Date:
July 14th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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
197/08:06:48
896 1
5 6
2 6
2
N/A 6
0 -0
0 196
2
000/00:18:37
791 -0
6 -0
3 186
7
Coasting Arc #1 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2010/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2651706
34 A = 6728770
05 meter
Y = -4402371
61 meter E =
0019593
Z = 4331766
28 I = 51
97336
XDOT = 3794
895870 Wp = 69
22895
YDOT = -5730
953929 meter/sec RA = 100
17331 deg
ZDOT = -3481
937271 TA = 55
87086
MA = 55
68516
Ha = 196
232 n
mi
Hp = 182
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8699823
94 X = -2623323
64
Y = -14443476
40 feet Y = -4431866
58 meter
Z = 14211831
63 Z = 4318952
78
XDOT = 12450
445768 XDOT = 3875
612665
YDOT = -18802
342287 feet/sec YDOT = -5688
065261 meter/sec
ZDOT = -11423
678711 ZDOT = -3463
306920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10682698
18 X = -3256086
41
Y = 13100930
70 feet Y = 3993163
68 meter
Z = 14160603
09 Z = 4316151
82
XDOT = -20947
334131 XDOT = -6384
747443
YDOT = -4744
645082 feet/sec YDOT = -1446
167821 meter/sec
ZDOT = -11349
211503 ZDOT = -3459
239666
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 10193
54155248
00016717 00000-0 10270-3 0 9005
2 25544 51
6470 100
8089 0009933 67
2682 292
9529 15
72351816 27462
Satellite: ISS
Catalog Number: 25544
Epoch time: 10193
54155248 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 100
8089 deg
Eccentricity:
0009933
Arg of perigee: 67
2682 deg
Mean anomaly: 292
9529 deg
Mean motion: 15
72351816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 321
Coasting Arc #2 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2010/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2525277
01 A = 6734026
11 meter
Y = 5675410
98 meter E =
0023689
Z = 2570564
97 I = 51
99572
XDOT = -3793
768031 Wp = 74
04988
YDOT = -4105
950301 meter/sec RA = 95
12060 deg
ZDOT = 5304
659703 TA = 314
97974
MA = 315
17151
Ha = 196
224 n
mi
Hp = 182
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8285029
56 X = -2601039
87
Y = 18620114
77 feet Y = 5646747
87 meter
Z = 8433612
12 Z = 2558114
18
XDOT = -12446
745510 XDOT = -3773
341094
YDOT = -13470
965555 feet/sec YDOT = -4148
260973 meter/sec
ZDOT = 17403
739183 ZDOT = 5286
279051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20359758
51 X = 6205654
39
Y = 1291361
33 feet Y = 393606
93 meter
Z = 8383842
88 Z = 2555395
31
XDOT = -8132
634312 XDOT = -2478
826938
YDOT = 14985
335263 feet/sec YDOT = 4567
530188 meter/sec
ZDOT = 17330
251271 ZDOT = 5282
260587
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 10194
55844721
00016717 00000-0 10270-3 0 9019
2 25544 51
6475 95
5999 0009931 70
8394 289
3843 15
72357526 27626
Satellite: ISS
Catalog Number: 25544
Epoch time: 10194
55844721 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 95
5999 deg
Eccentricity:
0009931
Arg of perigee: 70
8394 deg
Mean anomaly: 289
3843 deg
Mean motion: 15
72357526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 349
Coasting Arc #3 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2010/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3810136
81 A = 6726591
84 meter
Y = 2679839
37 meter E =
0020926
Z = -4870859
67 I = 51
97286
XDOT = -1883
705486 Wp = 92
44867
YDOT = 7047
123716 meter/sec RA = 89
98103 deg
ZDOT = 2411
664027 TA = 200
99239
MA = 201
07842
Ha = 196
107 n
mi
Hp = 182
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12500448
85 X = 3803548
45
Y = 8792123
92 feet Y = 2722410
27 meter
Z = -15980510
73 Z = -4852366
12
XDOT = -6180
136109 XDOT = -1974
082894
YDOT = 23120
484633 feet/sec YDOT = 7025
553414 meter/sec
ZDOT = 7912
283552 ZDOT = 2402
294394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3571587
50 X = 1088619
87
Y = -14938680
23 feet Y = -4553309
73 meter
Z = -15906570
45 Z = -4848322
67
XDOT = 22706
123164 XDOT = 6920
