Date:
February 16th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26909 78 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
050/05:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
9
000/00:00:00
000 0
0 0
0 179
9
050/06:00:30
000 -0
0 0
6 0
6
N/A 0
6 -0
1 189
0
000/00:05:00
000 -0
1 0
0 180
3
050/06:37:30
000 -1
0 1
8 1
9
N/A -0
8 0
0 190
7
000/00:39:00
000 1
5 -0
6 180
5
050/07:11:31
000 0
3 0
4 0
5
N/A -0
0 -0
0 190
6
000/00:04:58
000 -0
3 -0
0 180
7
050/07:19:00
000 0
0 0
0 0
0
N/A 0
0 0
0 190
6
000/00:00:00
000 0
0 0
0 180
7
Coasting Arc #1 (Orbit 398)
---------------------------------------
Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5146179
89 A = 6726496
63 meter
Y = 4265889
00 meter E =
0017065
Z = -641523
72 I = 51
85969
XDOT = -3496
770675 Wp = 359
76082
YDOT = -3315
468993 meter/sec RA = 144
66523 deg
ZDOT = 6019
944883 TA = 353
26235
MA = 353
28527
Ha = 188
271 n
mi
Hp = 181
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16883792
28 X = -5190383
03
Y = 13995698
82 feet Y = 4208094
20 meter
Z = -2104736
63 Z = -666630
57
XDOT = -11472
344733 XDOT = -3488
679527
YDOT = -10877
522942 feet/sec YDOT = -3354
526562 meter/sec
ZDOT = 19750
475338 ZDOT = 6002
977835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21902635
21 X = -6675923
21
Y = 887638
51 feet Y = 270552
22 meter
Z = -2204226
05 Z = -671848
10
XDOT = -2546
380869 XDOT = -776
136889
YDOT = -14080
159639 feet/sec YDOT = -4291
632658 meter/sec
ZDOT = 19682
989301 ZDOT = 5999
375139
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 10044
50129195
00016717 00000-0 10270-3 0 9008
2 25544 51
6469 145
6527 0011323 321
2984 38
7368 15
75930139 3991
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044
50129195 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 145
6527 deg
Eccentricity:
0011323
Arg of perigee: 321
2984 deg
Mean anomaly: 38
7368 deg
Mean motion: 15
75930139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 399
Checksum: 313
Coasting Arc #2 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2670246
96 A = 6714410
84 meter
Y = 3179303
38 meter E =
0012630
Z = -5284161
84 I = 51
84326
XDOT = -5874
355125 Wp = 43
01058
YDOT = 4975
354715 meter/sec RA = 139
53724 deg
ZDOT = 34
103849 TA = 227
25903
MA = 227
36539
Ha = 188
410 n
mi
Hp = 181
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8760652
75 X = 2660165
73
Y = 10430785
36 feet Y = 3209107
06 meter
Z = -17336488
97 Z = -5271214
78
XDOT = -19272
818652 XDOT = -5929
719497
YDOT = 16323
342240 feet/sec YDOT = 4909
354634 meter/sec
ZDOT = 111
889270 ZDOT = 5
432361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 950475
21 X = 289704
85
Y = 13653968
32 feet Y = 4161729
54 meter
Z = -17284962
12 Z = -5268456
45
XDOT = -24202
899230 XDOT = -7377
043685
YDOT = 1644
753780 feet/sec YDOT = 501
320952 meter/sec
ZDOT = -1
728691 ZDOT = -
526905
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 10045
51585118
00016717 00000-0 10270-3 0 9012
2 25544 51
6466 140
4288 0011336 324
9595 35
0822 15
75996186 4155
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045
51585118 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 140
4288 deg
Eccentricity:
0011336
Arg of perigee: 324
9595 deg
Mean anomaly: 35
0822 deg
Mean motion: 15
75996186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 311
Coasting Arc #3 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5069352
77 A = 6726170
86 meter
Y = -4362546
36 meter E =
0001807
Z = -724989
16 I = 51
90469
XDOT = 2623
204240 Wp = 36
29706
YDOT = 4044
355211 meter/sec RA = 134
41059 deg
ZDOT = -6000
358960 TA = 151
57371
MA = 151
56385
Ha = 188
464 n
mi
Hp = 181
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16631734
80 X = 5121280
55
Y = -14312816
16 feet Y = -4305567
55 meter
Z = -2378573
38 Z = -700236
49
XDOT = 8606
313123 XDOT = 2606
932505
YDOT = 13268
881925 feet/sec YDOT = 4073
598104 meter/sec
ZDOT = -19686
217061 ZDOT = -5987
655518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21858821
