Date:
February 14th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23142 41 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
046/05:01:30
000 -0
3 0
4 0
4
N/A -0
1 0
0 188
8
000/00:05:00
000 0
3 0
1 181
2
046/05:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
8
000/00:00:00
000 0
0 0
0 181
1
046/06:46:30
000 -0
0 0
4 0
4
N/A -0
3 -0
0 189
0
000/00:05:00
000 0
3 -0
0 181
2
046/07:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
9
000/00:00:00
000 0
0 0
0 181
3
049/05:46:30
000 -0
5 0
8 0
8
N/A 0
6 0
1 189
5
000/00:05:00
000 -0
1 0
1 180
7
049/06:17:00
000 -0
5 2
2 2
2
N/A -1
4 -0
1 191
1
000/00:26:00
000 1
6 -0
0 180
8
049/06:41:30
000 0
3 0
5 0
5
N/A -0
3 -0
0 191
1
000/00:05:00
000 -0
1 -0
1 181
0
049/07:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 191
2
000/00:00:00
000 0
0 0
0 180
9
Coasting Arc #1 (Orbit 384)
---------------------------------------
Vector Time (GMT): 2010/043/13:54:18
929
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5142457
34 A = 6726087
21 meter
Y = -4159304
37 meter E =
0004416
Z = 1222893
03 I = 51
83366
XDOT = 3891
370733 Wp = 76
74948
YDOT = 3074
601146 meter/sec RA = 149
38945 deg
ZDOT = -5887
791139 TA = 89
87983
MA = 89
82922
Ha = 188
112 n
mi
Hp = 182
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16871579
18 X = 5182644
81
Y = -13646011
71 feet Y = -4101573
65 meter
Z = 4012116
24 Z = 1247971
94
XDOT = 12766
964347 XDOT = 3885
301704
YDOT = 10087
274102 feet/sec YDOT = 3118
082781 meter/sec
ZDOT = -19316
900063 ZDOT = -5868
902225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18903370
51 X = 5761747
33
Y = -10616925
64 feet Y = -3236038
94 meter
Z = 4111492
36 Z = 1253182
87
XDOT = 10225
419141 XDOT = 3116
707754
YDOT = 10731
564823 feet/sec YDOT = 3270
980958 meter/sec
ZDOT = -19241
801506 ZDOT = -5864
901099
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 10043
61352491
00016717 00000-0 10270-3 0 9006
2 25544 51
6459 150
2251 0011255 317
4630 42
5661 15
75900006 3859
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043
61352491 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 150
2251 deg
Eccentricity:
0011255
Arg of perigee: 317
4630 deg
Mean anomaly: 42
5661 deg
Mean motion: 15
75900006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 385
Checksum: 269
Coasting Arc #2 (Orbit 400)
---------------------------------------
Vector Time (GMT): 2010/044/13:54:18
929
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2999465
40 A = 6714678
96 meter
Y = -2926965
43 meter E =
0008685
Z = 5249352
06 I = 51
82160
XDOT = 5912
621579 Wp = 329
07466
YDOT = -4891
462100 meter/sec RA = 144
27023 deg
ZDOT = 658
822095 TA = 114
72342
MA = 114
63300
Ha = 188
275 n
mi
Hp = 181
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9840765
75 X = -2992012
25
Y = -9602904
94 feet Y = -2960465
41 meter
Z = 17222283
68 Z = 5234799
29
XDOT = 19398
364762 XDOT = 5963
678999
YDOT = -16048
104004 feet/sec YDOT = -4825
058164 meter/sec
ZDOT = 2161
489812 ZDOT = 687
668870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8374915
73 X = -2552674
31
Y = -10995807
50 feet Y = -3351522
13 meter
Z = 17164396
67 Z = 5231708
10
XDOT = 20787
884827 XDOT = 6336
147295
YDOT = -12320
467574 feet/sec YDOT = -3755
278517 meter/sec
ZDOT = 2275
800258 ZDOT = 693
663919
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
62812066
00016717 00000-0 10270-3 0 9018
2 25544 51
6465 145
0001 0011367 320
9537 39
0806 15
75956628 4012
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044
62812066 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 145
0001 deg
Eccentricity:
0011367
Arg of perigee: 320
9537 deg
Mean anomaly: 39
0806 deg
Mean motion: 15
75956628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 401
Checksum: 284
Coasting Arc #3 (Orbit 416)
---------------------------------------
Vector Time (GMT): 2010/045/13:54:18
929
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5120433
98 A = 6726708
46 meter
Y = 4342532
39 meter E =
0018387
Z = 84959
15 I = 51
88510
XDOT = -3019
163695 Wp = 8
06503
YDOT = -3681
415992 meter/sec RA = 139
13061 deg
