Date:
February 26th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 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 572)
---------------------------------------
Vector Time (GMT): 2010/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3444208
30 A = 6726083
88 meter
Y = -3908371
07 meter E =
0011945
Z = 4255128
79 I = 51
97590
XDOT = 2637
316512 Wp = 34
46692
YDOT = -6267
798588 meter/sec RA = 88
30870 deg
ZDOT = -3607
788297 TA = 92
11072
MA = 91
97393
Ha = 191
822 n
mi
Hp = 185
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11299896
00 X = -3420918
41
Y = -12822739
71 feet Y = -3946756
05 meter
Z = 13960396
29 Z = 4238453
74
XDOT = 8652
613227 XDOT = 2724
733736
YDOT = -20563
643663 feet/sec YDOT = -6237
817754 meter/sec
ZDOT = -11836
575776 ZDOT = -3594
764201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4460159
91 X = -1359456
74
Y = -16554922
73 feet Y = -5045940
45 meter
Z = 13894044
59 Z = 4234904
79
XDOT = 15777
903159 XDOT = 4809
104883
YDOT = -14181
824666 feet/sec YDOT = -4322
620158 meter/sec
ZDOT = -11785
028265 ZDOT = -3592
076615
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 10055
54121520
00016717 00000-0 10270-3 0 9008
2 25544 51
6451 88
8859 0007492 337
9458 22
1381 15
73404053 5735
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
54121520 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 88
8859 deg
Eccentricity:
0007492
Arg of perigee: 337
9458 deg
Mean anomaly: 22
1381 deg
Mean motion: 15
73404053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 573
Checksum: 297
Coasting Arc #2 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2010/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1671948
98 A = 6730061
82 meter
Y = 5780699
72 meter E =
0014068
Z = 2993337
32 I = 51
98683
XDOT = -4398
885928 Wp = 51
48350
YDOT = -3868
664491 meter/sec RA = 83
25051 deg
ZDOT = 5006
961927 TA = 342
93854
MA = 342
98579
Ha = 192
071 n
mi
Hp = 184
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5485396
92 X = -1751006
24
Y = 18965550
26 feet Y = 5761560
99 meter
Z = 9820660
51 Z = 2985023
13
XDOT = -14432
040447 XDOT = -4379
621167
YDOT = -12692
468802 feet/sec YDOT = -3917
747680 meter/sec
ZDOT = 16427
040443 ZDOT = 4985
639542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13175673
56 X = -4015945
30
Y = 14725067
34 feet Y = 4488200
53 meter
Z = 9787801
95 Z = 2983322
03
XDOT = -6566
032979 XDOT = -2001
326852
YDOT = -16753
483292 feet/sec YDOT = -5106
461707 meter/sec
ZDOT = 16342
225366 ZDOT = 4981
110292
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 10056
55744440
00016717 00000-0 10270-3 0 9013
2 25544 51
6449 83
6720 0007500 343
4314 16
6603 15
73383520 5892
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
55744440 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 83
6720 deg
Eccentricity:
0007500
Arg of perigee: 343
4314 deg
Mean anomaly: 16
6603 deg
Mean motion: 15
73383520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 289
Coasting Arc #3 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2010/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4167615
54 A = 6725240
59 meter
Y = 2808840
45 meter E =
0008131
Z = -4472710
96 I = 51
96704
XDOT = -1151
715616 Wp = 60
77989
YDOT = 6877
925264 meter/sec RA = 78
09612 deg
ZDOT = 3254
436306 TA = 241
65177
MA = 241
73380
Ha = 192
140 n
mi
Hp = 184
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13673279
33 X = 4157623
82
Y = 9215355
82 feet Y = 2855389
17 meter
Z = -14674248
57 Z = -4452489
66
XDOT = -3778
594542 XDOT = -1244
349198
YDOT = 22565
371601 feet/sec YDOT = 6864