58 X = 6662568
82
Y = -2029838
33 feet Y = -618694
72 meter
Z = -2280481
41 Z = -695090
73
XDOT = -720
841225 XDOT = -219
712405
YDOT = 14274
025763 feet/sec YDOT = 4350
723053 meter/sec
ZDOT = -19635
619815 ZDOT = -5984
936920
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 10046
53038223
00016717 00000-0 10270-3 0 9026
2 25544 51
6458 135
2041 0011258 329
2145 30
8358 15
76036132 4319
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
53038223 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 135
2041 deg
Eccentricity:
0011258
Arg of perigee: 329
2145 deg
Mean anomaly: 30
8358 deg
Mean motion: 15
76036132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 269
Coasting Arc #4 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2010/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1947138
49 A = 6714900
05 meter
Y = -3927694
41 meter E =
0013116
Z = 5090507
87 I = 51
88834
XDOT = 5681
542971 Wp = 355
00678
YDOT = -4938
305022 meter/sec RA = 129
25693 deg
ZDOT = -1624
565219 TA = 110
61562
MA = 110
47489
Ha = 188
576 n
mi
Hp = 180
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6388249
63 X = -1927801
84
Y = -12886136
50 feet Y = -3949360
00 meter
Z = 16701141
32 Z = 5081096
11
XDOT = 18640
232845 XDOT = 5744
233389
YDOT = -16201
788130 feet/sec YDOT = -4874
420227 meter/sec
ZDOT = -5329
938384 ZDOT = -1596
812261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1928175
76 X = 587707
97
Y = -14296725
90 feet Y = -4357642
05 meter
Z = 16663617
12 Z = 5079070
50
XDOT = 23516
903022 XDOT = 7167
952041
YDOT = -2960
292254 feet/sec YDOT = -902
297079 meter/sec
ZDOT = -5219
951354 ZDOT = -1591
041173
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 10047
54488248
00016717 00000-0 10270-3 0 9035
2 25544 51
6464 129
9782 0011443 333
0559 27
0010 15
76122332 4474
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047
54488248 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 129
9782 deg
Eccentricity:
0011443
Arg of perigee: 333
0559 deg
Mean anomaly: 27
0010 deg
Mean motion: 15
76122332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 293
Coasting Arc #5 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4815405
36 A = 6724280
27 meter
Y = 4183785
31 meter E =
0017878
Z = 2088850
62 I = 51
93741
XDOT = -1901
694764 Wp = 29
88136
YDOT = -4976
115781 meter/sec RA = 124
15749 deg
ZDOT = 5577
684727 TA = 353
40024
MA = 353
42375
Ha = 188
811 n
mi
Hp = 180
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15798574
00 X = -4871978
38
Y = 13726329
77 feet Y = 4129620
42 meter
Z = 6853184
46 Z = 2065320
07
XDOT = -6239
156051 XDOT = -1873
004548
YDOT = -16325
839178 feet/sec YDOT = -4997
220856 meter/sec
ZDOT = 18299
490574 ZDOT = 5568
516485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20779658
90 X = -6333640
03
Y = 2735399
47 feet Y = 833749
76 meter
Z = 6759924
00 Z = 2060424
84
XDOT = 3892
246612 XDOT = 1186
356767
YDOT = -15606
684395 feet/sec YDOT = -4756
917403 meter/sec
ZDOT = 18262
893743 ZDOT = 5566
530013
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 10048
55935663
00016717 00000-0 10270-3 0 9046
2 25544 51
6457 124
7531 0011413 337
7995 22
2674 15
76128355 4635
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
55935663 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 124
7531 deg
Eccentricity:
0011413
Arg of perigee: 337
7995 deg
Mean anomaly: 22
2674 deg
Mean motion: 15
76128355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 315
Coasting Arc #6 (Orbit 477)
---------------------------------------
Vector Time (GMT): 2010/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1420284
26 A = 6717023
29 meter
Y = 4755104
75 meter E =
0009456
Z = -4527845
77 I = 51
92862
XDOT = -5343
916741 Wp = 38
71765
YDOT = 4574
064691 meter/sec RA = 118
98522 deg
ZDOT = 3138
088182 TA = 262
39489
MA = 262
50230
Ha = 188
877 n
mi
Hp = 180
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4659725
25 X = 1389001
45
Y = 15600737
36 feet Y = 4770812
