Date:
July 7th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 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
197/08:03:06
197 1
6 4
6 4
6
N/A 4
1 0
1 196
1
000/00:10:50
394 -1
3 -0
2 185
4
197/09:31:46
700 1
0 2
2 2
2
N/A 1
8 0
1 196
2
000/00:05:03
400 -0
9 -0
0 186
5
Coasting Arc #1 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2010/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3903032
34 A = 6725687
09 meter
Y = -1846181
04 meter E =
0011261
Z = 5147141
60 I = 51
86021
XDOT = 4642
571916 Wp = 65
35999
YDOT = -5996
757578 meter/sec RA = 135
91175 deg
ZDOT = 1371
769598 TA = 11
57315
MA = 11
54729
Ha = 196
100 n
mi
Hp = 183
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12805224
21 X = -3907101
84
Y = -6057024
41 feet Y = -1889850
48 meter
Z = 16886947
51 Z = 5128170
52
XDOT = 15231
535159 XDOT = 4702
619884
YDOT = -19674
401501 feet/sec YDOT = -5944
505994 meter/sec
ZDOT = 4500
556424 ZDOT = 1394
468353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3095542
08 X = -943521
23
Y = 13915213
85 feet Y = 4241357
18 meter
Z = 16811149
59 Z = 5124038
40
XDOT = -21502
489708 XDOT = -6553
958863
YDOT = -10320
998356 feet/sec YDOT = -3145
840299 meter/sec
ZDOT = 4591
167592 ZDOT = 1399
387882
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 10186
55007222
00016717 00000-0 10270-3 0 9006
2 25544 51
6443 136
6121 0009858 42
0516 318
1402 15
72262737 26361
Satellite: ISS
Catalog Number: 25544
Epoch time: 10186
55007222 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 136
6121 deg
Eccentricity:
0009858
Arg of perigee: 42
0516 deg
Mean anomaly: 318
1402 deg
Mean motion: 15
72262737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 281
Coasting Arc #2 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2010/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3099982
62 A = 6735800
59 meter
Y = 5708116
67 meter E =
0017394
Z = -1761986
56 I = 51
91473
XDOT = -5058
392496 Wp = 42
72095
YDOT = -996
097197 meter/sec RA = 130
77936 deg
ZDOT = 5717
816315 TA = 297
85151
MA = 298
02764
Ha = 196
092 n
mi
Hp = 183
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10170546
65 X = -3155021
98
Y = 18727416
89 feet Y = 5673143
32 meter
Z = -5780795
81 Z = -1777179
20
XDOT = -16595
775907 XDOT = -5074
654196
YDOT = -3268
035424 feet/sec YDOT = -1052
754897 meter/sec
ZDOT = 18759
239878 ZDOT = 5693
202930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20584196
99 X = 6274063
24
Y = 5453638
38 feet Y = 1662268
98 meter
Z = -5841440
37 Z = -1780471
03
XDOT = 1145
949297 XDOT = 349
285346
YDOT = 15505
435073 feet/sec YDOT = 4726
056610 meter/sec
ZDOT = 18660
905331 ZDOT = 5687
843945
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 10187
50348155
00016717 00000-0 10270-3 0 9016
2 25544 51
6440 131
7289 0009979 45
6679 314
5299 15
72242662 26518
Satellite: ISS
Catalog Number: 25544
Epoch time: 10187
50348155 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 131
7289 deg
Eccentricity:
0009979
Arg of perigee: 45
6679 deg
Mean anomaly: 314
5299 deg
Mean motion: 15
72242662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 328
Coasting Arc #3 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2010/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4734499
44 A = 6727240
09 meter
Y = -143495
56 meter E =
0021084
Z = -4796918
36 I = 51
90592
XDOT = -2410
609256 Wp = 61
55909
YDOT = 6820
914227 meter/sec RA = 125
71213 deg
ZDOT = -2582
030295 TA = 183
14927
MA = 183
16256
Ha = 196
099 n
mi
Hp = 183
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15533134
66 X = 4759054
77