528275 meter/sec
ZDOT = 10677
284469 ZDOT = 3248
616182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8688176
46 X = 2648156
19
Y = 14097889
98 feet Y = 4297036
87 meter
Z = -14593834
64 Z = -4448200
80
XDOT = -11839
780937 XDOT = -3608
765230
YDOT = 18297
429334 feet/sec YDOT = 5577
056461 meter/sec
ZDOT = 10654
363292 ZDOT = 3247
449931
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
51013987
00016717 00000-0 10270-3 0 9026
2 25544 51
6458 78
7845 0007567 345
7932 14
3017 15
73415977 6043
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
51013987 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 78
7845 deg
Eccentricity:
0007567
Arg of perigee: 345
7932 deg
Mean anomaly: 14
3017 deg
Mean motion: 15
73415977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 323
Coasting Arc #4 (Orbit 619)
---------------------------------------
Vector Time (GMT): 2010/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 339210
07 A = 6730546
62 meter
Y = -6154738
14 meter E =
0005445
Z = -2711776
51 I = 51
97665
XDOT = 5042
082239 Wp = 29
87391
YDOT = 2572
393925 meter/sec RA = 73
03373 deg
ZDOT = -5207
530252 TA = 180
86851
MA = 180
86946
Ha = 192
109 n
mi
Hp = 184
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1112893
93 X = 421181
17
Y = -20192710
43 feet Y = -6150486
75 meter
Z = -8896904
56 Z = -2709929
15
XDOT = 16542
264563 XDOT = 5038
239038
YDOT = 8439
612616 feet/sec YDOT = 2628
755634 meter/sec
ZDOT = -17085
073004 ZDOT = -5183
046049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9138868
38 X = 2785527
08
Y = -18044182
72 feet Y = -5499866
89 meter
Z = -8889744
26 Z = -2709594
05
XDOT = 10566
475268 XDOT = 3220
661662
YDOT = 13721
141996 feet/sec YDOT = 4182
204080 meter/sec
ZDOT = -16987
728583 ZDOT = -5177
859672
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
52633159
00016717 00000-0 10270-3 0 9038
2 25544 51
6445 73
5699 0007495 349
8804 10
2206 15
73452114 6209
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
52633159 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 73
5699 deg
Eccentricity:
0007495
Arg of perigee: 349
8804 deg
Mean anomaly: 10
2206 deg
Mean motion: 15
73452114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 620
Checksum: 301
Coasting Arc #5 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2010/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4586719
70 A = 6724401
98 meter
Y = -1670648
34 meter E =
0012997
Z = 4624349
49 I = 51
94555
XDOT = -397
692500 Wp = 30
97750
YDOT = -7102
511047 meter/sec RA = 67
87956 deg
ZDOT = -2945
852299 TA = 88
16792
MA = 88
01907
Ha = 192
257 n
mi
Hp = 184
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15048292
98 X = -4590161
00
Y = -5481129
72 feet Y = -1721958
56 meter
Z = 15171750
29 Z = 4602059
58
XDOT = -1304
765421 XDOT = -303
931347
YDOT = -23302
201597 feet/sec YDOT = -7106
434317 meter/sec
ZDOT = -9664
869747 ZDOT = -2947
555818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11873743
57 X = -3619117
04
Y = -10871462
86 feet Y = -3313621
88 meter
Z = 15083150
22 Z = 4597344
19
XDOT = 6999
743910 XDOT = 2133
521944
YDOT = -21130
449929 feet/sec YDOT = -6440
561138 meter/sec
ZDOT = -9671
841994 ZDOT = -2947
977440
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
54250400
00016717 00000-0 10270-3 0 9046
2 25544 51
6437 68
3551 0007597 353
8425 6
2643 15
73504010 6366
Satellite: ISS
Catalog Number: 25544
Epoch time: 10059
54250400 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 68
3551 deg
Eccentricity:
0007597
Arg of perigee: 353
8425 deg
Mean anomaly: 6
2643 deg