ZDOT = 6066
700877 TA = 352
85646
MA = 352
88262
Ha = 188
593 n
mi
Hp = 181
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16799324
07 X = -5169025
09
Y = 14247153
51 feet Y = 4285000
98 meter
Z = 278737
36 Z = 59966
57
XDOT = -9905
392701 XDOT = -3007
243157
YDOT = -12078
136457 feet/sec YDOT = -3715
111147 meter/sec
ZDOT = 19903
874267 ZDOT = 6052
063319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18561075
73 X = -5657415
88
Y = 11862990
49 feet Y = 3615839
50 meter
Z = 179697
75 Z = 54771
87
XDOT = -7445
159438 XDOT = -2269
284597
YDOT = -11960
187399 feet/sec YDOT = -3645
465119 meter/sec
ZDOT = 19845
615649 ZDOT = 6048
943650
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
64269586
00016717 00000-0 10270-3 0 9025
2 25544 51
6459 139
7757 0011526 326
4931 33
5503 15
75927042 4177
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045
64269586 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 139
7757 deg
Eccentricity:
0011526
Arg of perigee: 326
4931 deg
Mean anomaly: 33
5503 deg
Mean motion: 15
75927042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 417
Checksum: 316
Coasting Arc #4 (Orbit 425)
---------------------------------------
Vector Time (GMT): 2010/046/05:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 764501
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4076277
87 A = 6726151
74 meter
Y = 5210191
11 meter E =
0017659
Z = -1149928
37 I = 51
89486
XDOT = -4437
010247 Wp = 358
56977
YDOT = -2167
501649 meter/sec RA = 135
87363 deg
ZDOT = 5922
999857 TA = 348
85948
MA = 348
89852
Ha = 188
841 n
mi
Hp = 181
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13373615
07 X = -4128650
20
Y = 17093802
85 feet Y = 5164314
86 meter
Z = -3772730
87 Z = -1169857
90
XDOT = -14557
120233 XDOT = -4441
215198
YDOT = -7111
225882 feet/sec YDOT = -2217
142116 meter/sec
ZDOT = 19432
414229 ZDOT = 5901
435337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -884617
55 X = -269631
43
Y = -21671813
58 feet Y = -6605568
78 meter
Z = -3851638
87 Z = -1173979
53
XDOT = 14205
892463 XDOT = 4329
956023
YDOT = -4009
516918 feet/sec YDOT = -1222
100757 meter/sec
ZDOT = 19346
715455 ZDOT = 5896
878871
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
21337920
00016717 00000-0 10270-3 0 9038
2 25544 51
6435 136
8348 0011995 328
6936 31
3512 15
75908872 4260
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
21337920 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 136
8348 deg
Eccentricity:
0011995
Arg of perigee: 328
6936 deg
Mean anomaly: 31
3512 deg
Mean motion: 15
75908872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 426
Checksum: 312
Coasting Arc #5 (Orbit 426)
---------------------------------------
Vector Time (GMT): 2010/046/05:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010385
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166452
81 A = 6726079
13 meter
Y = -5182157
94 meter E =
0005915
Z = 1020281
08 I = 51
89590
XDOT = 4319
086139 Wp = 62
66645
YDOT = 2296
907005 meter/sec RA = 135
71043 deg
ZDOT = -5942
401112 TA = 106
22082
MA = 106
15573
Ha = 188
807 n
mi
Hp = 181
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13669464
60 X = 4219134
75
Y = -17001830
50 feet Y = -5135271
57 meter
Z = 3347378
87 Z = 1040649
42
XDOT = 14170
230115 XDOT = 4321
947069
YDOT = 7535
784138 feet/sec YDOT = 2345
221256 meter/sec
ZDOT = -19496
066641 ZDOT = -5921
412723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4942516
93 X = 1506479
16
Y = 21235385
16 feet Y = 6472545
40 meter
Z = 3428030
26 Z = 1044863
62
XDOT = -13199
871094 XDOT = -4023
320710
YDOT = 6220
953782 feet/sec YDOT = 1896
146713 meter/sec
ZDOT = -19412
649707 ZDOT = -5916
975631
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
27679015
00016717 00000-0 10270-3 0 9049
2 25544 51
6434 136
5078 0012119 329
2439 30
8014 15
75975756 4277
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
27679015 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 136
5078 deg
Eccentricity:
0012119
Arg of perigee: 329
2439 deg
Mean anomaly: 30
8014 deg
Mean motion: 15
75975756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 427
