Date:
October 8th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10548 63 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
293/19:21:35
102 2
0 3
1 3
1
N/A -2
4 -0
0 195
6
000/00:07:10
205 0
2 0
1 186
0
Coasting Arc #1 (Orbit 97)
---------------------------------------
Vector Time (GMT): 2010/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 210887
95 A = 6727134
61 meter
Y = -4293993
94 meter E =
0021179
Z = -5192611
76 I = 51
74878
XDOT = 7378
430894 Wp = 76
45104
YDOT = 1783
723929 meter/sec RA = 20
59689 deg
ZDOT = -1174
521818 TA = 182
31625
MA = 182
32608
Ha = 196
114 n
mi
Hp = 184
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 691889
60 X = 284113
62
Y = -14087906
63 feet Y = -4291226
84 meter
Z = -17036127
81 Z = -5191408
89
XDOT = 24207
450441 XDOT = 7363
642268
YDOT = 5852
112628 feet/sec YDOT = 1866
151155 meter/sec
ZDOT = -3853
418038 ZDOT = -1138
713059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2702185
42 X = 823626
12
Y = 13849600
36 feet Y = 4221358
19 meter
Z = -17031272
39 Z = -5191131
82
XDOT = -23914
860926 XDOT = -7289
249610
YDOT = 100
429702 feet/sec YDOT = 30
610973 meter/sec
ZDOT = -3709
861781 ZDOT = -1130
765871
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 10279
51784138
00016717 00000-0 10270-3 0 9003
2 25544 51
6469 21
0233 0006946 67
7125 292
4773 15
71686277 988
Satellite: ISS
Catalog Number: 25544
Epoch time: 10279
51784138 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 21
0233 deg
Eccentricity:
0006946
Arg of perigee: 67
7125 deg
Mean anomaly: 292
4773 deg
Mean motion: 15
71686277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 98
Checksum: 325
Coasting Arc #2 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2010/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6493521
53 A = 6737471
77 meter
Y = -381734
84 meter E =
0019835
Z = 1729557
55 I = 51
75462
XDOT = -1239
993068 Wp = 101
03174
YDOT = -5013
140001 meter/sec RA = 15
46198 deg
ZDOT = -5710
592907 TA = 59
86998
MA = 59
67355
Ha = 196
186 n
mi
Hp = 184
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21304204
51 X = -6497172
33
Y = -1252410
90 feet Y = -454369
53 meter
Z = 5674401
41 Z = 1698002
59
XDOT = -4068
218726 XDOT = -1156
101485
YDOT = -16447
309716 feet/sec YDOT = -5026
537885 meter/sec
ZDOT = -18735
541032 ZDOT = -5716
412605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20915730
84 X = 6375114
76
Y = -4403354
27 feet Y = -1342142
38 meter
Z = 5547897
69 Z = 1690999
21
XDOT = 7822
165388 XDOT = 2384
196010
YDOT = 13303
100334 feet/sec YDOT = 4054
784982 meter/sec
ZDOT = -18758
829888 ZDOT = -5717
691350
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 10280
53515699
00016717 00000-0 10270-3 0 9012
2 25544 51
6467 15
8177 0007086 72
2102 287
9832 15
71708218 1140
Satellite: ISS
Catalog Number: 25544
Epoch time: 10280
53515699 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 15
8177 deg
Eccentricity:
0007086
Arg of perigee: 72
2102 deg
Mean anomaly: 287
9832 deg
Mean motion: 15
71708218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 306
Coasting Arc #3 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2010/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2365038
38 A = 6728901
24 meter
Y = 4196969
83 meter E =
0013781
Z = 4686906
93 I = 51
69771
XDOT = -7131
789130 Wp = 97
02545
YDOT = 916
554614 meter/sec RA = 10
38672 deg
ZDOT = 2769
417330 TA = 325
67200
MA = 325
76098
Ha = 196
009 n
mi
Hp = 184
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7759312
28 X = 2295162
63
Y = 13769586
05 feet Y = 4223026
80 meter
Z = 15376991
23 Z = 4698226
47
XDOT = -23398
258302 XDOT = -7154
961802
YDOT = 3007
068942 feet/sec YDOT = 836
673326 meter/sec
ZDOT = 9086
014863 ZDOT = 2734
713927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11211566
82 X = -3417285
57
Y = -11077582