Y = -470785
97 feet Y = -90413
49 meter
Z = -15737921
14 Z = -4773858
49
XDOT = -7908
823017 XDOT = -2474
159731
YDOT = 22378
327516 feet/sec YDOT = 6793
602446 meter/sec
ZDOT = -8471
228002 ZDOT = -2593
894320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4387331
96 X = -1337258
78
Y = -15004750
97 feet Y = -4573448
10 meter
Z = -15645793
06 Z = -4768837
72
XDOT = 22541
194287 XDOT = 6870
556019
YDOT = 2295
870411 feet/sec YDOT = 699
781301 meter/sec
ZDOT = -8518
581835 ZDOT = -2596
463743
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 10188
52043654
00016717 00000-0 10270-3 0 9026
2 25544 51
6449 126
5199 0009979 49
5102 310
6928 15
72284120 26671
Satellite: ISS
Catalog Number: 25544
Epoch time: 10188
52043654 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 126
5199 deg
Eccentricity:
0009979
Arg of perigee: 49
5102 deg
Mean anomaly: 310
6928 deg
Mean motion: 15
72284120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 321
Coasting Arc #4 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2010/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1087914
52 A = 6733751
85 meter
Y = -6050662
54 meter E =
0021592
Z = 2734148
77 I = 51
94545
XDOT = 5523
883213 Wp = 80
95707
YDOT = -1367
872720 meter/sec RA = 120
56741 deg
ZDOT = -5187
147125 TA = 67
97383
MA = 67
74460
Ha = 196
107 n
mi
Hp = 183
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3569273
36 X = 1142211
28
Y = -19851255
04 feet Y = -6038193
74 meter
Z = 8970304
37 Z = 2739564
64
XDOT = 18122
976421 XDOT = 5563
966682
YDOT = -4487
771392 feet/sec YDOT = -1305
876298 meter/sec
ZDOT = -17018
199229 ZDOT = -5160
214985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20066733
90 X = -6116340
49
Y = 1936510
94 feet Y = 590248
53 meter
Z = 8991913
90 Z = 2740735
36
XDOT = -9070
035289 XDOT = -2764
546756
YDOT = -14888
657640 feet/sec YDOT = -4538
062849 meter/sec
ZDOT = -16910
594712 ZDOT = -5154
349268
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 10189
53737708
00016717 00000-0 10270-3 0 9039
2 25544 51
6454 121
3113 0009966 53
0671 307
1403 15
72304478 26839
Satellite: ISS
Catalog Number: 25544
Epoch time: 10189
53737708 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 121
3113 deg
Eccentricity:
0009966
Arg of perigee: 53
0671 deg
Mean anomaly: 307
1403 deg
Mean motion: 15
72304478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 302
Coasting Arc #5 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2010/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4726779
44 A = 6729326
21 meter
Y = 2251522
37 meter E =
0018310
Z = 4210389
52 I = 51
94538
XDOT = 50
956325 Wp = 81
97995
YDOT = -6778
257915 meter/sec RA = 115
51451 deg
ZDOT = 3670
920611 TA = 330
75669
MA = 330
85907
Ha = 196
228 n
mi
Hp = 183
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15507806
55 X = -4772058
28
Y = 7386884
42 feet Y = 2198410
71 meter
Z = 13813613
91 Z = 4187317
39
XDOT = 167
179543 XDOT = 108
915666
YDOT = -22238
378987 feet/sec YDOT = -6777
364744 meter/sec
ZDOT = 12043
702793 ZDOT = 3671
307609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11520197
26 X = 3511356
12
Y = 12840625
68 feet Y = 3913822
71 meter
Z = 13721422
73 Z = 4182289
65
XDOT = -20408
507044 XDOT = -6220
512947
YDOT = 5399
623171 feet/sec YDOT = 1645
805143 meter/sec
ZDOT = 12045
224991 ZDOT = 3671
384577
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 10190
55430303
00016717 00000-0 10270-3 0 9045
2 25544 51
6458 116
1030 0009906 57
1838 303
0277 15
72327356 26998
Satellite: ISS
Catalog Number: 25544
Epoch time: 10190