01 meter
Z = -14855137
02 Z = -4521022
40
XDOT = -17532
535240 XDOT = -5409
911643
YDOT = 15006
773919 feet/sec YDOT = 4513
937044 meter/sec
ZDOT = 10295
564902 ZDOT = 3111
967182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4359101
01 X = -1328653
99
Y = 15713174
24 feet Y = 4789375
51 meter
Z = -14827863
48 Z = -4519532
79
XDOT = -21751
003963 XDOT = -6629
706008
YDOT = 3550
463515 feet/sec YDOT = 1082
181279 meter/sec
ZDOT = 10192
025394 ZDOT = 3106
529340
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 10049
51039877
00016717 00000-0 10270-3 0 9056
2 25544 51
6446 119
8545 0011466 342
0208 18
0550 15
76194776 4789
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
51039877 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 119
8545 deg
Eccentricity:
0011466
Arg of perigee: 342
0208 deg
Mean anomaly: 18
0550 deg
Mean motion: 15
76194776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 478
Checksum: 319
Coasting Arc #7 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2010/050/05:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010367
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4422955
43 A = 6722441
45 meter
Y = -4211648
27 meter E =
0008862
Z = -2822054
28 I = 51
95531
XDOT = 1884
124371 Wp = 8
35019
YDOT = 5418
541579 meter/sec RA = 115
20402 deg
ZDOT = -5127
130841 TA = 203
83260
MA = 203
87366
Ha = 188
918 n
mi
Hp = 179
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14511008
63 X = 4483430
99
Y = -13817743
65 feet Y = -4161850
17 meter
Z = -9258708
28 Z = -2800420
68
XDOT = 6181
510402 XDOT = 1848
299656
YDOT = 17777
367386 feet/sec YDOT = 5439
410391 meter/sec
ZDOT = -16821
295411 ZDOT = -5118
065174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3502668
75 X = 1067613
44
Y = 19768943
16 feet Y = 6025573
88 meter
Z = -9172965
07 Z = -2795919
75
XDOT = -16853
107506 XDOT = -5136
827168
YDOT = -4812
495611 feet/sec YDOT = -1466
848662 meter/sec
ZDOT = -16785
098028 ZDOT = -5116
097879
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 10050
27121468
00016717 00000-0 10270-3 0 9060
2 25544 51
6425 115
9305 0011450 345
7763 14
3077 15
76226913 4902
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
27121468 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 115
9305 deg
Eccentricity:
0011450
Arg of perigee: 345
7763 deg
Mean anomaly: 14
3077 deg
Mean motion: 15
76226913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 286
Coasting Arc #8 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2010/050/06:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010288
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4465383
79 A = 6715337
93 meter
Y = -256172
22 meter E =
0016947
Z = -5021167
38 I = 51
93058
XDOT = -1747
517658 Wp = 34
26867
YDOT = 7244
527524 meter/sec RA = 115
16115 deg
ZDOT = -1913
106481 TA = 217
26085
MA = 217
37854
Ha = 188
985 n
mi
Hp = 180
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14650209
27 X = 4492308
14
Y = -840460
04 feet Y = -206087
38 meter
Z = -16473646
27 Z = -4999409
37
XDOT = -5733
325648 XDOT = -1819
103944
YDOT = 23768
134922 feet/sec YDOT = 7224
585381 meter/sec
ZDOT = -6276
596065 ZDOT = -1921
770104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6860186
86 X = -2090984
95
Y = 13080959
11 feet Y = 3987076
34 meter
Z = -16387262
47 Z = -4994837
60
XDOT = -16504
024110 XDOT = -5030
426549
YDOT = -16604
929722 feet/sec YDOT = -5061
182579 meter/sec
ZDOT = -6310
727789 ZDOT = -1923
509830
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 10050
27121574
00016717 00000-0 10270-3 0 9079
2 25544 51
6428 115
9310 0011243 343
4699 16
6098 15
76106772 4902
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
27121574 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 115
9310 deg
Eccentricity:
0011243
Arg of perigee: 343
4699 deg
Mean anomaly: 16
6098 deg
Mean motion: 15
76106772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 295
Coasting Arc #9 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2010/050/06:57:00
