Date:
October 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 777)
---------------------------------------
Vector Time (GMT): 2008/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3706050
24 A = 6725046
60 meter
Y = 1944931
15 meter E =
0012073
Z = -5274107
33 I = 51
92921
XDOT = -2869
523795 Wp = 105
96750
YDOT = 7108
633472 meter/sec RA = 108
45020 deg
ZDOT = 602
960698 TA = 169
76110
MA = 169
73649
Ha = 191
832 n
mi
Hp = 187
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12158957
48 X = 3709647
72
Y = 6381007
71 feet Y = 1986394
55 meter
Z = -17303501
75 Z = -5256094
01
XDOT = -9414
448146 XDOT = -2951
729579
YDOT = 23322
288293 feet/sec YDOT = 7076
085153 meter/sec
ZDOT = 1978
217513 ZDOT = 588
820551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13811789
07 X = -4209833
31
Y = -456446
55 feet Y = -139124
91 meter
Z = -17233537
60 Z = -5252782
26
XDOT = -1613
058158 XDOT = -491
660127
YDOT = -24098
136181 feet/sec YDOT = -7345
111908 meter/sec
ZDOT = 1924
096738 ZDOT = 586
464686
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 08291
51491923
00020000 00000-0 20000-3 0 9003
2 25544 51
6376 109
2143 0003834 236
5429 123
5367 15
72307498 7784
Satellite: ISS
Catalog Number: 25544
Epoch time: 08291
51491923 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 109
2143 deg
Eccentricity:
0003834
Arg of perigee: 236
5429 deg
Mean anomaly: 123
5367 deg
Mean motion: 15
72307498 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 778
Checksum: 299
Coasting Arc #2 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2008/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1547387
01 A = 6736796
53 meter
Y = -6549595
81 meter E =
0011506
Z = 9270
34 I = 51
97822
XDOT = 4618
638790 Wp = 152
53239
YDOT = 1078
418945 meter/sec RA = 103
35449 deg
ZDOT = -6065
801544 TA = 27
36742
MA = 27
30686
Ha = 191
547 n
mi
Hp = 187
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5076729
05 X = 1620465
61
Y = -21488175
23 feet Y = -6531883
43 meter
Z = 30414
50 Z = 16965
02
XDOT = 15153
014404 XDOT = 4635
703804
YDOT = 3538
119897 feet/sec YDOT = 1130
162866 meter/sec
ZDOT = -19900
923700 ZDOT = -6043
322116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5079451
24 X = 1548216
74
Y = 21487470
70 feet Y = 6549381
07 meter
Z = 59632
16 Z = 18175
88
XDOT = -13668
726926 XDOT = -4166
227967
YDOT = 3299
871811 feet/sec YDOT = 1005
800928 meter/sec
ZDOT = -19813
731457 ZDOT = -6039
225348
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 08292
53183661
00020000 00000-0 20000-3 0 9014
2 25544 51
6383 104
0048 0003785 245
3072 114
7697 15
72379426 7942
Satellite: ISS
Catalog Number: 25544
Epoch time: 08292
53183661 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 104
0048 deg
Eccentricity:
0003785
Arg of perigee: 245
3072 deg
Mean anomaly: 114
7697 deg
Mean motion: 15
72379426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 794
Checksum: 298
Coasting Arc #3 (Orbit 809)
---------------------------------------
Vector Time (GMT): 2008/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4181190
00 A = 6725036
96 meter
Y = 99365
98 meter E =
0002908
Z = 5267158
22 I = 51
94333
XDOT = 613
091654 Wp = 194
19167
YDOT = -7647
787931 meter/sec RA = 98
25908 deg
ZDOT = 628
279643 TA = 249
84317
MA = 249
87445
Ha = 191
768 n
mi
Hp = 187
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13717814
97 X = -4207577
79
Y = 326003
88 feet Y = 52461
74 meter
Z = 17280702
83 Z = 5246781
50
XDOT = 2011
455557 XDOT = 695
