Date:
October 12th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
293/19:22:34
464 1
5 2
2 2
2
N/A -1
5 -0
0 195
4
000/00:05:04
928 0
4 0
1 185
2
Coasting Arc #1 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2010/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4046076
84 A = 6731157
33 meter
Y = 3554831
10 meter E =
0017901
Z = 4024649
85 I = 51
61519
XDOT = -6136
699400 Wp = 79
62766
YDOT = -2557
671717 meter/sec RA = 354
99336 deg
ZDOT = -3892
490440 TA = 50
58509
MA = 50
42675
Ha = 195
943 n
mi
Hp = 184
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13274530
31 X = -4105078
32
Y = 11662831
69 feet Y = 3509255
60 meter
Z = 13204231
79 Z = 4004850
24
XDOT = -20133
528214 XDOT = -6088
733544
YDOT = -8391
311408 feet/sec YDOT = -2626
027843 meter/sec
ZDOT = -12770
637928 ZDOT = -3922
186579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8777013
38 X = 2675233
68
Y = -15404214
42 feet Y = -4695204
56 meter
Z = 13124814
26 Z = 4000443
38
XDOT = 20577
938635 XDOT = 6272
155696
YDOT = 692
564242 feet/sec YDOT = 211
093581 meter/sec
ZDOT = -12889
646798 ZDOT = -3928
764344
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 10284
54056141
00016717 00000-0 10270-3 0 9008
2 25544 51
6468 355
3215 0007052 83
2097 276
9867 15
71917245 1771
Satellite: ISS
Catalog Number: 25544
Epoch time: 10284
54056141 = yrday
fracday
Element set: 900
Inclination: 51
6468 deg
RA of node: 355
3215 deg
Eccentricity:
0007052
Arg of perigee: 83
2097 deg
Mean anomaly: 276
9867 deg
Mean motion: 15
71917245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 313
Coasting Arc #2 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5972924
81 A = 6734495
15 meter
Y = 1224113
95 meter E =
0020549
Z = 2839053
58 I = 51
59608
XDOT = -3390
746520 Wp = 83
01179
YDOT = 4693
564140 meter/sec RA = 349
92097 deg
ZDOT = 5081
012568 TA = 309
58078
MA = 309
76209
Ha = 195
823 n
mi
Hp = 184
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19596210
02 X = 5945000
79
Y = 4016121
88 feet Y = 1290750
67 meter
Z = 9314480
24 Z = 2868002
68
XDOT = -11124
496458 XDOT = -3467
661855
YDOT = 15398
832480 feet/sec YDOT = 4655
216759 meter/sec
ZDOT = 16669
988740 ZDOT = 5064
353187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19726829
31 X = -6012737
57
Y = 2969488
55 feet Y = 905100
11 meter
Z = 9430512
59 Z = 2874420
24
XDOT = 5439
947742 XDOT = 1658
096072
YDOT = -16886
852838 feet/sec YDOT = -5147
112745 meter/sec
ZDOT = 16603
141672 ZDOT = 5060
637582
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 10285
55774880
00016717 00000-0 10270-3 0 9018
2 25544 51
6463 350
1148 0007149 87
4763 272
7217 15
71929336 1932
Satellite: ISS
Catalog Number: 25544
Epoch time: 10285
55774880 = yrday
fracday
Element set: 901
Inclination: 51
6463 deg
RA of node: 350
1148 deg
Eccentricity:
0007149
Arg of perigee: 87
4763 deg
Mean anomaly: 272
7217 deg
Mean motion: 15
71929336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 324
Coasting Arc #3 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2010/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1803364
05 A = 6728218
40 meter
Y = -4413376
48 meter E =
0018396
Z = -4764465
89 I = 51
54468
XDOT = 7231
126726 Wp = 100
78493
YDOT = 162
299967 meter/sec RA = 344
75270 deg
ZDOT = 2591
746492 TA = 194
70390
MA = 194
75748
Ha = 195
872 n
mi
Hp = 184
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5916548
71 X = 1875726
41
Y = -14479581
63 feet Y = -4392805
63 meter
Z = -15631449
77 Z = -4755529
22
XDOT = 23724
169047 XDOT = 7216
184027
YDOT = 532
480207 feet/sec YDOT = 243
079247 meter/sec
ZDOT = 8503
105289 ZDOT = 2626
839442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -376840
10 X = -114860
86
Y = 15672983
48 feet Y = 4777125
36 meter
Z = -15595564
59 Z = -4753528
09
XDOT = -21126
392753 XDOT = -6439
324511
YDOT = 8076
486672 feet/sec YDOT = 2461