Mean motion: 15
73504010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 286
Coasting Arc #6 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2010/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1033919
48 A = 6730922
52 meter
Y = 6178678
46 meter E =
0017184
Z = 2432201
33 I = 51
95531
XDOT = -5371
833551 Wp = 48
99045
YDOT = -1227
865928 meter/sec RA = 62
81321 deg
ZDOT = 5389
304757 TA = 338
36894
MA = 338
44144
Ha = 192
248 n
mi
Hp = 184
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3392124
29 X = 952936
60
Y = 20271254
80 feet Y = 6189787
83 meter
Z = 7979663
16 Z = 2437026
63
XDOT = -17624
125824 XDOT = -5383
883848
YDOT = -4028
431523 feet/sec YDOT = -1288
003749 meter/sec
ZDOT = 17681
446052 ZDOT = 5363
179770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4347704
99 X = -1325180
48
Y = 20080305
24 feet Y = 6120477
04 meter
Z = 7999006
52 Z = 2438097
19
XDOT = -13538
042775 XDOT = -4126
395438
YDOT = -9950
823136 feet/sec YDOT = -3033
010892 meter/sec
ZDOT = 17577
626171 ZDOT = 5357
660457
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
55865778
00016717 00000-0 10270-3 0 9050
2 25544 51
6436 63
1410 0007576 357
2460 2
8660 15
73533932 6520
Satellite: ISS
Catalog Number: 25544
Epoch time: 10060
55865778 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 63
1410 deg
Eccentricity:
0007576
Arg of perigee: 357
2460 deg
Mean anomaly: 2
8660 deg
Mean motion: 15
73533932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 652
Checksum: 304
Coasting Arc #7 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2010/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4724093
90 A = 6723781
29 meter
Y = 475872
10 meter E =
0011647
Z = -4768470
55 I = 51
91615
XDOT = 1955
311380 Wp = 69
40769
YDOT = 6956
411997 meter/sec RA = 57
66038 deg
ZDOT = 2640
497376 TA = 226
39613
MA = 226
49283
Ha = 192
464 n
mi
Hp = 183
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15498995
73 X = 4741585
56
Y = 1561260
16 feet Y = 528797
01 meter
Z = -15644588
42 Z = -4745478
78
XDOT = 6415
063582 XDOT = 1864
551333
YDOT = 22822
874007 feet/sec YDOT = 6977
770268 meter/sec
ZDOT = 8663
049135 ZDOT = 2649
774950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14044427
33 X = 4280741
45
Y = 6946964
98 feet Y = 2117434
93 meter
Z = -15553240
41 Z = -4740627
68
XDOT = -1567
102972 XDOT = -477
652986
YDOT = 22578
687278 feet/sec YDOT = 6881
983882 meter/sec
ZDOT = 8700
092945 ZDOT = 2651
788330
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
51128538
00016717 00000-0 10270-3 0 9064
2 25544 51
6436 58
2522 0007695
9919 359
1258 15
73520918 6679
Satellite: ISS
Catalog Number: 25544
Epoch time: 10061
51128538 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 58
2522 deg
Eccentricity:
0007695
Arg of perigee:
9919 deg
Mean anomaly: 359
1258 deg
Mean motion: 15
73520918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 667
Checksum: 317
Coasting Arc #8 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2010/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2348506
86 A = 6731246
03 meter
Y = -5914021
59 meter E =
0005836
Z = -2205361
18 I = 51
92461
XDOT = 5369
103712 Wp = 56
11180
YDOT = -81
321615 meter/sec RA = 52
58738 deg
ZDOT = -5506
696877 TA = 148
46990
MA = 148
43492
Ha = 192
446 n
mi
Hp = 183
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7705075
00 X = -2271487
52
Y = -19402957
99 feet Y = -5939853
56 meter
Z = -7235436
93 Z = -2216582
50
XDOT = 17615
169660 XDOT = 5396
364319
YDOT = -266
803200 feet/sec YDOT = -21
129194 meter/sec
ZDOT = -18066
590804 ZDOT = -5480
