Date:
March 4th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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
There are no maneuvers
Coasting Arc #1 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2010/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2334582
12 A = 6731191
76 meter
Y = -5914448
52 meter E =
0005984
Z = -2219041
34 I = 51
92461
XDOT = 5376
637737 Wp = 56
36566
YDOT = -61
683272 meter/sec RA = 52
59302 deg
ZDOT = -5499
509581 TA = 148
37862
MA = 148
34266
Ha = 192
468 n
mi
Hp = 183
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7659390
15 X = -2257492
59
Y = -19404358
67 feet Y = -5940124
38 meter
Z = -7280319
37 Z = -2230194
85
XDOT = 17639
887588 XDOT = 5403
643270
YDOT = -202
372939 feet/sec YDOT = -1
408026 meter/sec
ZDOT = -18043
010435 ZDOT = -5473
324514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -660027
86 X = -201176
49
Y = -20835317
22 feet Y = -6350604
69 meter
Z = -7324777
30 Z = -2232592
12
XDOT = 15264
498189 XDOT = 4652
619048
YDOT = 5814
604550 feet/sec YDOT = 1772
291467 meter/sec
ZDOT = -17938
994350 ZDOT = -5467
805478
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 10062
52737403
00016717 00000-0 10270-3 0 9007
2 25544 51
6434 53
0429 0007756 6
5608 353
5655 15
73583780 6834
Satellite: ISS
Catalog Number: 25544
Epoch time: 10062
52737403 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 53
0429 deg
Eccentricity:
0007756
Arg of perigee: 6
5608 deg
Mean anomaly: 353
5655 deg
Mean motion: 15
73583780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 683
Checksum: 305
Coasting Arc #2 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2010/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4620269
52 A = 6723154
28 meter
Y = 590969
84 meter E =
0013420
Z = 4846222
21 I = 51
87837
XDOT = -3379
481698 Wp = 32
42543
YDOT = -6484
569647 meter/sec RA = 47
44043 deg
ZDOT = -2416
995361 TA = 81
16161
MA = 81
00967
Ha = 192
587 n
mi
Hp = 183
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15158364
58 X = -4650076
37
Y = 1938877
44 feet Y = 539136
93 meter
Z = 15899679
15 Z = 4823704
65
XDOT = -11087
538379 XDOT = -3294
977670
YDOT = -21274
834799 feet/sec YDOT = -6521
888702 meter/sec
ZDOT = -7929
774805 ZDOT = -2433
207047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15071889
77 X = -4593912
00
Y = -3034685
51 feet Y = -924972
14 meter
Z = 15810246
12 Z = 4818963
02
XDOT = -3886
899659 XDOT = -1184
727016
YDOT = -22588
225302 feet/sec YDOT = -6884
891072 meter/sec
ZDOT = -7994
328838 ZDOT = -2436
671430
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 10063
54346368
00016717 00000-0 10270-3 0 9017
2 25544 51
6433 47
8282 0007790 9
0495 351
0807 15
73620520 6994
Satellite: ISS
Catalog Number: 25544
Epoch time: 10063
54346368 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 47
8282 deg
Eccentricity:
0007790
Arg of perigee: 9
0495 deg
Mean anomaly: 351
0807 deg
Mean motion: 15
73620520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 699
Checksum: 305
Coasting Arc #3 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2010/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3537615
89 A = 6731282
66 meter
Y = 5351031
40 meter E =
0019427
Z = 2001381
67 I = 51
88573
XDOT = -5127
180459 Wp = 49
54347
YDOT = 1282
212240 meter/sec RA = 42
36303 deg
ZDOT = 5611
505950 TA = 332
70072
MA = 332
80269
Ha = 192
410 n
mi
Hp = 183
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11606351
34 X = 3467794
50
Y = 17555877
29 feet Y = 5390200
83 meter
Z = 6566212
83 Z = 2018397
42
XDOT = -16821
458200 XDOT = -5168
396805
YDOT = 4206
