Date:
March 20th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 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
083/09:34:24
264 2
0 3
9 3
9
N/A -3
4 -0
4 192
0
000/00:08:48
528 0
1 0
3 182
7
Coasting Arc #1 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2010/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6458701
24 A = 6730661
02 meter
Y = -867847
26 meter E =
0021641
Z = 1639718
98 I = 51
55359
XDOT = -783
116464 Wp = 60
43713
YDOT = 5091
660470 meter/sec RA = 340
82412 deg
ZDOT = 5733
544586 TA = 317
71612
MA = 317
88277
Ha = 192
465 n
mi
Hp = 181
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21189964
70 X = 6459960
19
Y = -2847267
91 feet Y = -795615
00 meter
Z = 5379655
45 Z = 1671098
44
XDOT = -2569
279736 XDOT = -867
846591
YDOT = 16704
922802 feet/sec YDOT = 5082
430080 meter/sec
ZDOT = 18810
841816 ZDOT = 5729
533841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21337577
39 X = 6503693
59
Y = -687913
78 feet Y = -209676
12 meter
Z = 5504252
64 Z = 1677696
21
XDOT = -4409
479655 XDOT = -1344
009399
YDOT = 14791
726546 feet/sec YDOT = 4508
518251 meter/sec
ZDOT = 18795
023215 ZDOT = 5728
723076
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 10076
56021846
00016717 00000-0 10270-3 0 9003
2 25544 51
6475 341
0180 0007593 54
9708 305
2167 15
74105643 9047
Satellite: ISS
Catalog Number: 25544
Epoch time: 10076
56021846 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 341
0180 deg
Eccentricity:
0007593
Arg of perigee: 54
9708 deg
Mean anomaly: 305
2167 deg
Mean motion: 15
74105643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 904
Checksum: 294
Coasting Arc #2 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2010/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 784184
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 358115
50 A = 6720946
90 meter
Y = -4513695
42 meter E =
0018888
Z = -4982829
43 I = 51
49354
XDOT = 7264
586460 Wp = 87
73164
YDOT = -1577
729051 meter/sec RA = 335
64787 deg
ZDOT = 1958
407007 TA = 201
22758
MA = 201
30605
Ha = 192
398 n
mi
Hp = 181
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1174919
62 X = 432767
56
Y = -14808711
99 feet Y = -4509273
83 meter
Z = -16347865
60 Z = -4980907
94
XDOT = 23833
945078 XDOT = 7272
175382
YDOT = -5176
276415 feet/sec YDOT = -1496
449507 meter/sec
ZDOT = 6425
219839 ZDOT = 1993
717002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2513929
28 X = 766245
64
Y = -14649397
32 feet Y = -4465136
30 meter
Z = -16340330
91 Z = -4980532
86
XDOT = 23078
922042 XDOT = 7034
455438
YDOT = -3336
685691 feet/sec YDOT = -1017
021798 meter/sec
ZDOT = 6565
404748 ZDOT = 2001
135367
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 10077
51247524
00016717 00000-0 10270-3 0 9013
2 25544 51
6478 336
1274 0007470 58
1714 302
0176 15
74166981 9199
Satellite: ISS
Catalog Number: 25544
Epoch time: 10077
51247524 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 336
1274 deg
Eccentricity:
0007470
Arg of perigee: 58
1714 deg
Mean anomaly: 302
0176 deg
Mean motion: 15
74166981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 306
Coasting Arc #3 (Orbit 934)
---------------------------------------
Vector Time (GMT): 2010/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 784184
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6212047
95 A = 6730175
65 meter
Y = 1855666
06 meter E =
0011196
Z = -1810384
95 I = 51
49795
XDOT = 81
625034 Wp = 101
38142
YDOT = -5214
967191 meter/sec RA = 330
53370 deg
ZDOT = -5657
153744 TA = 98
71910
MA = 98
59227
Ha = 192
334 n
mi
Hp = 181
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20380734
75 X = -6223542
09
Y = 6088143
24 feet Y = 1786134
84 meter
Z = -5939583
17 Z = -1840591
24
XDOT = 267
798669 XDOT = 167
415189
YDOT = -17109
472413 feet/sec YDOT = -5213
575163 meter/sec
ZDOT = -18560
215697 ZDOT = -5656
548428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20708002
39 X = -6311799
13
