Date:
February 27th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 604)
---------------------------------------
Vector Time (GMT): 2010/057/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3797523
60 A = 6722012
65 meter
Y = -1849179
60 meter E =
0015712
Z = -5241338
99 I = 51
95368
XDOT = 2291
928459 Wp = 54
63244
YDOT = 7284
528366 meter/sec RA = 77
84134 deg
ZDOT = -902
456925 TA = 206
75656
MA = 206
83770
Ha = 192
096 n
mi
Hp = 184
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12459066
94 X = 3843379
94
Y = -6066862
22 feet Y = -1806457
25 meter
Z = -17195994
07 Z = -5222779
72
XDOT = 7519
450324 XDOT = 2214
685070
YDOT = 23899
371281 feet/sec YDOT = 7309
726145 meter/sec
ZDOT = -2960
816684 ZDOT = -891
510970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12973645
43 X = 3954367
13
Y = -5123292
07 feet Y = -1561579
42 meter
Z = -17122318
22 Z = -5218882
59
XDOT = 5377
867337 XDOT = 1639
173964
YDOT = 23444
510419 feet/sec YDOT = 7145
886776 meter/sec
ZDOT = -2917
120110 ZDOT = -889
138209
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 10057
57364726
00016717 00000-0 10270-3 0 9000
2 25544 51
6436 78
4603 0007514 346
9736 13
1231 15
73422785 6056
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
57364726 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 78
4603 deg
Eccentricity:
0007514
Arg of perigee: 346
9736 deg
Mean anomaly: 13
1231 deg
Mean motion: 15
73422785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 605
Checksum: 300
Coasting Arc #2 (Orbit 620)
---------------------------------------
Vector Time (GMT): 2010/058/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2670749
16 A = 6733274
34 meter
Y = -6107401
92 meter E =
0010006
Z = 940966
02 I = 51
98403
XDOT = 4045
119320 Wp = 91
36619
YDOT = -2696
361325 meter/sec RA = 72
71597 deg
ZDOT = -5965
667639 TA = 78
41441
MA = 78
30210
Ha = 192
166 n
mi
Hp = 184
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8762300
38 X = -2606827
52
Y = -20037407
88 feet Y = -6136910
35 meter
Z = 3087158
87 Z = 928147
60
XDOT = 13271
388845 XDOT = 4103
949164
YDOT = -8846
329808 feet/sec YDOT = -2650
797888 meter/sec
ZDOT = -19572
400392 ZDOT = -5945
873940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7630605
90 X = -2325808
68
Y = -20502740
88 feet Y = -6249235
42 meter
Z = 3036057
05 Z = 925390
19
XDOT = 12370
992423 XDOT = 3770
678490
YDOT = -7517
487652 feet/sec YDOT = -2291
330236 meter/sec
ZDOT = -19493
843171 ZDOT = -5941
723399
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 10058
58983413
00016717 00000-0 10270-3 0 9013
2 25544 51
6430 73
2455 0007678 351
4177 8
6853 15
73482793 6211
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
58983413 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 73
2455 deg
Eccentricity:
0007678
Arg of perigee: 351
4177 deg
Mean anomaly: 8
6853 deg
Mean motion: 15
73482793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 621
Checksum: 318
Coasting Arc #3 (Orbit 636)
---------------------------------------
Vector Time (GMT): 2010/059/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3219410
09 A = 6722049
52 meter
Y = 2827732
60 meter E =
0005905
Z = 5176144
93 I = 51
93556
XDOT = -3778
718397 Wp = 25
97182
YDOT = -6594
114983 meter/sec RA = 67
62587 deg
ZDOT = 1256
777093 TA = 52
09536
MA = 52
04198
Ha = 192
363 n
mi
Hp = 184
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10562369
05 X = -3275935
17
Y = 9277337
94 feet Y = 2791415
70 meter
Z = 16982102
78 Z = 5160367
86
XDOT = -12397
370070 XDOT = -3710
806031
YDOT = -21634
235508 feet/sec YDOT = -6635
991016 meter/sec
ZDOT = 4123