547789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -703779
68 X = -214512
05
Y = -20849422
29 feet Y = -6354903
91 meter
Z = -7280164
24 Z = -2218994
06
XDOT = 15261
947637 XDOT = 4651
841640
YDOT = 5748
852013 feet/sec YDOT = 1752
250094 meter/sec
ZDOT = -17962
718148 ZDOT = -5475
036492
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
52740241
00016717 00000-0 10270-3 0 9078
2 25544 51
6434 53
0370 0007728 5
4915 354
6331 15
73573956 6834
Satellite: ISS
Catalog Number: 25544
Epoch time: 10062
52740241 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 53
0370 deg
Eccentricity:
0007728
Arg of perigee: 5
4915 deg
Mean anomaly: 354
6331 deg
Mean motion: 15
73573956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 296
Coasting Arc #9 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2010/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4609923
73 A = 6723156
37 meter
Y = 611290
43 meter E =
0013306
Z = 4853676
00 I = 51
87818
XDOT = -3398
535326 Wp = 31
71910
YDOT = -6481
728877 meter/sec RA = 47
43507 deg
ZDOT = -2397
487980 TA = 81
66677
MA = 81
51593
Ha = 192
570 n
mi
Hp = 183
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15124421
70 X = -4639994
79
Y = 2005546
03 feet Y = 559571
73 meter
Z = 15924133
87 Z = 4831208
07
XDOT = -11150
050283 XDOT = -3314
156411
YDOT = -21265
514688 feet/sec YDOT = -6519
261700 meter/sec
ZDOT = -7865
774213 ZDOT = -2413
792533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15061160
63 X = -4590641
76
Y = -2960712
51 feet Y = -902425
17 meter
Z = 15834898
41 Z = 4826477
04
XDOT = -3944
075077 XDOT = -1202
154084
YDOT = -22600
264640 feet/sec YDOT = -6888
560662 meter/sec
ZDOT = -7930
697064 ZDOT = -2417
276465
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
54349903
00016717 00000-0 10270-3 0 9082
2 25544 51
6434 47
8224 0007767 7
9823 352
1462 15
73608816 6990
Satellite: ISS
Catalog Number: 25544
Epoch time: 10063
54349903 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 47
8224 deg
Eccentricity:
0007767
Arg of perigee: 7
9823 deg
Mean anomaly: 352
1462 deg
Mean motion: 15
73608816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 699
Checksum: 326
Coasting Arc #10 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2010/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3557165
22 A = 6731356
67 meter
Y = 5345934
22 meter E =
0019349
Z = 1980561
98 I = 51
88578
XDOT = -5109
659827 Wp = 49
05158
YDOT = 1308
883689 meter/sec RA = 42
35748 deg
ZDOT = 5621
230116 TA = 332
94872
MA = 333
04942
Ha = 192
397 n
mi
Hp = 183
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11670489
57 X = 3487500
51
Y = 17539154
26 feet Y = 5385323
13 meter
Z = 6497906
75 Z = 1997673
08
XDOT = -16763
975809 XDOT = -5151
222957
YDOT = 4294
237826 feet/sec YDOT = 1251
512325 meter/sec
ZDOT = 18442
356024 ZDOT = 5596
306552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5768405
82 X = 1758210
09
Y = 20240015
36 feet Y = 6169156
68 meter
Z = 6565997
54 Z = 2001316
05
XDOT = -15904
195860 XDOT = -4847
598898
YDOT = -1442
218954 feet/sec YDOT = -439
588337 meter/sec
ZDOT = 18343
380936 ZDOT = 5591
062509
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
55957479
00016717 00000-0 10270-3 0 9098
2 25544 51
6438 42
6083 0007585 12
1418 347
9927 15
73678707 7159
Satellite: ISS
Catalog Number: 25544
Epoch time: 10064
55957479 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 42
6083 deg
Eccentricity:
0007585
Arg of perigee: 12
1418 deg
Mean anomaly: 347
9927 deg
Mean motion: 15
73678707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 341