03 feet Y = -3376447
00 meter
Z = 15422329
01 Z = 4700725
88
XDOT = 20868
331521 XDOT = 6360
667448
YDOT = -8625
725455 feet/sec YDOT = -2629
121119 meter/sec
ZDOT = 8946
883729 ZDOT = 2727
010161
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 10281
55245304
00016717 00000-0 10270-3 0 9029
2 25544 51
6473 10
6114 0007045 75
0201 285
1740 15
71775953 1303
Satellite: ISS
Catalog Number: 25544
Epoch time: 10281
55245304 = yrday
fracday
Element set: 902
Inclination: 51
6473 deg
RA of node: 10
6114 deg
Eccentricity:
0007045
Arg of perigee: 75
0201 deg
Mean anomaly: 285
1740 deg
Mean motion: 15
71775953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 266
Coasting Arc #4 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2010/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5699786
01 A = 6734601
20 meter
Y = -1898086
77 meter E =
0011561
Z = -3049527
95 I = 51
68615
XDOT = 4056
026440 Wp = 74
35789
YDOT = 4284
846317 meter/sec RA = 5
22819 deg
ZDOT = 4932
543353 TA = 250
41030
MA = 250
53515
Ha = 196
121 n
mi
Hp = 184
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18700085
34 X = 5735401
57
Y = -6227318
80 feet Y = -1834149
37 meter
Z = -10005012
96 Z = -3021751
08
XDOT = 13307
173360 XDOT = 3983
849037
YDOT = 14057
894740 feet/sec YDOT = 4329
799952 meter/sec
ZDOT = 16182
885016 ZDOT = 4952
072455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16074892
18 X = -4899627
14
Y = 11501594
63 feet Y = 3505686
04 meter
Z = -9893641
29 Z = -3015581
86
XDOT = -15941
654679 XDOT = -4859
016346
YDOT = -8345
480651 feet/sec YDOT = -2543
702503 meter/sec
ZDOT = 16261
124614 ZDOT = 4956
390782
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 10282
50615475
00016717 00000-0 10270-3 0 9036
2 25544 51
6470 5
7317 0007052 77
1929 283
0021 15
71763688 1455
Satellite: ISS
Catalog Number: 25544
Epoch time: 10282
50615475 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 5
7317 deg
Eccentricity:
0007052
Arg of perigee: 77
1929 deg
Mean anomaly: 283
0021 deg
Mean motion: 15
71763688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 295
Coasting Arc #5 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2010/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4565574
79 A = 6731868
89 meter
Y = -3084444
05 meter E =
0013752
Z = -3881761
42 I = 51
64621
XDOT = 5650
165259 Wp = 76
96858
YDOT = -3223
159425 meter/sec RA =
16164 deg
ZDOT = -4093
488137 TA = 150
29062
MA = 150
21245
Ha = 196
070 n
mi
Hp = 184
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14978919
92 X = -4511887
30
Y = -10119567
08 feet Y = -3135198
99 meter
Z = -12735437
73 Z = -3903811
00
XDOT = 18537
287595 XDOT = 5705
673180
YDOT = -10574
670029 feet/sec YDOT = -3159
665651 meter/sec
ZDOT = -13430
079191 ZDOT = -4065
904057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17318688
76 X = 5278736
33
Y = 4957670
08 feet Y = 1511097
84 meter
Z = -12823789
65 Z = -3908691
09
XDOT = -14019
646711 XDOT = -4273
188318
YDOT = 14598
868977 feet/sec YDOT = 4449
735264 meter/sec
ZDOT = -13319
463295 ZDOT = -4059
772412
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 10283
52341906
00016717 00000-0 10270-3 0 9045
2 25544 51
6460
5253 0007117 81
3102 278
8866 15
71787174 1611
Satellite: ISS
Catalog Number: 25544
Epoch time: 10283
52341906 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node:
5253 deg
Eccentricity:
0007117
Arg of perigee: 81
3102 deg
Mean anomaly: 278
8866 deg
Mean motion: 15
71787174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 290
Coasting Arc #6 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2010/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3992048
91 A = 6731207
62 meter
Y = 3577340
18 meter E =
0017861
Z = 4058577
94 I = 51
61442
XDOT = -6182
900978 Wp = 79
23803
YDOT = -2516
449433 meter/sec RA = 354
99104 deg
ZDOT = -3845