713138 meter/sec
ZDOT = 8643
782364 ZDOT = 2634
624865
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 10286
51134049
00016717 00000-0 10270-3 0 9023
2 25544 51
6456 345
2332 0007231 89
5596 270
6394 15
71960809 2083
Satellite: ISS
Catalog Number: 25544
Epoch time: 10286
51134049 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 345
2332 deg
Eccentricity:
0007231
Arg of perigee: 89
5596 deg
Mean anomaly: 270
6394 deg
Mean motion: 15
71960809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 310
Coasting Arc #4 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2010/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6448988
39 A = 6736566
93 meter
Y = 960728
00 meter E =
0013580
Z = -1688068
81 I = 51
54491
XDOT = 723
535054 Wp = 117
60285
YDOT = -5104
881833 meter/sec RA = 339
66172 deg
ZDOT = -5710
653254 TA = 81
06359
MA = 80
90989
Ha = 195
797 n
mi
Hp = 184
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21158098
38 X = -6451051
71
Y = 3151994
76 feet Y = 888599
97 meter
Z = -5538283
50 Z = -1719403
32
XDOT = 2373
802670 XDOT = 808
306595
YDOT = -16748
299977 feet/sec YDOT = -5096
316960 meter/sec
ZDOT = -18735
739023 ZDOT = -5706
932275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18378119
70 X = 5601650
89
Y = -10882905
39 feet Y = -3317109
56 meter
Z = -5663909
30 Z = -1726359
55
XDOT = 3218
752021 XDOT = 981
075616
YDOT = 15109
856322 feet/sec YDOT = 4605
484207 meter/sec
ZDOT = -18720
754775 ZDOT = -5706
086055
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 10287
52848191
00016717 00000-0 10270-3 0 9036
2 25544 51
6461 340
0254 0007320 92
9095 267
2905 15
72003031 2240
Satellite: ISS
Catalog Number: 25544
Epoch time: 10287
52848191 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 340
0254 deg
Eccentricity:
0007320
Arg of perigee: 92
9095 deg
Mean anomaly: 267
2905 deg
Mean motion: 15
72003031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 280
Coasting Arc #5 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 543819
01 A = 6726153
60 meter
Y = 4281856
76 meter E =
0010663
Z = 5149831
30 I = 51
48187
XDOT = -7228
672550 Wp = 81
12215
YDOT = 2379
014157 meter/sec RA = 334
50682 deg
ZDOT = -1210
953363 TA = 20
48591
MA = 20
44318
Ha = 195
687 n
mi
Hp = 184
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1784183
10 X = 470880
93
Y = 14048086
49 feet Y = 4287530
43 meter
Z = 16895771
97 Z = 5152295
87
XDOT = -23716
117290 XDOT = -7248
855233
YDOT = 7805
164556 feet/sec YDOT = 2298
065908 meter/sec
ZDOT = -3972
944103 ZDOT = -1246
119630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7067552
44 X = -2154189
98
Y = -12257634
67 feet Y = -3736127
05 meter
Z = 16905598
14 Z = 5152826
31
XDOT = 17827
170739 XDOT = 5433
721641
YDOT = -15969
718126 feet/sec YDOT = -4867
570085 meter/sec
ZDOT = -4113
946903 ZDOT = -1253
931016
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 10288
54559799
00016717 00000-0 10270-3 0 9043
2 25544 51
6458 334
8183 0007198 96
5193 263
6789 15
72056124 2409
Satellite: ISS
Catalog Number: 25544
Epoch time: 10288
54559799 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 334
8183 deg
Eccentricity:
0007198
Arg of perigee: 96
5193 deg
Mean anomaly: 263
6789 deg
Mean motion: 15
72056124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 346
Coasting Arc #6 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5946017
80 A = 6737714
03 meter
Y = -3127727
02 meter E =
0018811
Z = 422001
36 I = 51
49353
XDOT = 1890
676035 Wp = 66
40199
YDOT = 4431
837669 meter/sec RA = 329
39018 deg
ZDOT = 6004
111398 TA = 298
19286
MA = 298
38271
Ha = 195
820 n
mi
Hp = 184
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19507932
40 X = 5978500
67
Y = -10261571
59 feet Y = -3061053
43 meter
Z = 1384518
90 Z = 450966
40
XDOT = 6203
005365 XDOT = 1811
810767
YDOT = 14540
149833 feet/sec YDOT = 4452