Y = 4709530
75 feet Y = 1435464
97 meter
Z = -6059491
94 Z = -1846933
14
XDOT = 1867
252438 XDOT = 569
138543
YDOT = -15536
030053 feet/sec YDOT = -4735
381960 meter/sec
ZDOT = -18557
920817 ZDOT = -5656
454265
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 10078
52818906
00016717 00000-0 10270-3 0 9024
2 25544 51
6478 330
9102 0007290 62
3949 297
7954 15
74179527 9350
Satellite: ISS
Catalog Number: 25544
Epoch time: 10078
52818906 = yrday
fracday
Element set: 902
Inclination: 51
6478 deg
RA of node: 330
9102 deg
Eccentricity:
0007290
Arg of perigee: 62
3949 deg
Mean anomaly: 297
7954 deg
Mean motion: 15
74179527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 935
Checksum: 338
Coasting Arc #4 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2010/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 784184
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 227975
31 A = 6720858
97 meter
Y = 4588144
47 meter E =
0013727
Z = 4897756
22 I = 51
44164
XDOT = -6898
938446 Wp = 60
59997
YDOT = 2668
224826 meter/sec RA = 325
34981 deg
ZDOT = -2167
239968 TA = 50
53425
MA = 50
41290
Ha = 192
192 n
mi
Hp = 180
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 747950
49 X = 152860
42
Y = 15052967
43 feet Y = 4590274
11 meter
Z = 16068754
01 Z = 4898681
03
XDOT = -22634
312487 XDOT = -6917
734169
YDOT = 8754
018457 feet/sec YDOT = 2590
971585 meter/sec
ZDOT = -7110
367349 ZDOT = -2200
800921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -98653
30 X = -30069
53
Y = 15067197
97 feet Y = 4592481
94 meter
Z = 16072520
86 Z = 4898904
36
XDOT = -21902
106397 XDOT = -6675
762030
YDOT = 7622
633808 feet/sec YDOT = 2323
378785 meter/sec
ZDOT = -7243
579460 ZDOT = -2207
843020
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 10079
54387165
00016717 00000-0 10270-3 0 9036
2 25544 51
6476 325
6928 0007306 64
3639 295
8279 15
74298090 9515
Satellite: ISS
Catalog Number: 25544
Epoch time: 10079
54387165 = yrday
fracday
Element set: 903
Inclination: 51
6476 deg
RA of node: 325
6928 deg
Eccentricity:
0007306
Arg of perigee: 64
3639 deg
Mean anomaly: 295
8279 deg
Mean motion: 15
74298090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 951
Checksum: 345
Coasting Arc #5 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2010/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 784184
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5793428
93 A = 6729601
98 meter
Y = -2771114
44 meter E =
0021445
Z = 1977201
16 I = 51
44680
XDOT = 607
520693 Wp = 67
98562
YDOT = 5281
050136 meter/sec RA = 320
23398 deg
ZDOT = 5581
196369 TA = 314
11658
MA = 314
29281
Ha = 192
196 n
mi
Hp = 180
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19007312
76 X = 5814380
54
Y = -9091582
81 feet Y = -2706211
66 meter
Z = 6486880
45 Z = 2005396
66
XDOT = 1993
178127 XDOT = 521
309417
YDOT = 17326
279973 feet/sec YDOT = 5287
361964 meter/sec
ZDOT = 18311
011709 ZDOT = 5583
938108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19256138
64 X = 5869271
06
Y = -8465907
12 feet Y = -2580408
49 meter
Z = 6598785
90 Z = 2011309
94
XDOT = 700
162403 XDOT = 213
409501
YDOT = 15974
948827 feet/sec YDOT = 4869
164403 meter/sec
ZDOT = 18322
007322 ZDOT = 5584
547832
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 10080
55952826
00016717 00000-0 10270-3 0 9042
2 25544 51
6474 320
4751 0007336 68
0008 292
1935 15
74289173 9672
Satellite: ISS
Catalog Number: 25544
Epoch time: 10080
55952826 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 320
4751 deg
Eccentricity:
0007336
Arg of perigee: 68
0008 deg
Mean anomaly: 292
1935 deg
Mean motion: 15
74289173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 318
Coasting Arc #6 (Orbit 981)
---------------------------------------
Vector Time (GMT): 2010/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 784184
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -815156
63 A = 6721070
78 meter
Y = -4626957
95 meter E =
0018228