938831 TA = 50
39965
MA = 50
24208
Ha = 196
065 n
mi
Hp = 184
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13097273
33 X = -4051470
93
Y = 11736680
37 feet Y = 3532366
50 meter
Z = 13315544
41 Z = 4039039
78
XDOT = -20285
108195 XDOT = -6135
618788
YDOT = -8256
067693 feet/sec YDOT = -2585
326034 meter/sec
ZDOT = -12617
909551 ZDOT = -3875
861083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8585957
49 X = 2616999
84
Y = -15415917
06 feet Y = -4698771
52 meter
Z = 13237174
66 Z = 4034690
84
XDOT = 20676
640071 XDOT = 6302
239894
YDOT = 528
641236 feet/sec YDOT = 161
129849 meter/sec
ZDOT = -12737
825381 ZDOT = -3882
489176
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
54066456
00016717 00000-0 10270-3 0 9053
2 25544 51
6465 355
3185 0007134 83
2420 276
9553 15
71857704 1770
Satellite: ISS
Catalog Number: 25544
Epoch time: 10284
54066456 = yrday
fracday
Element set: 905
Inclination: 51
6465 deg
RA of node: 355
3185 deg
Eccentricity:
0007134
Arg of perigee: 83
2420 deg
Mean anomaly: 276
9553 deg
Mean motion: 15
71857704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 317
Coasting Arc #7 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6014346
81 A = 6734850
71 meter
Y = 1165887
53 meter E =
0020707
Z = 2776178
63 I = 51
59624
XDOT = -3293
697984 Wp = 82
38243
YDOT = 4713
000604 meter/sec RA = 349
91871 deg
ZDOT = 5126
406323 TA = 309
40072
MA = 309
58390
Ha = 195
965 n
mi
Hp = 184
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19732108
95 X = 5987376
24
Y = 3825090
31 feet Y = 1232992
79 meter
Z = 9108197
59 Z = 2805331
27
XDOT = -10806
095748 XDOT = -3371
058392
YDOT = 15462
600406 feet/sec YDOT = 4675
735990 meter/sec
ZDOT = 16818
918382 ZDOT = 5110
217330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19789648
21 X = -6031884
78
Y = 3196097
60 feet Y = 974170
55 meter
Z = 9225046
69 Z = 2811794
23
XDOT = 5136
448526 XDOT = 1565
589511
YDOT = -16832
623393 feet/sec YDOT = -5130
583610 meter/sec
ZDOT = 16753
956708 ZDOT = 5106
606005
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
55789414
00016717 00000-0 10270-3 0 9062
2 25544 51
6459 350
1120 0007234 87
5207 272
6783 15
71859121 1937
Satellite: ISS
Catalog Number: 25544
Epoch time: 10285
55789414 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 350
1120 deg
Eccentricity:
0007234
Arg of perigee: 87
5207 deg
Mean anomaly: 272
6783 deg
Mean motion: 15
71859121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 313
Coasting Arc #8 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2010/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1684391
85 A = 6728275
64 meter
Y = -4415547
67 meter E =
0018753
Z = -4806291
49 I = 51
54375
XDOT = 7268
086413 Wp = 100
55900
YDOT = 68
024702 meter/sec RA = 344
75189 deg
ZDOT = 2489
495986 TA = 193
85818
MA = 193
90972
Ha = 196
022 n
mi
Hp = 184
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5526219
98 X = 1756990
52
Y = -14486704
94 feet Y = -4396305
91 meter
Z = -15768672
86 Z = -4797932
22
XDOT = 23845
427864 XDOT = 7254
691891
YDOT = 223
178156 feet/sec YDOT = 149
225942 meter/sec
ZDOT = 8167
637749 ZDOT = 2524
772249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11024
60 X = -3360
30
Y = 15539022
00 feet Y = 4736293
91 meter
Z = -15735102
32 Z = -4796059
19
XDOT = -21139
439421 XDOT = -6443
301136
YDOT = 8382
758547 feet/sec YDOT = 2555
064805 meter/sec
ZDOT = 8309
050971 ZDOT = 2532
598736
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
51153094
00016717 00000-0 10270-3 0 9079
2 25544 51
6453 345
2306 0007303 89
6485 270
5513 15
71879902 2084
Satellite: ISS
Catalog Number: 25544
Epoch time: 10286
51153094 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 345
2306 deg
Eccentricity:
0007303
Arg of perigee: 89
6485 deg
Mean anomaly: 270
5513 deg
Mean motion: 15
71879902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 307