55430303 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 116
1030 deg
Eccentricity:
0009906
Arg of perigee: 57
1838 deg
Mean anomaly: 303
0277 deg
Mean motion: 15
72327356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 297
Coasting Arc #6 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2010/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 953610
04 A = 6731182
29 meter
Y = 5592775
34 meter E =
0014650
Z = -3630622
81 I = 51
96459
XDOT = -5071
693238 Wp = 74
29127
YDOT = 3723
220144 meter/sec RA = 110
36362 deg
ZDOT = 4421
854518 TA = 242
52465
MA = 242
67367
Ha = 196
123 n
mi
Hp = 183
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3128641
86 X = 908636
46
Y = 18349000
46 feet Y = 5603188
44 meter
Z = -11911492
14 Z = -3626098
35
XDOT = -16639
413512 XDOT = -5134
430365
YDOT = 12215
289185 feet/sec YDOT = 3666
153786 meter/sec
ZDOT = 14507
396711 ZDOT = 4397
064835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16533226
01 X = 5039327
29
Y = -8576563
35 feet Y = -2614136
51 meter
Z = -11893395
72 Z = -3625107
02
XDOT = 16060
239891 XDOT = 4895
161119
YDOT = 11063
727404 feet/sec YDOT = 3372
224113 meter/sec
ZDOT = 14408
330618 ZDOT = 4391
659172
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 10191
50765859
00016717 00000-0 10270-3 0 9059
2 25544 51
6464 111
2199 0009926 60
3455 299
8694 15
72347137 27142
Satellite: ISS
Catalog Number: 25544
Epoch time: 10191
50765859 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 111
2199 deg
Eccentricity:
0009926
Arg of perigee: 60
3455 deg
Mean anomaly: 299
8694 deg
Mean motion: 15
72347137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 335
Coasting Arc #7 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2010/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3981773
36 A = 6731547
96 meter
Y = -4156138
80 meter E =
0014795
Z = -3507398
18 I = 51
97641
XDOT = 2090
332406 Wp = 71
37064
YDOT = 5831
592302 meter/sec RA = 105
31529 deg
ZDOT = -4548
122429 TA = 149
97308
MA = 149
88816
Ha = 196
112 n
mi
Hp = 182
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13063560
88 X = 4044990
15
Y = -13635625
99 feet Y = -4111258
12 meter
Z = -11507211
86 Z = -3487902
26
XDOT = 6858
045950 XDOT = 2047
060713
YDOT = 19132
520677 feet/sec YDOT = 5854
726550 meter/sec
ZDOT = -14921
661513 ZDOT = -4538
071776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17099921
30 X = -5212056
01
Y = -8121996
28 feet Y = -2475584
46 meter
Z = -11429291
85 Z = -3483648
16
XDOT = 15344
036573 XDOT = 4676
862347
YDOT = -11414
729808 feet/sec YDOT = -3479
209645 meter/sec
ZDOT = -14881
477513 ZDOT = -4535
874346
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 10192
52455679
00016717 00000-0 10270-3 0 9069
2 25544 51
6474 106
0110 0009942 63
9057 296
3127 15
72374879 27307
Satellite: ISS
Catalog Number: 25544
Epoch time: 10192
52455679 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 106
0110 deg
Eccentricity:
0009942
Arg of perigee: 63
9057 deg
Mean anomaly: 296
3127 deg
Mean motion: 15
72374879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 320
Coasting Arc #8 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2010/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2615768
66 A = 6728789
50 meter
Y = -4456439
48 meter E =
0019719
Z = 4298184
67 I = 51
97364
XDOT = 3827
292341 Wp = 69
75934
YDOT = -5676
000074 meter/sec RA = 100
16642 deg
ZDOT = -3536
121456 TA = 55
96778
MA = 55
78068
Ha = 196
171 n
mi
Hp = 182
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8581918
18 X = -2586620
91
Y = -14620864
45 feet Y = -4485528
30 meter
Z = 14101655