539691 meter/sec
ZDOT = 19698
528210 ZDOT = 6013
104583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13604170
16 X = -4146551
06
Y = 17333514
43 feet Y = 5283255
20 meter
Z = 1500667
28 Z = 457403
39
XDOT = -10232
300963 XDOT = -3118
805334
YDOT = -9792
642914 feet/sec YDOT = -2984
797560 meter/sec
ZDOT = 19734
527270 ZDOT = 6015
083912
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 10289
56269440
00016717 00000-0 10270-3 0 9058
2 25544 51
6457 329
6105 0007385 98
0295 262
1705 15
72025883 2569
Satellite: ISS
Catalog Number: 25544
Epoch time: 10289
56269440 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 329
6105 deg
Eccentricity:
0007385
Arg of perigee: 98
0295 deg
Mean anomaly: 262
1705 deg
Mean motion: 15
72025883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 321
Coasting Arc #7 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2010/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2631062
08 A = 6725580
74 meter
Y = -3281558
34 meter E =
0022205
Z = -5267132
73 I = 51
42849
XDOT = 6139
888998 Wp = 93
03695
YDOT = -4611
743676 meter/sec RA = 324
25365 deg
ZDOT = -195
656967 TA = 175
10695
MA = 175
08521
Ha = 195
688 n
mi
Hp = 183
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8632093
45 X = -2568584
52
Y = -10766267
53 feet Y = -3310631
48 meter
Z = -17280619
21 Z = -5279762
58
XDOT = 20143
992774 XDOT = 6191
952511
YDOT = -15130
392637 feet/sec YDOT = -4542
792656 meter/sec
ZDOT = -641
919182 ZDOT = -165
702337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12291567
25 X = 3746469
70
Y = 6131217
53 feet Y = 1868795
10 meter
Z = -17331211
74 Z = -5282553
34
XDOT = -11378
114493 XDOT = -3468
049298
YDOT = 21352
581982 feet/sec YDOT = 6508
266988 meter/sec
ZDOT = -521
794010 ZDOT = -159
042814
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 10290
51619607
00016717 00000-0 10270-3 0 9060
2 25544 51
6465 324
7280 0007328 102
9750 257
2230 15
72084708 2712
Satellite: ISS
Catalog Number: 25544
Epoch time: 10290
51619607 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 324
7280 deg
Eccentricity:
0007328
Arg of perigee: 102
9750 deg
Mean anomaly: 257
2230 deg
Mean motion: 15
72084708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 271
Checksum: 296
Coasting Arc #8 (Orbit 286)
---------------------------------------
Vector Time (GMT): 2010/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4641801
56 A = 6737229
35 meter
Y = 4812888
32 meter E =
0020531
Z = 752456
97 I = 51
44356
XDOT = -3951
193756 Wp = 119
36434
YDOT = -2861
568707 meter/sec RA = 319
10930 deg
ZDOT = -5959
199137 TA = 52
41407
MA = 52
22781
Ha = 195
611 n
mi
Hp = 183
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15229007
73 X = -4698930
52
Y = 15790316
00 feet Y = 4760661
53 meter
Z = 2468690
85 Z = 729767
68
XDOT = -12963
234108 XDOT = -3889
952420
YDOT = -9388
348776 feet/sec YDOT = -2905
411373 meter/sec
ZDOT = -19551
178270 ZDOT = -5978
245298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6746127
42 X = 2056219
64
Y = -20885102
90 feet Y = -6365779
36 meter
Z = 2377694
67 Z = 724721
34
XDOT = 14143
980217 XDOT = 4311
085170
YDOT = 2290
748482 feet/sec YDOT = 698
220137 meter/sec
ZDOT = -19627
495448 ZDOT = -5982
460612
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 10291
53324256
00016717 00000-0 10270-3 0 9077
2 25544 51
6457 319
5199 0007452 105
9647 254
2337 15
72148109 2878
Satellite: ISS
Catalog Number: 25544
Epoch time: 10291
53324256 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 319
5199 deg
Eccentricity:
0007452
Arg of perigee: 105
9647 deg
Mean anomaly: 254
2337 deg
Mean motion: 15
72148109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 287
Checksum: 319
Coasting Arc #9 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2010/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4113849
50 A = 6726035
49 meter
Y = 1574809
