Date:
January 11th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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
013/09:05:18
976 -3
7 4
5 4
5
N/A -2
3 -0
4 194
1
000/00:10:33
952 -1
3 0
2 186
7
Coasting Arc #1 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2011/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4576197
23 A = 6728868
14 meter
Y = 2888808
39 meter E =
0014361
Z = 3986384
65 I = 51
32349
XDOT = -751
031385 Wp = 90
53969
YDOT = 6598
204233 meter/sec RA = 248
39495 deg
ZDOT = -3907
375836 TA = 40
02309
MA = 39
91735
Ha = 193
485 n
mi
Hp = 184
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15013770
44 X = 4524189
04
Y = 9477717
80 feet Y = 2939691
21 meter
Z = 13078689
78 Z = 4008489
31
XDOT = -2464
013729 XDOT = -805
776856
YDOT = 21647
651684 feet/sec YDOT = 6589
499821 meter/sec
ZDOT = -12819
474527 ZDOT = -3911
156981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4135191
57 X = -1260406
39
Y = 17199036
13 feet Y = 5242266
21 meter
Z = 13167608
39 Z = 4013487
04
XDOT = -20000
824633 XDOT = -6096
251348
YDOT = 5047
431772 feet/sec YDOT = 1538
457204 meter/sec
ZDOT = -12834
823993 ZDOT = -3912
054353
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 11010
54056776
00016717 00000-0 10270-3 0 9000
2 25544 51
6456 249
0926 0004470 122
3255 237
8341 15
72701344 16094
Satellite: ISS
Catalog Number: 25544
Epoch time: 11010
54056776 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 249
0926 deg
Eccentricity:
0004470
Arg of perigee: 122
3255 deg
Mean anomaly: 237
8341 deg
Mean motion: 15
72701344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1609
Checksum: 288
Coasting Arc #2 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2011/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -253391
12 A = 6731845
30 meter
Y = -5976760
14 meter E =
0016721
Z = 3074709
47 I = 51
34498
XDOT = 5510
538492 Wp = 94
90573
YDOT = 2284
694995 meter/sec RA = 243
29741 deg
ZDOT = 4871
080379 TA = 300
92403
MA = 301
08829
Ha = 193
584 n
mi
Hp = 184
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -831335
69 X = -201475
26
Y = -19608793
11 feet Y = -5979303
58 meter
Z = 10087629
48 Z = 3073604
33
XDOT = 18079
194526 XDOT = 5460
918466
YDOT = 7495
718488 feet/sec YDOT = 2346
039494 meter/sec
ZDOT = 15981
234840 ZDOT = 4897
729878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18138513
25 X = 5528618
84
Y = -7501846
77 feet Y = -2286562
90 meter
Z = 10083292
45 Z = 3073387
54
XDOT = -1486
035427 XDOT = -452
943598
YDOT = 18138
112017 feet/sec YDOT = 5528
496543 meter/sec
ZDOT = 16088
466544 ZDOT = 4903
764603
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 11011
55725541
00016717 00000-0 10270-3 0 9016
2 25544 51
6451 243
8815 0004428 126
1019 234
0554 15
72677513 16254
Satellite: ISS
Catalog Number: 25544
Epoch time: 11011
55725541 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 243
8815 deg
Eccentricity:
0004428
Arg of perigee: 126
1019 deg
Mean anomaly: 234
0554 deg
Mean motion: 15
72677513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1625
Checksum: 284
Coasting Arc #3 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2011/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4906504
72 A = 6726974
87 meter
Y = -1095638
25 meter E =
0014066
Z = -4483856
85 I = 51
34357
XDOT = -1329
663071 Wp = 116
99533
YDOT = -6889
299020 meter/sec RA = 238
10237 deg
ZDOT = 3139
695407 TA = 184
53499
MA = 184
54775
Ha = 193
420 n
mi
Hp = 184
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16097456
42 X = -4872106
83
Y = -3594613
67 feet Y = -1150313
17 meter
Z = -14710816
44 Z = -4507608
97
XDOT = -4362
411651 XDOT = -1267
778763
YDOT = -22602
687075 feet/sec YDOT = -6903
822272 meter/sec
ZDOT = 10300
837948 ZDOT = 3133
385896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2338848
48 X = -712881
02
Y = -16240608
61 feet Y = -4950137
50 meter
Z = -14806413
84 Z = -4512994
94
XDOT = 18362