Checksum: 310
Coasting Arc #6 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2010/046/06:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010305
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5512724
10 A = 6721636
95 meter
Y = 1565010
99 meter E =
0011808
Z = 3497904
55 I = 51
87995
XDOT = 1144
844989 Wp = 33
79726
YDOT = -6121
221022 meter/sec RA = 135
53406 deg
ZDOT = 4545
334217 TA = 7
67441
MA = 7
65636
Ha = 189
039 n
mi
Hp = 181
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18086365
16 X = -5546806
36
Y = 5134550
50 feet Y = 1503174
07 meter
Z = 11476064
79 Z = 3471041
56
XDOT = 3756
053114 XDOT = 1191
128645
YDOT = -20082
746136 feet/sec YDOT = -6108
159647 meter/sec
ZDOT = 14912
513834 ZDOT = 4551
008490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2480374
75 X = 756018
22
Y = -18701948
66 feet Y = -5700353
95 meter
Z = 11369482
58 Z = 3465418
29
XDOT = 15620
207748 XDOT = 4761
039322
YDOT = 11146
275553 feet/sec YDOT = 3397
384789 meter/sec
ZDOT = 14934
791923 ZDOT = 4552
124578
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
34020703
00016717 00000-0 10270-3 0 9052
2 25544 51
6428 136
1795 0011754 330
3629 29
6868 15
75862958 4283
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
34020703 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 136
1795 deg
Eccentricity:
0011754
Arg of perigee: 330
3629 deg
Mean anomaly: 29
6868 deg
Mean motion: 15
75862958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 319
Coasting Arc #7 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2010/046/07:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1882723
15 A = 6715278
86 meter
Y = 3852782
04 meter E =
0011521
Z = -5173717
71 I = 51
86096
XDOT = -6041
013640 Wp = 47
75328
YDOT = 4608
524018 meter/sec RA = 135
28147 deg
ZDOT = 1242
889326 TA = 234
03736
MA = 234
14427
Ha = 188
949 n
mi
Hp = 181
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6176913
24 X = 1864633
07
Y = 12640361
02 feet Y = 3873734
33 meter
Z = -16974139
47 Z = -5164615
84
XDOT = -19819
598558 XDOT = -6098
135570
YDOT = 15119
829457 feet/sec YDOT = 4540
650505 meter/sec
ZDOT = 4077
720886 ZDOT = 1213
403841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13394904
21 X = -4082766
80
Y = 4442996
92 feet Y = 1354225
46 meter
Z = -16937848
57 Z = -5162656
24
XDOT = -11865
513707 XDOT = -3616
608578
YDOT = -20789
744566 feet/sec YDOT = -6336
714144 meter/sec
ZDOT = 3960
850690 ZDOT = 1207
267290
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
34020830
00016717 00000-0 10270-3 0 9064
2 25544 51
6442 136
1803 0011561 330
7963 29
2553 15
75858410 4285
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
34020830 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 136
1803 deg
Eccentricity:
0011561
Arg of perigee: 330
7963 deg
Mean anomaly: 29
2553 deg
Mean motion: 15
75858410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 283
Coasting Arc #8 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2010/047/07:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5131978
33 A = 6725515
30 meter
Y = -4001066
05 meter E =
0004455
Z = -1710052
38 I = 51
91602
XDOT = 1828
524853 Wp = 357
13626
YDOT = 4797
457699 meter/sec RA = 130
17467 deg
ZDOT = -5732
257946 TA = 201
70222
MA = 201
72111
Ha = 189
051 n
mi
Hp = 180
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16837199
24 X = 5184644
49
Y = -13126857
10 feet Y = -3943382
86 meter
Z = -5610408
07 Z = -1684993
58
XDOT = 5999
097288 XDOT = 1802
588596
YDOT = 15739
690614 feet/sec YDOT = 4817
759947 meter/sec
ZDOT = -18806
620559 ZDOT = -5723
438488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10950367
61 X = 3337672
05
Y = 18357553
48 feet Y = 5595382
30 meter
Z = -5511081
00 Z = -1679777
49
XDOT = -15032
993575 XDOT = -4582
056442
YDOT = 3326
923308 feet/sec YDOT = 1014
046224 meter/sec
ZDOT = -18771
412714 ZDOT = -5721
526595
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
35483542
00016717 00000-0 10270-3 0 9070
2 25544 51
6437 130
9548 0011728 334
9521 25
1073 15
75908869 4442
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047