826340
YDOT = -2928
370694 feet/sec YDOT = -892
567388 meter/sec
ZDOT = 7874
830165 ZDOT = 2400
248234
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 10195
51177223
00016717 00000-0 10270-3 0 9023
2 25544 51
6478 90
7165 0009796 74
0998 286
1244 15
72392558 27776
Satellite: ISS
Catalog Number: 25544
Epoch time: 10195
51177223 = yrday
fracday
Element set: 902
Inclination: 51
6478 deg
RA of node: 90
7165 deg
Eccentricity:
0009796
Arg of perigee: 74
0998 deg
Mean anomaly: 286
1244 deg
Mean motion: 15
72392558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 343
Coasting Arc #4 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2010/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 719034
03 A = 6735601
60 meter
Y = -6490144
89 meter E =
0014906
Z = -1652988
22 I = 52
00192
XDOT = 4696
079169 Wp = 106
77454
YDOT = 1976
239413 meter/sec RA = 84
91573 deg
ZDOT = -5763
292738 TA = 91
36980
MA = 91
19904
Ha = 196
093 n
mi
Hp = 182
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2359035
54 X = 799584
36
Y = -21293126
29 feet Y = -6481653
70 meter
Z = -5423189
70 Z = -1649300
13
XDOT = 15407
083889 XDOT = 4701
628049
YDOT = 6483
725107 feet/sec YDOT = 2028
785305 meter/sec
ZDOT = -18908
440741 ZDOT = -5740
465908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20592026
77 X = -6276449
76
Y = 5923715
11 feet Y = 1805548
37 meter
Z = -5408446
65 Z = -1648494
54
XDOT = 495
756241 XDOT = 151
106502
YDOT = -15316
725996 feet/sec YDOT = -4668
538084 meter/sec
ZDOT = -18817
175382 ZDOT = -5735
475056
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 10196
52864013
00016717 00000-0 10270-3 0 9036
2 25544 51
6477 85
5069 0009663 78
5874 281
6374 15
72380903 27938
Satellite: ISS
Catalog Number: 25544
Epoch time: 10196
52864013 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 85
5069 deg
Eccentricity:
0009663
Arg of perigee: 78
5874 deg
Mean anomaly: 281
6374 deg
Mean motion: 15
72380903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2793
Checksum: 338
Coasting Arc #5 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2010/197/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4065483
86 A = 6731721
41 meter
Y = 2915211
67 meter E =
0013746
Z = -4517207
42 I = 51
97101
XDOT = -1385
362601 Wp = 99
88132
YDOT = 6856
115528 meter/sec RA = 80
57003 deg
ZDOT = 3183
683327 TA = 201
81940
MA = 201
87800
Ha = 196
202 n
mi
Hp = 186
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13338201
64 X = 4054526
78
Y = 9564342
73 feet Y = 2960613
44 meter
Z = -14820234
31 Z = -4497483
92
XDOT = -4545
152890 XDOT = -1477
391534
YDOT = 22493
817350 feet/sec YDOT = 6840
108753 meter/sec
ZDOT = 10445
155272 ZDOT = 3176
730347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15298936
94 X = 4663115
98
Y = -6136605
50 feet Y = -1870437
36 meter
Z = -14741377
86 Z = -4493171
97
XDOT = 15998
602123 XDOT = 4876
373927
YDOT = 14907
378823 feet/sec YDOT = 4543
769065 meter/sec
ZDOT = 10417
353056 ZDOT = 3175
209211
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 10197
35483866
00016717 00000-0 10270-3 0 9042
2 25544 51
6454 81
2737 0004500 76
5016 283
6647 15
71097445 28064
Satellite: ISS
Catalog Number: 25544
Epoch time: 10197
35483866 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 81
2737 deg
Eccentricity:
0004500
Arg of perigee: 76
5016 deg
Mean anomaly: 283
6647 deg
Mean motion: 15
71097445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 320
Coasting Arc #6 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2010/198/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -81057
85 A = 6738697
28 meter
Y = -6445718
61 meter E =
0009891
Z = -1961580
10 I = 51
98955
XDOT = 4972
081924 Wp = 116
98400
YDOT = 1643
993260 meter/sec RA = 75
52080 deg
ZDOT = -5633
613929 TA = 84
70002
MA = 84
58717
Ha = 196
161 n
mi
Hp = 186
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -265937
84 X = 554
30