Coasting Arc #9 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2010/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6462514
13 A = 6736991
71 meter
Y = 1067743
22 meter E =
0013982
Z = -1567908
05 I = 51
54517
XDOT = 546
477922 Wp = 118
37293
YDOT = -5077
054634 meter/sec RA = 339
65989 deg
ZDOT = -5755
247360 TA = 78
92097
MA = 78
76376
Ha = 195
961 n
mi
Hp = 184
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21202474
16 X = -6466356
83
Y = 3503094
56 feet Y = 995453
99 meter
Z = -5144055
29 Z = -1599312
59
XDOT = 1792
906569 XDOT = 631
168086
YDOT = -16657
003391 feet/sec YDOT = -5070
470175 meter/sec
ZDOT = -18882
045144 ZDOT = -5752
386730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18289026
24 X = 5574495
20
Y = -11225724
63 feet Y = -3421600
87 meter
Z = -5269963
25 Z = -1606284
80
XDOT = 3696
562645 XDOT = 1126
712294
YDOT = 14813
142228 feet/sec YDOT = 4515
045751 meter/sec
ZDOT = -18870
510216 ZDOT = -5751
731514
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
52872652
00016717 00000-0 10270-3 0 9080
2 25544 51
6457 340
0232 0007396 93
0369 267
1640 15
71915051 2248
Satellite: ISS
Catalog Number: 25544
Epoch time: 10287
52872652 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 340
0232 deg
Eccentricity:
0007396
Arg of perigee: 93
0369 deg
Mean anomaly: 267
1640 deg
Mean motion: 15
71915051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 302
Coasting Arc #10 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 732369
12 A = 6726299
10 meter
Y = 4218014
34 meter E =
0010434
Z = 5179277
19 I = 51
48109
XDOT = -7206
690746 Wp = 82
73995
YDOT = 2524
502300 meter/sec RA = 334
50812 deg
ZDOT = -1033
833994 TA = 17
15138
MA = 17
11615
Ha = 195
864 n
mi
Hp = 184
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2402785
81 X = 659987
88
Y = 13838629
73 feet Y = 4225799
61 meter
Z = 16992379
24 Z = 5182659
11
XDOT = -23643
998509 XDOT = -7229
362358
YDOT = 8282
487860 feet/sec YDOT = 2443
785954 meter/sec
ZDOT = -3391
843811 ZDOT = -1068
899523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7553596
93 X = -2302336
34
Y = -11822229
12 feet Y = -3603415
44 meter
Z = 17005883
60 Z = 5183393
32
XDOT = 17608
247585 XDOT = 5366
993864
YDOT = -16346
263206 feet/sec YDOT = -4982
341025 meter/sec
ZDOT = -3532
444605 ZDOT = -1076
689116
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
54590308
00016717 00000-0 10270-3 0 9099
2 25544 51
6454 334
8165 0007279 96
7090 263
4901 15
71957160 2406
Satellite: ISS
Catalog Number: 25544
Epoch time: 10288
54590308 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 334
8165 deg
Eccentricity:
0007279
Arg of perigee: 96
7090 deg
Mean anomaly: 263
4901 deg
Mean motion: 15
71957160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 319
Coasting Arc #11 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5882299
08 A = 6738076
36 meter
Y = -3266624
30 meter E =
0018419
Z = 231157
70 I = 51
49343
XDOT = 2136
389378 Wp = 65
58426
YDOT = 4298
907389 meter/sec RA = 329
38891 deg
ZDOT = 6017
539387 TA = 296
93048
MA = 297
11854
Ha = 196
008 n
mi
Hp = 184
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19298881
50 X = 5917266
96
Y = -10717271
31 feet Y = -3200649
37 meter
Z = 758391
39 Z = 259819
23
XDOT = 7009
151502 XDOT = 2058
927068
YDOT = 14104
026867 feet/sec YDOT = 4322
364970 meter/sec
ZDOT = 19742
583291 ZDOT = 6027
729671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13230549
74 X = -4032671
56
Y = 17665552
53 feet Y = 5384460
41 meter
Z = 873324
74 Z = 266189
38
XDOT = -10765
404987 XDOT = -3281
295440
YDOT = -9092
545314 feet/sec YDOT = -2771
407812 meter/sec
ZDOT = 19783
382703 ZDOT = 6029
975048
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
56306613
00016717 00000-0 10270-3 0 9108
2 25544 51
6454 329
6092 0007442 98
2633 261