35483542 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 130
9548 deg
Eccentricity:
0011728
Arg of perigee: 334
9521 deg
Mean anomaly: 25
1073 deg
Mean motion: 15
75908869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 444
Checksum: 316
Coasting Arc #9 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2010/048/07:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1357261
62 A = 6717008
94 meter
Y = -4554260
62 meter E =
0014628
Z = 4750964
91 I = 51
90605
XDOT = 5675
545956 Wp = 9
74219
YDOT = -4476
244262 meter/sec RA = 125
00782 deg
ZDOT = -2654
220585 TA = 106
31364
MA = 106
15271
Ha = 189
215 n
mi
Hp = 180
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4452958
06 X = -1329313
12
Y = -14941799
94 feet Y = -4569281
73 meter
Z = 15587155
23 Z = 4744439
66
XDOT = 18620
557600 XDOT = 5738
071795
YDOT = -14685
840753 feet/sec YDOT = -4412
427524 meter/sec
ZDOT = -8708
072787 ZDOT = -2626
497083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15339023
91 X = 4675334
49
Y = -2934814
32 feet Y = -894531
41 meter
Z = 15561068
08 Z = 4743013
55
XDOT = 12409
788714 XDOT = 3782
503600
YDOT = 19004
598162 feet/sec YDOT = 5792
601520 meter/sec
ZDOT = -8598
177707 ZDOT = -2620
724565
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
36944030
00016717 00000-0 10270-3 0 9087
2 25544 51
6440 125
7300 0011565 339
0346 21
0343 15
75888783 4609
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
36944030 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 125
7300 deg
Eccentricity:
0011565
Arg of perigee: 339
0346 deg
Mean anomaly: 21
0343 deg
Mean motion: 15
75888783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 460
Checksum: 290
Coasting Arc #10 (Orbit 473)
---------------------------------------
Vector Time (GMT): 2010/049/05:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 764501
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3208659
36 A = 6715037
72 meter
Y = 2682467
87 meter E =
0014694
Z = -5261943
44 I = 51
91254
XDOT = -4293
501201 Wp = 47
26879
YDOT = 6356
819571 meter/sec RA = 120
32547 deg
ZDOT = 633
363146 TA = 228
66905
MA = 228
79558
Ha = 189
536 n
mi
Hp = 180
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10527097
62 X = 3203986
27
Y = 8800747
61 feet Y = 2718322
53 meter
Z = -17263593
98 Z = -5246367
52
XDOT = -14086
290031 XDOT = -4367
341906
YDOT = 20855
707254 feet/sec YDOT = 6308
394269 meter/sec
ZDOT = 2077
963078 ZDOT = 612
325833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13332259
68 X = -4063672
75
Y = 3557922
34 feet Y = 1084454
73 meter
Z = -17201647
02 Z = -5243062
01
XDOT = -8560
248800 XDOT = -2609
163834
YDOT = -22606
096224 feet/sec YDOT = -6890
338129 meter/sec
ZDOT = 1994
679378 ZDOT = 607
978274
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
25719685
00016717 00000-0 10270-3 0 9093
2 25544 51
6428 121
1595 0011944 340
0727 19
9969 15
75818372 4749
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
25719685 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 121
1595 deg
Eccentricity:
0011944
Arg of perigee: 340
0727 deg
Mean anomaly: 19
9969 deg
Mean motion: 15
75818372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 474
Checksum: 336
Coasting Arc #11 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/06:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010385
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4212841
14 A = 6717019
98 meter
Y = -810426
65 meter E =
0010628
Z = 5166396
50 I = 51
91455
XDOT = 2915
182875 Wp =
93923
YDOT = -7015
408752 meter/sec RA = 120
19433 deg
ZDOT = 1287
022761 TA = 76
86791
MA = 76
74933
Ha = 191
142 n
mi
Hp = 180
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13821657
27 X = -4228562
77
Y = -2658880
08 feet Y = -857624
70 meter
Z = 16950119
75 Z = 5145892
67
XDOT = 9564
248279 XDOT = 2987
161720
YDOT = -23016
432914 feet/sec YDOT = -6982
406908 meter/sec
ZDOT = 4222
515621 ZDOT = 1301
359818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8323719
82 X = 2537069
80
Y = -11470736
00 feet Y = -3496280
33 meter
Z = 16868678
58 Z = 5141573
23