58 meter E =
0012130
Z = 5074627
29 I = 51
38324
XDOT = -4288
506547 Wp = 115
26096
YDOT = 6213
575395 meter/sec RA = 313
99195 deg
ZDOT = 1540
335917 TA = 319
87038
MA = 319
95990
Ha = 195
452 n
mi
Hp = 183
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13496881
57 X = 4071281
90
Y = 5166698
11 feet Y = 1620575
54 meter
Z = 16649039
65 Z = 5094509
17
XDOT = -14069
903370 XDOT = -4365
151962
YDOT = 20385
746046 feet/sec YDOT = 6165
190317 meter/sec
ZDOT = 5053
595528 ZDOT = 1519
315315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14281454
90 X = -4352987
45
Y = 1497049
27 feet Y = 456300
62 meter
Z = 16728717
59 Z = 5098913
12
XDOT = 3384
984570 XDOT = 1031
743297
YDOT = -23527
969338 feet/sec YDOT = -7171
325054 meter/sec
ZDOT = 4969
282413 ZDOT = 1514
637280
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 10292
55026501
00016717 00000-0 10270-3 0 9083
2 25544 51
6448 314
3118 0007507 109
4249 250
7725 15
72182822 3031
Satellite: ISS
Catalog Number: 25544
Epoch time: 10292
55026501 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 314
3118 deg
Eccentricity:
0007507
Arg of perigee: 109
4249 deg
Mean anomaly: 250
7725 deg
Mean motion: 15
72182822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 303
Checksum: 288
Coasting Arc #10 (Orbit 317)
---------------------------------------
Vector Time (GMT): 2010/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2754166
80 A = 6735592
95 meter
Y = -5846087
13 meter E =
0011677
Z = -1902921
55 I = 51
39661
XDOT = 5225
242430 Wp = 77
05165
YDOT = 646
867316 meter/sec RA = 308
82292 deg
ZDOT = 5606
871716 TA = 261
75883
MA = 261
89127
Ha = 195
456 n
mi
Hp = 183
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9035980
33 X = 2828578
38
Y = -19180075
88 feet Y = -5814872
48 meter
Z = -6243180
95 Z = -1889360
29
XDOT = 17143
183827 XDOT = 5190
382941
YDOT = 2122
268097 feet/sec YDOT = 705
104679 meter/sec
ZDOT = 18395
248413 ZDOT = 5632
171743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1016047
60 X = 309691
31
Y = 21193590
08 feet Y = 6459806
26 meter
Z = -6188775
83 Z = -1886338
87
XDOT = -14484
532797 XDOT = -4414
885597
YDOT = 6065
226812 feet/sec YDOT = 1848
681132 meter/sec
ZDOT = 18496
648596 ZDOT = 5637
778492
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 10293
50370130
00016717 00000-0 10270-3 0 9090
2 25544 51
6456 309
4296 0007547 113
3164 246
8794 15
72255648 3181
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
50370130 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 309
4296 deg
Eccentricity:
0007547
Arg of perigee: 113
3164 deg
Mean anomaly: 246
8794 deg
Mean motion: 15
72255648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 318
Checksum: 315
Coasting Arc #11 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2010/293/19:25:06
928
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1782707
94 A = 6727730
02 meter
Y = -4203948
44 meter E =
0018243
Z = -4957455
81 I = 51
36068
XDOT = 5663
347461 Wp = 108
32956
YDOT = -4783
083684 meter/sec RA = 307
23469 deg
ZDOT = 2019
977947 TA = 181
33727
MA = 181
34216
Ha = 195
362 n
mi
Hp = 185
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5848779
33 X = -1711483
15
Y = -13792481
75 feet Y = -4223485
92 meter
Z = -16264618
81 Z = -4965943
04
XDOT = 18580
536291 XDOT = 5706
598964
YDOT = -15692
531773 feet/sec YDOT = -4719
510729 meter/sec
ZDOT = 6627
224236 ZDOT = 2047
596554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4548181
59 X = 1386285
75
Y = -14235457
29 feet Y = -4338967
38 meter
Z = -16298601
08 Z = -4967813
61
XDOT = 23252
046606 XDOT = 7087
223806
YDOT = -283
872191 feet/sec YDOT = -86
524244 meter/sec
ZDOT = 6737
962041 ZDOT = 2053
730830
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 10293
82150950
00016717 00000-0 10270-3 0 9103
2 25544 51
6463 307
8018 0005490 116
5494 243
6232 15
71817662 3236