733070 feet/sec YDOT = 1224
646888 meter/sec
ZDOT = 18410
452591 ZDOT = 5586
498114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5701833
93 X = 1737918
98
Y = 20236390
46 feet Y = 6168051
81 meter
Z = 6633924
98 Z = 2022020
33
XDOT = -15932
534299 XDOT = -4856
236454
YDOT = -1538
119812 feet/sec YDOT = -468
818919 meter/sec
ZDOT = 18311
142150 ZDOT = 5581
236127
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 10064
55953136
00016717 00000-0 10270-3 0 9027
2 25544 51
6438 42
6142 0007607 13
2273 346
9088 15
73691943 7155
Satellite: ISS
Catalog Number: 25544
Epoch time: 10064
55953136 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 42
6142 deg
Eccentricity:
0007607
Arg of perigee: 13
2273 deg
Mean anomaly: 346
9088 deg
Mean motion: 15
73691943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 306
Coasting Arc #4 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2010/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284171
28 A = 6722692
42 meter
Y = -1615506
44 meter E =
0014793
Z = -4933241
14 I = 51
83342
XDOT = 4666
201052 Wp = 73
84525
YDOT = 5707
098354 meter/sec RA = 37
20977 deg
ZDOT = 2192
772911 TA = 217
36506
MA = 217
46802
Ha = 192
676 n
mi
Hp = 183
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055680
06 X = 4325882
32
Y = -5300217
98 feet Y = -1567365
24 meter
Z = -16185174
34 Z = -4912327
46
XDOT = 15309
058569 XDOT = 4591
384465
YDOT = 18724
075966 feet/sec YDOT = 5758
860336 meter/sec
ZDOT = 7194
136848 ZDOT = 2215
259185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15076217
25 X = 4595231
02
Y = -1021440
69 feet Y = -311335
12 meter
Z = -16102131
96 Z = -4907929
82
XDOT = 9183
389187 XDOT = 2799
097024
YDOT = 21215
533041 feet/sec YDOT = 6466
494471 meter/sec
ZDOT = 7283
580584 ZDOT = 2220
035362
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 10065
51207836
00016717 00000-0 10270-3 0 9034
2 25544 51
6440 37
7250 0007851 16
6668 343
4751 15
73659748 7302
Satellite: ISS
Catalog Number: 25544
Epoch time: 10065
51207836 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 37
7250 deg
Eccentricity:
0007851
Arg of perigee: 16
6668 deg
Mean anomaly: 343
4751 deg
Mean motion: 15
73659748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 310
Coasting Arc #5 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2010/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4564765
70 A = 6731416
27 meter
Y = -4589599
11 meter E =
0007425
Z = -1857296
59 I = 51
83951
XDOT = 4648
403512 Wp = 74
99013
YDOT = -2337
600932 meter/sec RA = 32
12512 deg
ZDOT = -5664
970243 TA = 125
54360
MA = 125
47435
Ha = 192
636 n
mi
Hp = 182
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14976265
43 X = -4504082
43
Y = -15057739
85 feet Y = -4640305
77 meter
Z = -6093492
73 Z = -1879324
43
XDOT = 15250
667690 XDOT = 4701
716555
YDOT = -7669
294395 feet/sec YDOT = -2285
321772 meter/sec
ZDOT = -18585
860376 ZDOT = -5642
259034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10316657
94 X = -3144517
34
Y = -18534169
11 feet Y = -5649214
74 meter
Z = -6181088
41 Z = -1883995
75
XDOT = 15509
050852 XDOT = 4727
158700
YDOT = -2482
716142 feet/sec YDOT = -756
731880 meter/sec
ZDOT = -18495
689094 ZDOT = -5637
486036
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 10066
52810532
00016717 00000-0 10270-3 0 9040
2 25544 51
6446 32
5097 0007920 20
2338 339
9138 15
73723016 7468
Satellite: ISS
Catalog Number: 25544
Epoch time: 10066
52810532 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 32
5097 deg
Eccentricity:
0007920
Arg of perigee: 20
2338 deg
Mean anomaly: 339
9138 deg