Coasting Arc #11 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2010/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262888
93 A = 6722692
68 meter
Y = -1641618
28 meter E =
0014736
Z = -4943017
37 I = 51
83322
XDOT = 4691
945386 Wp = 73
62112
YDOT = 5697
128878 meter/sec RA = 37
20467 deg
ZDOT = 2163
659339 TA = 217
29374
MA = 217
39615
Ha = 192
668 n
mi
Hp = 183
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13985856
08 X = 4304941
03
Y = -5385886
74 feet Y = -1593713
16 meter
Z = -16217248
59 Z = -4922206
26
XDOT = 15393
521607 XDOT = 4617
379793
YDOT = 18691
367709 feet/sec YDOT = 5749
180150 meter/sec
ZDOT = 7098
619877 ZDOT = 2186
271287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15034065
42 X = 4582383
14
Y = -1123477
02 feet Y = -342435
80 meter
Z = -16134614
17 Z = -4917830
40
XDOT = 9266
780439 XDOT = 2824
514678
YDOT = 21211
643592 feet/sec YDOT = 6465
308967 meter/sec
ZDOT = 7188
562619 ZDOT = 2191
073886
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
51213044
00016717 00000-0 10270-3 0 9100
2 25544 51
6440 37
7193 0007831 15
6075 344
5329 15
73644847 7304
Satellite: ISS
Catalog Number: 25544
Epoch time: 10065
51213044 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 37
7193 deg
Eccentricity:
0007831
Arg of perigee: 15
6075 deg
Mean anomaly: 344
5329 deg
Mean motion: 15
73644847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 288
Coasting Arc #12 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2010/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4590315
25 A = 6731513
94 meter
Y = -4576436
86 meter E =
0007309
Z = -1826588
25 I = 51
83962
XDOT = 4615
863638 Wp = 75
23840
YDOT = -2370
393849 meter/sec RA = 32
11971 deg
ZDOT = -5677
995956 TA = 124
94086
MA = 124
87218
Ha = 192
633 n
mi
Hp = 182
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15060089
39 X = -4529926
43
Y = -15014556
62 feet Y = -4627430
88 meter
Z = -5992743
61 Z = -1848740
92
XDOT = 15143
909572 XDOT = 4669
609071
YDOT = -7776
882706 feet/sec YDOT = -2318
476152 meter/sec
ZDOT = -18628
595655 ZDOT = -5655
441773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10409600
86 X = -3172846
34
Y = -18515394
56 feet Y = -5643492
26 meter
Z = -6080834
90 Z = -1853438
48
XDOT = 15436
941148 XDOT = 4705
179662
YDOT = -2608
300456 feet/sec YDOT = -795
009979 meter/sec
ZDOT = -18539
048804 ZDOT = -5650
702075
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
52816774
00016717 00000-0 10270-3 0 9112
2 25544 51
6447 32
5041 0007903 19
1761 340
9698 15
73706129 7465
Satellite: ISS
Catalog Number: 25544
Epoch time: 10066
52816774 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 32
5041 deg
Eccentricity:
0007903
Arg of perigee: 19
1761 deg
Mean anomaly: 340
9698 deg
Mean motion: 15
73706129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 311
Coasting Arc #13 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2010/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3768007
94 A = 6722251
27 meter
Y = 2482093
52 meter E =
0013293
Z = 4979380
14 I = 51
78233
XDOT = -5763
146145 Wp = 36
65647
YDOT = -4702
494222 meter/sec RA = 26
96591 deg
ZDOT = -2003
835685 TA = 72
75094
MA = 72
60550
Ha = 192
761 n
mi
Hp = 182
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12362230
77 X = -3819671
64
Y = 8143351
43 feet Y = 2439668
67 meter
Z = 16336549
00 Z = 4960949
90
XDOT = -18907
959793 XDOT = -5700
399575
YDOT = -15428
130650 feet/sec YDOT = -4766
590358 meter/sec
ZDOT = -6574
264059 ZDOT = -2031
680065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14115844
27 X = -4302509
33
Y = 4718796
52 feet Y = 1438289