9373 15
71919564 2568
Satellite: ISS
Catalog Number: 25544
Epoch time: 10289
56306613 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 329
6092 deg
Eccentricity:
0007442
Arg of perigee: 98
2633 deg
Mean anomaly: 261
9373 deg
Mean motion: 15
71919564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 320
Coasting Arc #12 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2010/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2861432
74 A = 6725963
18 meter
Y = -3103944
43 meter E =
0022147
Z = -5255069
31 I = 51
42838
XDOT = 6004
546407 Wp = 91
80683
YDOT = -4768
731955 meter/sec RA = 324
25729 deg
ZDOT = -455
183146 TA = 173
85988
MA = 173
83269
Ha = 195
893 n
mi
Hp = 184
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9387902
70 X = -2800982
77
Y = -10183544
71 feet Y = -3135605
04 meter
Z = -17241041
05 Z = -5268823
24
XDOT = 19699
955404 XDOT = 6059
636195
YDOT = -15645
446046 feet/sec YDOT = -4701
277514 meter/sec
ZDOT = -1493
383025 ZDOT = -425
878656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12728961
45 X = 3879787
45
Y = 5282785
84 feet Y = 1610193
12 meter
Z = -17296141
49 Z = -5271863
93
XDOT = -10823
947385 XDOT = -3299
139163
YDOT = 21600
878097 feet/sec YDOT = 6583
947644 meter/sec
ZDOT = -1375
862298 ZDOT = -419
362828
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
51663616
00016717 00000-0 10270-3 0 9115
2 25544 51
6462 324
7270 0007402 103
2155 256
9833 15
71968210 2717
Satellite: ISS
Catalog Number: 25544
Epoch time: 10290
51663616 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 324
7270 deg
Eccentricity:
0007402
Arg of perigee: 103
2155 deg
Mean anomaly: 256
9833 deg
Mean motion: 15
71968210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 271
Checksum: 286
Coasting Arc #13 (Orbit 286)
---------------------------------------
Vector Time (GMT): 2010/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4459809
92 A = 6737390
88 meter
Y = 4934445
32 meter E =
0020975
Z = 1017155
93 I = 51
44254
XDOT = -4217
132950 Wp = 117
53495
YDOT = -2576
652389 meter/sec RA = 319
10912 deg
ZDOT = -5907
177720 TA = 51
31865
MA = 51
13121
Ha = 195
833 n
mi
Hp = 184
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14631922
31 X = -4519597
56
Y = 16189125
07 feet Y = 4884238
83 meter
Z = 3337125
74 Z = 995344
29
XDOT = -13835
738026 XDOT = -4159
310550
YDOT = -8453
583952 feet/sec YDOT = -2623
488059 meter/sec
ZDOT = -19380
504331 ZDOT = -5927
524157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6039122
53 X = 1840724
55
Y = -20982996
13 feet Y = -6395617
22 meter
Z = 3249646
41 Z = 990492
23
XDOT = 14510
259881 XDOT = 4422
727212
YDOT = 1118
637412 feet/sec YDOT = 340
960683 meter/sec
ZDOT = -19462
036399 ZDOT = -5932
028695
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
53376164
00016717 00000-0 10270-3 0 9128
2 25544 51
6453 319
5194 0007519 106
1256 254
0734 15
72022409 2875
Satellite: ISS
Catalog Number: 25544
Epoch time: 10291
53376164 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 319
5194 deg
Eccentricity:
0007519
Arg of perigee: 106
1256 deg
Mean anomaly: 254
0734 deg
Mean motion: 15
72022409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 287
Checksum: 297
Coasting Arc #14 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2010/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4329093
36 A = 6726816
97 meter
Y = 1250139
82 meter E =
0013033
Z = 4986095
92 I = 51
38427
XDOT = -4001
616252 Wp = 115
62757
YDOT = 6309
372104 meter/sec RA = 313
99781 deg
ZDOT = 1883
039400 TA = 316
09372
MA = 316
19722
Ha = 195
688 n
mi
Hp = 184
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14203062
20 X = 4290570
35
Y = 4101508
61 feet Y = 1298335
37 meter
Z = 16358582
40 Z = 5007033
32
XDOT = -13128
662244 XDOT = -4081
019026
YDOT = 20700
039711 feet/sec YDOT = 6264
179818 meter/sec
