
Y = 20392539
00 feet Y = 6215645
89 meter
Z = 5246356
45 Z = 1599089
45
XDOT = -15317
275680 XDOT = -4668
705627
YDOT = 8
994347 feet/sec YDOT = 2
741477 meter/sec
ZDOT = 18885
887860 ZDOT = 5756
418620
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 07278
56032051
00020000 00000-0 20000-3 0 9072
2 25544 51
6312 254
5388 0002576 67
1434 293
0001 15
75479890 28190
Satellite: ISS
Catalog Number: 25544
Epoch time: 07278
56032051 = yrday
fracday
Element set: 907
Inclination: 51
6312 deg
RA of node: 254
5388 deg
Eccentricity:
0002576
Arg of perigee: 67
1434 deg
Mean anomaly: 293
0001 deg
Mean motion: 15
75479890 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2819
Checksum: 294
Coasting Arc #9 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2007/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4561951
91 A = 6717892
01 meter
Y = -1090950
13 meter E =
0014243
Z = -4822207
52 I = 51
31652
XDOT = -771
620048 Wp = 100
03263
YDOT = -7274
206530 meter/sec RA = 248
85016 deg
ZDOT = 2379
171239 TA = 193
29091
MA = 193
32847
Ha = 188
812 n
mi
Hp = 180
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14967033
82 X = -4525988
21
Y = -3579232
70 feet Y = -1141763
62 meter
Z = -15820890
82 Z = -4844282
13
XDOT = -2531
561838 XDOT = -701
779046
YDOT = -23865
506988 feet/sec YDOT = -7282
444598 meter/sec
ZDOT = 7805
679919 ZDOT = 2375
592719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15301662
36 X = 4663946
69
Y = -134659
74 feet Y = -41044
29 meter
Z = -15904860
58 Z = -4847801
51
XDOT = 8274
806064 XDOT = 2522
160888
YDOT = 21413
334687 feet/sec YDOT = 6526
784413 meter/sec
ZDOT = 7791
166043 ZDOT = 2374
747410
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 07279
51179055
00020000 00000-0 20000-3 0 9085
2 25544 51
6311 249
6406 0002711 65
3880 294
7566 15
75431895 28345
Satellite: ISS
Catalog Number: 25544
Epoch time: 07279
51179055 = yrday
fracday
Element set: 908
Inclination: 51
6311 deg
RA of node: 249
6406 deg
Eccentricity:
0002711
Arg of perigee: 65
3880 deg
Mean anomaly: 294
7566 deg
Mean motion: 15
75431895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2834
Checksum: 312
Coasting Arc #10 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2007/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 775607
65 A = 6725122
52 meter
Y = 6175491
28 meter E =
0006927
Z = -2549483
50 I = 51
35365
XDOT = -5422
267333 Wp = 109
02085
YDOT = -1484
206797 meter/sec RA = 243
72198 deg
ZDOT = -5258
547101 TA = 100
01347
MA = 99
93530
Ha = 188
761 n
mi
Hp = 180
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2544644
54 X = 718879
74
Y = 20260798
16 feet Y = 6183847
20 meter
Z = -8364447
19 Z = -2545853
81
XDOT = -17789
590988 XDOT = -5379
722500
YDOT = -4869
444873 feet/sec YDOT = -1544
604146 meter/sec
ZDOT = -17252
451120 ZDOT = -5284
785173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7752643
41 X = -2363005
71
Y = -18897495
12 feet Y = -5759956
51 meter
Z = -8349870
25 Z = -2545040
45
XDOT = 16971
688070 XDOT = 5172
970524
YDOT = 684
414129 feet/sec YDOT = 208
609426 meter/sec
ZDOT = -17352
287542 ZDOT = -5288
977243
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 07280
52667401
00020000 00000-0 20000-3 0 9096
2 25544 51
6317 244
4159 0002743 67
7380 292
4074 15
75488050 28507
Satellite: ISS
Catalog Number: 25544