976122 XDOT = 5597
035122
YDOT = -12008
808745 feet/sec YDOT = -3660
284905 meter/sec
ZDOT = 10275
561820 ZDOT = 3131
991243
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 11012
51038159
00016717 00000-0 10270-3 0 9026
2 25544 51
6446 238
9959 0004341 131
4196 228
7340 15
72729603 16409
Satellite: ISS
Catalog Number: 25544
Epoch time: 11012
51038159 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 238
9959 deg
Eccentricity:
0004341
Arg of perigee: 131
4196 deg
Mean anomaly: 228
7340 deg
Mean motion: 15
72729603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1640
Checksum: 299
Coasting Arc #4 (Orbit 1653)
---------------------------------------
Vector Time (GMT): 2011/013/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2702052
34 A = 6726499
13 meter
Y = 3332797
06 meter E =
0014775
Z = -5192506
22 I = 51
34866
XDOT = -5124
100458 Wp = 101
70258
YDOT = -5648
750501 meter/sec RA = 233
59277 deg
ZDOT = -964
448128 TA = 159
08320
MA = 159
02269
Ha = 194
094 n
mi
Hp = 186
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8865001
11 X = -2713895
39
Y = 10934373
56 feet Y = 3302515
20 meter
Z = -17035781
57 Z = -5205661
26
XDOT = -16811
353209 XDOT = -5055
869149
YDOT = -18532
646001 feet/sec YDOT = -5705
669718 meter/sec
ZDOT = -3164
199895 ZDOT = -989
175482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7145257
24 X = -2177874
41
Y = -12053415
32 feet Y = -3673880
99 meter
Z = -17088800
49 Z = -5208666
39
XDOT = 22381
631630 XDOT = 6821
921321
YDOT = -8665
183161 feet/sec YDOT = -2641
147827 meter/sec
ZDOT = -3263
650520 ZDOT = -994
760679
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 11013
39995961
00016717 00000-0 10270-3 0 9037
2 25544 51
6447 234
4358 0004868 179
0565 181
0607 15
71872128 16548
Satellite: ISS
Catalog Number: 25544
Epoch time: 11013
39995961 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 234
4358 deg
Eccentricity:
0004868
Arg of perigee: 179
0565 deg
Mean anomaly: 181
0607 deg
Mean motion: 15
71872128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1654
Checksum: 329
Coasting Arc #5 (Orbit 1669)
---------------------------------------
Vector Time (GMT): 2011/014/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5175909
34 A = 6737281
47 meter
Y = 4025188
83 meter E =
0016751
Z = 1505598
39 I = 51
40357
XDOT = -1976
251579 Wp = 133
57879
YDOT = 4708
955465 meter/sec RA = 228
43238 deg
ZDOT = -5766
797835 TA = 29
78174
MA = 29
68650
Ha = 194
029 n
mi
Hp = 186
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16981329
87 X = 5123200
36
Y = 13206000
11 feet Y = 4082774
14 meter
Z = 4939627
25 Z = 1530615
09
XDOT = -6483
765023 XDOT = -2000
747246
YDOT = 15449
328954 feet/sec YDOT = 4686
719336 meter/sec
ZDOT = -18919
940402 ZDOT = -5776
457519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18136110
43 X = -5527886
46
Y = 11525666
08 feet Y = 3513023
02 meter
Z = 5040281
78 Z = 1536277
89
XDOT = -11567
443773 XDOT = -3525
756862
YDOT = -9870
730110 feet/sec YDOT = -3008
598537 meter/sec
ZDOT = -18958
913123 ZDOT = -5778
676720
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 11014
41717264
00016717 00000-0 10270-3 0 9040
2 25544 51
6444 229
2289 0004955 183
0066 177
1068 15
71850779 16701
Satellite: ISS
Catalog Number: 25544
Epoch time: 11014
41717264 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 229
2289 deg
Eccentricity:
0004955
Arg of perigee: 183
0066 deg
Mean anomaly: 177
1068 deg
Mean motion: 15
71850779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1670
Checksum: 315
Coasting Arc #6 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2011/015/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 624619
02 A = 6728149
53 meter
Y = -4675360
04 meter E =
0010038
Z = 4796249
10 I = 51
39449
XDOT = 6457
715711 Wp = 146
48594
YDOT = 3394
528723 meter/sec RA = 223
32965 deg
ZDOT = 2457
284521 TA = 279
34881
MA = 279
46229
Ha = 193
841 n
mi
Hp = 187