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
82150950 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 307
8018 deg
Eccentricity:
0005490
Arg of perigee: 116
5494 deg
Mean anomaly: 243
6232 deg
Mean motion: 15
71817662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 293
Coasting Arc #12 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2010/294/19:25:06
928
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4255403
01 A = 6737803
54 meter
Y = 5095610
28 meter E =
0014704
Z = -1119425
93 I = 51
37741
XDOT = -3110
842900 Wp = 134
45176
YDOT = -3876
487714 meter/sec RA = 302
12349 deg
ZDOT = -5877
687327 TA = 57
83595
MA = 57
69340
Ha = 195
277 n
mi
Hp = 185
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13961295
98 X = -4306628
69
Y = 16717881
50 feet Y = 5047737
31 meter
Z = -3672657
26 Z = -1140224
03
XDOT = -10206
177492 XDOT = -3038
710591
YDOT = -12718
135546 feet/sec YDOT = -3910
872147 meter/sec
ZDOT = -19283
751074 ZDOT = -5892
624700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21380488
43 X = -6516772
87
Y = 4081729
16 feet Y = 1244111
05 meter
Z = -3756056
47 Z = -1144846
01
XDOT = 564
245016 XDOT = 171
981881
YDOT = -14674
659321 feet/sec YDOT = -4472
836161 meter/sec
ZDOT = -19343
588051 ZDOT = -5895
925638
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 10294
83874244
00016717 00000-0 10270-3 0 9115
2 25544 51
6464 302
5947 0005512 121
8467 238
3232 15
71824703 3396
Satellite: ISS
Catalog Number: 25544
Epoch time: 10294
83874244 = yrday
fracday
Element set: 911
Inclination: 51
6464 deg
RA of node: 302
5947 deg
Eccentricity:
0005512
Arg of perigee: 121
8467 deg
Mean anomaly: 238
3232 deg
Mean motion: 15
71824703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 305
Coasting Arc #13 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2010/295/19:25:06
928
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3481132
67 A = 6726085
98 meter
Y = 2389344
23 meter E =
0007255
Z = 5229589
46 I = 51
32366
XDOT = -3834
034818 Wp = 105
88051
YDOT = 6663
537524 meter/sec RA = 296
96831 deg
ZDOT = -493
725026 TA = 348
82036
MA = 348
83647
Ha = 194
965 n
mi
Hp = 185
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11421038
94 X = 3428750
70
Y = 7839055
86 feet Y = 2427979
76 meter
Z = 17157445
74 Z = 5246373
92
XDOT = -12578
854389 XDOT = -3905
864274
YDOT = 21861
999751 feet/sec YDOT = 6620
261393 meter/sec
ZDOT = -1619
832761 ZDOT = -512
526168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4004498
53 X = 1220571
15
Y = 13173559
72 feet Y = 4015301
00 meter
Z = 17224697
01 Z = 5250087
65
XDOT = -22466
654143 XDOT = -6847
836183
YDOT = 9040
025634 feet/sec YDOT = 2755
399813 meter/sec
ZDOT = -1695
238833 ZDOT = -516
708796
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 10295
85594865
00016717 00000-0 10270-3 0 9127
2 25544 51
6462 297
3876 0005373 124
7297 235
4371 15
71928436 3552
Satellite: ISS
Catalog Number: 25544
Epoch time: 10295
85594865 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 297
3876 deg
Eccentricity:
0005373
Arg of perigee: 124
7297 deg
Mean anomaly: 235
4371 deg
Mean motion: 15
71928436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 343
Coasting Arc #14 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2010/296/19:25:06
928
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2317380
73 A = 6738010
20 meter
Y = -6318725
09 meter E =
0013398
Z = -247955
71 I = 51
35151
XDOT = 4587
849823 Wp = 66
78734
YDOT = 1457
291131 meter/sec RA = 291
82869 deg
ZDOT = 6003
392061 TA = 290
51067
MA = 290
65442
Ha = 195
037 n
mi
Hp = 185
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7602955
16 X = 2389070
21
Y = -20730725
38 feet Y = -6292409
92 meter
Z = -813502
99 Z = -236523
17
XDOT = 15052
000732 XDOT = 4542
048847
YDOT = 4781
138881 feet/sec YDOT = 1508
339350 meter/sec
ZDOT = 19696