000
Vector Time (MET): N/A
Weight (LBS) : 1009667
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2916068
08 A = 6716731
15 meter
Y = -3233388
70 meter E =
0015351
Z = 5116456
19 I = 51
92959
XDOT = 4227
555472 Wp = 5
49356
YDOT = -6253
838415 meter/sec RA = 114
93948 deg
ZDOT = -1527
389421 TA = 99
18403
MA = 99
01034
Ha = 190
715 n
mi
Hp = 180
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9567152
51 X = -2904549
59
Y = -10608230
63 feet Y = -3265933
22 meter
Z = 16786273
60 Z = 5102318
24
XDOT = 13869
932651 XDOT = 4304
592506
YDOT = -20517
842569 feet/sec YDOT = -6206
132726 meter/sec
ZDOT = -5011
120147 ZDOT = -1506
664718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13012926
88 X = 3966340
11
Y = -6050967
39 feet Y = -1844334
86 meter
Z = 16730017
14 Z = 5099309
22
XDOT = 14981
144550 XDOT = 4566
252859
YDOT = 18450
116522 feet/sec YDOT = 5623
595516 meter/sec
ZDOT = -4929
060942 ZDOT = -1502
377775
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 10050
33464714
00016717 00000-0 10270-3 0 9083
2 25544 51
6429 115
6034 0012763 349
2304 10
8585 15
75447248 4911
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
33464714 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 115
6034 deg
Eccentricity:
0012763
Arg of perigee: 349
2304 deg
Mean anomaly: 10
8585 deg
Mean motion: 15
75447248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 298
Coasting Arc #10 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2010/050/07:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 1009588
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2252895
29 A = 6727893
67 meter
Y = -6294206
54 meter E =
0009335
Z = 773156
02 I = 51
96694
XDOT = 4729
397495 Wp = 63
79607
YDOT = 949
039550 meter/sec RA = 114
88419 deg
ZDOT = -5995
361493 TA = 107
81700
MA = 107
71514
Ha = 190
611 n
mi
Hp = 180
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7391388
74 X = 2319354
97
Y = -20650283
91 feet Y = -6268641
69 meter
Z = 2536601
11 Z = 784262
23
XDOT = 15516
395981 XDOT = 4747
557746
YDOT = 3113
646819 feet/sec YDOT = 1002
027699 meter/sec
ZDOT = -19669
821172 ZDOT = -5972
342264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18432849
82 X = 5618332
63
Y = 11877391
72 feet Y = 3620229
00 meter
Z = 2580467
30 Z = 786526
43
XDOT = -5718
924886 XDOT = -1743
128305
YDOT = 13170
652452 feet/sec YDOT = 4014
414867 meter/sec
ZDOT = -19578
384668 ZDOT = -5967
491647
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 10050
33464749
00016717 00000-0 10270-3 0 9092
2 25544 51
6428 115
6035 0012470 348
6862 11
4019 15
75409154 4911
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
33464749 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 115
6035 deg
Eccentricity:
0012470
Arg of perigee: 348
6862 deg
Mean anomaly: 11
4019 deg
Mean motion: 15
75409154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 297
Coasting Arc #11 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2010/051/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3859278
10 A = 6715962
58 meter
Y = -1501108
40 meter E =
0012619
Z = 5286909
78 I = 51
93983
XDOT = 2670
934507 Wp = 3
55806
YDOT = -7226
090579 meter/sec RA = 109
76337 deg
ZDOT = -89
664321 TA = 87
36108
MA = 87
21663
Ha = 190
811 n
mi
Hp = 180
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12661673
57 X = -3867888
23
Y = -4924896
34 feet Y = -1544313
09 meter
Z = 17345504
53 Z = 5268140
72
XDOT = 8762
908488 XDOT = 2751
974994
YDOT = -23707
646255 feet/sec YDOT = -7195
769486 meter/sec
ZDOT = -294
174281 ZDOT = -76
491924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7451091
61 X = 2271092
72
Y = -11473255
30 feet Y = -3497048
22 meter
Z = 17270922
25 Z = 5264177
10
XDOT = 20553
563770 XDOT = 6264
726237
YDOT = 12922
467315 feet/sec YDOT = 3938
768038 meter/sec
ZDOT = -242
124166 ZDOT = -73
799446
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 10051
34956323
00016717 00000-0 10270-3 0 9100
2 25544 51
6439 110
3808 0012543 352