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2049274
99 X = 653554
23
Y = -15339107
75 feet Y = -4668213
87 meter
Z = 15735725
39 Z = 4799353
29
XDOT = 21186
731336 XDOT = 6407
340555
YDOT = 11136
905260 feet/sec YDOT = 3466
460888 meter/sec
ZDOT = 8061
957089 ZDOT = 2488
533826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13906844
49 X = 4238806
20
Y = 6759543
29 feet Y = 2060308
79 meter
Z = 15748303
37 Z = 4800082
87
XDOT = -16821
388553 XDOT = -5127
159231
YDOT = 15450
385667 feet/sec YDOT = 4709
277551 meter/sec
ZDOT = 8187
731246 ZDOT = 2495
620484
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 11015
43436663
00016717 00000-0 10270-3 0 9055
2 25544 51
6446 224
0218 0004768 187
7026 172
4064 15
71903274 16867
Satellite: ISS
Catalog Number: 25544
Epoch time: 11015
43436663 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 224
0218 deg
Eccentricity:
0004768
Arg of perigee: 187
7026 deg
Mean anomaly: 172
4064 deg
Mean motion: 15
71903274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 306
Coasting Arc #7 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2011/016/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5873946
88 A = 6734711
23 meter
Y = -1835251
91 meter E =
0003688
Z = -2741493
89 I = 51
43991
XDOT = -617
542843 Wp = 125
89694
YDOT = -5691
137523 meter/sec RA = 218
15147 deg
ZDOT = 5135
694238 TA = 202
74384
MA = 202
76018
Ha = 193
627 n
mi
Hp = 187
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19271479
25 X = -5839670
65
Y = -6021167
69 feet Y = -1900745
97 meter
Z = -8994402
52 Z = -2769946
14
XDOT = -2026
059196 XDOT = -578
805555
YDOT = -18671
711032 feet/sec YDOT = -5697
827250 meter/sec
ZDOT = 16849
390545 ZDOT = 5132
787695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11571153
92 X = 3526887
72
Y = -16482687
21 feet Y = -5023923
06 meter
Z = -9108955
41 Z = -2776409
61
XDOT = 17233
546042 XDOT = 5252
784834
YDOT = 2797
904403 feet/sec YDOT = 852
801262 meter/sec
ZDOT = 16837
778175 ZDOT = 5132
154788
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 11016
38797042
00016717 00000-0 10270-3 0 9062
2 25544 51
6444 219
1398 0004677 193
4241 166
6797 15
71936246 17012
Satellite: ISS
Catalog Number: 25544
Epoch time: 11016
38797042 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 219
1398 deg
Eccentricity:
0004677
Arg of perigee: 193
4241 deg
Mean anomaly: 166
6797 deg
Mean motion: 15
71936246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1701
Checksum: 328
Coasting Arc #8 (Orbit 1716)
---------------------------------------
Vector Time (GMT): 2011/017/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1711127
57 A = 6730660
97 meter
Y = 5037558
72 meter E =
0005999
Z = -4126330
68 I = 51
45031
XDOT = -6676
177941 Wp = 108
37280
YDOT = -790
479224 meter/sec RA = 213
06615 deg
ZDOT = -3739
855656 TA = 123
22270
MA = 123
16517
Ha = 193
456 n
mi
Hp = 187
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5613935
61 X = 1674714
10
Y = 16527423
63 feet Y = 5056490
48 meter
Z = -13537830
32 Z = -4118106
01
XDOT = -21903
470934 XDOT = -6648
675229
YDOT = -2593
435774 feet/sec YDOT = -864
982048 meter/sec
ZDOT = -12269
867638 ZDOT = -3772
221280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17466035
89 X = -5323647
74
Y = 709437
24 feet Y = 216236
47 meter
Z = -13504782
26 Z = -4116257
63
XDOT = 8804
487147 XDOT = 2683
607682
YDOT = -18892
207070 feet/sec YDOT = -5758
344715 meter/sec
ZDOT = -12400
216421 ZDOT = -3779
585965
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 11017
40513111
00016717 00000-0 10270-3 0 9070
2 25544 51
6438 213
9323 0004696 199
3834 160
7150 15
71952835 17176
Satellite: ISS
Catalog Number: 25544
Epoch time: 11017
40513111 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 213
9323 deg
Eccentricity:
0004696
Arg of perigee: 199
3834 deg
Mean anomaly: 160
7150 deg
Mean motion: 15
71952835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1717
