Date:
September 22nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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
There are no maneuvers
Coasting Arc #1 (Orbit 3846)
---------------------------------------
Vector Time (GMT): 2010/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3801557
22 A = 6734654
23 meter
Y = 4203383
86 meter E =
0014319
Z = 3621534
01 I = 51
97596
XDOT = -2275
628398 Wp = 65
81265
YDOT = -5879
205799 meter/sec RA = 102
14776 deg
ZDOT = 4427
141616 TA = 337
30798
MA = 337
37122
Ha = 196
073 n
mi
Hp = 187
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12472300
59 X = -3865870
37
Y = 13790629
46 feet Y = 4160513
29 meter
Z = 11881673
25 Z = 3602909
54
XDOT = -7465
972434 XDOT = -2231
223063
YDOT = -19288
732936 feet/sec YDOT = -5904
404570 meter/sec
ZDOT = 14524
742834 ZDOT = 4416
195040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12901150
99 X = 3932270
82
Y = -13456149
79 feet Y = -4101434
46 meter
Z = 11807041
88 Z = 3598786
37
XDOT = 6060
562851 XDOT = 1847
259557
YDOT = 18539
573868 feet/sec YDOT = 5650
862115 meter/sec
ZDOT = 14480
797172 ZDOT = 4413
746978
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 10263
55601800
00016717 00000-0 10270-3 0 9004
2 25544 51
6427 102
6711 0006798 9
0623 351
0660 15
71158318 38478
Satellite: ISS
Catalog Number: 25544
Epoch time: 10263
55601800 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 102
6711 deg
Eccentricity:
0006798
Arg of perigee: 9
0623 deg
Mean anomaly: 351
0660 deg
Mean motion: 15
71158318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3847
Checksum: 286
Coasting Arc #2 (Orbit 3861)
---------------------------------------
Vector Time (GMT): 2010/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3005582
91 A = 6731693
36 meter
Y = 4068630
24 meter E =
0010900
Z = -4448787
78 I = 51
97045
XDOT = -3352
082445 Wp = 72
90508
YDOT = 6080
023378 meter/sec RA = 97
00702 deg
ZDOT = 3305
566970 TA = 230
12217
MA = 230
21807
Ha = 196
063 n
mi
Hp = 187
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9860836
31 X = 2981474
74
Y = 13348524
40 feet Y = 4102105
22 meter
Z = -14595760
45 Z = -4434245
65
XDOT = -10997
645816 XDOT = -3435
879085
YDOT = 19947
583261 feet/sec YDOT = 6042
070180 meter/sec
ZDOT = 10845
035991 ZDOT = 3289
078418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9825147
02 X = -2994704
81
Y = -13438205
20 feet Y = -4095964
94 meter
Z = -14537418
84 Z = -4431005
26
XDOT = 10263
264334 XDOT = 3128
242969
YDOT = -19129
779682 feet/sec YDOT = -5830
756847 meter/sec
ZDOT = 10778
980529 ZDOT = 3285
433265
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 10264
51007865
00016717 00000-0 10270-3 0 9013
2 25544 51
6416 97
7912 0006732 13
6971 346
4372 15
71186451 38622
Satellite: ISS
Catalog Number: 25544
Epoch time: 10264
51007865 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 97
7912 deg
Eccentricity:
0006732
Arg of perigee: 13
6971 deg
Mean anomaly: 346
4372 deg
Mean motion: 15
71186451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3862
Checksum: 309
Coasting Arc #3 (Orbit 3877)
---------------------------------------
Vector Time (GMT): 2010/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1852734
22 A = 6738193
15 meter
Y = -6131173
34 meter E =
0006479
Z = -2101330
74 I = 51
99499
XDOT = 4242
190581 Wp = 75
24490
YDOT = 3184
870838 meter/sec RA = 91
95924 deg
ZDOT = -5564
946401 TA = 128
05958
MA = 128
00110
Ha = 196
079 n
mi
Hp = 186
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6078524
36 X = 1931364
36
Y = -20115398
11 feet Y = -6110015
54 meter
Z = -6894129
74 Z = -2092138
47
XDOT = 13917