XDOT = 15942
227700 XDOT = 4859
191003
YDOT = 17811
087247 feet/sec YDOT = 5428
819393 meter/sec
ZDOT = 4279
171085 ZDOT = 1304
291347
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
32063536
00016717 00000-0 10270-3 0 9100
2 25544 51
6429 120
8319 0013493 345
9081 14
1704 15
75273208 4756
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32063536 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 120
8319 deg
Eccentricity:
0013493
Arg of perigee: 345
9081 deg
Mean anomaly: 14
1704 deg
Mean motion: 15
75273208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 290
Coasting Arc #12 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/06:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010305
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -321516
70 A = 6722351
16 meter
Y = -5489597
78 meter E =
0016742
Z = 3871134
96 I = 51
93169
XDOT = 5623
600894 Wp = 29
65172
YDOT = -3254
843545 meter/sec RA = 120
10810 deg
ZDOT = -4126
787908 TA = 103
36304
MA = 103
17634
Ha = 191
133 n
mi
Hp = 180
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1054844
82 X = -278912
17
Y = -18010491
40 feet Y = -5492954
70 meter
Z = 12700574
03 Z = 3869676
90
XDOT = 18450
134167 XDOT = 5679
626092
YDOT = -10678
620555 feet/sec YDOT = -3191
644119 meter/sec
ZDOT = -13539
330408 ZDOT = -4099
332535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17156819
94 X = 5229398
72
Y = 5593424
67 feet Y = 1704875
84 meter
Z = 12694574
00 Z = 3869306
15
XDOT = 3499
055508 XDOT = 1066
512119
YDOT = 19910
701850 feet/sec YDOT = 6068
781924 meter/sec
ZDOT = -13430
444317 ZDOT = -4093
599428
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
32063880
00016717 00000-0 10270-3 0 9113
2 25544 51
6429 120
8321 0013106 347
2021 12
8809 15
75166501 4757
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32063880 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 120
8321 deg
Eccentricity:
0013106
Arg of perigee: 347
2021 deg
Mean anomaly: 12
8809 deg
Mean motion: 15
75166501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 274
Coasting Arc #13 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 254298
69 A = 6722513
85 meter
Y = 5530583
05 meter E =
0011620
Z = -3806624
26 I = 51
93462
XDOT = -5625
949308 Wp = 15
72893
YDOT = 3151
165171 meter/sec RA = 119
94522 deg
ZDOT = 4216
351463 TA = 298
24796
MA = 298
36521
Ha = 191
154 n
mi
Hp = 180
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 834313
30 X = 210927
47
Y = 18144957
52 feet Y = 5533184
02 meter
Z = -12488924
73 Z = -3805494
60
XDOT = -18457
838938 XDOT = -5681
250061
YDOT = 10338
468409 feet/sec YDOT = 3087
943539 meter/sec
ZDOT = 13833
174092 ZDOT = 4188
886446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18022108
34 X = -5493138
62
Y = -2292702
29 feet Y = -698815
66 meter
Z = -12484227
26 Z = -3805192
47
XDOT = -7089
830086 XDOT = -2160
980210
YDOT = -18752
060993 feet/sec YDOT = -5715
628191 meter/sec
ZDOT = 13724
245461 ZDOT = 4183
150016
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
32063851
00016717 00000-0 10270-3 0 9122
2 25544 51
6447 120
8330 0013136 347
0001 13
0823 15
75175572 4753
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32063851 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 120
8330 deg
Eccentricity:
0013136
Arg of perigee: 347
0001 deg
Mean anomaly: 13
0823 deg
Mean motion: 15
75175572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 269
Coasting Arc #14 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2010/050/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4695542
15 A = 6721951
75 meter
Y = -2731374
71 meter E =
0015673
Z = -3974461
28 I = 51
94693
XDOT = 415
107647 Wp = 16
65822
YDOT = 6553
491477 meter/sec RA = 114
87343 deg
ZDOT = -4002
538218 TA = 211
92125
MA = 212
01630
Ha = 191
218 n
mi
Hp = 180
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15405322
01 X = 4745042
90
Y = -8961203
12 feet Y = -2678589
81 meter
Z = -13039571
13 Z = -3951530
20
XDOT = 1361
901729 XDOT = 361
237895
YDOT = 21500
956289 feet/sec YDOT = 6557
832042 meter/sec
ZDOT = -13131
687066 ZDOT = -4000