512759
YDOT = -25091
167751 feet/sec YDOT = -7640
471172 meter/sec
ZDOT = 2061
284918 ZDOT = 631
457989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12095904
01 X = 3686831
54
Y = -6685515
06 feet Y = -2037744
99 meter
Z = 17201756
05 Z = 5243095
24
XDOT = 9356
091694 XDOT = 2851
736748
YDOT = 22284
047852 feet/sec YDOT = 6792
177785 meter/sec
ZDOT = 2072
916820 ZDOT = 631
825047
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 08293
54874113
00020000 00000-0 20000-3 0 9026
2 25544 51
6380 98
7946 0003692 245
3439 114
7339 15
72316058 8103
Satellite: ISS
Catalog Number: 25544
Epoch time: 08293
54874113 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 98
7946 deg
Eccentricity:
0003692
Arg of perigee: 245
3439 deg
Mean anomaly: 114
7339 deg
Mean motion: 15
72316058 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 810
Checksum: 301
Coasting Arc #4 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2008/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 475962
52 A = 6736268
98 meter
Y = 6629421
36 meter E =
0006629
Z = -1072983
53 I = 51
98594
XDOT = -4720
585562 Wp = 21
66965
YDOT = 1297
298276 meter/sec RA = 93
14304 deg
ZDOT = 5938
939060 TA = 326
65970
MA = 326
70143
Ha = 191
462 n
mi
Hp = 187
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1561556
83 X = 407008
32
Y = 21750070
08 feet Y = 6634358
34 meter
Z = -3520287
19 Z = -1070838
55
XDOT = -15487
485439 XDOT = -4763
592040
YDOT = 4256
227938 feet/sec YDOT = 1244
269307 meter/sec
ZDOT = 19484
708203 ZDOT = 5915
901689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11788584
76 X = -3593160
64
Y = -18346548
67 feet Y = -5592028
04 meter
Z = -3511388
78 Z = -1070271
30
XDOT = 10327
458279 XDOT = 3147
809283
YDOT = -10337
003073 feet/sec YDOT = -3150
718537 meter/sec
ZDOT = 19395
549263 ZDOT = 5911
763415
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 08294
50206900
00020000 00000-0 20000-3 0 9037
2 25544 51
6392 93
9104 0003767 247
7233 112
3530 15
72387165 8250
Satellite: ISS
Catalog Number: 25544
Epoch time: 08294
50206900 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 93
9104 deg
Eccentricity:
0003767
Arg of perigee: 247
7233 deg
Mean anomaly: 112
3530 deg
Mean motion: 15
72387165 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 825
Checksum: 279
Coasting Arc #5 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2008/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3894839
61 A = 6725629
03 meter
Y = -2120969
37 meter E =
0009766
Z = -5064959
63 I = 51
95133
XDOT = 1647
372798 Wp = 78
10333
YDOT = 7296
219888 meter/sec RA = 88
06848 deg
ZDOT = -1789
444954 TA = 174
71687
MA = 174
70656
Ha = 191
362 n
mi
Hp = 187
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12778345
19 X = 3942872
10
Y = -6958560
92 feet Y = -2077146
40 meter
Z = -16617321
61 Z = -5045921
63
XDOT = 5404
766399 XDOT = 1574
355748
YDOT = 23937
729292 feet/sec YDOT = 7314
233526 meter/sec
ZDOT = -5870
882396 ZDOT = -1781
619194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7767256
70 X = -2367459
84
Y = 12402333
49 feet Y = 3780231
25 meter
Z = -16543726
93 Z = -5042527
97
XDOT = -15631
923750 XDOT = -4764
610359
YDOT = -17575
799538 feet/sec YDOT = -5357
103699 meter/sec
ZDOT = -5839
913041 ZDOT = -1780
005495
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 08295
51893625
00020000 00000-0 20000-3 0 9046
2 25544 51
6397 88
7015 0003629 252
6465 107
4301 15
72430077 8417
Satellite: ISS
Catalog Number: 25544
Epoch time: 08295