284426 ZDOT = 1238
586141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11020087
62 X = -3358922
71
Y = 8849431
36 feet Y = 2697306
68 meter
Z = 16919506
13 Z = 5157065
47
XDOT = -10912
038917 XDOT = -3325
989462
YDOT = -21304
203790 feet/sec YDOT = -6493
521315 meter/sec
ZDOT = 4050
826763 ZDOT = 1234
691998
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 10059
60600087
00016717 00000-0 10270-3 0 9021
2 25544 51
6423 68
0307 0007678 354
5347 5
5731 15
73488815 6373
Satellite: ISS
Catalog Number: 25544
Epoch time: 10059
60600087 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 68
0307 deg
Eccentricity:
0007678
Arg of perigee: 354
5347 deg
Mean anomaly: 5
5731 deg
Mean motion: 15
73488815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 637
Checksum: 308
Coasting Arc #4 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2010/060/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3885439
43 A = 6732814
22 meter
Y = 5343277
82 meter E =
0015851
Z = -1250591
37 I = 51
95970
XDOT = -3255
462998 Wp = 20
04003
YDOT = 3739
048587 meter/sec RA = 62
49396 deg
ZDOT = 5897
507991 TA = 326
30020
MA = 326
40088
Ha = 192
331 n
mi
Hp = 183
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12747504
68 X = 3831476
20
Y = 17530439
06 feet Y = 5386425
25 meter
Z = -4102990
07 Z = -1231847
93
XDOT = -10680
652881 XDOT = -3325
680232
YDOT = 12267
219774 feet/sec YDOT = 3702
252108 meter/sec
ZDOT = 19348
779497 ZDOT = 5881
522294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12377349
33 X = 3772616
08
Y = 17810757
52 feet Y = 5428718
89 meter
Z = -4028378
88 Z = -1227849
88
XDOT = -9766
284051 XDOT = -2976
763379
YDOT = 11121
354609 feet/sec YDOT = 3389
788885 meter/sec
ZDOT = 19285
379305 ZDOT = 5878
183612
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 10060
55863733
00016717 00000-0 10270-3 0 9037
2 25544 51
6423 63
1425 0007595 359
2370
8781 15
73545517 6529
Satellite: ISS
Catalog Number: 25544
Epoch time: 10060
55863733 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 63
1425 deg
Eccentricity:
0007595
Arg of perigee: 359
2370 deg
Mean anomaly:
8781 deg
Mean motion: 15
73545517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 300
Coasting Arc #5 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2010/061/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2437522
48 A = 6722172
08 meter
Y = -3633820
31 meter E =
0017361
Z = -5117276
97 I = 51
90944
XDOT = 5035
150953 Wp = 52
50121
YDOT = 5594
349734 meter/sec RA = 57
40646 deg
ZDOT = -1567
474029 TA = 202
44689
MA = 202
52295
Ha = 192
399 n
mi
Hp = 183
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7997121
01 X = 2502833
83
Y = -11921982
64 feet Y = -3606197
85 meter
Z = -16788966
43 Z = -5105276
62
XDOT = 16519
524123 XDOT = 4979
834121
YDOT = 18354
165793 feet/sec YDOT = 5650
346323 meter/sec
ZDOT = -5142
631328 ZDOT = -1543
148553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8156342
06 X = 2486053
06
Y = -11880944
68 feet Y = -3621311
94 meter
Z = -16741393
19 Z = -5102776
65
XDOT = 15589
333190 XDOT = 4751
628756
YDOT = 17843
395070 feet/sec YDOT = 5438
666817 meter/sec
ZDOT = -5045
846966 ZDOT = -1537
974155
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 10061
57476291
00016717 00000-0 10270-3 0 9040
2 25544 51
6428 57
9270 0007718 2
2846 357
8350 15
73551258 6686
Satellite: ISS
Catalog Number: 25544
Epoch time: 10061
57476291 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 57
9270 deg
Eccentricity:
0007718
Arg of perigee: 2
2846 deg
Mean anomaly: 357
8350 deg
Mean motion: 15
73551258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 668