Z = -4822306
44 I = 51
39589
XDOT = 6342
204713 Wp = 93
79686
YDOT = -3618
066558 meter/sec RA = 315
04268 deg
ZDOT = 2406
053686 TA = 199
77616
MA = 199
84692
Ha = 192
107 n
mi
Hp = 180
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2674398
41 X = -739930
75
Y = -15180308
25 feet Y = -4635653
03 meter
Z = -15821215
37 Z = -4826083
63
XDOT = 20807
758244 XDOT = 6370
503066
YDOT = -11870
297106 feet/sec YDOT = -3546
985972 meter/sec
ZDOT = 7893
876921 ZDOT = 2436
932862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2345331
02 X = -714856
89
Y = -15218925
77 feet Y = -4638728
57 meter
Z = -15836310
87 Z = -4826907
55
XDOT = 19832
934830 XDOT = 6045
078536
YDOT = -11375
387737 feet/sec YDOT = -3467
218182 meter/sec
ZDOT = 8016
423691 ZDOT = 2443
405941
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 10081
51167742
00016717 00000-0 10270-3 0 9055
2 25544 51
6472 315
5832 0007178 71
3458 288
8484 15
74351942 9827
Satellite: ISS
Catalog Number: 25544
Epoch time: 10081
51167742 = yrday
fracday
Element set: 905
Inclination: 51
6472 deg
RA of node: 315
5832 deg
Eccentricity:
0007178
Arg of perigee: 71
3458 deg
Mean anomaly: 288
8484 deg
Mean motion: 15
74351942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 982
Checksum: 326
Coasting Arc #7 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2010/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 784184
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5282657
12 A = 6728872
74 meter
Y = 3509477
28 meter E =
0011178
Z = -2253270
77 I = 51
40169
XDOT = -1217
477062 Wp = 102
51922
YDOT = -5307
248573 meter/sec RA = 309
92698 deg
ZDOT = -5436
812229 TA = 102
84457
MA = 102
71966
Ha = 192
040 n
mi
Hp = 180
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17331552
24 X = -5310562
20
Y = 11514033
06 feet Y = 3450247
39 meter
Z = -7392620
63 Z = -2279001
60
XDOT = -3994
347317 XDOT = -1131
629110
YDOT = -17412
232852 feet/sec YDOT = -5320
383248 meter/sec
ZDOT = -17837
310463 ZDOT = -5442
518047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17268406
92 X = -5263410
43
Y = 11542863
40 feet Y = 3518264
76 meter
Z = -7494726
63 Z = -2284392
68
XDOT = -3076
855795 XDOT = -937
825646
YDOT = -16146
873451 feet/sec YDOT = -4921
567028 meter/sec
ZDOT = -17860
083128 ZDOT = -5443
753337
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 10082
52727590
00016717 00000-0 10270-3 0 9061
2 25544 51
6469 310
3655 0007026 75
6346 284
5597 15
74361436 9988
Satellite: ISS
Catalog Number: 25544
Epoch time: 10082
52727590 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 310
3655 deg
Eccentricity:
0007026
Arg of perigee: 75
6346 deg
Mean anomaly: 284
5597 deg
Mean motion: 15
74361436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 333
Coasting Arc #8 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2010/083/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2646901
30 A = 6721440
34 meter
Y = -3412482
18 meter E =
0018155
Z = -5166165
80 I = 51
35363
XDOT = 5091
741041 Wp = 92
89241
YDOT = -5647
981015 meter/sec RA = 305
24450 deg
ZDOT = 1124
473973 TA = 187
88843
MA = 187
91702
Ha = 192
043 n
mi
Hp = 182
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8684059
39 X = -2583449
56
Y = -11195807
68 feet Y = -3441726
79 meter
Z = -16949362
86 Z = -5178870
08
XDOT = 16705
187142 XDOT = 5149
056912
YDOT = -18530
121441 feet/sec YDOT = -5590
721636 meter/sec
ZDOT = 3689
219073 ZDOT = 1149
348773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -778924
53 X = -237416
20
Y = -14086761
32 feet Y = -4293644
85 meter
Z = -16999892
07 Z = -5181567
10
XDOT = 23198
191267 XDOT = 7070
808698
YDOT = -5844
073721 feet/sec YDOT = -1781
273670 meter/sec
ZDOT = 3787
877309 ZDOT = 1154
545004
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 10083
41590237
00016717 00000-0 10270-3 0 9077
2 25544 51
6473 305
7986 0004124 72
8923 287
2691 15
73685381 10124
Satellite: ISS
Catalog Number: 25544
Epoch time: 10083