Checksum: 300
Coasting Arc #9 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2011/018/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5562951
87 A = 6731575
55 meter
Y = -437835
03 meter E =
0010006
Z = 3754541
58 I = 51
48046
XDOT = 3288
669943 Wp = 105
60700
YDOT = 5540
222730 meter/sec RA = 207
88266 deg
ZDOT = -4219
957162 TA = 28
87253
MA = 28
81721
Ha = 193
083 n
mi
Hp = 187
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18251154
42 X = 5549195
90
Y = -1436466
65 feet Y = -375704
09 meter
Z = 12318049
82 Z = 3781532
34
XDOT = 10789
599551 XDOT = 3246
973038
YDOT = 18176
583760 feet/sec YDOT = 5576
765957 meter/sec
ZDOT = -13845
003812 ZDOT = -4204
081814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3536618
03 X = -1077961
18
Y = 17887698
96 feet Y = 5452170
64 meter
Z = 12426784
94 Z = 3787684
05
XDOT = -19135
541095 XDOT = -5832
512926
YDOT = 5805
622640 feet/sec YDOT = 1769
553781 meter/sec
ZDOT = -13781
133742 ZDOT = -4200
489565
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 11018
42227391
00016717 00000-0 10270-3 0 9086
2 25544 51
6437 208
7247 0004511 203
3381 156
7577 15
72023473 17335
Satellite: ISS
Catalog Number: 25544
Epoch time: 11018
42227391 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 208
7247 deg
Eccentricity:
0004511
Arg of perigee: 203
3381 deg
Mean anomaly: 156
7577 deg
Mean motion: 15
72023473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1733
Checksum: 295
Coasting Arc #10 (Orbit 1748)
---------------------------------------
Vector Time (GMT): 2011/019/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3945286
64 A = 6733504
43 meter
Y = -4416981
64 meter E =
0011285
Z = 3198224
42 I = 51
51311
XDOT = 5787
257109 Wp = 106
57806
YDOT = -1692
954425 meter/sec RA = 202
80219 deg
ZDOT = 4783
906558 TA = 290
79789
MA = 290
91874
Ha = 193
142 n
mi
Hp = 187
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12943853
81 X = -3911137
87
Y = -14491409
59 feet Y = -4460909
58 meter
Z = 10492862
26 Z = 3179141
27
XDOT = 18987
064006 XDOT = 5782
519208
YDOT = -5554
312419 feet/sec YDOT = -1628
264764 meter/sec
ZDOT = 15695
231490 ZDOT = 4812
008620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17319429
35 X = 5278962
07
Y = -8898764
17 feet Y = -2712343
32 meter
Z = 10416036
92 Z = 3174808
05
XDOT = -76
464310 XDOT = -23
306322
YDOT = 18421
144015 feet/sec YDOT = 5614
764696 meter/sec
ZDOT = 15808
476235 ZDOT = 4818
423557
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 11019
43940045
00016717 00000-0 10270-3 0 9097
2 25544 51
6429 203
5160 0004489 208
0061 152
0860 15
72000637 17492
Satellite: ISS
Catalog Number: 25544
Epoch time: 11019
43940045 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 203
5160 deg
Eccentricity:
0004489
Arg of perigee: 208
0061 deg
Mean anomaly: 152
0860 deg
Mean motion: 15
72000637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1749
Checksum: 283
Coasting Arc #11 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2011/020/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4360767
19 A = 6728705
95 meter
Y = 2398729
65 meter E =
0010295
Z = -4538179
42 I = 51
52579
XDOT = -5570
660421 Wp = 136
29959
YDOT = -4324
567757 meter/sec RA = 197
62481 deg
ZDOT = 3063
883744 TA = 164
31220
MA = 164
28028
Ha = 192
906 n
mi
Hp = 187
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14306978
97 X = -4365221
15
Y = 7869847
92 feet Y = 2349940
31 meter
Z = -14889040
08 Z = -4559374
05
XDOT = -18276
444950 XDOT = -5536
771612
YDOT = -14188
214425 feet/sec YDOT = -4386
672961 meter/sec
ZDOT = 10052
112020 ZDOT = 3036
904321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4269961
02 X = -1301484
12
Y = -15679294
18 feet Y = -4779048
87 meter
Z = -14974472
78 Z = -4564219
30
XDOT = 16990
909174 XDOT = 5178
829116
YDOT = -14133
530615 feet/sec YDOT = -4307
900131 meter/sec
ZDOT = 9943
451216 ZDOT = 3030
763931