7510 7
3470 15
75450446 5073
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
34956323 = yrday
fracday
Element set: 910
Inclination: 51
6439 deg
RA of node: 110
3808 deg
Eccentricity:
0012543
Arg of perigee: 352
7510 deg
Mean anomaly: 7
3470 deg
Mean motion: 15
75450446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 277
Coasting Arc #12 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2010/052/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2117257
02 A = 6727845
76 meter
Y = 6345189
17 meter E =
0022958
Z = 568165
63 I = 51
98999
XDOT = -4358
001915 Wp = 24
69667
YDOT = -2001
151010 meter/sec RA = 104
64637 deg
ZDOT = 6042
199399 TA = 341
46976
MA = 341
55323
Ha = 190
853 n
mi
Hp = 180
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6946381
31 X = -2190812
72
Y = 20817549
76 feet Y = 6321101
48 meter
Z = 1864060
46 Z = 557701
30
XDOT = -14297
906546 XDOT = -4364
652429
YDOT = -6565
456069 feet/sec YDOT = -2049
921839 meter/sec
ZDOT = 19823
488843 ZDOT = 6021
012312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19123198
25 X = -5828750
83
Y = -10773963
79 feet Y = -3283904
16 meter
Z = 1822719
29 Z = 555564
84
XDOT = 8390
433390 XDOT = 2557
404097
YDOT = -11515
439601 feet/sec YDOT = -3509
905991 meter/sec
ZDOT = 19739
285238 ZDOT = 6016
534141
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 10052
36445148
00016717 00000-0 10270-3 0 9112
2 25544 51
6447 105
1582 0012541 357
0644 3
0444 15
75480749 5238
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
36445148 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 105
1582 deg
Eccentricity:
0012541
Arg of perigee: 357
0644 deg
Mean anomaly: 3
0444 deg
Mean motion: 15
75480749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 284
Coasting Arc #13 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2010/053/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3776384
50 A = 6716164
67 meter
Y = 2015822
54 meter E =
0017555
Z = -5185520
20 I = 51
95796
XDOT = -2199
117240 Wp = 54
43517
YDOT = 7269
224580 meter/sec RA = 99
50849 deg
ZDOT = 1237
205706 TA = 227
27109
MA = 227
41899
Ha = 190
909 n
mi
Hp = 179
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12389712
91 X = 3778752
56
Y = 6613591
02 feet Y = 2058065
54 meter
Z = -17012861
56 Z = -5167169
00
XDOT = -7214
951576 XDOT = -2286
249608
YDOT = 23849
162007 feet/sec YDOT = 7244
145568 meter/sec
ZDOT = 4059
073837 ZDOT = 1226
310853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8668180
79 X = -2642061
50
Y = 11161715
33 feet Y = 3402090
83 meter
Z = -16939916
87 Z = -5163286
66
XDOT = -21429
458023 XDOT = -6531
698805
YDOT = -10611
458604 feet/sec YDOT = -3234
372583 meter/sec
ZDOT = 4016
039326 ZDOT = 1224
088787
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 10053
31588360
00016717 00000-0 10270-3 0 9123
2 25544 51
6449 100
2629 0012551
7753 359
3429 15
75552496 5387
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
31588360 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 100
2629 deg
Eccentricity:
0012551
Arg of perigee:
7753 deg
Mean anomaly: 359
3429 deg
Mean motion: 15
75552496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 538
Checksum: 304
Coasting Arc #14 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2010/054/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1748807
77 A = 6726557
64 meter
Y = -6297560
47 meter E =
0008475
Z = -1611814
08 I = 51
99746
XDOT = 4319
695436 Wp = 43
66269
YDOT = 2674
651562 meter/sec RA = 94
40991 deg
ZDOT = -5775
292211 TA = 154
02693
MA = 153
98437
Ha = 190
931 n
mi
Hp = 179
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5737558
30 X = 1826928
01
Y = -20661287
63 feet Y = -6277567
46 meter
Z = -5288103
92 Z = -1603128
80
XDOT = 14172
229120 XDOT = 4317
520836
YDOT = 8775
103551 feet/sec YDOT = 2722
944840 meter/sec
ZDOT = -18947
809090 ZDOT = -5754
312729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19513043
50 X = 5947575
66
Y = 8911291
84 feet Y = 2716161
75 meter
Z = -5253802