Y = -21147370
77 feet Y = -6446168
56 meter
Z = -6435630
26 Z = -1961776
21
XDOT = 16312
604736 XDOT = 4980
695810
YDOT = 5393
678675 feet/sec YDOT = 1699
642703 meter/sec
ZDOT = -18482
985331 ZDOT = -5609
438682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18113560
52 X = -5521013
25
Y = -10916546
83 feet Y = -3327363
47 meter
Z = -6436402
81 Z = -1961815
58
XDOT = 12420
309869 XDOT = 3785
710448
YDOT = -9818
452804 feet/sec YDOT = -2992
664415 meter/sec
ZDOT = -18386
331038 ZDOT = -5604
153700
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 10198
37253986
00016717 00000-0 10270-3 0 9054
2 25544 51
6462 76
0698 0004509 79
8406 280
3265 15
71125268 28222
Satellite: ISS
Catalog Number: 25544
Epoch time: 10198
37253986 = yrday
fracday
Element set: 905
Inclination: 51
6462 deg
RA of node: 76
0698 deg
Eccentricity:
0004509
Arg of perigee: 79
8406 deg
Mean anomaly: 280
3265 deg
Mean motion: 15
71125268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 330
Coasting Arc #7 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2010/199/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4274188
53 A = 6728691
29 meter
Y = 106186
43 meter E =
0008228
Z = 5189609
56 I = 51
94752
XDOT = -1647
084382 Wp = 69
57551
YDOT = -7427
541696 meter/sec RA = 70
40328 deg
ZDOT = -1200
237713 TA = 31
86336
MA = 31
81361
Ha = 196
231 n
mi
Hp = 186
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14022928
23 X = -4300268
31
Y = 348380
66 feet Y = 58243
55 meter
Z = 17026278
09 Z = 5168782
32
XDOT = -5403
820152 XDOT = -1558
075334
YDOT = -24368
575119 feet/sec YDOT = -7445
462580 meter/sec
ZDOT = -3937
787772 ZDOT = -1208
023760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6912282
44 X = -2106863
69
Y = 12321239
47 feet Y = 3755513
79 meter
Z = 16943005
64 Z = 5164228
12
XDOT = -22800
865207 XDOT = -6949
703715
YDOT = -7314
124326 feet/sec YDOT = -2229
345095 meter/sec
ZDOT = -3968
892664 ZDOT = -1209
718484
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 10199
39022849
00016717 00000-0 10270-3 0 9060
2 25544 51
6463 70
8669 0004427 82
9761 277
1905 15
71156546 28386
Satellite: ISS
Catalog Number: 25544
Epoch time: 10199
39022849 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 70
8669 deg
Eccentricity:
0004427
Arg of perigee: 82
9761 deg
Mean anomaly: 277
1905 deg
Mean motion: 15
71156546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 340
Coasting Arc #8 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2010/200/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2734782
95 A = 6740298
87 meter
Y = 6152825
08 meter E =
0016161
Z = 107146
54 I = 51
97547
XDOT = -4376
604752 Wp = 56
39259
YDOT = 1828
556457 meter/sec RA = 65
32301 deg
ZDOT = 6062
008942 TA = 304
76476
MA = 304
91679
Ha = 196
125 n
mi
Hp = 186
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8972385
00 X = 2665257
19
Y = 20186434
00 feet Y = 6183018
31 meter
Z = 351530
64 Z = 120263
93
XDOT = -14358
939474 XDOT = -4426
174751
YDOT = 5999
200973 feet/sec YDOT = 1779
336760 meter/sec
ZDOT = 19888
480782 ZDOT = 6040
627290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21978059
52 X = 6698912
54
Y = 2218357
83 feet Y = 676155
47 meter
Z = 403946
00 Z = 123122
74
XDOT = -1805
067255 XDOT = -550
184499
YDOT = 13943
869560 feet/sec YDOT = 4250
091442 meter/sec
ZDOT = 19802
980672 ZDOT = 6035
948509
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 10200
40790639
00016717 00000-0 10270-3 0 9075
2 25544 51
6465 65
6630 0004444 86
1649 274
0021 15
71149158 28542
Satellite: ISS
Catalog Number: 25544
Epoch time: 10200
40790639 = yrday
fracday
Element set: 907
Inclination: 51
6465 deg
RA of node: 65
6630 deg
Eccentricity:
0004444
Arg of perigee: 86
1649 deg
Mean anomaly: 274
0021 deg
Mean motion: 15
71149158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2854
Checksum: 301
Coasting Arc #9 (Orbit 2868)
---------------------------------------