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 11020
39293822
00016717 00000-0 10270-3 0 9100
2 25544 51
6423 198
6327 0004571 212
3920 147
6962 15
72051752 17643
Satellite: ISS
Catalog Number: 25544
Epoch time: 11020
39293822 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 198
6327 deg
Eccentricity:
0004571
Arg of perigee: 212
3920 deg
Mean anomaly: 147
6962 deg
Mean motion: 15
72051752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1764
Checksum: 297
Coasting Arc #12 (Orbit 1779)
---------------------------------------
Vector Time (GMT): 2011/021/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5639694
25 A = 6735818
90 meter
Y = 2989743
71 meter E =
0008678
Z = -2135551
33 I = 51
57875
XDOT = -3989
803206 Wp = 170
78111
YDOT = 3594
515915 meter/sec RA = 192
54017 deg
ZDOT = -5515
733580 TA = 33
10779
MA = 33
05350
Ha = 192
846 n
mi
Hp = 187
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18502933
89 X = 5616217
03
Y = 9808870
45 feet Y = 3052678
99 meter
Z = -7006402
01 Z = -2108211
44
XDOT = -13089
905532 XDOT = -4002
907600
YDOT = 11793
031216 feet/sec YDOT = 3549
826454 meter/sec
ZDOT = -18096
238778 ZDOT = -5535
147161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13657718
46 X = -4162872
59
Y = 15923898
75 feet Y = 4853604
34 meter
Z = -6896255
95 Z = -2101978
81
XDOT = -7476
957157 XDOT = -2278
976541
YDOT = -14267
240240 feet/sec YDOT = -4348
654825 meter/sec
ZDOT = -18174
513322 ZDOT = -5539
591661
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 11021
41002892
00016717 00000-0 10270-3 0 9110
2 25544 51
6422 193
4252 0004626 216
9093 143
1751 15
72047827 17807
Satellite: ISS
Catalog Number: 25544
Epoch time: 11021
41002892 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 193
4252 deg
Eccentricity:
0004626
Arg of perigee: 216
9093 deg
Mean anomaly: 143
1751 deg
Mean motion: 15
72047827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1780
Checksum: 281
Coasting Arc #13 (Orbit 1795)
---------------------------------------
Vector Time (GMT): 2011/022/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2476935
91 A = 6726509
42 meter
Y = -3706823
27 meter E =
0001349
Z = 5035670
20 I = 51
57844
XDOT = 7115
766298 Wp = 107
35603
YDOT = 2342
226011 meter/sec RA = 187
38091 deg
ZDOT = -1775
951795 TA = 359
76729
MA = 359
76736
Ha = 192
521 n
mi
Hp = 187
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8126430
14 X = 2493740
50
Y = -12161493
65 feet Y = -3679030
77 meter
Z = 16521227
69 Z = 5047743
60
XDOT = 23345
689953 XDOT = 7097
673245
YDOT = 7684
468541 feet/sec YDOT = 2421
697664 meter/sec
ZDOT = -5826
613500 ZDOT = -1741
428263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10269746
96 X = 3130218
87
Y = 10337392
58 feet Y = 3150837
26 meter
Z = 16569923
69 Z = 5050512
74
XDOT = -11533
609988 XDOT = -3515
444324
YDOT = 20574
657306 feet/sec YDOT = 6271
155547 meter/sec
ZDOT = -5687
495045 ZDOT = -1733
548490
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 11022
42710037
00016717 00000-0 10270-3 0 9120
2 25544 51
6425 188
2162 0004559 221
3609 138
7209 15
72099713 17966
Satellite: ISS
Catalog Number: 25544
Epoch time: 11022
42710037 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 188
2162 deg
Eccentricity:
0004559
Arg of perigee: 221
3609 deg
Mean anomaly: 138
7209 deg
Mean motion: 15
72099713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1796
Checksum: 300
Coasting Arc #14 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2011/023/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6585360
97 A = 6737130
46 meter
Y = -1022683
24 meter E =
0009191
Z = 960203
69 I = 51
64388
XDOT = 1590
697392 Wp = 60
10096
YDOT = -4636
138160 meter/sec RA = 182
28032 deg
ZDOT = 5933
903083 TA = 310
37717
MA = 310
45737
Ha = 192
404 n
mi
Hp = 187
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21605515
00 X = -6578100
09
Y = -3355259
97 feet Y = -1096284
12 meter
Z = 3150274