ZDOT = 6177
950787 ZDOT = 1863
405828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14426943
57 X = -4397332
40
Y = 2767716
16 feet Y = 843599
89 meter
Z = 16442494
14 Z = 5011672
21
XDOT = 2502
440150 XDOT = 762
743758
YDOT = -23371
882423 feet/sec YDOT = -7123
749763 meter/sec
ZDOT = 6099
196405 ZDOT = 1859
035064
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
55086963
00016717 00000-0 10270-3 0 9137
2 25544 51
6445 314
3119 0007577 109
5985 250
5996 15
72044720 3036
Satellite: ISS
Catalog Number: 25544
Epoch time: 10292
55086963 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 314
3119 deg
Eccentricity:
0007577
Arg of perigee: 109
5985 deg
Mean anomaly: 250
5996 deg
Mean motion: 15
72044720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 303
Checksum: 317
Coasting Arc #15 (Orbit 317)
---------------------------------------
Vector Time (GMT): 2010/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2436699
74 A = 6735429
36 meter
Y = -5871447
43 meter E =
0011226
Z = -2232698
49 I = 51
39438
XDOT = 5427
011392 Wp = 82
29408
YDOT = 191
066560 meter/sec RA = 308
82478 deg
ZDOT = 5445
289920 TA = 252
61561
MA = 252
73841
Ha = 195
708 n
mi
Hp = 184
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7994421
72 X = 2513020
53
Y = -19263278
98 feet Y = -5843772
25 meter
Z = -7325126
29 Z = -2220674
88
XDOT = 17805
155487 XDOT = 5398
018707
YDOT = 626
858794 feet/sec YDOT = 251
593014 meter/sec
ZDOT = 17865
124408 ZDOT = 5471
584449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1968643
77 X = 600042
62
Y = 20780124
43 feet Y = 6333781
93 meter
Z = -7276884
04 Z = -2217994
26
XDOT = -14398
157390 XDOT = -4388
558373
YDOT = 7628
273246 feet/sec YDOT = 2325
097685 meter/sec
ZDOT = 17970
514578 ZDOT = 5477
412843
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
50439188
00016717 00000-0 10270-3 0 9145
2 25544 51
6453 309
4302 0007613 113
3236 246
8728 15
72106406 3184
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
50439188 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 309
4302 deg
Eccentricity:
0007613
Arg of perigee: 113
3236 deg
Mean anomaly: 246
8728 deg
Mean motion: 15
72106406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 318
Checksum: 293
Coasting Arc #16 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2010/293/19:25:10
205
Vector Time (MET): N/A
Weight (LBS) : 812333
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2111791
88 A = 6728189
11 meter
Y = -3913623
21 meter E =
0018329
Z = -5065414
62 I = 51
35885
XDOT = 5514
475955 Wp = 107
67109
YDOT = -5093
341563 meter/sec RA = 307
24201 deg
ZDOT = 1635
586223 TA = 178
14881
MA = 178
14202
Ha = 195
635 n
mi
Hp = 185
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6928451
05 X = -2043264
64
Y = -12839971
16 feet Y = -3936855
80 meter
Z = -16618814
37 Z = -5075507
15
XDOT = 18092
112714 XDOT = 5563
075231
YDOT = -16710
438199 feet/sec YDOT = -5031
403509 meter/sec
ZDOT = 5366
096533 ZDOT = 1662
494611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3106879
12 X = 946976
76
Y = -14208115
06 feet Y = -4330633
47 meter
Z = -16659233
26 Z = -5077734
30
XDOT = 23546
467009 XDOT = 7176
963144
YDOT = -1271
774629 feet/sec YDOT = -387
636907 meter/sec
ZDOT = 5473
990340 ZDOT = 1668
472256
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
82223057
00016717 00000-0 10270-3 0 9157
2 25544 51
6460 307
8026 0004975 122
6603 237
5039 15
71491079 3236
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
82223057 = yrday
fracday
Element set: 915
Inclination: 51
6460 deg
RA of node: 307
8026 deg
Eccentricity:
0004975
Arg of perigee: 122
6603 deg
Mean anomaly: 237
5039 deg
Mean motion: 15
71491079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 297
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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