Vector Time (GMT): 2010/201/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3061581
10 A = 6728395
34 meter
Y = -2924823
63 meter E =
0019066
Z = -5245565
64 I = 51
92311
XDOT = 4391
870438 Wp = 84
44871
YDOT = 6236
250878 meter/sec RA = 60
23725 deg
ZDOT = -914
923828 TA = 176
85536
MA = 176
84336
Ha = 196
059 n
mi
Hp = 186
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10044557
42 X = 3119541
35
Y = -9595878
04 feet Y = -2890262
40 meter
Z = -17209861
03 Z = -5230552
17
XDOT = 14409
023748 XDOT = 4326
253643
YDOT = 20460
140676 feet/sec YDOT = 6284
996639 meter/sec
ZDOT = -3001
718597 ZDOT = -893
746742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3536382
21 X = -1077889
30
Y = -13510415
67 feet Y = -4117974
70 meter
Z = -17149810
35 Z = -5227262
19
XDOT = 23891
021108 XDOT = 7281
983234
YDOT = -2554
970600 feet/sec YDOT = -778
755039 meter/sec
ZDOT = -2917
086419 ZDOT = -889
127941
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 10201
36196710
00016717 00000-0 10270-3 0 9082
2 25544 51
6475 60
7845 0004468 89
7483 270
4191 15
71187614 28691
Satellite: ISS
Catalog Number: 25544
Epoch time: 10201
36196710 = yrday
fracday
Element set: 908
Inclination: 51
6475 deg
RA of node: 60
7845 deg
Eccentricity:
0004468
Arg of perigee: 89
7483 deg
Mean anomaly: 270
4191 deg
Mean motion: 15
71187614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2869
Checksum: 327
Coasting Arc #10 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2010/202/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4731171
57 A = 6739025
54 meter
Y = -4482310
21 meter E =
0018256
Z = 1683619
95 I = 51
94277
XDOT = 2285
841718 Wp = 110
62487
YDOT = -4587
363830 meter/sec RA = 55
12114 deg
ZDOT = -5745
943073 TA = 50
85396
MA = 50
69186
Ha = 196
082 n
mi
Hp = 186
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15522216
45 X = -4688876
59
Y = -14705742
17 feet Y = -4534980
77 meter
Z = 5523687
48 Z = 1660738
14
XDOT = 7499
480702 XDOT = 2364
881097
YDOT = -15050
406268 feet/sec YDOT = -4561
359379 meter/sec
ZDOT = -18851
519270 ZDOT = -5734
647251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20256833
90 X = -6174282
97
Y = 6918145
63 feet Y = 2108650
79 meter
Z = 5432229
87 Z = 1655743
66
XDOT = -9271
489708 XDOT = -2825
950063
YDOT = -12266
564667 feet/sec YDOT = -3738
848911 meter/sec
ZDOT = -18806
313118 ZDOT = -5732
164238
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 10202
37962111
00016717 00000-0 10270-3 0 9091
2 25544 51
6475 55
5810 0004430 93
8790 266
2878 15
71181865 28856
Satellite: ISS
Catalog Number: 25544
Epoch time: 10202
37962111 = yrday
fracday
Element set: 909
Inclination: 51
6475 deg
RA of node: 55
5810 deg
Eccentricity:
0004430
Arg of perigee: 93
8790 deg
Mean anomaly: 266
2878 deg
Mean motion: 15
71181865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 321
Coasting Arc #11 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2010/203/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -723233
20 A = 6730763
72 meter
Y = 4809744
21 meter E =
0012346
Z = 4644483
96 I = 51
89739
XDOT = -6085
106950 Wp = 109
11745
YDOT = -3725
464120 meter/sec RA = 50
06385 deg
ZDOT = 2900
273601 TA = 312
24015
MA = 312
34482
Ha = 196
020 n
mi
Hp = 186
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2372812
33 X = -799524
67
Y = 15780000
70 feet Y = 4801229
29 meter
Z = 15237808
25 Z = 4640785
98
XDOT = -19964
261647 XDOT = -6057
084707
YDOT = -12222
651312 feet/sec YDOT = -3793
355194 meter/sec
ZDOT = 9515
333337 ZDOT = 2870
779980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12980579
47 X = 3956480
62
Y = 9305646
28 feet Y = 2836360
99 meter
Z = 15222974
90 Z = 4639962
75
XDOT = -19250
126270 XDOT = -5867
438487
YDOT = 11424
437583 feet/sec YDOT = 3482
168575 meter/sec
ZDOT = 9397
430164 ZDOT = 2864
336714
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 10203
39726210