948100 XDOT = 4233
295076
YDOT = 10449
051306 feet/sec YDOT = 3232
259218 meter/sec
ZDOT = -18257
698166 ZDOT = -5544
359726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5956480
45 X = -1815535
24
Y = 20164429
02 feet Y = 6146117
96 meter
Z = -6857322
16 Z = -2090111
79
XDOT = -12639
623469 XDOT = -3852
557233
YDOT = -9900
389852 feet/sec YDOT = -3017
638827 meter/sec
ZDOT = -18175
132366 ZDOT = -5539
780345
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 10265
52772459
00016717 00000-0 10270-3 0 9024
2 25544 51
6413 92
5871 0006855 17
3105 342
8289 15
71223149 38782
Satellite: ISS
Catalog Number: 25544
Epoch time: 10265
52772459 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 92
5871 deg
Eccentricity:
0006855
Arg of perigee: 17
3105 deg
Mean anomaly: 342
8289 deg
Mean motion: 15
71223149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3878
Checksum: 320
Coasting Arc #4 (Orbit 3893)
---------------------------------------
Vector Time (GMT): 2010/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110176
88 A = 6728701
00 meter
Y = -1348506
10 meter E =
0010773
Z = 5150571
41 I = 51
96239
XDOT = 690
246063 Wp = 34
50423
YDOT = -7537
446804 meter/sec RA = 86
83720 deg
ZDOT = -1412
500520 TA = 69
02246
MA = 68
90723
Ha = 196
247 n
mi
Hp = 186
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13484832
27 X = -4119812
90
Y = -4424232
61 feet Y = -1394521
87 meter
Z = 16898200
18 Z = 5130580
76
XDOT = 2264
586822 XDOT = 781
341612
YDOT = -24729
156181 feet/sec YDOT = -7529
218872 meter/sec
ZDOT = -4634
188058 ZDOT = -1408
925169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13692353
49 X = 4173429
34
Y = 4078806
67 feet Y = 1243220
27 meter
Z = 16818040
82 Z = 5126138
84
XDOT = -1368
603160 XDOT = -417
150243
YDOT = 23780
885055 feet/sec YDOT = 7248
413765 meter/sec
ZDOT = -4619
902333 ZDOT = -1408
146231
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 10266
54535207
00016717 00000-0 10270-3 0 9036
2 25544 51
6409 87
3816 0006727 21
4388 338
7054 15
71216431 38943
Satellite: ISS
Catalog Number: 25544
Epoch time: 10266
54535207 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 87
3816 deg
Eccentricity:
0006727
Arg of perigee: 21
4388 deg
Mean anomaly: 338
7054 deg
Mean motion: 15
71216431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3894
Checksum: 313
Coasting Arc #5 (Orbit 3909)
---------------------------------------
Vector Time (GMT): 2010/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 705881
99 A = 6739929
37 meter
Y = 6684207
41 meter E =
0019220
Z = 331904
05 I = 51
99765
XDOT = -4753
998307 Wp = 40
52376
YDOT = 192
351007 meter/sec RA = 81
76044 deg
ZDOT = 6056
800388 TA = 323
06475
MA = 323
19694
Ha = 196
161 n
mi
Hp = 186
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2315885
80 X = 629473
14
Y = 21929814
33 feet Y = 6691673
81 meter
Z = 1088924
04 Z = 335146
95
XDOT = -15597
107307 XDOT = -4785
219089
YDOT = 631
072856 feet/sec YDOT = 139
015021 meter/sec
ZDOT = 19871
392349 ZDOT = 6033
629326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3238809
69 X = -987189
19
Y = -21811960
86 feet Y = -6648285
67 meter
Z = 1101959
22 Z = 335877
17
XDOT = 14083
152605 XDOT = 4292
544914
YDOT = -1062
453199 feet/sec YDOT = -323
835735 meter/sec
ZDOT = 19778
491956 ZDOT = 6028
484348
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 10267
56295917
00016717 00000-0 10270-3 0 9041
2 25544 51
6408 82
1760 0006735 25
4371 334
7122 15
71265608 39109
Satellite: ISS
Catalog Number: 25544
Epoch time: 10267
56295917 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 82
1760 deg
Eccentricity:
0006735
Arg of perigee: 25
4371 deg
Mean anomaly: 334
7122 deg
Mean motion: 15
71265608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3910
Checksum: 304
Coasting Arc #6 (Orbit 3924)
---------------------------------------
Vector Time (GMT): 2010/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3860186
44 A = 6727917
77 meter
Y = -1630390
47 meter E =
0019528
Z = -5279794
16 I = 51
95255
XDOT = 2235
486159 Wp = 68
65066
YDOT = 7323
850209 meter/sec RA = 76
67126 deg
ZDOT = -622
070834 TA = 195
41796
MA = 195
47753
Ha = 196
190 n
mi
Hp = 186
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12664653
68 X = 3903779
56
Y = -5349050
10 feet Y = -1586980
30 meter
Z = -17322159
31 Z = -5260935
04
XDOT = 7334
272174 XDOT = 2156
445321
YDOT = 24028
379950 feet/sec YDOT = 7348
406758 meter/sec
ZDOT = -2040
914811 ZDOT = -611
403356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12425321
18 X = -3787237
90
Y = 6101707
61 feet Y = 1859800
48 meter
Z = -17246551
85 Z = -5256749
00
XDOT = -8321
663944 XDOT = -2536
443170
YDOT = -22641
203424 feet/sec YDOT = -6901
038804 meter/sec
ZDOT = -1998
122104 ZDOT = -609
027617
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 10268
51694793
00016717 00000-0 10270-3 0 9053
2 25544 51
6413 77
2968 0006776 30
3483 329
8069 15
71307408 39250
Satellite: ISS
Catalog Number: 25544
Epoch time: 10268
51694793 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 77
2968 deg
Eccentricity:
0006776
Arg of perigee: 30
3483 deg
Mean anomaly: 329
8069 deg
Mean motion: 15
71307408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3925
Checksum: 337
Coasting Arc #7 (Orbit 3940)
---------------------------------------
Vector Time (GMT): 2010/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3087564
83 A = 6738876
34 meter
Y = -5822165
25 meter E =
0015743
Z = 1390926
61 I = 51
98181
XDOT = 3695
534799 Wp = 93
96197
YDOT = -3370
063598 meter/sec RA = 71
56004 deg
ZDOT = -5847
779708 TA = 70
84151
MA = 70
67117
Ha = 196
144 n
mi
Hp = 186
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10129805
89 X = -3028987
82
Y = -19101592
04 feet Y = -5856364
63 meter
Z = 4563407
51 Z = 1376069
69
XDOT = 12124
458003 XDOT = 3761
352771
YDOT = -11056
639102 feet/sec YDOT = -3328
370347 meter/sec
ZDOT = -19185
628962 ZDOT = -5829
666352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11594027
44 X = 3533859
56
Y = 18264788
02 feet Y = 5567107
39 meter
Z = 4503833
95 Z = 1372768
59
XDOT = -10020
619369 XDOT = -3054
284784
YDOT = 11119
226840 feet/sec YDOT = 3389
140341 meter/sec
ZDOT = -19113
010390 ZDOT = -5825
645567
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 10269
53451472
00016717 00000-0 10270-3 0 9062
2 25544 51
6412 72
0910 0006826 31
6511 328
5060 15
71363052 39413
Satellite: ISS
Catalog Number: 25544
Epoch time: 10269
53451472 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 72
0910 deg
Eccentricity:
0006826
Arg of perigee: 31
6511 deg
Mean anomaly: 328
5060 deg
Mean motion: 15
71363052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 279
Coasting Arc #8 (Orbit 3956)
---------------------------------------
Vector Time (GMT): 2010/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2329890
87 A = 6729657
10 meter
Y = 4081234
34 meter E =
0010395
Z = 4807528
14 I = 51
94080
XDOT = -4612
084152 Wp = 79
81922
YDOT = -5625
020932 meter/sec RA = 66
49958 deg
ZDOT = 2537
240310 TA = 345
43955
MA = 345
46947
Ha = 196
262 n
mi
Hp = 186
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7643998
91 X = -2398709
35
Y = 13389876
45 feet Y = 4054795
59 meter
Z = 15772730
12 Z = 4796041
94
XDOT = -15131