18 meter
Z = 16263383
88 Z = 4957079
41
XDOT = -13996
334153 XDOT = -4266
082650
YDOT = -18679
088067 feet/sec YDOT = -5693
386043 meter/sec
ZDOT = -6684
966228 ZDOT = -2037
577706
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
54418451
00016717 00000-0 10270-3 0 9126
2 25544 51
6447 27
2894 0007853 22
6650 337
4859 15
73728098 7629
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067
54418451 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 27
2894 deg
Eccentricity:
0007853
Arg of perigee: 22
6650 deg
Mean anomaly: 337
4859 deg
Mean motion: 15
73728098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 329
Coasting Arc #14 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2010/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5424342
93 A = 6731558
21 meter
Y = 3596481
97 meter E =
0020803
Z = 1672210
81 I = 51
78710
XDOT = -3957
742820 Wp = 50
71933
YDOT = 3283
067031 meter/sec RA = 21
87504 deg
ZDOT = 5742
849920 TA = 327
74529
MA = 327
87234
Ha = 192
617 n
mi
Hp = 182
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17796400
71 X = 5375600
15
Y = 11799481
53 feet Y = 3656867
71 meter
Z = 5486255
93 Z = 1698443
23
XDOT = -12984
720539 XDOT = -4022
057694
YDOT = 10771
217292 feet/sec YDOT = 3238
449785 meter/sec
ZDOT = 18841
371130 ZDOT = 5723
467259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14463187
42 X = 4408379
52
Y = 15671655
77 feet Y = 4776720
68 meter
Z = 5590533
23 Z = 1703994
53
XDOT = -14131
367788 XDOT = -4307
240902
YDOT = 6308
426513 feet/sec YDOT = 1922
808401 meter/sec
ZDOT = 18764
436499 ZDOT = 5719
400245
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
56017913
00016717 00000-0 10270-3 0 9138
2 25544 51
6450 22
0743 0007784 26
6021 333
5540 15
73776870 7780
Satellite: ISS
Catalog Number: 25544
Epoch time: 10068
56017913 = yrday
fracday
Element set: 913
Inclination: 51
6450 deg
RA of node: 22
0743 deg
Eccentricity:
0007784
Arg of perigee: 26
6021 deg
Mean anomaly: 333
5540 deg
Mean motion: 15
73776870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 302
Coasting Arc #15 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2010/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3121637
06 A = 6721887
08 meter
Y = -3205715
30 meter E =
0017024
Z = -5029413
77 I = 51
72652
XDOT = 6584
448094 Wp = 77
30218
YDOT = 3509
231286 meter/sec RA = 16
71861 deg
ZDOT = 1858
976291 TA = 210
58393
MA = 210
68329
Ha = 192
725 n
mi
Hp = 182
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10241591
42 X = 3181683
39
Y = -10517438
64 feet Y = -3170471
80 meter
Z = -16500701
35 Z = -5014103
19
XDOT = 21602
519994 XDOT = 6535
687500
YDOT = 11513
226005 feet/sec YDOT = 3582
589949 meter/sec
ZDOT = 6099
003579 ZDOT = 1890
844237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12400154
88 X = 3779567
21
Y = -7984004
23 feet Y = -2433524
49 meter
Z = -16439941
93 Z = -5010894
30
XDOT = 17920
603884 XDOT = 5462
200064
YDOT = 15074
136505 feet/sec YDOT = 4594
596807 meter/sec
ZDOT = 6225
666468 ZDOT = 1897
583139
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
51265564
00016717 00000-0 10270-3 0 9142
2 25544 51
6454 17
1849 0007858 29
4274 330
7331 15
73789114 7938
Satellite: ISS
Catalog Number: 25544
Epoch time: 10069
51265564 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 17
1849 deg
Eccentricity:
0007858
Arg of perigee: 29
4274 deg
Mean anomaly: 330
7331 deg
Mean motion: 15
73789114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 324
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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