51893625 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 88
7015 deg
Eccentricity:
0003629
Arg of perigee: 252
6465 deg
Mean anomaly: 107
4301 deg
Mean motion: 15
72430077 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 841
Checksum: 295
Coasting Arc #6 (Orbit 856)
---------------------------------------
Vector Time (GMT): 2008/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2346403
03 A = 6734855
94 meter
Y = -5967508
56 meter E =
0011150
Z = 2039335
92 I = 51
97939
XDOT = 3978
435804 Wp = 122
14570
YDOT = -3482
851142 meter/sec RA = 82
93383 deg
ZDOT = -5597
721919 TA = 35
22785
MA = 35
15420
Ha = 191
262 n
mi
Hp = 187
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7698172
66 X = -2289405
82
Y = -19578440
15 feet Y = -5993428
68 meter
Z = 6690734
65 Z = 2028075
50
XDOT = 13052
610906 XDOT = 4044
278926
YDOT = -11426
676976 feet/sec YDOT = -3437
993892 meter/sec
ZDOT = -18365
229392 ZDOT = -5578
234503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16610541
13 X = 5062892
94
Y = 12932753
91 feet Y = 3941903
39 meter
Z = 6646571
34 Z = 2025874
95
XDOT = -4584
494690 XDOT = -1397
353982
YDOT = 15315
775647 feet/sec YDOT = 4668
248417 meter/sec
ZDOT = -18290
007182 ZDOT = -5574
794189
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 08296
53578500
00020000 00000-0 20000-3 0 9052
2 25544 51
6389 83
4904 0003785 257
3454 102
7286 15
72435533 8579
Satellite: ISS
Catalog Number: 25544
Epoch time: 08296
53578500 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 83
4904 deg
Eccentricity:
0003785
Arg of perigee: 257
3454 deg
Mean anomaly: 102
7286 deg
Mean motion: 15
72435533 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 857
Checksum: 313
Coasting Arc #7 (Orbit 872)
---------------------------------------
Vector Time (GMT): 2008/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2909374
40 A = 6727049
95 meter
Y = 3866678
87 meter E =
0005396
Z = 4672053
63 I = 51
94987
XDOT = -3610
540010 Wp = 140
76109
YDOT = -6171
517736 meter/sec RA = 77
87232 deg
ZDOT = 2853
446207 TA = 281
12964
MA = 281
19030
Ha = 191
146 n
mi
Hp = 187
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9545191
60 X = -2975092
26
Y = 12685954
30 feet Y = 3833777
28 meter
Z = 15328259
93 Z = 4657759
96
XDOT = -11845
603706 XDOT = -3555
122444
YDOT = -20247
761601 feet/sec YDOT = -6211
582928 meter/sec
ZDOT = 9361
700155 ZDOT = 2836
040818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1579405
02 X = 481402
65
Y = -15850381
51 feet Y = -4831196
28 meter
Z = 15273197
36 Z = 4655270
56
XDOT = 19573
133095 XDOT = 5965
890967
YDOT = 10924
250005 feet/sec YDOT = 3329
711402 meter/sec
ZDOT = 9293
704151 ZDOT = 2832
721025
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 08297
55261482
00020000 00000-0 20000-3 0 9064
2 25544 51
6399 78
2801 0003828 261
6657 98
4072 15
72496955 8736
Satellite: ISS
Catalog Number: 25544
Epoch time: 08297
55261482 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 78
2801 deg
Eccentricity:
0003828
Arg of perigee: 261
6657 deg
Mean anomaly: 98
4072 deg
Mean motion: 15
72496955 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 873
Checksum: 332
Coasting Arc #8 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2008/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3848623
58 A = 6732824
14 meter
Y = 4690174
01 meter E =
0001779
Z = -2917315
34 I = 51
96278
XDOT = -2524
119268 Wp = 15
73342
YDOT = 5217
969472 meter/sec RA = 72
72584 deg
ZDOT = 5061
422485 TA = 310
88545