Checksum: 320
Coasting Arc #6 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2010/062/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4870180
59 A = 6732384
91 meter
Y = -4405200
19 meter E =
0013064
Z = 1475521
78 I = 51
92758
XDOT = 2286
330307 Wp = 85
15229
YDOT = -4491
169247 meter/sec RA = 52
26727 deg
ZDOT = -5817
140006 TA = 78
67851
MA = 78
53175
Ha = 192
442 n
mi
Hp = 183
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15978282
78 X = -4827726
65
Y = -14452756
54 feet Y = -4459423
94 meter
Z = 4840950
73 Z = 1451966
18
XDOT = 7501
083683 XDOT = 2364
639802
YDOT = -14734
807241 feet/sec YDOT = -4465
164822 meter/sec
ZDOT = -19085
105007 ZDOT = -5805
842492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16180240
20 X = -4931737
21
Y = -14257832
57 feet Y = -4345787
37 meter
Z = 4747265
92 Z = 1446966
65
XDOT = 6394
525989 XDOT = 1949
051521
YDOT = -13646
437676 feet/sec YDOT = -4159
434204 meter/sec
ZDOT = -19040
341553 ZDOT = -5803
496105
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 10062
59086632
00016717 00000-0 10270-3 0 9050
2 25544 51
6434 52
7123 0007852 5
4663 354
6585 15
73607232 6841
Satellite: ISS
Catalog Number: 25544
Epoch time: 10062
59086632 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 52
7123 deg
Eccentricity:
0007852
Arg of perigee: 5
4663 deg
Mean anomaly: 354
6585 deg
Mean motion: 15
73607232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 684
Checksum: 305
Coasting Arc #7 (Orbit 699)
---------------------------------------
Vector Time (GMT): 2010/063/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1532519
38 A = 6722132
93 meter
Y = 4167108
52 meter E =
0007176
Z = 5041209
43 I = 51
87493
XDOT = -6043
245406 Wp = 49
96266
YDOT = -4420
701890 meter/sec RA = 47
18249 deg
ZDOT = 1819
882500 TA = 22
58186
MA = 22
55030
Ha = 192
496 n
mi
Hp = 183
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5027950
72 X = -1603491
94
Y = 13671615
89 feet Y = 4149574
50 meter
Z = 16539401
02 Z = 5033591
82
XDOT = -19826
920624 XDOT = -6002
203782
YDOT = -14503
615126 feet/sec YDOT = -4488
051447 meter/sec
ZDOT = 5970
743109 ZDOT = 1790
624619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4722262
72 X = -1439345
68
Y = 13816307
34 feet Y = 4211210
48 meter
Z = 16509241
11 Z = 5032016
69
XDOT = -19270
646791 XDOT = -5873
693142
YDOT = -13570
888777 feet/sec YDOT = -4136
406899 meter/sec
ZDOT = 5854
415245 ZDOT = 1784
425767
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 10063
60694782
00016717 00000-0 10270-3 0 9065
2 25544 51
6441 47
4983 0007771 8
5056 351
6238 15
73651280 7007
Satellite: ISS
Catalog Number: 25544
Epoch time: 10063
60694782 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 47
4983 deg
Eccentricity:
0007771
Arg of perigee: 8
5056 deg
Mean anomaly: 351
6238 deg
Mean motion: 15
73651280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 700
Checksum: 306
Coasting Arc #8 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2010/064/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5621845
78 A = 6731942
69 meter
Y = 3276469
65 meter E =
0015293
Z = -1696578
30 I = 51
88658
XDOT = -1187
744095 Wp = 24
99086
YDOT = 4994
988878 meter/sec RA = 42
03662 deg
ZDOT = 5742
901523 TA = 316
30583
MA = 316
42679
Ha = 192
610 n
mi
Hp = 183
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18444375
91 X = 5593031
49
Y = 10749572
35 feet Y = 3339175
28 meter
Z = -5566201
79 Z = -1669337
73
XDOT = -3896
798212 XDOT = -1271
408447
YDOT = 16387
758786 feet/sec YDOT = 4981
239304 meter/sec
ZDOT = 18841
540429 ZDOT = 5736
928044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18956572