Mean motion: 15
73723016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 292
Coasting Arc #6 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2010/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3804745
86 A = 6722253
86 meter
Y = 2451668
28 meter E =
0013431
Z = 4966380
11 I = 51
78256
XDOT = -5731
218394 Wp = 37
50146
YDOT = -4723
704914 meter/sec RA = 26
97066 deg
ZDOT = -2045
484842 TA = 72
32458
MA = 72
17798
Ha = 192
759 n
mi
Hp = 182
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12482762
02 X = -3856003
46
Y = 8043531
10 feet Y = 2408834
88 meter
Z = 16293897
99 Z = 4947772
39
XDOT = -18803
209955 XDOT = -5668
034695
YDOT = -15497
719533 feet/sec YDOT = -4787
441572 meter/sec
ZDOT = -6710
908273 ZDOT = -2073
173057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14206881
84 X = -4330257
59
Y = 4591740
03 feet Y = 1399562
36 meter
Z = 16220027
24 Z = 4943864
30
XDOT = -13885
851649 XDOT = -4232
407583
YDOT = -18713
004267 feet/sec YDOT = -5703
723701 meter/sec
ZDOT = -6820
990503 ZDOT = -2079
037905
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 10067
54411056
00016717 00000-0 10270-3 0 9052
2 25544 51
6447 27
2950 0007867 23
7194 336
4331 15
73747089 7627
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067
54411056 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 27
2950 deg
Eccentricity:
0007867
Arg of perigee: 23
7194 deg
Mean anomaly: 336
4331 deg
Mean motion: 15
73747089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 313
Coasting Arc #7 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2010/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5394416
55 A = 6731435
60 meter
Y = 3621172
07 meter E =
0020847
Z = 1714726
39 I = 51
78693
XDOT = -4010
902729 Wp = 51
44422
YDOT = 3247
448369 meter/sec RA = 21
88029 deg
ZDOT = 5726
281284 TA = 327
50790
MA = 327
63606
Ha = 192
609 n
mi
Hp = 182
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17698217
01 X = 5345193
36
Y = 11880485
79 feet Y = 3681220
47 meter
Z = 5625742
76 Z = 1740812
27
XDOT = -13159
129689 XDOT = -4074
734872
YDOT = 10654
358166 feet/sec YDOT = 3202
239357 meter/sec
ZDOT = 18787
012086 ZDOT = 5706
641550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14347813
92 X = 4373213
68
Y = 15726906
28 feet Y = 4793561
03 meter
Z = 5729438
38 Z = 1746332
82
XDOT = -14268
789008 XDOT = -4349
126890
YDOT = 6162
067855 feet/sec YDOT = 1878
198282 meter/sec
ZDOT = 18709
055551 ZDOT = 5702
520132
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 10068
56009246
00016717 00000-0 10270-3 0 9060
2 25544 51
6449 22
0798 0007794 27
6772 332
4805 15
73797559 7782
Satellite: ISS
Catalog Number: 25544
Epoch time: 10068
56009246 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 22
0798 deg
Eccentricity:
0007794
Arg of perigee: 27
6772 deg
Mean anomaly: 332
4805 deg
Mean motion: 15
73797559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 346
Coasting Arc #8 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2010/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3178566
06 A = 6721895
08 meter
Y = -3175024
31 meter E =
0016997
Z = -5013167
78 I = 51
72678
XDOT = 6548
669012 Wp = 77
70541
YDOT = 3545
643113 meter/sec RA = 16
72294 deg
ZDOT = 1915
539017 TA = 210
74558
MA = 210
84526
Ha = 192
714 n
mi
Hp = 182
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10428366
33 X = 3238186
04
Y = -10416746
42 feet Y = -3139146
58 meter
Z = -16447400
86 Z = -4997581
68
XDOT = 21485
134554 XDOT = 6499
229148
YDOT = 11632
687379 feet/sec YDOT = 3618
597878 meter/sec
ZDOT = 6284
576829 ZDOT = 1947