652843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6391940
55 X = 1948263
48
Y = 16707299
03 feet Y = 5092384
74 meter
Z = -12948620
70 Z = -3946739
59
XDOT = -20238
342391 XDOT = -6168
646761
YDOT = -2456
244738 feet/sec YDOT = -748
663396 meter/sec
ZDOT = -13123
958632 ZDOT = -4000
182591
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
33569496
00016717 00000-0 10270-3 0 9132
2 25544 51
6446 115
6111 0013139 350
8429 9
2493 15
75217294 4916
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
33569496 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 115
6111 deg
Eccentricity:
0013139
Arg of perigee: 350
8429 deg
Mean anomaly: 9
2493 deg
Mean motion: 15
75217294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 302
Coasting Arc #15 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2010/051/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -499324
20 A = 6724325
62 meter
Y = -5920555
66 meter E =
0016929
Z = 3152488
14 I = 51
96711
XDOT = 5131
279004 Wp = 44
39670
YDOT = -3038
620711 meter/sec RA = 109
70020 deg
ZDOT = -4866
499296 TA = 99
08719
MA = 98
89559
Ha = 191
309 n
mi
Hp = 180
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1638202
75 X = -448396
46
Y = -19424395
22 feet Y = -5925854
53 meter
Z = 10342808
84 Z = 3150186
36
XDOT = 16834
904868 XDOT = 5188
516395
YDOT = -9969
228054 feet/sec YDOT = -2980
919853 meter/sec
ZDOT = -15966
205041 ZDOT = -4841
432628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19468965
49 X = 5934140
68
Y = 1069359
33 feet Y = 325940
73 meter
Z = 10333459
54 Z = 3149638
47
XDOT = 7549
379602 XDOT = 2301
050903
YDOT = 16750
133202 feet/sec YDOT = 5105
440600 meter/sec
ZDOT = -15866
776262 ZDOT = -4836
193405
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
35072853
00016717 00000-0 10270-3 0 9142
2 25544 51
6449 110
3891 0013101 354
9924 5
1106 15
75244650 5070
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
35072853 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 110
3891 deg
Eccentricity:
0013101
Arg of perigee: 354
9924 deg
Mean anomaly: 5
1106 deg
Mean motion: 15
75244650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 276
Coasting Arc #16 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2010/052/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4293648
12 A = 6719689
73 meter
Y = 2537732
67 meter E =
0012571
Z = 4491248
24 I = 51
96232
XDOT = -772
313839 Wp = 39
37051
YDOT = -6970
711934 meter/sec RA = 104
62608 deg
ZDOT = 3205
055716 TA = 18
80016
MA = 18
75378
Ha = 191
460 n
mi
Hp = 180
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14086772
03 X = -4343523
85
Y = 8325894
60 feet Y = 2489439
77 meter
Z = 14735066
42 Z = 4470268
70
XDOT = -2533
838055 XDOT = -709
878135
YDOT = -22869
789811 feet/sec YDOT = -6978
999247 meter/sec
ZDOT = 10515
274658 ZDOT = 3201
455641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6495564
90 X = -1979848
18
Y = -15100035
56 feet Y = -4602490
84 meter
Z = 14651839
89 Z = 4465880
80
XDOT = 21913
621938 XDOT = 6679
271967
YDOT = 747
577750 feet/sec YDOT = 227
861698 meter/sec
ZDOT = 10500
743612 ZDOT = 3200
626653
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
36573680
00016717 00000-0 10270-3 0 9159
2 25544 51
6459 105
1671 0013166 358
6749 1
4378 15
75325918 5231
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
36573680 = yrday
fracday
Element set: 915
Inclination: 51
6459 deg
RA of node: 105
1671 deg
Eccentricity:
0013166
Arg of perigee: 358
6749 deg
Mean anomaly: 1
4378 deg
Mean motion: 15
75325918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 314
Coasting Arc #17 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2010/053/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 878195
81 A = 6725934
91 meter
Y = 6206619
67 meter E =
0017753
Z = -2413679
95 I = 51
98994
XDOT = -4746
023867 Wp = 15
08970
YDOT = 2764
837876 meter/sec RA = 99
46085 deg
ZDOT = 5408
359657 TA = 317
77684
MA = 317
91342
Ha = 191
604 n
mi
Hp = 179
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2881219
84 X = 820452
10
Y = 20362925
42 feet Y = 6216117
30 meter
Z = -7918897
49 Z = -2409554