73 Z = 4285547
60
XDOT = 12556
733402 XDOT = 3907
655435
YDOT = -18622
047486 feet/sec YDOT = -5632
751098 meter/sec
ZDOT = -11601
448345 ZDOT = -3517
334576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10889488
77 X = -3319116
18
Y = 13048387
02 feet Y = 3977148
36 meter
Z = 14051132
40 Z = 4282785
16
XDOT = -20817
045415 XDOT = -6345
035442
YDOT = -4890
925961 feet/sec YDOT = -1490
754233 meter/sec
ZDOT = -11526
355321 ZDOT = -3513
233102
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
54144099
00016717 00000-0 10270-3 0 9074
2 25544 51
6469 100
8025 0009923 67
5483 292
6729 15
72388785 27465
Satellite: ISS
Catalog Number: 25544
Epoch time: 10193
54144099 = yrday
fracday
Element set: 907
Inclination: 51
6469 deg
RA of node: 100
8025 deg
Eccentricity:
0009923
Arg of perigee: 67
5483 deg
Mean anomaly: 292
6729 deg
Mean motion: 15
72388785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 343
Coasting Arc #9 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2010/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2568616
72 A = 6733776
61 meter
Y = 5627269
55 meter E =
0023610
Z = 2632113
45 I = 51
99510
XDOT = -3755
292430 Wp = 74
70186
YDOT = -4192
008022 meter/sec RA = 95
11395 deg
ZDOT = 5264
759764 TA = 315
09340
MA = 315
28416
Ha = 196
162 n
mi
Hp = 182
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8427220
22 X = -2644137
02
Y = 18462170
44 feet Y = 5598123
14 meter
Z = 8635542
82 Z = 2619452
70
XDOT = -12320
513222 XDOT = -3733
712217
YDOT = -13753
307160 feet/sec YDOT = -4233
881983 meter/sec
ZDOT = 17272
833873 ZDOT = 5246
568813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20261985
94 X = 6175853
31
Y = 1480948
87 feet Y = 451393
21 meter
Z = 8584934
13 Z = 2616687
92
XDOT = -8427
747454 XDOT = -2568
777424
YDOT = 14972
300955 feet/sec YDOT = 4563
557331 meter/sec
ZDOT = 17200
104252 ZDOT = 5242
591776
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
55831083
00016717 00000-0 10270-3 0 9083
2 25544 51
6474 95
5934 0009918 71
1098 289
1139 15
72396543 27622
Satellite: ISS
Catalog Number: 25544
Epoch time: 10194
55831083 = yrday
fracday
Element set: 908
Inclination: 51
6474 deg
RA of node: 95
5934 deg
Eccentricity:
0009918
Arg of perigee: 71
1098 deg
Mean anomaly: 289
1139 deg
Mean motion: 15
72396543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 339
Coasting Arc #10 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2010/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3783894
89 A = 6726619
62 meter
Y = 2776457
37 meter E =
0020685
Z = -4836830
32 I = 51
97317
XDOT = -1951
102188 Wp = 92
68716
YDOT = 6998
404938 meter/sec RA = 89
97318 deg
ZDOT = 2499
077472 TA = 201
65769
MA = 201
74530
Ha = 196
043 n
mi
Hp = 182
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12414353
31 X = 3776062
78
Y = 9109112
10 feet Y = 2818727
86 meter
Z = -15868865
89 Z = -4818467
26
XDOT = -6401
253899 XDOT = -2041
354435
YDOT = 22960
646122 feet/sec YDOT = 6976
081657 meter/sec
ZDOT = 8199
073070 ZDOT = 2489
380732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3898336
16 X = 1188212
86
Y = -14973971
35 feet Y = -4564066
47 meter
Z = -15795447
23 Z = -4814452
31
XDOT = 22636
364713 XDOT = 6899
563965
YDOT = -2686
347913 feet/sec YDOT = -818
798844 meter/sec
ZDOT = 8160
311838 ZDOT = 2487
263048
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
51161201
00016717 00000-0 10270-3 0 9099
2 25544 51
6477 90
7097 0009781 74
3570 285
8671 15
72431976 27770
Satellite: ISS
Catalog Number: 25544
Epoch time: 10195
51161201 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 90