41590237 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 305
7986 deg
Eccentricity:
0004124
Arg of perigee: 72
8923 deg
Mean anomaly: 287
2691 deg
Mean motion: 15
73685381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 315
Coasting Arc #9 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2010/084/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3961694
98 A = 6732675
69 meter
Y = 5360514
10 meter E =
0012299
Z = -923520
28 I = 51
37513
XDOT = -3418
988819 Wp = 124
36482
YDOT = -3536
222424 meter/sec RA = 300
11053 deg
ZDOT = -5921
953294 TA = 65
75263
MA = 65
62417
Ha = 191
995 n
mi
Hp = 182
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12997686
95 X = -4016856
53
Y = 17586988
53 feet Y = 5315903
60 meter
Z = -3029922
18 Z = -942900
18
XDOT = -11217
154919 XDOT = -3350
424659
YDOT = -11601
779605 feet/sec YDOT = -3574
072521 meter/sec
ZDOT = -19428
980622 ZDOT = -5938
395794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20507660
80 X = -6250735
01
Y = 7563488
21 feet Y = 2305351
21 meter
Z = -3106759
46 Z = -946940
28
XDOT = -2350
795648 XDOT = -716
522513
YDOT = -14298
775662 feet/sec YDOT = -4358
266822 meter/sec
ZDOT = -19494
365371 ZDOT = -5941
882565
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 10084
43193120
00016717 00000-0 10270-3 0 9081
2 25544 51
6472 300
5837 0003993 78
0578 282
1032 15
73686461 10288
Satellite: ISS
Catalog Number: 25544
Epoch time: 10084
43193120 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 300
5837 deg
Eccentricity:
0003993
Arg of perigee: 78
0578 deg
Mean anomaly: 282
1032 deg
Mean motion: 15
73686461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1028
Checksum: 303
Coasting Arc #10 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2010/085/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3296184
81 A = 6720986
18 meter
Y = 2734655
64 meter E =
0007385
Z = 5174115
24 I = 51
32250
XDOT = -3913
240373 Wp = 68
04430
YDOT = 6566
581021 meter/sec RA = 294
93884 deg
ZDOT = -973
834359 TA = 31
29358
MA = 31
24964
Ha = 191
712 n
mi
Hp = 182
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10814254
63 X = 3240225
87
Y = 8971967
32 feet Y = 2771203
04 meter
Z = 16975443
69 Z = 5189991
74
XDOT = -12838
715133 XDOT = -3981
647571
YDOT = 21543
900989 feet/sec YDOT = 6522
438283 meter/sec
ZDOT = -3194
994617 ZDOT = -993
011254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4252269
06 X = 1296091
61
Y = 13312228
39 feet Y = 4057567
21 meter
Z = 17038567
21 Z = 5193355
29
XDOT = -21385
451261 XDOT = -6518
285544
YDOT = 11033
705968 feet/sec YDOT = 3363
073579 meter/sec
ZDOT = -3270
986961 ZDOT = -996
996826
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 10085
44792926
00016717 00000-0 10270-3 0 9093
2 25544 51
6470 295
3687 0003921 78
4329 281
7274 15
73800422 10445
Satellite: ISS
Catalog Number: 25544
Epoch time: 10085
44792926 = yrday
fracday
Element set: 909
Inclination: 51
6470 deg
RA of node: 295
3687 deg
Eccentricity:
0003921
Arg of perigee: 78
4329 deg
Mean anomaly: 281
7274 deg
Mean motion: 15
73800422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 322
Coasting Arc #11 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2010/086/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2845513
10 A = 6732421
76 meter
Y = -6042249
32 meter E =
0017088
Z = 788543
38 I = 51
34914
XDOT = 4079
246710 Wp = 59
44774
YDOT = 2708
428606 meter/sec RA = 289
79928 deg
ZDOT = 5946
300139 TA = 309
18721
MA = 309
33885
Ha = 191
780 n
mi
Hp = 182
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9335672
89 X = 2909036
57
Y = -19823652
61 feet Y = -6010073
84 meter
Z = 2587084
58 Z = 802521
61
XDOT = 13383
355349 XDOT = 4019
771698
YDOT = 8885
920625 feet/sec YDOT = 2753
713217 meter/sec
ZDOT = 19508
858724 ZDOT = 5965
972142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18274307
56 X = 5570008
94
Y = -12078585
35 feet Y = -3681552
81 meter
Z = 2642433
91 Z = 805413