00016717 00000-0 10270-3 0 9104
2 25544 51
6477 50
3774 0004391 96
6936 263
4725 15
71215098 29014
Satellite: ISS
Catalog Number: 25544
Epoch time: 10203
39726210 = yrday
fracday
Element set: 910
Inclination: 51
6477 deg
RA of node: 50
3774 deg
Eccentricity:
0004391
Arg of perigee: 96
6936 deg
Mean anomaly: 263
4725 deg
Mean motion: 15
71215098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 302
Coasting Arc #12 (Orbit 2915)
---------------------------------------
Vector Time (GMT): 2010/204/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5563014
51 A = 6735413
32 meter
Y = 1893295
35 meter E =
0008892
Z = -3299304
65 I = 51
89329
XDOT = 759
842136 Wp = 91
05142
YDOT = 6006
591683 meter/sec RA = 44
92098 deg
ZDOT = 4738
823109 TA = 230
47333
MA = 230
55195
Ha = 195
931 n
mi
Hp = 186
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18251359
93 X = 5557457
04
Y = 6211598
91 feet Y = 1955473
73 meter
Z = -10824490
32 Z = -3272293
17
XDOT = 2492
920394 XDOT = 669
598891
YDOT = 19706
665628 feet/sec YDOT = 6014
583387 meter/sec
ZDOT = 15547
319912 ZDOT = 4742
296088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13558555
54 X = 4132647
73
Y = -13790868
83 feet Y = -4203456
82 meter
Z = -10716491
95 Z = -3266386
75
XDOT = 17784
284593 XDOT = 5420
649944
YDOT = 5420
328221 feet/sec YDOT = 1652
116042 meter/sec
ZDOT = 15561
146253 ZDOT = 4743
037378
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 10204
35128963
00016717 00000-0 10270-3 0 9113
2 25544 51
6482 45
4987 0004305 99
2511 260
9138 15
71242045 29162
Satellite: ISS
Catalog Number: 25544
Epoch time: 10204
35128963 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 45
4987 deg
Eccentricity:
0004305
Arg of perigee: 99
2511 deg
Mean anomaly: 260
9138 deg
Mean motion: 15
71242045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2916
Checksum: 299
Coasting Arc #13 (Orbit 2931)
---------------------------------------
Vector Time (GMT): 2010/205/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2060178
66 A = 6734548
79 meter
Y = -5347399
53 meter E =
0009304
Z = -3545422
53 I = 51
86854
XDOT = 6207
751997 Wp = 91
37965
YDOT = 584
230399 meter/sec RA = 39
87399 deg
ZDOT = -4498
705602 TA = 130
60067
MA = 130
51968
Ha = 195
818 n
mi
Hp = 186
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6759116
32 X = -1983007
27
Y = -17543961
72 feet Y = -5370005
69 meter
Z = -11631963
69 Z = -3555244
00
XDOT = 20366
640411 XDOT = 6222
611114
YDOT = 1916
766400 feet/sec YDOT = 653
732910 meter/sec
ZDOT = -14759
532816 ZDOT = -4468
512763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18732691
48 X = -5709724
36
Y = -1283965
85 feet Y = -391352
79 meter
Z = -11671183
64 Z = -3557376
77
XDOT = 10223
469992 XDOT = 3116
113654
YDOT = -16398
590723 feet/sec YDOT = -4998
290453 meter/sec
ZDOT = -14638
794650 ZDOT = -4461
904609
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 10205
36890708
00016717 00000-0 10270-3 0 9129
2 25544 51
6483 40
2946 0004129 103
0905 257
0718 15
71244540 29327
Satellite: ISS
Catalog Number: 25544
Epoch time: 10205
36890708 = yrday
fracday
Element set: 912
Inclination: 51
6483 deg
RA of node: 40
2946 deg
Eccentricity:
0004129
Arg of perigee: 103
0905 deg
Mean anomaly: 257
0718 deg
Mean motion: 15
71244540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2932
Checksum: 290
Coasting Arc #14 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2010/206/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4952979
46 A = 6731285
38 meter
Y = 842237
85 meter E =
0012668
Z = 4470479
01 I = 51
83371
XDOT = -3909
551824 Wp = 79
02888
YDOT = -5797
708569 meter/sec RA = 34
72540 deg
ZDOT = -3229
176345 TA = 43
24573
MA = 43
14634
Ha = 195
841 n
mi
Hp = 186
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16249932
62 X = -4983745
69
Y = 2763247
52 feet Y = 786678
09 meter
Z = 14666925
88 Z = 4446343
34
XDOT = -12826
613595 XDOT = -3828