7097 deg
Eccentricity:
0009781
Arg of perigee: 74
3570 deg
Mean anomaly: 285
8671 deg
Mean motion: 15
72431976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 333
Coasting Arc #11 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2010/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828323
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 793415
67 A = 6735349
82 meter
Y = -6457333
26 meter E =
0014700
Z = -1745040
35 I = 52
00131
XDOT = 4680
571998 Wp = 106
14798
YDOT = 2111
187569 meter/sec RA = 84
90886 deg
ZDOT = -5727
699123 TA = 93
04525
MA = 92
87703
Ha = 196
024 n
mi
Hp = 182
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2603069
79 X = 874040
73
Y = -21185476
58 feet Y = -6448009
86 meter
Z = -5725197
99 Z = -1740990
73
XDOT = 15356
207344 XDOT = 4684
440111
YDOT = 6926
468401 feet/sec YDOT = 2163
550650 meter/sec
ZDOT = -18791
663790 ZDOT = -5704
951696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20586444
35 X = -6274748
24
Y = 5655422
38 feet Y = 1723772
74 meter
Z = -5709009
49 Z = -1740106
09
XDOT = 905
064035 XDOT = 275
863518
YDOT = -15438
594509 feet/sec YDOT = -4705
683606 meter/sec
ZDOT = -18700
715850 ZDOT = -5699
978191
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
52845386
00016717 00000-0 10270-3 0 9106
2 25544 51
6476 85
5000 0009644 78
8337 281
3910 15
72421954 27933
Satellite: ISS
Catalog Number: 25544
Epoch time: 10196
52845386 = yrday
fracday
Element set: 910
Inclination: 51
6476 deg
RA of node: 85
5000 deg
Eccentricity:
0009644
Arg of perigee: 78
8337 deg
Mean anomaly: 281
3910 deg
Mean motion: 15
72421954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2793
Checksum: 323
Coasting Arc #12 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2010/197/08:08:31
394
Vector Time (MET): N/A
Weight (LBS) : 827859
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4150945
74 A = 6727084
60 meter
Y = -324113
31 meter E =
0021047
Z = -5301775
82 I = 51
95976
XDOT = 1003
545531 Wp = 90
89162
YDOT = 7608
811969 meter/sec RA = 80
60918 deg
ZDOT = 321
333939 TA = 182
14857
MA = 182
15763
Ha = 196
060 n
mi
Hp = 185
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13618588
38 X = 4180016
27
Y = -1063363
87 feet Y = -277531
97 meter
Z = -17394277
61 Z = -5281540
19
XDOT = 3292
472216 XDOT = 916
826862
YDOT = 24963
293861 feet/sec YDOT = 7619
549318 meter/sec
ZDOT = 1054
245208 ZDOT = 325
999091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6912866
93 X = 2107041
84
Y = -11900294
14 feet Y = -3627209
65 meter
Z = -17313372
17 Z = -5277115
84
XDOT = 21549
275183 XDOT = 6568
219076
YDOT = 10960
732035 feet/sec YDOT = 3340
831124 meter/sec
ZDOT = 1072
893896 ZDOT = 327
018060
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
35463099
00016717 00000-0 10270-3 0 9116
2 25544 51
6453 81
2664 0006088 87
1344 273
0515 15
71567723 28065
Satellite: ISS
Catalog Number: 25544
Epoch time: 10197
35463099 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 81
2664 deg
Eccentricity:
0006088
Arg of perigee: 87
1344 deg
Mean anomaly: 273
0515 deg
Mean motion: 15
71567723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 315
Coasting Arc #13 (Orbit 2806)
---------------------------------------
Vector Time (GMT): 2010/197/09:34:18
400
Vector Time (MET): N/A
Weight (LBS) : 827643
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3475457
28 A = 6729535
47 meter
Y = -2890673
88 meter E =
0017327
Z = -5000628
41 I = 51
96521
XDOT = 2785
631687 Wp = 80
84932
YDOT = 6864
890395 meter/sec RA = 80
32546 deg
ZDOT = -2035
579686 TA = 169
51252
MA = 169
47634
Ha = 196