Epoch time: 07280
52667401 = yrday
fracday
Element set: 909
Inclination: 51
6317 deg
RA of node: 244
4159 deg
Eccentricity:
0002743
Arg of perigee: 67
7380 deg
Mean anomaly: 292
4074 deg
Mean motion: 15
75488050 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2850
Checksum: 295
Coasting Arc #11 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2007/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4936650
47 A = 6719655
41 meter
Y = 1456213
42 meter E =
0012216
Z = 4312506
39 I = 51
34968
XDOT = 981
075966 Wp = 70
72618
YDOT = 6837
085885 meter/sec RA = 238
50776 deg
ZDOT = -3419
915069 TA = 53
95247
MA = 53
83935
Ha = 188
594 n
mi
Hp = 180
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16196359
81 X = 4899050
38
Y = 4777603
10 feet Y = 1511207
96 meter
Z = 14148643
01 Z = 4336397
42
XDOT = 3218
753169 XDOT = 921
163224
YDOT = 22431
384137 feet/sec YDOT = 6847
721565 meter/sec
ZDOT = -11220
193797 ZDOT = -3415
295040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16809046
71 X = -5123397
44
Y = -149546
94 feet Y = -45581
91 meter
Z = 14239566
22 Z = 4340219
79
XDOT = -9349
257149 XDOT = -2849
653579
YDOT = -19431
849229 feet/sec YDOT = -5922
827645 meter/sec
ZDOT = -11201
763651 ZDOT = -3414
297561
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 07281
54154104
00020000 00000-0 20000-3 0 9102
2 25544 51
6318 239
1918 0002653 70
3976 289
7474 15
75513951 28662
Satellite: ISS
Catalog Number: 25544
Epoch time: 07281
54154104 = yrday
fracday
Element set: 910
Inclination: 51
6318 deg
RA of node: 239
1918 deg
Eccentricity:
0002653
Arg of perigee: 70
3976 deg
Mean anomaly: 289
7474 deg
Mean motion: 15
75513951 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2866
Checksum: 306
Coasting Arc #12 (Orbit 2881)
---------------------------------------
Vector Time (GMT): 2007/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -885209
74 A = 6722755
39 meter
Y = -5730683
81 meter E =
0015077
Z = 3388155
87 I = 51
37751
XDOT = 5918
208061 Wp = 88
07821
YDOT = 1811
922474 meter/sec RA = 233
39114 deg
ZDOT = 4593
826240 TA = 312
14233
MA = 312
27034
Ha = 188
625 n
mi
Hp = 180
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2904231
41 X = -837521
87
Y = -18801456
06 feet Y = -5740315
80 meter
Z = 11115996
96 Z = 3383971
78
XDOT = 19416
693113 XDOT = 5875
190704
YDOT = 5944
627538 feet/sec YDOT = 1877
863089 meter/sec
ZDOT = 15071
608399 ZDOT = 4622
472676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8330417
53 X = 2539111
26
Y = 17114409
66 feet Y = 5216472
06 meter
Z = 11099361
44 Z = 3383085
37
XDOT = -18976
900251 XDOT = -5784
159196
YDOT = -644
614425 feet/sec YDOT = -196
478477 meter/sec
ZDOT = 15180
641552 ZDOT = 4627
059545
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 07282
55639056
00020000 00000-0 20000-3 0 9119
2 25544 51
6327 233
9676 0002578 76
9734 283
1718 15
75560730 28829
Satellite: ISS
Catalog Number: 25544
Epoch time: 07282
55639056 = yrday
fracday
Element set: 911
Inclination: 51
6327 deg
RA of node: 233
9676 deg
Eccentricity:
0002578
Arg of perigee: 76
9734 deg
Mean anomaly: 283
1718 deg
Mean motion: 15
75560730 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2882
Checksum: 320
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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