54 X = 5777963
31
Y = 9878784
12 feet Y = 3011053
40 meter
Z = -5457920
19 Z = -1663574
07
XDOT = -2520
862893 XDOT = -768
359010
YDOT = 15174
460187 feet/sec YDOT = 4625
175465 meter/sec
ZDOT = 18817
923486 ZDOT = 5735
703078
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 10064
55950511
00016717 00000-0 10270-3 0 9076
2 25544 51
6442 42
6096 0007826 13
0453 347
0911 15
73658250 7150
Satellite: ISS
Catalog Number: 25544
Epoch time: 10064
55950511 = yrday
fracday
Element set: 907
Inclination: 51
6442 deg
RA of node: 42
6096 deg
Eccentricity:
0007826
Arg of perigee: 13
0453 deg
Mean anomaly: 347
0911 deg
Mean motion: 15
73658250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 290
Coasting Arc #9 (Orbit 730)
---------------------------------------
Vector Time (GMT): 2010/065/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 555362
84 A = 6722271
18 meter
Y = -4488988
74 meter E =
0018295
Z = -4988755
79 I = 51
83222
XDOT = 6744
171609 Wp = 53
39950
YDOT = 3085
881540 meter/sec RA = 36
95097 deg
ZDOT = -2020
388765 TA = 197
03921
MA = 197
10073
Ha = 192
557 n
mi
Hp = 182
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1822056
55 X = 629752
47
Y = -14727653
36 feet Y = -4482362
57 meter
Z = -16367309
03 Z = -4985877
03
XDOT = 22126
547273 XDOT = 6718
978080
YDOT = 10124
283268 feet/sec YDOT = 3161
157942 meter/sec
ZDOT = -6628
572063 ZDOT = -1987
687189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 976648
62 X = 297682
50
Y = -14820288
05 feet Y = -4517223
80 meter
Z = -16355967
96 Z = -4985299
03
XDOT = 21684
042781 XDOT = 6609
296240
YDOT = 8621
147616 feet/sec YDOT = 2627
725793 meter/sec
ZDOT = -6498
604921 ZDOT = -1980
774780
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 10065
57554371
00016717 00000-0 10270-3 0 9084
2 25544 51
6451 37
3945 0007823 16
3479 343
7935 15
73697851 7312
Satellite: ISS
Catalog Number: 25544
Epoch time: 10065
57554371 = yrday
fracday
Element set: 908
Inclination: 51
6451 deg
RA of node: 37
3945 deg
Eccentricity:
0007823
Arg of perigee: 16
3479 deg
Mean anomaly: 343
7935 deg
Mean motion: 15
73697851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 731
Checksum: 330
Coasting Arc #10 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2010/066/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6123633
66 A = 6731548
55 meter
Y = -2109881
54 meter E =
0015630
Z = 1824373
11 I = 51
83933
XDOT = 86
025580 Wp = 84
01677
YDOT = -5196
884505 meter/sec RA = 31
79911 deg
ZDOT = -5678
420445 TA = 75
81263
MA = 75
63904
Ha = 192
620 n
mi
Hp = 182
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20090661
62 X = -6108447
83
Y = -6922183
54 feet Y = -2178274
70 meter
Z = 5985476
09 Z = 1794661
82
XDOT = 282
236156 XDOT = 171
716060
YDOT = -17050
146015 feet/sec YDOT = -5195
443531 meter/sec
ZDOT = -18629
988338 ZDOT = -5677
794275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20619140
47 X = -6284714
01
Y = -5272741
04 feet Y = -1607131
47 meter
Z = 5867408
42 Z = 1788386
09
XDOT = -1372
130308 XDOT = -418
225318
YDOT = -15522
893543 feet/sec YDOT = -4731
377952 meter/sec
ZDOT = -18627
604956 ZDOT = -5677
693991
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 10066
59155953
00016717 00000-0 10270-3 0 9091
2 25544 51
6456 32
1797 0007854 20
2383 339
9090 15
73733107 7478
Satellite: ISS
Catalog Number: 25544
Epoch time: 10066
59155953 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 32
1797 deg
Eccentricity:
0007854
Arg of perigee: 20
2383 deg
Mean anomaly: 339
9090 deg
Mean motion: 15
73733107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 323