166 n
mi
Hp = 186
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11402418
90 X = 3531814
87
Y = -9483838
19 feet Y = -2851493
72 meter
Z = -16406261
20 Z = -4983608
19
XDOT = 9139
211572 XDOT = 2718
548555
YDOT = 22522
606284 feet/sec YDOT = 6895
666078 meter/sec
ZDOT = -6678
411044 ZDOT = -2022
209631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6635544
75 X = -2022514
04
Y = -13347516
09 feet Y = -4068322
90 meter
Z = -16338210
12 Z = -4979886
45
XDOT = 23042
040758 XDOT = 7023
214023
YDOT = -3358
875443 feet/sec YDOT = -1023
785235 meter/sec
ZDOT = -6624
958839 ZDOT = -2019
287454
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
41822116
00016717 00000-0 10270-3 0 9123
2 25544 51
6466 80
9417 0004688 97
4627 262
7068 15
71168605 28078
Satellite: ISS
Catalog Number: 25544
Epoch time: 10197
41822116 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 80
9417 deg
Eccentricity:
0004688
Arg of perigee: 97
4627 deg
Mean anomaly: 262
7068 deg
Mean motion: 15
71168605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2807
Checksum: 325
Coasting Arc #14 (Orbit 2822)
---------------------------------------
Vector Time (GMT): 2010/198/09:34:18
400
Vector Time (MET): N/A
Weight (LBS) : 827643
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3473310
08 A = 6737332
15 meter
Y = -5134628
29 meter E =
0018375
Z = 2617542
15 I = 51
98506
XDOT = 3010
687936 Wp = 102
46286
YDOT = -4738
002331 meter/sec RA = 75
19696 deg
ZDOT = -5272
200199 TA = 47
95049
MA = 47
79427
Ha = 196
186 n
mi
Hp = 186
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11395374
28 X = -3428351
03
Y = -16845893
33 feet Y = -5173217
77 meter
Z = 8587736
73 Z = 2600777
70
XDOT = 9877
585092 XDOT = 3089
056572
YDOT = -15544
627069 feet/sec YDOT = -4703
896375 meter/sec
ZDOT = -17297
244746 ZDOT = -5257
384450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18870093
27 X = -5751604
43
Y = 7661907
65 feet Y = 2335349
45 meter
Z = 8520718
89 Z = 2597115
12
XDOT = -12550
117106 XDOT = -3825
275694
YDOT = -11639
603170 feet/sec YDOT = -3547
751046 meter/sec
ZDOT = -17237
999660 ZDOT = -5254
142296
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
43588834
00016717 00000-0 10270-3 0 9133
2 25544 51
6465 75
7380 0004638 101
5843 258
5839 15
71166536 28238
Satellite: ISS
Catalog Number: 25544
Epoch time: 10198
43588834 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 75
7380 deg
Eccentricity:
0004638
Arg of perigee: 101
5843 deg
Mean anomaly: 258
5839 deg
Mean motion: 15
71166536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2823
Checksum: 335
Coasting Arc #15 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2010/199/09:34:18
400
Vector Time (MET): N/A
Weight (LBS) : 827643
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1533054
72 A = 6733032
90 meter
Y = 5131715
72 meter E =
0015266
Z = 4070122
41 I = 51
96250
XDOT = -4863
895789 Wp = 103
36185
YDOT = -4540
662049 meter/sec RA = 70
15356 deg
ZDOT = 3877
408285 TA = 306
83238
MA = 306
97231
Ha = 196
127 n
mi
Hp = 186
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5029707
08 X = -1610096
38
Y = 16836337
67 feet Y = 5114141
01 meter
Z = 13353419
99 Z = 4062488
26
XDOT = -15957
663349 XDOT = -4831
595437
YDOT = -14897
185200 feet/sec YDOT = -4594
872832 meter/sec
ZDOT = 12721
155792 ZDOT = 3853
857585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15536808
09 X = 4735619
10
Y = 8257271
98 feet Y = 2516816
50 meter
Z = 13322878
77 Z = 4060813
45
XDOT = -17104
893899 XDOT = -5213
571660
YDOT = 11728
642438 feet/sec YDOT = 3574
890215 meter/sec
ZDOT = 12627