03 Z = -1601358
86
XDOT = -10239
205078 XDOT = -3120
909708
YDOT = 11322
180828 feet/sec YDOT = 3451
000716 meter/sec
ZDOT = -18864
401780 ZDOT = -5749
869663
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 10054
33071808
00016717 00000-0 10270-3 0 9131
2 25544 51
6453 95
0392 0012556 4
5677 355
5600 15
75580438 5546
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
33071808 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 95
0392 deg
Eccentricity:
0012556
Arg of perigee: 4
5677 deg
Mean anomaly: 355
5600 deg
Mean motion: 15
75580438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 554
Checksum: 301
Coasting Arc #15 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2010/055/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3822830
64 A = 6717449
51 meter
Y = -2655240
57 meter E =
0017956
Z = 4842804
98 I = 51
96870
XDOT = 1811
276091 Wp = 26
13087
YDOT = -7081
259806 meter/sec RA = 89
25274 deg
ZDOT = -2433
593670 TA = 87
61588
MA = 87
41031
Ha = 191
109 n
mi
Hp = 179
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12542095
27 X = -3816380
12
Y = -8711419
20 feet Y = -2697953
70 meter
Z = 15888467
77 Z = 4824249
70
XDOT = 5942
506861 XDOT = 1902
147089
YDOT = -23232
479678 feet/sec YDOT = -7060
496937 meter/sec
ZDOT = -7984
231202 ZDOT = -2424
574008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10376944
87 X = 3162892
80
Y = -11307126
92 feet Y = -3446412
29 meter
Z = 15814685
64 Z = 4820316
18
XDOT = 21354
815621 XDOT = 6508
947801
YDOT = 8392
380117 feet/sec YDOT = 2557
997460 meter/sec
ZDOT = -7948
615479 ZDOT = -2422
737998
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 10055
34552495
00016717 00000-0 10270-3 0 9140
2 25544 51
6458 89
8161 0012666 8
7498 351
3884 15
75617136 5707
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
34552495 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 89
8161 deg
Eccentricity:
0012666
Arg of perigee: 8
7498 deg
Mean anomaly: 351
3884 deg
Mean motion: 15
75617136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 331
Coasting Arc #16 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/056/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1436818
79 A = 6724489
67 meter
Y = 6012285
49 meter E =
0022298
Z = 2610332
59 I = 51
99138
XDOT = -4496
110087 Wp = 46
36520
YDOT = -3374
442008 meter/sec RA = 84
17049 deg
ZDOT = 5284
674367 TA = 343
22041
MA = 343
29406
Ha = 191
114 n
mi
Hp = 178
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4713972
40 X = -1516622
64
Y = 19725346
09 feet Y = 5995771
93 meter
Z = 8564083
29 Z = 2603158
83
XDOT = -14751
017346 XDOT = -4483
713646
YDOT = -11071
003963 feet/sec YDOT = -3424
650837 meter/sec
ZDOT = 17338
170495 ZDOT = 5262
862960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19001039
20 X = -5791516
75
Y = -7124296
85 feet Y = -2171485
68 meter
Z = 8535762
42 Z = 2601700
39
XDOT = 12272
758121 XDOT = 3740
736675
YDOT = -12012
849353 feet/sec YDOT = -3661
516483 meter/sec
ZDOT = 17251
428294 ZDOT = 5258
235344
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 10056
36030270
00016717 00000-0 10270-3 0 9156
2 25544 51
6459 84
5927 0012627 12
7024 347
4456 15
75666336 5861
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
36030270 = yrday
fracday
Element set: 915
Inclination: 51
6459 deg
RA of node: 84
5927 deg
Eccentricity:
0012627
Arg of perigee: 12
7024 deg
Mean anomaly: 347
4456 deg
Mean motion: 15
75666336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 311
Coasting Arc #17 (Orbit 600)
---------------------------------------
Vector Time (GMT): 2010/057/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4049901
84 A = 6719307
92 meter
Y = 3208026
81 meter E =
0014726
Z = -4300303
77 I = 51
96988
XDOT = -1529
954071 Wp = 51
77015
YDOT = 6660
725219 meter/sec RA = 79
00050 deg
ZDOT = 3545
071179 TA = 253
92177
MA = 254
08397
Ha = 191
149 n
mi
Hp = 178
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13287079
54 X = 4034617
61
Y = 10525022
35 feet Y = 3253229