01
XDOT = -15570
944445 XDOT = -4802
860561
YDOT = 9070
990406 feet/sec YDOT = 2711
447249 meter/sec
ZDOT = 17743
962129 ZDOT = 5385
165685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20559467
62 X = -6266525
73
Y = 721695
61 feet Y = 219972
82 meter
Z = -7902312
54 Z = -2408624
86
XDOT = -7281
117542 XDOT = -2219
284627
YDOT = -15060
086795 feet/sec YDOT = -4590
314455 meter/sec
ZDOT = 17651
938122 ZDOT = 5380
310739
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
31728834
00016717 00000-0 10270-3 0 9169
2 25544 51
6463 100
2722 0013383 2
3814 357
7412 15
75303568 5385
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
31728834 = yrday
fracday
Element set: 916
Inclination: 51
6463 deg
RA of node: 100
2722 deg
Eccentricity:
0013383
Arg of perigee: 2
3814 deg
Mean anomaly: 357
7412 deg
Mean motion: 15
75303568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 538
Checksum: 288
Coasting Arc #18 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2010/054/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4025309
92 A = 6717955
52 meter
Y = -2224395
48 meter E =
0021335
Z = -4914021
18 I = 51
96759
XDOT = 1223
145073 Wp = 38
50759
YDOT = 7244
420435 meter/sec RA = 94
37869 deg
ZDOT = -2266
275764 TA = 209
45600
MA = 209
57639
Ha = 191
588 n
mi
Hp = 179
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13206397
39 X = 4073755
38
Y = -7297885
44 feet Y = -2179111
17 meter
Z = -16122116
74 Z = -4894348
88
XDOT = 4012
943154 XDOT = 1153
054752
YDOT = 23767
783579 feet/sec YDOT = 7257
706489 meter/sec
ZDOT = -7435
287938 ZDOT = -2260
504016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6066193
26 X = 1848975
70
Y = 13906128
48 feet Y = 4238587
96 meter
Z = -16044051
93 Z = -4890227
03
XDOT = -23022
925974 XDOT = -7017
387837
YDOT = 1449
381124 feet/sec YDOT = 441
771366 meter/sec
ZDOT = -7412
141218 ZDOT = -2259
220643
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
33225277
00016717 00000-0 10270-3 0 9176
2 25544 51
6467 95
0505 0013254 6
1858 353
9467 15
75352304 5544
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
33225277 = yrday
fracday
Element set: 917
Inclination: 51
6467 deg
RA of node: 95
0505 deg
Eccentricity:
0013254
Arg of perigee: 6
1858 deg
Mean anomaly: 353
9467 deg
Mean motion: 15
75352304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 554
Checksum: 304
Coasting Arc #19 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2010/055/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1269400
84 A = 6727224
39 meter
Y = -6432032
87 meter E =
0016172
Z = 1513290
21 I = 52
00013
XDOT = 4508
628346 Wp = 66
68520
YDOT = -2269
576367 meter/sec RA = 89
22518 deg
ZDOT = -5809
562200 TA = 96
73132
MA = 96
54726
Ha = 191
650 n
mi
Hp = 179
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4164700
91 X = -1204733
49
Y = -21102470
06 feet Y = -6445866
50 meter
Z = 4964862
91 Z = 1507280
62
XDOT = 14792
087750 XDOT = 4561
893271
YDOT = -7446
116689 feet/sec YDOT = -2218
860347 meter/sec
ZDOT = -19060
243437 ZDOT = -5787
530384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21352835
19 X = 6508344
16
Y = -2636998
11 feet Y = -803757
02 meter
Z = 4940800
59 Z = 1505956
02
XDOT = 6142
708287 XDOT = 1872
297486
YDOT = 13852
146518 feet/sec YDOT = 4222
134259 meter/sec
ZDOT = -18972
798866 ZDOT = -5782
909094
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
34719378
00016717 00000-0 10270-3 0 9189
2 25544 51
6464 89
8285 0013258 10
7221 349
4223 15
75393811 5702
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
34719378 = yrday
fracday
Element set: 918
Inclination: 51
6464 deg
RA of node: 89
8285 deg
Eccentricity:
0013258
Arg of perigee: 10
7221 deg
Mean anomaly: 349
4223 deg
Mean motion: 15
75393811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 315
Coasting Arc #20 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/056/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3898075
17 A = 6716347
89 meter
Y = 1726516
03 meter E =
0012482
Z = 5182377
12 I = 51
96320
XDOT = -1706
273144 Wp = 31
39194
YDOT = -7422
957546 meter/sec RA = 84
12693 deg
ZDOT = 1198