MA = 310
90086
Ha = 191
107 n
mi
Hp = 187
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12626717
77 X = 3810063
26
Y = 15387710
02 feet Y = 4732995
80 meter
Z = -9571244
57 Z = -2898712
34
XDOT = -8281
231193 XDOT = -2606
867710
YDOT = 17119
322414 feet/sec YDOT = 5189
280892 meter/sec
ZDOT = 16605
716813 ZDOT = 5048
958866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18963808
55 X = -5780168
85
Y = -6162164
94 feet Y = -1878227
87 meter
Z = -9498738
47 Z = -2895215
48
XDOT = -2585
006897 XDOT = -787
910102
YDOT = -17555
881645 feet/sec YDOT = -5351
032725 meter/sec
ZDOT = 16557
860980 ZDOT = 5046
836027
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 08298
50587756
00020000 00000-0 20000-3 0 9076
2 25544 51
6409 73
3960 0003685 266
5227 93
5514 15
72494391 8883
Satellite: ISS
Catalog Number: 25544
Epoch time: 08298
50587756 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 73
3960 deg
Eccentricity:
0003685
Arg of perigee: 266
5227 deg
Mean anomaly: 93
5514 deg
Mean motion: 15
72494391 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 888
Checksum: 331
Coasting Arc #9 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2008/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1412602
03 A = 6728955
96 meter
Y = -5110252
32 meter E =
0004537
Z = -4148471
03 I = 51
94038
XDOT = 5018
181337 Wp = 52
67068
YDOT = 4447
928716 meter/sec RA = 67
67228 deg
ZDOT = -3770
503315 TA = 178
83270
MA = 178
83164
Ha = 191
022 n
mi
Hp = 187
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4634521
10 X = 1489793
65
Y = -16765919
68 feet Y = -5094024
42 meter
Z = -13610469
27 Z = -4141420
69
XDOT = 16463
849531 XDOT = 4986
387712
YDOT = 14592
941981 feet/sec YDOT = 4503
866946 meter/sec
ZDOT = -12370
417700 ZDOT = -3746
201966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5321606
15 X = 1622025
55
Y = 16582719
23 feet Y = 5054412
82 meter
Z = -13583580
29 Z = -4140275
27
XDOT = -20632
580431 XDOT = -6288
810515
YDOT = -3434
081060 feet/sec YDOT = -1046
707907 meter/sec
ZDOT = -12275
852181 ZDOT = -3741
679745
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 08299
52267193
00020000 00000-0 20000-3 0 9080
2 25544 51
6411 68
1858 0003752 271
5048 88
5685 15
72520777 9046
Satellite: ISS
Catalog Number: 25544
Epoch time: 08299
52267193 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 68
1858 deg
Eccentricity:
0003752
Arg of perigee: 271
5048 deg
Mean anomaly: 88
5685 deg
Mean motion: 15
72520777 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 904
Checksum: 318
Coasting Arc #10 (Orbit 919)
---------------------------------------
Vector Time (GMT): 2008/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4785270
45 A = 6730660
34 meter
Y = -3008380
15 meter E =
0008402
Z = 3648161
53 I = 51
93430
XDOT = 602
123786 Wp = 81
32301
YDOT = -6295
208824 meter/sec RA = 62
51795 deg
ZDOT = -4391
626021 TA = 55
14312
MA = 55
06414
Ha = 191
126 n
mi
Hp = 187
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15699706
21 X = -4768997
17
Y = -9870013
60 feet Y = -3061800
63 meter
Z = 11969033
88 Z = 3624953
77
XDOT = 1975
471739 XDOT = 693
807352
YDOT = -20653
572256 feet/sec YDOT = -6287
963119 meter/sec
ZDOT = -14408
221853 ZDOT = -4388
477807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18585625
29 X = 5664898
59
Y = -789633
61 feet Y = -240680
32 meter
Z = 11878835
26 Z = 3620668
99
XDOT = 9937
381097 XDOT = 3028
913758
YDOT = 16835
632350 feet/sec YDOT = 5131
500740 meter/sec
ZDOT = -14396