63 meter
Z = -14108608
16 Z = -4280667
14
XDOT = -5019
534354 XDOT = -1621
542588
YDOT = 21852
773027 feet/sec YDOT = 6643
104376 meter/sec
ZDOT = 11630
810956 ZDOT = 3537
416212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11862258
51 X = -3615616
39
Y = 12198652
61 feet Y = 3718149
31 meter
Z = -14030506
05 Z = -4276498
24
XDOT = -20313
355939 XDOT = -6191
510890
YDOT = -6475
194700 feet/sec YDOT = -1973
639345 meter/sec
ZDOT = 11600
594455 ZDOT = 3535
861190
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 10057
31163175
00016717 00000-0 10270-3 0 9164
2 25544 51
6456 79
6966 0012628 16
1923 343
9643 15
75721935 6017
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
31163175 = yrday
fracday
Element set: 916
Inclination: 51
6456 deg
RA of node: 79
6966 deg
Eccentricity:
0012628
Arg of perigee: 16
1923 deg
Mean anomaly: 343
9643 deg
Mean motion: 15
75721935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 601
Checksum: 315
Coasting Arc #18 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2010/058/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1301941
36 A = 6721734
25 meter
Y = -5558910
13 meter E =
0015787
Z = -3567548
01 I = 51
97052
XDOT = 4799
507933 Wp = 37
27460
YDOT = 4000
700320 meter/sec RA = 73
92547 deg
ZDOT = -4480
308639 TA = 185
00445
MA = 185
02025
Ha = 191
151 n
mi
Hp = 178
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4271461
15 X = 1381335
31
Y = -18237894
11 feet Y = -5543907
35 meter
Z = -11704553
84 Z = -3561030
18
XDOT = 15746
417104 XDOT = 4776
178570
YDOT = 13125
657217 feet/sec YDOT = 4054
240543 meter/sec
ZDOT = -14699
175325 ZDOT = -4457
050240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17790121
02 X = 5422428
89
Y = 5914343
75 feet Y = 1802691
97 meter
Z = -11678821
64 Z = -3559704
83
XDOT = -14024
902045 XDOT = -4274
790143
YDOT = 13330
183007 feet/sec YDOT = 4063
039781 meter/sec
ZDOT = -14606
659537 ZDOT = -4452
109827
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 10058
32635473
00016717 00000-0 10270-3 0 9172
2 25544 51
6448 74
4724 0012622 19
9911 340
1745 15
75736254 6174
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
32635473 = yrday
fracday
Element set: 917
Inclination: 51
6448 deg
RA of node: 74
4724 deg
Eccentricity:
0012622
Arg of perigee: 19
9911 deg
Mean anomaly: 340
1745 deg
Mean motion: 15
75736254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 310
Coasting Arc #19 (Orbit 632)
---------------------------------------
Vector Time (GMT): 2010/059/07:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4369184
28 A = 6721884
17 meter
Y = -3746709
62 meter E =
0021255
Z = 3468965
46 I = 51
96208
XDOT = 1500
428210 Wp = 55
62704
YDOT = -6013
334898 meter/sec RA = 68
74760 deg
ZDOT = -4573
496889 TA = 83
42266
MA = 83
18075
Ha = 191
243 n
mi
Hp = 178
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14334594
08 X = -4343814
34
Y = -12292354
41 feet Y = -3795426
27 meter
Z = 11381120
27 Z = 3447802
49
XDOT = 4922
664730 XDOT = 1589
775510
YDOT = -19728
789035 feet/sec YDOT = -5996
057070 meter/sec
ZDOT = -15004
911052 ZDOT = -4565
990433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13270966
29 X = 4044990
52
Y = -13504559
58 feet Y = -4116189
76 meter
Z = 11296937
08 Z = 3443306
42
XDOT = 18344
770323 XDOT = 5591
485994
YDOT = 5413
138571 feet/sec YDOT = 1649
924637 meter/sec
ZDOT = -14975
263297 ZDOT = -4564
460253
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 10059
34104795
00016717 00000-0 10270-3 0 9184
2 25544 51
6449 69
2477 0012788 23
8747 336
3008 15
75805174 6331
Satellite: ISS
Catalog Number: 25544
Epoch time: 10059
34104795 = yrday
fracday
Element set: 918
Inclination: 51
6449 deg
RA of node: 69
2477 deg
Eccentricity:
0012788
Arg of perigee: 23
8747 deg
Mean anomaly: 336
3008 deg
Mean motion: 15
75805174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 633
Checksum: 329
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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