743822
YDOT = -19021
353574 feet/sec YDOT = -5840
975286 meter/sec
ZDOT = -10594
410582 ZDOT = -3247
972974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4066226
37 X = -1239385
80
Y = 16061880
25 feet Y = 4895661
10 meter
Z = 14570393
53 Z = 4441055
95
XDOT = -21384
168756 XDOT = -6517
894637
YDOT = 4295
243932 feet/sec YDOT = 1309
190351 meter/sec
ZDOT = -10669
519690 ZDOT = -3252
069601
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 10206
38651178
00016717 00000-0 10270-3 0 9139
2 25544 51
6481 35
0904 0004093 104
6192 255
5424 15
71306768 29481
Satellite: ISS
Catalog Number: 25544
Epoch time: 10206
38651178 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 35
0904 deg
Eccentricity:
0004093
Arg of perigee: 104
6192 deg
Mean anomaly: 255
5424 deg
Mean motion: 15
71306768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 304
Coasting Arc #15 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2010/207/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4620138
51 A = 6738112
23 meter
Y = 4459088
81 meter E =
0017425
Z = 2020223
39 I = 51
83107
XDOT = -4737
848522 Wp = 77
08208
YDOT = 2359
301619 meter/sec RA = 29
66530 deg
ZDOT = 5591
268077 TA = 305
35963
MA = 305
52235
Ha = 195
710 n
mi
Hp = 186
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15157934
73 X = 4560119
14
Y = 14629556
46 feet Y = 4510418
16 meter
Z = 6628029
49 Z = 2042522
18
XDOT = -15544
122449 XDOT = -4791
039267
YDOT = 7740
490875 feet/sec YDOT = 2306
022169 meter/sec
ZDOT = 18344
055370 ZDOT = 5568
123199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19348602
95 X = 5897454
18
Y = -8260085
00 feet Y = -2517673
91 meter
Z = 6717160
29 Z = 2047390
46
XDOT = 461
320192 XDOT = 140
610395
YDOT = 16018
702882 feet/sec YDOT = 4882
500638 meter/sec
ZDOT = 18251
468688 ZDOT = 5563
047656
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 10207
40410577
00016717 00000-0 10270-3 0 9140
2 25544 51
6481 29
8857 0004058 108
0821 252
0783 15
71281997 29641
Satellite: ISS
Catalog Number: 25544
Epoch time: 10207
40410577 = yrday
fracday
Element set: 914
Inclination: 51
6481 deg
RA of node: 29
8857 deg
Eccentricity:
0004058
Arg of perigee: 108
0821 deg
Mean anomaly: 252
0783 deg
Mean motion: 15
71281997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 315
Coasting Arc #16 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2010/208/08:16:07
791
Vector Time (MET): N/A
Weight (LBS) : 828051
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3070629
34 A = 6728397
31 meter
Y = -3065191
00 meter E =
0017889
Z = -5158418
87 I = 51
77163
XDOT = 6363
937665 Wp = 102
79264
YDOT = 4083
601117 meter/sec RA = 24
53156 deg
ZDOT = 1361
788654 TA = 180
24692
MA = 180
24781
Ha = 195
602 n
mi
Hp = 186
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10074243
24 X = 3129734
74
Y = -10056400
92 feet Y = -3030522
47 meter
Z = -16923946
43 Z = -5143358
79
XDOT = 20879
060581 XDOT = 6311
185941
YDOT = 13397
641459 feet/sec YDOT = 4154
471403 meter/sec
ZDOT = 4467
810546 ZDOT = 1392
576174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5550735
51 X = -1691864
18
Y = -13185103
09 feet Y = -4018819
42 meter
Z = -16863686
75 Z = -5140051
72
XDOT = 19231
430355 XDOT = 5861
739972
YDOT = -13967
556397 feet/sec YDOT = -4257
311190 meter/sec
ZDOT = 4590
893683 ZDOT = 1399
304395
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 10208
35808716
00016717 00000-0 10270-3 0 9152
2 25544 51
6479 25
0062 0003941 112
1895 247
9685 15
71321941 29795
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208
35808716 = yrday
fracday
Element set: 915
Inclination: 51
6479 deg
RA of node: 25
0062 deg
Eccentricity:
0003941
Arg of perigee: 112
1895 deg
Mean anomaly: 247
9685 deg
Mean motion: 15
71321941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
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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