Coasting Arc #11 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2010/067/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 405593
80 A = 6722130
74 meter
Y = 4546673
06 meter E =
0008984
Z = 4926386
59 I = 51
78257
XDOT = -7195
627875 Wp = 65
60466
YDOT = -1708
389561 meter/sec RA = 26
71229 deg
ZDOT = 2169
693353 TA = 3
40220
MA = 3
39610
Ha = 192
518 n
mi
Hp = 182
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1330688
34 X = 330790
85
Y = 14916906
36 feet Y = 4550790
53 meter
Z = 16162685
67 Z = 4928175
13
XDOT = -23607
703001 XDOT = -7186
529368
YDOT = -5604
952628 feet/sec YDOT = -1788
804419 meter/sec
ZDOT = 7118
416513 ZDOT = 2134
759717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2690963
44 X = 820205
66
Y = 14724502
28 feet Y = 4488028
29 meter
Z = 16169878
88 Z = 4928579
08
XDOT = -23010
720837 XDOT = -7013
667711
YDOT = -3457
418761 feet/sec YDOT = -1053
821238 meter/sec
ZDOT = 6979
610659 ZDOT = 2127
385329
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 10067
60755018
00016717 00000-0 10270-3 0 9104
2 25544 51
6459 26
9652 0007694 23
1786 336
9723 15
73807525 7637
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067
60755018 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 26
9652 deg
Eccentricity:
0007694
Arg of perigee: 23
1786 deg
Mean anomaly: 336
9723 deg
Mean motion: 15
73807525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 325
Coasting Arc #12 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2010/068/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6376558
43 A = 6731164
43 meter
Y = 863368
26 meter E =
0014785
Z = -1955399
90 I = 51
78490
XDOT = 1016
061238 Wp = 32
15429
YDOT = 5162
710748 meter/sec RA = 21
55373 deg
ZDOT = 5624
475326 TA = 306
12643
MA = 306
26319
Ha = 192
717 n
mi
Hp = 182
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20920467
30 X = 6375928
97
Y = 2832573
04 feet Y = 934671
14 meter
Z = -6415354
00 Z = -1924424
75
XDOT = 3333
534245 XDOT = 930
933226
YDOT = 16938
027387 feet/sec YDOT = 5173
597161 meter/sec
ZDOT = 18453
003039 ZDOT = 5629
204309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21144539
99 X = 6444855
79
Y = 402145
01 feet Y = 122573
80 meter
Z = -6292288
69 Z = -1917889
59
XDOT = 5181
858244 XDOT = 1579
430393
YDOT = 14913
002597 feet/sec YDOT = 4545
483192 meter/sec
ZDOT = 18471
887932 ZDOT = 5630
231442
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 10068
56002300
00016717 00000-0 10270-3 0 9110
2 25544 51
6456 22
0757 0007854 26
7696 333
3871 15
73791779 7788
Satellite: ISS
Catalog Number: 25544
Epoch time: 10068
56002300 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 22
0757 deg
Eccentricity:
0007854
Arg of perigee: 26
7696 deg
Mean anomaly: 333
3871 deg
Mean motion: 15
73791779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 322
Coasting Arc #13 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2010/069/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1324711
20 A = 6722149
40 meter
Y = -4424188
63 meter E =
0019017
Z = -4901825
67 I = 51
72771
XDOT = 7339
859036 Wp = 57
08318
YDOT = 310
058473 meter/sec RA = 16
46325 deg
ZDOT = -2259
626309 TA = 190
90440
MA = 190
94569
Ha = 192
636 n
mi
Hp = 182
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4346165
37 X = -1251329
02
Y = -14515054
55 feet Y = -4438592
27 meter
Z = -16082105
23 Z = -4908082
52
XDOT = 24080
902349 XDOT = 7346
823011
YDOT = 1017
252209 feet/sec YDOT = 392
175965 meter/sec
ZDOT = -7413
472144 ZDOT = -2223
953156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6132204
75 X = -1869096
01
Y = -13826395
36 feet Y = -4214285
31 meter
Z = -16107045