231501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12559873
51 X = 3828249
45
Y = -7844735
39 feet Y = -2391075
35 meter
Z = -16385546
36 Z = -4994314
53
XDOT = 17788
892806 XDOT = 5422
054527
YDOT = 15152
944846 feet/sec YDOT = 4618
617589 meter/sec
ZDOT = 6410
543402 ZDOT = 1953
933629
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 10069
51255595
00016717 00000-0 10270-3 0 9077
2 25544 51
6454 17
1903 0007865 30
4957 329
6662 15
73811450 7930
Satellite: ISS
Catalog Number: 25544
Epoch time: 10069
51255595 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 17
1903 deg
Eccentricity:
0007865
Arg of perigee: 30
4957 deg
Mean anomaly: 329
6662 deg
Mean motion: 15
73811450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 321
Coasting Arc #9 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2010/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5997778
08 A = 6731321
84 meter
Y = -2571201
07 meter E =
0009159
Z = -1660214
99 I = 51
73078
XDOT = 3272
014471 Wp = 87
04164
YDOT = -3946
279278 meter/sec RA = 11
62647 deg
ZDOT = -5735
622960 TA = 111
26145
MA = 111
16361
Ha = 192
687 n
mi
Hp = 182
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19677749
60 X = -5960515
84
Y = -8435699
05 feet Y = -2638063
55 meter
Z = -5446899
58 Z = -1689260
87
XDOT = 10734
955615 XDOT = 3343
761284
YDOT = -12947
110493 feet/sec YDOT = -3909
288882 meter/sec
ZDOT = -18817
660631 ZDOT = -5719
553348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17519862
64 X = -5340054
13
Y = -12253914
76 feet Y = -3734993
22 meter
Z = -5562333
05 Z = -1695399
11
XDOT = 12357
821470 XDOT = 3766
663984
YDOT = -9194
445456 feet/sec YDOT = -2802
466975 meter/sec
ZDOT = -18753
902306 ZDOT = -5716
189423
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 10070
52849443
00016717 00000-0 10270-3 0 9082
2 25544 51
6462 11
9747 0007882 34
2779 325
8891 15
73858835 8098
Satellite: ISS
Catalog Number: 25544
Epoch time: 10070
52849443 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 11
9747 deg
Eccentricity:
0007882
Arg of perigee: 34
2779 deg
Mean anomaly: 325
8891 deg
Mean motion: 15
73858835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 344
Coasting Arc #10 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2010/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2516562
54 A = 6721615
48 meter
Y = 3700908
99 meter E =
0013404
Z = 5009562
18 I = 51
66863
XDOT = -7115
203417 Wp = 44
80012
YDOT = -2292
849937 meter/sec RA = 6
46607 deg
ZDOT = -1868
086842 TA = 63
27109
MA = 63
13397
Ha = 192
776 n
mi
Hp = 181
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8256438
79 X = -2582094
76
Y = 12142089
86 feet Y = 3672401
29 meter
Z = 16435571
44 Z = 4997177
50
XDOT = -23343
843233 XDOT = -7079
960911
YDOT = -7522
473548 feet/sec YDOT = -2372
219472 meter/sec
ZDOT = -6128
893840 ZDOT = -1902
565961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10470418
84 X = -3191383
66
Y = 10372161
38 feet Y = 3161434
79 meter
Z = 16386449
70 Z = 4994589
87
XDOT = -20739
774533 XDOT = -6321
483278
YDOT = -10972
798902 feet/sec YDOT = -3344
509105 meter/sec
ZDOT = -6265
902416 ZDOT = -1909
847056
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 10071
54441006
00016717 00000-0 10270-3 0 9099
2 25544 51
6464 6
7597 0007856 38
0241 322
1476 15
73891192 8252
Satellite: ISS
Catalog Number: 25544
Epoch time: 10071
54441006 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 6
7597 deg
Eccentricity:
0007856
Arg of perigee: 38
0241 deg
Mean anomaly: 322
1476 deg
Mean motion: 15
73891192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 305