59 Z = 928230
38
XDOT = 5218
823464 XDOT = 1613
596166
YDOT = -15210
427035 feet/sec YDOT = -4618
221989 meter/sec
ZDOT = 19468
185967 ZDOT = 5941
686133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7337767
73 X = 2236551
60
Y = -20615734
81 feet Y = -6283675
97 meter
Z = 3021410
37 Z = 920925
88
XDOT = 12484
551334 XDOT = 3805
291246
YDOT = 7320
395368 feet/sec YDOT = 2231
256508 meter/sec
ZDOT = 19499
599298 ZDOT = 5943
477866
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 11023
44415359
00016717 00000-0 10270-3 0 9133
2 25544 51
6416 183
0068 0004542 225
3048 134
7745 15
72132533 18125
Satellite: ISS
Catalog Number: 25544
Epoch time: 11023
44415359 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 183
0068 deg
Eccentricity:
0004542
Arg of perigee: 225
3048 deg
Mean anomaly: 134
7745 deg
Mean motion: 15
72132533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 282
Coasting Arc #15 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2011/024/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -272952
41 A = 6725400
75 meter
Y = 4187344
43 meter E =
0012207
Z = -5265907
00 I = 51
63442
XDOT = -7677
366559 Wp = 108
27105
YDOT = 42
752550 meter/sec RA = 177
14572 deg
ZDOT = 429
001429 TA = 165
82647
MA = 165
79219
Ha = 192
245 n
mi
Hp = 187
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -895513
15 X = -294175
44
Y = 13738006
65 feet Y = 4184173
45 meter
Z = -17276597
76 Z = -5267284
52
XDOT = -25188
210495 XDOT = -7679
358001
YDOT = 140
264271 feet/sec YDOT = -43
111535 meter/sec
ZDOT = 1407
485002 ZDOT = 391
700624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13402690
15 X = -4085139
96
Y = -3115998
41 feet Y = -949756
32 meter
Z = -17282188
85 Z = -5267611
16
XDOT = 3917
487024 XDOT = 1194
050045
YDOT = -23875
983236 feet/sec YDOT = -7277
399690 meter/sec
ZDOT = 1257
125955 ZDOT = 383
171991
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 11024
39762432
00016717 00000-0 10270-3 0 9146
2 25544 51
6407 178
1232 0004450 228
3565 131
7217 15
72159871 18279
Satellite: ISS
Catalog Number: 25544
Epoch time: 11024
39762432 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 178
1232 deg
Eccentricity:
0004450
Arg of perigee: 228
3565 deg
Mean anomaly: 131
7217 deg
Mean motion: 15
72159871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 299
Coasting Arc #16 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2011/025/09:10:35
952
Vector Time (MET): N/A
Weight (LBS) : 828189
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6636621
46 A = 6737226
50 meter
Y = -1095257
05 meter E =
0012479
Z = 208073
36 I = 51
70579
XDOT = 965
720784 Wp = 152
68596
YDOT = 4679
489444 meter/sec RA = 172
02840 deg
ZDOT = -6038
842758 TA = 25
05626
MA = 24
99575
Ha = 191
967 n
mi
Hp = 187
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21773692
46 X = 6647364
82
Y = -3593363
03 feet Y = -1020982
28 meter
Z = 682655
37 Z = 240339
67
XDOT = 3168
375277 XDOT = 942
657253
YDOT = 15352
655655 feet/sec YDOT = 4690
159852 meter/sec
ZDOT = -19812
476239 ZDOT = -6034
207306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 220121
89 X = 67093
15
Y = 22062705
12 feet Y = 6724712
52 meter
Z = 812741
62 Z = 247723
65
XDOT = -14065
120766 XDOT = -4287
048809
YDOT = 882
837533 feet/sec YDOT = 269
088880 meter/sec
ZDOT = -19793
834183 ZDOT = -6033
160659
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 11025
41463983
00016717 00000-0 10270-3 0 9150
2 25544 51
6413 172
9152 0004364 235
3437 124
7314 15
72218868 18439
Satellite: ISS
Catalog Number: 25544
Epoch time: 11025
41463983 = yrday
fracday
Element set: 915
Inclination: 51
6413 deg
RA of node: 172
9152 deg
Eccentricity:
0004364
Arg of perigee: 235
3437 deg
Mean anomaly: 124
7314 deg
Mean motion: 15
72218868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 303
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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