010591 ZDOT = 3848
712828
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
45354246
00016717 00000-0 10270-3 0 9145
2 25544 51
6469 70
5341 0004604 104
6344 255
5329 15
71189203 28399
Satellite: ISS
Catalog Number: 25544
Epoch time: 10199
45354246 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 70
5341 deg
Eccentricity:
0004604
Arg of perigee: 104
6344 deg
Mean anomaly: 255
5329 deg
Mean motion: 15
71189203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 308
Coasting Arc #16 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2010/200/09:34:18
400
Vector Time (MET): N/A
Weight (LBS) : 827643
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4713181
38 A = 6733121
46 meter
Y = 2617515
96 meter E =
0011679
Z = -4045659
20 I = 51
95243
XDOT = -307
230679 Wp = 107
89106
YDOT = 6603
698511 meter/sec RA = 65
01110 deg
ZDOT = 3920
346341 TA = 202
45269
MA = 202
50385
Ha = 195
996 n
mi
Hp = 186
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15463193
49 X = 4703214
54
Y = 8587650
77 feet Y = 2670166
33 meter
Z = -13273160
09 Z = -4022786
54
XDOT = -1007
974669 XDOT = -400
095864
YDOT = 21665
677530 feet/sec YDOT = 6599
743162 meter/sec
ZDOT = 12862
028678 ZDOT = 3918
629051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11185519
46 X = 3409346
33
Y = -13789896
35 feet Y = -4203160
41 meter
Z = -13181721
84 Z = -4017788
82
XDOT = 20132
570359 XDOT = 6136
407446
YDOT = 4060
186105 feet/sec YDOT = 1237
544725 meter/sec
ZDOT = 12855
127326 ZDOT = 3918
242809
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
40758135
00016717 00000-0 10270-3 0 9159
2 25544 51
6477 65
6556 0004499 107
6184 252
5469 15
71218220 28549
Satellite: ISS
Catalog Number: 25544
Epoch time: 10200
40758135 = yrday
fracday
Element set: 915
Inclination: 51
6477 deg
RA of node: 65
6556 deg
Eccentricity:
0004499
Arg of perigee: 107
6184 deg
Mean anomaly: 252
5469 deg
Mean motion: 15
71218220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2854
Checksum: 312
Coasting Arc #17 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2010/201/09:34:18
400
Vector Time (MET): N/A
Weight (LBS) : 827643
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1062632
80 A = 6736911
83 meter
Y = -6075866
35 meter E =
0009167
Z = -2710114
57 I = 51
95200
XDOT = 5493
561011 Wp = 117
85478
YDOT = 1355
344407 meter/sec RA = 59
96671 deg
ZDOT = -5210
103660 TA = 92
86303
MA = 92
75811
Ha = 195
915 n
mi
Hp = 186
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3486328
08 X = -981447
20
Y = -19933944
72 feet Y = -6087295
03 meter
Z = -8891452
00 Z = -2715080
46
XDOT = 18023
494130 XDOT = 5503
306620
YDOT = 4446
668002 feet/sec YDOT = 1416
831903 meter/sec
ZDOT = -17093
515945 ZDOT = -5183
392209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20226560
93 X = -6165055
77
Y = 223914
94 feet Y = 68249
27 meter
Z = -8911265
29 Z = -2716153
66
XDOT = 7284
681026 XDOT = 2220
370777
YDOT = -15713
128472 feet/sec YDOT = -4789
361558 meter/sec
ZDOT = -16986
721031 ZDOT = -5177
552570
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
42521106
00016717 00000-0 10270-3 0 9169
2 25544 51
6483 60
4517 0004366 112
7179 247
4445 15
71215513 28707
Satellite: ISS
Catalog Number: 25544
Epoch time: 10201
42521106 = yrday
fracday
Element set: 916
Inclination: 51
6483 deg
RA of node: 60
4517 deg
Eccentricity:
0004366
Arg of perigee: 112
7179 deg
Mean anomaly: 247
4445 deg
Mean motion: 15
71215513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 280
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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