693312 TA = 47
27623
MA = 47
17121
Ha = 191
771 n
mi
Hp = 178
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12788960
53 X = -3942266
06
Y = 5664422
69 feet Y = 1682678
39 meter
Z = 17002549
62 Z = 5163333
42
XDOT = -5598
009004 XDOT = -1628
964385
YDOT = -24353
535255 feet/sec YDOT = -7441
605841 meter/sec
ZDOT = 3932
720839 ZDOT = 1190
592273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4933181
44 X = -1503633
70
Y = -13186050
71 feet Y = -4019108
26 meter
Z = 16926951
20 Z = 5159334
73
XDOT = 23668
779976 XDOT = 7214
244137
YDOT = -3886
841522 feet/sec YDOT = -1184
709296 meter/sec
ZDOT = 3900
322972 ZDOT = 1188
818442
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
36210893
00016717 00000-0 10270-3 0 9191
2 25544 51
6470 84
6057 0013314 14
2502 345
9035 15
75474021 5865
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
36210893 = yrday
fracday
Element set: 919
Inclination: 51
6470 deg
RA of node: 84
6057 deg
Eccentricity:
0013314
Arg of perigee: 14
2502 deg
Mean anomaly: 345
9035 deg
Mean motion: 15
75474021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 290
Coasting Arc #21 (Orbit 600)
---------------------------------------
Vector Time (GMT): 2010/057/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1710608
48 A = 6727940
79 meter
Y = 6468081
98 meter E =
0024091
Z = -568014
59 I = 51
99742
XDOT = -4478
724968 Wp = 28
07813
YDOT = 1704
342748 meter/sec RA = 78
98980 deg
ZDOT = 6043
051390 TA = 325
75894
MA = 325
91404
Ha = 191
899 n
mi
Hp = 178
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5612232
55 X = 1640913
33
Y = 21220741
40 feet Y = 6486821
31 meter
Z = -1863564
92 Z = -559874
18
XDOT = -14693
979553 XDOT = -4526
805558
YDOT = 5591
675682 feet/sec YDOT = 1653
990344 meter/sec
ZDOT = 19826
284087 ZDOT = 6021
177545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21423336
83 X = -6529833
07
Y = 4793519
87 feet Y = 1461064
86 meter
Z = -1831037
97 Z = -558100
37
XDOT = -4662
355037 XDOT = -1421
085815
YDOT = -13454
338200 feet/sec YDOT = -4100
882283 meter/sec
ZDOT = 19739
437152 ZDOT = 6016
580444
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
31357247
00016717 00000-0 10270-3 0 9204
2 25544 51
6468 79
7104 0013544 17
9048 342
2591 15
75443780 6013
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
31357247 = yrday
fracday
Element set: 920
Inclination: 51
6468 deg
RA of node: 79
7104 deg
Eccentricity:
0013544
Arg of perigee: 17
9048 deg
Mean anomaly: 342
2591 deg
Mean motion: 15
75443780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 601
Checksum: 301
Coasting Arc #22 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2010/058/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3965740
61 A = 6715840
69 meter
Y = -1216102
64 meter E =
0023623
Z = -5298846
39 I = 51
94925
XDOT = 2175
029836 Wp = 57
69039
YDOT = 7374
346666 meter/sec RA = 73
87276 deg
ZDOT = -52
450661 TA = 211
74189
MA = 211
88452
Ha = 191
868 n
mi
Hp = 178
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13010960
00 X = 4004784
62
Y = -3989838
07 feet Y = -1171537
41 meter
Z = -17384666
65 Z = -5279486
49
XDOT = 7135
924660 XDOT = 2092
661717
YDOT = 24194
050742 feet/sec YDOT = 7398
208593 meter/sec
ZDOT = -172
082222 ZDOT = -42
085213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3704773
96 X = 1129215
10
Y = 13196422
77 feet Y = 4022269
66 meter
Z = -17307790
11 Z = -5275414
43
XDOT = -23380
907613 XDOT = -7126
500641
YDOT = 6340
015213 feet/sec YDOT = 1932
436637 meter/sec
ZDOT = -130
688790 ZDOT = -39
833943
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
32844198
00016717 00000-0 10270-3 0 9213
2 25544 51
6459 74
4877 0013427 21
5646 338
6081 15
75497316 6171
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
32844198 = yrday
fracday
Element set: 921
Inclination: 51
6459 deg
RA of node: 74
4877 deg
Eccentricity:
0013427
Arg of perigee: 21
5646 deg
Mean anomaly: 338
6081 deg
Mean motion: 15
75497316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 328
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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