Coasting Arc #11 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2010/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6369724
42 A = 6731251
17 meter
Y = 1418921
21 meter E =
0021579
Z = 1602497
16 I = 51
67151
XDOT = -2460
695945 Wp = 55
26551
YDOT = 4495
045370 meter/sec RA = 1
36421 deg
ZDOT = 5758
392842 TA = 322
43237
MA = 322
58294
Ha = 192
678 n
mi
Hp = 181
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20898045
99 X = 6345599
88
Y = 4655253
33 feet Y = 1490016
53 meter
Z = 5257536
60 Z = 1633381
94
XDOT = -8073
149425 XDOT = -2538
750157
YDOT = 14747
524179 feet/sec YDOT = 4467
092543 meter/sec
ZDOT = 18892
364968 ZDOT = 5746
248984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19775572
62 X = 6027594
53
Y = 8125336
12 feet Y = 2476602
45 meter
Z = 5380245
47 Z = 1639898
82
XDOT = -9973
236978 XDOT = -3039
842631
YDOT = 11705
073431 feet/sec YDOT = 3567
706382 meter/sec
ZDOT = 18844
220002 ZDOT = 5743
718257
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 10072
56030268
00016717 00000-0 10270-3 0 9108
2 25544 51
6465 1
5437 0007854 41
5707 318
6052 15
73917605 8419
Satellite: ISS
Catalog Number: 25544
Epoch time: 10072
56030268 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 1
5437 deg
Eccentricity:
0007854
Arg of perigee: 41
5707 deg
Mean anomaly: 318
6052 deg
Mean motion: 15
73917605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 291
Coasting Arc #12 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2010/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1783892
58 A = 6721394
67 meter
Y = -4109398
13 meter E =
0018486
Z = -5025795
78 I = 51
60905
XDOT = 7400
848175 Wp = 82
31116
YDOT = 970
596474 meter/sec RA = 356
19904 deg
ZDOT = 1841
483080 TA = 205
43751
MA = 205
52861
Ha = 192
701 n
mi
Hp = 181
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5852665
96 X = 1854126
05
Y = -13482277
34 feet Y = -4089057
44 meter
Z = -16488831
29 Z = -5016958
72
XDOT = 24280
997948 XDOT = 7380
499291
YDOT = 3184
371634 feet/sec YDOT = 1053
243584 meter/sec
ZDOT = 6041
611156 ZDOT = 1877
386301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7936593
18 X = 2419073
60
Y = -12417304
10 feet Y = -3784794
29 meter
Z = -16453817
36 Z = -5015123
53
XDOT = 22570
044194 XDOT = 6879
349470
YDOT = 6266
904388 feet/sec YDOT = 1910
152457 meter/sec
ZDOT = 6184
237830 ZDOT = 1884
955691
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 10073
51268022
00016717 00000-0 10270-3 0 9116
2 25544 51
6472 356
6539 0007834 44
9494 315
2302 15
73956941 8565
Satellite: ISS
Catalog Number: 25544
Epoch time: 10073
51268022 = yrday
fracday
Element set: 911
Inclination: 51
6472 deg
RA of node: 356
6539 deg
Eccentricity:
0007834
Arg of perigee: 44
9494 deg
Mean anomaly: 315
2302 deg
Mean motion: 15
73956941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 315
Coasting Arc #13 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2010/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6522442
87 A = 6730973
01 meter
Y = -295001
84 meter E =
0010645
Z = -1642622
09 I = 51
61241
XDOT = 1655
169590 Wp = 95
20098
YDOT = -4856
577287 meter/sec RA = 351
09277 deg
ZDOT = -5732
787818 TA = 102
93475
MA = 102
81584
Ha = 192
662 n
mi
Hp = 181
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21399090
79 X = -6510679
87
Y = -967853
79 feet Y = -367874
09 meter
Z = -5389180
09 Z = -1674279
15
XDOT = 5430
346423 XDOT = 1737
202230
YDOT = -15933
652515 feet/sec YDOT = -4837
610200 meter/sec
ZDOT = -18808
358983 ZDOT = -5724
547270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21038724
94 X = -6412603
36