549731 ZDOT = -4388
068358
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 08300
53944827
00020000 00000-0 20000-3 0 9091
2 25544 51
6416 62
9754 0003659 275
3666 84
7079 15
72534976 9201
Satellite: ISS
Catalog Number: 25544
Epoch time: 08300
53944827 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 62
9754 deg
Eccentricity:
0003659
Arg of perigee: 275
3666 deg
Mean anomaly: 84
7079 deg
Mean motion: 15
72534976 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 920
Checksum: 324
Coasting Arc #11 (Orbit 935)
---------------------------------------
Vector Time (GMT): 2008/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 401134
75 A = 6730784
76 meter
Y = 5729661
75 meter E =
0008592
Z = 3501493
94 I = 51
92226
XDOT = -5741
977709 Wp = 88
43966
YDOT = -2380
827587 meter/sec RA = 57
46486 deg
ZDOT = 4544
371993 TA = 312
95625
MA = 313
02827
Ha = 190
944 n
mi
Hp = 187
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1316058
89 X = 320024
80
Y = 18798102
87 feet Y = 5733694
10 meter
Z = 11487841
02 Z = 3503245
48
XDOT = -18838
509543 XDOT = -5737
004541
YDOT = -7811
114129 feet/sec YDOT = -2445
009725 meter/sec
ZDOT = 14909
356931 ZDOT = 4516
488808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11924419
53 X = -3634563
07
Y = -14585678
66 feet Y = -4445714
86 meter
Z = 11495102
03 Z = 3503707
10
XDOT = 18881
389821 XDOT = 5755
047617
YDOT = -3747
450603 feet/sec YDOT = -1142
222944 meter/sec
ZDOT = 14801
096164 ZDOT = 4511
374111
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 08301
55620302
00020000 00000-0 20000-3 0 9105
2 25544 51
6429 57
7650 0003739 280
5060 79
5681 15
72618770 9360
Satellite: ISS
Catalog Number: 25544
Epoch time: 08301
55620302 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 57
7650 deg
Eccentricity:
0003739
Arg of perigee: 280
5060 deg
Mean anomaly: 79
5681 deg
Mean motion: 15
72618770 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 936
Checksum: 287
Coasting Arc #12 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2008/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5091434
49 A = 6728381
07 meter
Y = 1132202
72 meter E =
0004511
Z = -4255145
97 I = 51
89738
XDOT = 1540
682844 Wp = 113
15407
YDOT = 6619
140430 meter/sec RA = 52
30978 deg
ZDOT = 3605
965679 TA = 193
39736
MA = 193
40934
Ha = 191
049 n
mi
Hp = 187
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16704181
39 X = 5099067
00
Y = 3714575
85 feet Y = 1189180
68 meter
Z = -13960452
65 Z = -4230392
46
XDOT = 5054
733741 XDOT = 1449
034335
YDOT = 21716
339995 feet/sec YDOT = 6635
856870 meter/sec
ZDOT = 11830
596060 ZDOT = 3613
227815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15707695
15 X = -4787705
48
Y = 6983405
85 feet Y = 2128542
10 meter
Z = -13864427
28 Z = -4225877
43
XDOT = -16403
762784 XDOT = -4999
866897
YDOT = -13360
463610 feet/sec YDOT = -4072
269308 meter/sec
ZDOT = 11859
275318 ZDOT = 3614
707117
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 08302
50939659
00020000 00000-0 20000-3 0 9110
2 25544 51
6432 52
8813 0003794 286
6802 73
3944 15
72612115 9511
Satellite: ISS
Catalog Number: 25544
Epoch time: 08302
50939659 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 52
8813 deg
Eccentricity:
0003794
Arg of perigee: 286
6802 deg
Mean anomaly: 73
3944 deg
Mean motion: 15
72612115 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 951
Checksum: 293
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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