509686 XDOT = -4561
167025
YDOT = -18454
793084 feet/sec YDOT = -5676
311190 meter/sec
ZDOT = 8324
279231 ZDOT = 2514
958399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6445090
40 X = 1964463
55
Y = -14058130
85 feet Y = -4284918
28 meter
Z = 15726674
57 Z = 4793490
41
XDOT = 15822
277742 XDOT = 4822
630256
YDOT = 16476
577616 feet/sec YDOT = 5022
060857 meter/sec
ZDOT = 8234
946756 ZDOT = 2510
011771
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 10270
55206356
00016717 00000-0 10270-3 0 9076
2 25544 51
6417 66
8859 0006739 36
6593 323
5029 15
71378559 39574
Satellite: ISS
Catalog Number: 25544
Epoch time: 10270
55206356 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 66
8859 deg
Eccentricity:
0006739
Arg of perigee: 36
6593 deg
Mean anomaly: 323
5029 deg
Mean motion: 15
71378559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3957
Checksum: 344
Coasting Arc #9 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2010/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4716271
97 A = 6735823
73 meter
Y = 3776858
13 meter E =
0011076
Z = -2975910
41 I = 51
94994
XDOT = -1382
036678 Wp = 51
70983
YDOT = 5664
863146 meter/sec RA = 61
36270 deg
ZDOT = 5018
483904 TA = 274
15926
MA = 274
28584
Ha = 196
293 n
mi
Hp = 185
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15473333
24 X = 4688144
60
Y = 12391266
84 feet Y = 3829440
94 meter
Z = -9763485
59 Z = -2953066
84
XDOT = -4534
241069 XDOT = -1469
658804
YDOT = 18585
509008 feet/sec YDOT = 5648
918653 meter/sec
ZDOT = 16464
842205 ZDOT = 5011
556803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16811141
77 X = -5124036
01
Y = -10589284
72 feet Y = -3227613
98 meter
Z = -9671905
08 Z = -2947996
67
XDOT = 1766
683356 XDOT = 538
485087
YDOT = -17759
605153 feet/sec YDOT = -5413
127651 meter/sec
ZDOT = 16437
053605 ZDOT = 5010
013939
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 10271
50599657
00016717 00000-0 10270-3 0 9082
2 25544 51
6432 62
0067 0006805 41
4727 318
6950 15
71396216 39722
Satellite: ISS
Catalog Number: 25544
Epoch time: 10271
50599657 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 62
0067 deg
Eccentricity:
0006805
Arg of perigee: 41
4727 deg
Mean anomaly: 318
6950 deg
Mean motion: 15
71396216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 318
Coasting Arc #10 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2010/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -25840
43 A = 6732989
48 meter
Y = -5515139
85 meter E =
0012955
Z = -3876963
46 I = 51
92560
XDOT = 5806
141579 Wp = 58
52019
YDOT = 2875
048755 meter/sec RA = 56
31762 deg
ZDOT = -4132
055675 TA = 168
41121
MA = 168
38136
Ha = 196
243 n
mi
Hp = 185
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -84778
33 X = 54666
65
Y = -18094290
85 feet Y = -5514978
77 meter
Z = -12719696
38 Z = -3876893
29
XDOT = 19049
020928 XDOT = 5793
633782
YDOT = 9432
574657 feet/sec YDOT = 2939
906474 meter/sec
ZDOT = -13556
613106 ZDOT = -4103
879506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2328010
97 X = 709577
74
Y = 17944320
97 feet Y = 5469429
03 meter
Z = -12719392
05 Z = -3876870
70
XDOT = -18871
588722 XDOT = -5752
060242
YDOT = -7072
794261 feet/sec YDOT = -2155
787691 meter/sec
ZDOT = -13443
650802 ZDOT = -4097
624765
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 10272
52350370
00016717 00000-0 10270-3 0 9093
2 25544 51
6435 56
8019 0006881 44
4611 315
7102 15
71433928 39888
Satellite: ISS
Catalog Number: 25544
Epoch time: 10272
52350370 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 56
8019 deg
Eccentricity:
0006881
Arg of perigee: 44
4611 deg
Mean anomaly: 315