168180 ZDOT = 6025
569215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18634831
31 X = 5679896
58
Y = -11848353
96 feet Y = -3611378
29 meter
Z = -767632
30 Z = -233974
32
XDOT = 8096
218662 XDOT = 2467
727448
YDOT = 11510
773207 feet/sec YDOT = 3508
483673 meter/sec
ZDOT = 19785
040143 ZDOT = 6030
480236
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 10296
80955963
00016717 00000-0 10270-3 0 9134
2 25544 51
6465 292
5056 0005392 127
8871 232
2779 15
71942082 3702
Satellite: ISS
Catalog Number: 25544
Epoch time: 10296
80955963 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 292
5056 deg
Eccentricity:
0005392
Arg of perigee: 127
8871 deg
Mean anomaly: 232
2779 deg
Mean motion: 15
71942082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 330
Coasting Arc #15 (Orbit 385)
---------------------------------------
Vector Time (GMT): 2010/297/19:25:06
928
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4302312
28 A = 6726172
30 meter
Y = -113076
96 meter E =
0018445
Z = -5184643
49 I = 51
30185
XDOT = 1404
174992 Wp = 94
72406
YDOT = -7487
659206 meter/sec RA = 286
69684 deg
ZDOT = -1006
481151 TA = 165
64093
MA = 165
58844
Ha = 194
885 n
mi
Hp = 185
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14115197
77 X = -4275541
24
Y = -370987
39 feet Y = -161038
37 meter
Z = -17009985
19 Z = -5205479
73
XDOT = 4606
873334 XDOT = 1492
688476
YDOT = -24565
811042 feet/sec YDOT = -7471
461983 meter/sec
ZDOT = -3302
103514 ZDOT = -999
444365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11057178
97 X = -3370228
15
Y = -8617844
52 feet Y = -2626719
01 meter
Z = -17093495
40 Z = -5210097
40
XDOT = 17677
272788 XDOT = 5388
032746
YDOT = -16216
908540 feet/sec YDOT = -4942
913723 meter/sec
ZDOT = -3273
840777 ZDOT = -997
866669
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 10297
82671882
00016717 00000-0 10270-3 0 9143
2 25544 51
6465 287
2978 0005308 131
3525 228
8095 15
71988314 3866
Satellite: ISS
Catalog Number: 25544
Epoch time: 10297
82671882 = yrday
fracday
Element set: 914
Inclination: 51
6465 deg
RA of node: 287
2978 deg
Eccentricity:
0005308
Arg of perigee: 131
3525 deg
Mean anomaly: 228
8095 deg
Mean motion: 15
71988314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 386
Checksum: 343
Coasting Arc #16 (Orbit 401)
---------------------------------------
Vector Time (GMT): 2010/298/19:25:06
928
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -114755
35 A = 6736972
34 meter
Y = 6557261
19 meter E =
0019348
Z = 1497446
38 I = 51
33066
XDOT = -4959
519101 Wp = 122
94091
YDOT = 1239
112309 meter/sec RA = 281
53119 deg
ZDOT = -5762
678698 TA = 40
49390
MA = 40
35009
Ha = 194
900 n
mi
Hp = 185
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -376493
93 X = -195345
86
Y = 21513324
11 feet Y = 6555527
31 meter
Z = 4912881
81 Z = 1496693
18
XDOT = -16271
388126 XDOT = -4945
011622
YDOT = 4065
329098 feet/sec YDOT = 1183
733152 meter/sec
ZDOT = -18906
426176 ZDOT = -5786
737483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12801489
85 X = -3901894
11
Y = 17294995
69 feet Y = 5271514
69 meter
Z = 4909811
73 Z = 1496510
62
XDOT = -14261
958889 XDOT = -4347
045069
YDOT = -5121
368167 feet/sec YDOT = -1560
993017 meter/sec
ZDOT = -19002
866637 ZDOT = -5792
073751
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 10298
84385465
00016717 00000-0 10270-3 0 9156
2 25544 51
6466 282
0906 0005483 135
5631 224
5972 15
71977829 4024
Satellite: ISS
Catalog Number: 25544
Epoch time: 10298
84385465 = yrday
fracday
Element set: 915
Inclination: 51
6466 deg
RA of node: 282
0906 deg
Eccentricity:
0005483
Arg of perigee: 135
5631 deg
Mean anomaly: 224
5972 deg
Mean motion: 15
71977829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 402
Checksum: 334
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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