86
XDOT = 5825
709187 XDOT = 1775
676160
YDOT = 13160
152141 feet/sec YDOT = 4011
214373 meter/sec
ZDOT = 19587
059787 ZDOT = 5970
135823
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 10086
46390133
00016717 00000-0 10270-3 0 9102
2 25544 51
6465 290
1531 0003906 81
2248 278
9358 15
73817004 10608
Satellite: ISS
Catalog Number: 25544
Epoch time: 10086
46390133 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 290
1531 deg
Eccentricity:
0003906
Arg of perigee: 81
2248 deg
Mean anomaly: 278
9358 deg
Mean motion: 15
73817004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 294
Coasting Arc #12 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2010/087/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3781443
07 A = 6720749
42 meter
Y = -2002825
80 meter E =
0018379
Z = -5198417
70 I = 51
30050
XDOT = 2599
922455 Wp = 94
02795
YDOT = -7180
787750 meter/sec RA = 284
62654 deg
ZDOT = 876
740894 TA = 184
36733
MA = 184
38339
Ha = 191
688 n
mi
Hp = 182
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12406309
30 X = -3733513
28
Y = -6570950
80 feet Y = -2044844
76 meter
Z = -17055176
19 Z = -5216671
16
XDOT = 8529
929315 XDOT = 2675
767058
YDOT = -23559
014928 feet/sec YDOT = -7151
289700 meter/sec
ZDOT = 2876
446501 ZDOT = 889
556273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7294736
10 X = -2223435
56
Y = -11891205
21 feet Y = -3624439
35 meter
Z = -17127726
16 Z = -5220530
93
XDOT = 18388
620722 XDOT = 5604
851596
YDOT = -15490
204544 feet/sec YDOT = -4721
414345 meter/sec
ZDOT = 2927
135823 ZDOT = 892
190999
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 10087
41634833
00016717 00000-0 10270-3 0 9117
2 25544 51
6458 285
2629 0003821 83
6112 276
5486 15
73865833 10750
Satellite: ISS
Catalog Number: 25544
Epoch time: 10087
41634833 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 285
2629 deg
Eccentricity:
0003821
Arg of perigee: 83
6112 deg
Mean anomaly: 276
5486 deg
Mean motion: 15
73865833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 321
Coasting Arc #13 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2010/088/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1699082
84 A = 6732323
53 meter
Y = 6465036
86 meter E =
0013132
Z = -763017
54 I = 51
33278
XDOT = -4512
525757 Wp = 127
67721
YDOT = -1878
884082 meter/sec RA = 279
48422 deg
ZDOT = -5948
971522 TA = 60
67455
MA = 60
54342
Ha = 191
664 n
mi
Hp = 182
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5574418
76 X = -1767543
16
Y = 21210750
84 feet Y = 6445653
83 meter
Z = -2503338
37 Z = -771438
72
XDOT = -14804
874532 XDOT = -4462
281359
YDOT = -6164
317854 feet/sec YDOT = -1929
065598 meter/sec
ZDOT = -19517
623104 ZDOT = -5970
771078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15251758
95 X = -4648736
13
Y = 15753931
51 feet Y = 4801798
32 meter
Z = -2536590
21 Z = -773152
70
XDOT = -8626
219119 XDOT = -2629
271587
YDOT = -11467
295969 feet/sec YDOT = -3495
231811 meter/sec
ZDOT = -19604
252802 ZDOT = -5975
376254
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 10088
43226476
00016717 00000-0 10270-3 0 9121
2 25544 51
6456 280
0472 0003736 89
4600 270
6991 15
73856218 10919
Satellite: ISS
Catalog Number: 25544
Epoch time: 10088
43226476 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 280
0472 deg
Eccentricity:
0003736
Arg of perigee: 89
4600 deg
Mean anomaly: 270
6991 deg
Mean motion: 15
73856218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 314
Coasting Arc #14 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2010/089/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4073618
67 A = 6720480
57 meter
Y = 1267303
85 meter E =
0006766
Z = 5187303
02 I = 51
28972
XDOT = -1257
179639 Wp = 75
36362
YDOT = 7554
634688 meter/sec RA = 274
31011 deg
ZDOT = -855
775380 TA = 22
83320
MA = 22
80313
Ha = 191
388 n
mi
Hp = 182
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13364890
63 X = 4033945
59
Y = 4157821