7102 deg
Mean motion: 15
71433928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 305
Coasting Arc #11 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2010/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5144826
28 A = 6732038
13 meter
Y = -1176588
90 meter E =
0016782
Z = 4171206
76 I = 51
90431
XDOT = -1533
999675 Wp = 64
39176
YDOT = -6562
933736 meter/sec RA = 51
17003 deg
ZDOT = -3724
633157 TA = 63
61778
MA = 63
44559
Ha = 196
383 n
mi
Hp = 185
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16879351
31 X = -5151550
24
Y = -3860199
81 feet Y = -1234158
94 meter
Z = 13685061
54 Z = 4146196
64
XDOT = -5032
807333 XDOT = -1442
403950
YDOT = -21531
934828 feet/sec YDOT = -6579
575783 meter/sec
ZDOT = -12219
925056 ZDOT = -3731
862770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17340940
91 X = 5285518
79
Y = 1356442
92 feet Y = 413443
80 meter
Z = 13584785
01 Z = 4140642
47
XDOT = 8132
791122 XDOT = 2478
874734
YDOT = 19319
495000 feet/sec YDOT = 5888
582076 meter/sec
ZDOT = -12248
878056 ZDOT = -3733
458031
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 10273
54099041
00016717 00000-0 10270-3 0 9103
2 25544 51
6434 51
5963 0006849 48
7255 311
4496 15
71438063 40046
Satellite: ISS
Catalog Number: 25544
Epoch time: 10273
54099041 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 51
5963 deg
Eccentricity:
0006849
Arg of perigee: 48
7255 deg
Mean anomaly: 311
4496 deg
Mean motion: 15
71438063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 303
Coasting Arc #12 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2010/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2641513
56 A = 6736374
16 meter
Y = 5634182
11 meter E =
0020144
Z = 2552600
49 I = 51
90126
XDOT = -5580
908753 Wp = 68
20788
YDOT = 200
207919 meter/sec RA = 46
11948 deg
ZDOT = 5307
497693 TA = 320
62570
MA = 320
77197
Ha = 196
161 n
mi
Hp = 185
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8666383
06 X = 2565914
62
Y = 18484849
44 feet Y = 5663298
48 meter
Z = 8374673
52 Z = 2565249
25
XDOT = -18310
068088 XDOT = -5608
515751
YDOT = 656
850129 feet/sec YDOT = 137
644636 meter/sec
ZDOT = 17413
050174 ZDOT = 5280
318410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11500466
58 X = -3505342
21
Y = -16842910
39 feet Y = -5133719
09 meter
Z = 8425357
50 Z = 2568048
97
XDOT = 16834
470034 XDOT = 5131
146466
YDOT = -2796
407812 feet/sec YDOT = -852
345101 meter/sec
ZDOT = 17304
065228 ZDOT = 5274
279082
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 10274
55845272
00016717 00000-0 10270-3 0 9111
2 25544 51
6447 46
3914 0006798 52
1047 308
0729 15
71524925 40201
Satellite: ISS
Catalog Number: 25544
Epoch time: 10274
55845272 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 46
3914 deg
Eccentricity:
0006798
Arg of perigee: 52
1047 deg
Mean anomaly: 308
0729 deg
Mean motion: 15
71524925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 306
Coasting Arc #13 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2010/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4311829
78 A = 6728591
20 meter
Y = -1433091
97 meter E =
0017919
Z = -4977802
11 I = 51
85322
XDOT = 4375
154577 Wp = 87
79250
YDOT = 5964
616177 meter/sec RA = 40
98217 deg
ZDOT = 2079
702657 TA = 202
29867
MA = 202
37668
Ha = 196
241 n
mi
Hp = 185
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14146423
17 X = 4351715
76
Y = -4701745
31 feet Y = -1384651
71 meter
Z = -16331371
76 Z = -4956758
23
XDOT = 14354
181682 XDOT = 4298
029111
YDOT = 19568
950711 feet/sec YDOT = 6013
110642 meter/sec
ZDOT = 6823
171446 ZDOT = 2100