Y = -3854712
00 feet Y = -1174916
22 meter
Z = -5514919
57 Z = -1680947
48
XDOT = 7368
052543 XDOT = 2245
782415
YDOT = -13502
013637 feet/sec YDOT = -4115
413757 meter/sec
ZDOT = -18775
733554 ZDOT = -5722
843587
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 10074
52852742
00016717 00000-0 10270-3 0 9127
2 25544 51
6478 351
4379 0007768 48
9447 311
2387 15
73988746 8729
Satellite: ISS
Catalog Number: 25544
Epoch time: 10074
52852742 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 351
4379 deg
Eccentricity:
0007768
Arg of perigee: 48
9447 deg
Mean anomaly: 311
2387 deg
Mean motion: 15
73988746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 350
Coasting Arc #14 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2010/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1092183
43 A = 6721173
96 meter
Y = 4359355
71 meter E =
0013530
Z = 4990793
11 I = 51
54979
XDOT = -7462
642849 Wp = 52
89349
YDOT = 317
162407 meter/sec RA = 345
92257 deg
ZDOT = -1898
600882 TA = 55
50487
MA = 55
37716
Ha = 192
638 n
mi
Hp = 181
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3583278
98 X = -1165093
58
Y = 14302348
11 feet Y = 4346735
19 meter
Z = 16373993
16 Z = 4985309
71
XDOT = -24483
736381 XDOT = -7456
411771
YDOT = 1040
559077 feet/sec YDOT = 233
745313 meter/sec
ZDOT = -6229
005520 ZDOT = -1934
839069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5347874
62 X = -1630032
18
Y = 13766150
73 feet Y = 4195922
74 meter
Z = 16352309
71 Z = 4984184
00
XDOT = -23393
953499 XDOT = -7130
477027
YDOT = -1472
830015 feet/sec YDOT = -448
918589 meter/sec
ZDOT = -6372
917929 ZDOT = -1942
465385
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 10075
54435011
00016717 00000-0 10270-3 0 9137
2 25544 51
6473 346
2223 0007757 51
8041 308
3818 15
74059815 8885
Satellite: ISS
Catalog Number: 25544
Epoch time: 10075
54435011 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 346
2223 deg
Eccentricity:
0007757
Arg of perigee: 51
8041 deg
Mean anomaly: 308
3818 deg
Mean motion: 15
74059815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 888
Checksum: 306
Coasting Arc #15 (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 = 6453768
25 A = 6730755
41 meter
Y = -838810
89 meter E =
0021877
Z = 1673894
22 I = 51
55353
XDOT = -832
859680 Wp = 60
95937
YDOT = 5098
534806 meter/sec RA = 340
81216 deg
ZDOT = 5720
484312 TA = 317
58589
MA = 317
75477
Ha = 192
631 n
mi
Hp = 181
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21173780
34 X = 6454536
86
Y = -2752004
24 feet Y = -766636
54 meter
Z = 5491778
93 Z = 1705248
52
XDOT = -2732
479265 XDOT = -917
599536
YDOT = 16727
476398 feet/sec YDOT = 5088
748102 meter/sec
ZDOT = 18767
993150 ZDOT = 5716
231891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21311164
47 X = 6495642
93
Y = -594845
43 feet Y = -181308
89 meter
Z = 5616276
81 Z = 1711841
17
XDOT = -4567
084438 XDOT = -1392
047337
YDOT = 14799
573020 feet/sec YDOT = 4510
909856 meter/sec
ZDOT = 18751
214945 ZDOT = 5715
370315
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
56015147
00016717 00000-0 10270-3 0 9145
2 25544 51
6476 341
0058 0007819 55
8034 304
3870 15
74054821 9047
Satellite: ISS
Catalog Number: 25544
Epoch time: 10076
56015147 = yrday
fracday
Element set: 914
Inclination: 51
6476 deg
RA of node: 341
0058 deg
Eccentricity:
0007819
Arg of perigee: 55
8034 deg
Mean anomaly: 304
3870 deg
Mean motion: 15
74054821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 904
Checksum: 296
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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