05 feet Y = 1312636
21 meter
Z = 17018710
71 Z = 5206996
25
XDOT = -4124
605114 XDOT = -1337
406256
YDOT = 24785
546877 feet/sec YDOT = 7540
127495 meter/sec
ZDOT = -2807
662008 ZDOT = -862
078462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9690547
54 X = 2953678
89
Y = 9966525
74 feet Y = 3037797
05 meter
Z = 17096957
18 Z = 5211152
55
XDOT = -14675
049674 XDOT = -4472
955141
YDOT = 19142
276996 feet/sec YDOT = 5834
566028 meter/sec
ZDOT = -2832
465726 ZDOT = -863
335553
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 10089
44814982
00016717 00000-0 10270-3 0 9139
2 25544 51
6453 274
8303 0003690 90
1037 270
0549 15
73948838 11073
Satellite: ISS
Catalog Number: 25544
Epoch time: 10089
44814982 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 274
8303 deg
Eccentricity:
0003690
Arg of perigee: 90
1037 deg
Mean anomaly: 270
0549 deg
Mean motion: 15
73948838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 316
Coasting Arc #15 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2010/090/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 498659
53 A = 6731930
69 meter
Y = -6665337
46 meter E =
0016369
Z = 744338
93 I = 51
32689
XDOT = 4779
119269 Wp = 61
11626
YDOT = 1032
325745 meter/sec RA = 269
16488 deg
ZDOT = 5951
624531 TA = 307
03362
MA = 307
18324
Ha = 191
395 n
mi
Hp = 182
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1636022
09 X = 569539
57
Y = -21867905
04 feet Y = -6659364
77 meter
Z = 2442056
87 Z = 746934
18
XDOT = 15679
525160 XDOT = 4738
308259
YDOT = 3386
895489 feet/sec YDOT = 1085
541021 meter/sec
ZDOT = 19526
327203 ZDOT = 5974
742465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11507628
26 X = 3507525
09
Y = -18665660
37 feet Y = -5689293
28 meter
Z = 2452161
46 Z = 747418
81
XDOT = 10895
924421 XDOT = 3321
077763
YDOT = 9333
772158 feet/sec YDOT = 2844
933754 meter/sec
ZDOT = 19618
168004 ZDOT = 5979
617608
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 10090
46400604
00016717 00000-0 10270-3 0 9146
2 25544 51
6444 269
6130 0003603 93
5906 266
5669 15
74003027 11233
Satellite: ISS
Catalog Number: 25544
Epoch time: 10090
46400604 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 269
6130 deg
Eccentricity:
0003603
Arg of perigee: 93
5906 deg
Mean anomaly: 266
5669 deg
Mean motion: 15
74003027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 283
Coasting Arc #16 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2010/091/09:38:48
528
Vector Time (MET): N/A
Weight (LBS) : 783814
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4245634
13 A = 6720256
10 meter
Y = -561032
39 meter E =
0018230
Z = -5194843
68 I = 51
28864
XDOT = -83
753764 Wp = 96
73188
YDOT = -7634
922756 meter/sec RA = 263
98931 deg
ZDOT = 893
587663 TA = 181
83178
MA = 181
83847
Ha = 191
340 n
mi
Hp = 182
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13929245
83 X = -4213809
17
Y = -1840657
43 feet Y = -608331
96 meter
Z = -17043450
38 Z = -5215391
82
XDOT = -274
782690 XDOT = -2
713396
YDOT = -25048
959173 feet/sec YDOT = -7635
406166 meter/sec
ZDOT = 2931
718056 ZDOT = 893
378089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11564164
55 X = -3524757
35
Y = -7803399
91 feet Y = -2378476
29 meter
Z = -17125073
97 Z = -5219722
55
XDOT = 10317
930601 XDOT = 3144
905247
YDOT = -21717
891854 feet/sec YDOT = -6619
613437 meter/sec
ZDOT = 2930
654246 ZDOT = 893
263414
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 10091
41634533
00016717 00000-0 10270-3 0 9153
2 25544 51
6435 264
7213 0003592 95
9006 264
2567 15
74039466 11389
Satellite: ISS
Catalog Number: 25544
Epoch time: 10091
41634533 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 264
7213 deg
Eccentricity:
0003592
Arg of perigee: 95
9006 deg
Mean anomaly: 264
2567 deg
Mean motion: 15
74039466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 306
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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