769624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13170365
83 X = -4014327
50
Y = 7177641
72 feet Y = 2187745
20 meter
Z = -16246978
93 Z = -4952079
18
XDOT = -17064
028080 XDOT = -5201
115759
YDOT = -15728
199573 feet/sec YDOT = -4793
955230 meter/sec
ZDOT = 6907
607543 ZDOT = 2105
438779
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 10275
51230649
00016717 00000-0 10270-3 0 9125
2 25544 51
6447 41
5123 0006923 54
7985 305
3824 15
71538592 40356
Satellite: ISS
Catalog Number: 25544
Epoch time: 10275
51230649 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 41
5123 deg
Eccentricity:
0006923
Arg of perigee: 54
7985 deg
Mean anomaly: 305
3824 deg
Mean motion: 15
71538592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 305
Coasting Arc #14 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4850196
23 A = 6738558
83 meter
Y = -4551985
40 meter E =
0012360
Z = -1073082
20 I = 51
86382
XDOT = 3982
820423 Wp = 107
59285
YDOT = -2860
675777 meter/sec RA = 35
90676 deg
ZDOT = -5926
307660 TA = 84
08961
MA = 83
94874
Ha = 196
205 n
mi
Hp = 185
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15912717
28 X = -4793721
75
Y = -14934335
30 feet Y = -4605907
51 meter
Z = -3520610
90 Z = -1096507
02
XDOT = 13066
996139 XDOT = 4043
302011
YDOT = -9385
419217 feet/sec YDOT = -2815
799716 meter/sec
ZDOT = -19443
266601 ZDOT = -5906
811976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18510830
42 X = 5642101
11
Y = 11529445
60 feet Y = 3514175
02 meter
Z = -3614510
28 Z = -1101702
73
XDOT = -10245
695187 XDOT = -3122
887893
YDOT = 10438
215100 feet/sec YDOT = 3181
567963 meter/sec
ZDOT = -19365
071921 ZDOT = -5902
473921
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 10276
52972757
00016717 00000-0 10270-3 0 9131
2 25544 51
6449 36
3056 0006970 57
8867 302
2971 15
71573322 40517
Satellite: ISS
Catalog Number: 25544
Epoch time: 10276
52972757 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 36
3056 deg
Eccentricity:
0006970
Arg of perigee: 57
8867 deg
Mean anomaly: 302
2971 deg
Mean motion: 15
71573322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 322
Coasting Arc #15 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2010/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2432444
21 A = 6726918
72 meter
Y = 3382125
97 meter E =
0009492
Z = 5274578
61 I = 51
80079
XDOT = -6480
041834 Wp = 63
47324
YDOT = -4154
421684 meter/sec RA = 30
79029 deg
ZDOT = -319
896369 TA = 29
58236
MA = 29
52869
Ha = 196
265 n
mi
Hp = 185
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7980460
02 X = -2495706
03
Y = 11096213
81 feet Y = 3354571
69 meter
Z = 17305047
92 Z = 5262607
78
XDOT = -21259
979769 XDOT = -6431
550704
YDOT = -13629
992403 feet/sec YDOT = -4226
614307 meter/sec
ZDOT = -1049
528771 ZDOT = -351
258352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5535599
06 X = 1687250
59
Y = -12563066
48 feet Y = -3829222
66 meter
Z = 17257024
38 Z = 5259941
03
XDOT = 22751
571395 XDOT = 6934
678961
YDOT = 8389
768388 feet/sec YDOT = 2557
201405 meter/sec
ZDOT = -1175
254540 ZDOT = -358
217584
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 10277
54712588
00016717 00000-0 10270-3 0 9149
2 25544 51
6460 31
1000 0006979 60
4939 299
6919 15
71621120 40679
Satellite: ISS
Catalog Number: 25544
Epoch time: 10277
54712588 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 31
1000 deg
Eccentricity:
0006979
Arg of perigee: 60
4939 deg
Mean anomaly: 299
6919 deg
Mean motion: 15
71621120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 312
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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