87 Z = -4909427
58
XDOT = 23038
716082 XDOT = 7022
200662
YDOT = -1732
253441 feet/sec YDOT = -527
990849 meter/sec
ZDOT = -7271
754754 ZDOT = -2216
430849
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 10069
57596950
00016717 00000-0 10270-3 0 9122
2 25544 51
6465 16
8598 0007857 31
2212 328
9416 15
73855303 7947
Satellite: ISS
Catalog Number: 25544
Epoch time: 10069
57596950 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 16
8598 deg
Eccentricity:
0007857
Arg of perigee: 31
2212 deg
Mean anomaly: 328
9416 deg
Mean motion: 15
73855303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 333
Coasting Arc #14 (Orbit 809)
---------------------------------------
Vector Time (GMT): 2010/070/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6419405
50 A = 6730878
70 meter
Y = 315628
30 meter E =
0017546
Z = 1986561
51 I = 51
72811
XDOT = -1986
469352 Wp = 86
11263
YDOT = -4900
100857 meter/sec RA = 11
29947 deg
ZDOT = -5597
137841 TA = 71
79226
MA = 71
60134
Ha = 192
678 n
mi
Hp = 182
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21061041
68 X = -6432107
95
Y = 1035525
92 feet Y = 243771
80 meter
Z = 6517590
27 Z = 1955345
87
XDOT = -6517
287901 XDOT = -1904
338636
YDOT = -16076
446382 feet/sec YDOT = -4921
855889 meter/sec
ZDOT = -18363
313126 ZDOT = -5606
588078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20708476
62 X = -6311943
67
Y = 4171297
39 feet Y = 1271411
44 meter
Z = 6393594
27 Z = 1948767
53
XDOT = -8431
391321 XDOT = -2569
888074
YDOT = -13430
909844 feet/sec YDOT = -4093
741321 meter/sec
ZDOT = -18400
949707 ZDOT = -5608
609471
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 10070
59189214
00016717 00000-0 10270-3 0 9138
2 25544 51
6468 11
6442 0007808 34
8993 325
2681 15
73877272 8104
Satellite: ISS
Catalog Number: 25544
Epoch time: 10070
59189214 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 11
6442 deg
Eccentricity:
0007808
Arg of perigee: 34
8993 deg
Mean anomaly: 325
2681 deg
Mean motion: 15
73877272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 810
Checksum: 316
Coasting Arc #15 (Orbit 825)
---------------------------------------
Vector Time (GMT): 2010/071/13:21:01
001
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2129901
06 A = 6721967
82 meter
Y = 4104052
88 meter E =
0010648
Z = 4869285
18 I = 51
66921
XDOT = -7281
684006 Wp = 75
82763
YDOT = 1041
759847 meter/sec RA = 6
20538 deg
ZDOT = 2305
457549 TA = 351
75210
MA = 351
76959
Ha = 192
560 n
mi
Hp = 181
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6987864
39 X = 2060196
91
Y = 13464740
43 feet Y = 4127481
37 meter
Z = 15975345
07 Z = 4879462
36
XDOT = -23890
039389 XDOT = -7303
991218
YDOT = 3417
847266 feet/sec YDOT = 960
207194 meter/sec
ZDOT = 7563
837104 ZDOT = 2270
029623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9035206
45 X = 2753930
93
Y = 12132542
03 feet Y = 3697998
81 meter
Z = 16015854
70 Z = 4881632
51
XDOT = -22148
810002 XDOT = -6750
957289
YDOT = 6688
320539 feet/sec YDOT = 2038
600100 meter/sec
ZDOT = 7423
126761 ZDOT = 2262
569037
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 10071
60778961
00016717 00000-0 10270-3 0 9145
2 25544 51
6469 6
4285 0007716 38
5814 321
5900 15
73933746 8262
Satellite: ISS
Catalog Number: 25544
Epoch time: 10071
60778961 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 6
4285 deg
Eccentricity:
0007716
Arg of perigee: 38
5814 deg
Mean anomaly: 321
5900 deg
Mean motion: 15
73933746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 826
Checksum: 321
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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