Date:
March 10th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 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 763)
---------------------------------------
Vector Time (GMT): 2010/067/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6234802
97 A = 6730671
74 meter
Y = 1045767
73 meter E =
0013586
Z = -2295663
59 I = 51
81059
XDOT = 1106
466435 Wp = 32
18011
YDOT = 5321
865514 meter/sec RA = 26
11907 deg
ZDOT = 5455
335592 TA = 302
08120
MA = 302
21303
Ha = 192
727 n
mi
Hp = 182
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20455390
31 X = 6233797
35
Y = 3430996
50 feet Y = 1115483
32 meter
Z = -7531704
71 Z = -2265377
91
XDOT = 3630
139224 XDOT = 1020
373567
YDOT = 17460
188693 feet/sec YDOT = 5333
757445 meter/sec
ZDOT = 17898
082651 ZDOT = 5460
501464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16820256
55 X = 5126814
20
Y = -12209495
86 feet Y = -3721454
34 meter
Z = -7411375
44 Z = -2258987
23
XDOT = 14030
020551 XDOT = 4276
350264
YDOT = 8503
839446 feet/sec YDOT = 2591
970263 meter/sec
ZDOT = 17918
706991 ZDOT = 5461
621891
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
67113940
00016717 00000-0 10270-3 0 9002
2 25544 51
6488 26
6488 0007819 24
1633 335
9895 15
73746945 7642
Satellite: ISS
Catalog Number: 25544
Epoch time: 10067
67113940 = yrday
fracday
Element set: 900
Inclination: 51
6488 deg
RA of node: 26
6488 deg
Eccentricity:
0007819
Arg of perigee: 24
1633 deg
Mean anomaly: 335
9895 deg
Mean motion: 15
73746945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 764
Checksum: 338
Coasting Arc #2 (Orbit 779)
---------------------------------------
Vector Time (GMT): 2010/068/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1443844
14 A = 6723017
77 meter
Y = -4559344
27 meter E =
0017924
Z = -4741953
17 I = 51
75796
XDOT = 7188
652573 Wp = 53
22008
YDOT = 507
495855 meter/sec RA = 21
03651 deg
ZDOT = -2673
210459 TA = 190
47779
MA = 190
51519
Ha = 192
674 n
mi
Hp = 182
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4737021
46 X = -1369718
34
Y = -14958478
58 feet Y = -4575075
90 meter
Z = -15557589
14 Z = -4748787
02
XDOT = 23584
818152 XDOT = 7195
429101
YDOT = 1665
012649 feet/sec YDOT = 587
921434 meter/sec
ZDOT = -8770
375521 ZDOT = -2638
272246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14043872
28 X = -4280572
27
Y = -6936637
72 feet Y = -2114287
18 meter
Z = -15584824
09 Z = -4750254
38
XDOT = 16982
356658 XDOT = 5176
222309
YDOT = -14963
235532 feet/sec YDOT = -4560
794190 meter/sec
ZDOT = -8631
573660 ZDOT = -2630
903652
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
68713421
00016717 00000-0 10270-3 0 9015
2 25544 51
6491 21
4339 0007864 27
3490 332
8086 15
73783857 7809
Satellite: ISS
Catalog Number: 25544
Epoch time: 10068
68713421 = yrday
fracday
Element set: 901
Inclination: 51
6491 deg
RA of node: 21
4339 deg
Eccentricity:
0007864
Arg of perigee: 27
3490 deg
Mean anomaly: 332
8086 deg
Mean motion: 15
73783857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 780
Checksum: 318
Coasting Arc #3 (Orbit 795)
---------------------------------------
Vector Time (GMT): 2010/069/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6292390
47 A = 6730441
09 meter
Y = 155696
46 meter E =
0017698
Z = 2372968
72 I = 51
75390
XDOT = -2174
373279 Wp = 81
17621
YDOT = -5041
776060 meter/sec RA = 15
86985 deg
ZDOT = -5398
225279 TA = 72
13291
MA = 71
93996
Ha = 192
794 n
mi
Hp = 182
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20644325
69 X = -6305191
03
Y = 510815
15 feet Y = 85259
76 meter
Z = 7785330
45 Z = 2342369
86
XDOT = -7133
770601 XDOT = -2091
610609
YDOT = -16541
260041 feet/sec YDOT = -5065
628714 meter/sec
ZDOT = -17710
712859 ZDOT = -5408
586872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13615335
18 X = -4149954
16
Y = 15586841
02 feet Y = 4750869
14 meter
Z = 7663779
78 Z = 2335920
08
XDOT = -15802
752564 XDOT = -4816
678981
YDOT = -5015
382351 feet/sec YDOT = -1528
688541 meter/sec
ZDOT = -17751
971505 ZDOT = -5410
800915
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
70311080
00016717 00000-0 10270-3 0 9025
2 25544 51
6489 16
2186 0007818 32
0999 328
0639 15
73777997 7960
Satellite: ISS
Catalog Number: 25544
Epoch time: 10069
70311080 = yrday
fracday
Element set: 902
Inclination: 51
6489 deg
RA of node: 16
2186 deg
Eccentricity:
0007818
Arg of perigee: 32
0999 deg
Mean anomaly: 328
0639 deg
Mean motion: 15
73777997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 796
Checksum: 339
Coasting Arc #4 (Orbit 811)
---------------------------------------
Vector Time (GMT): 2010/070/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2338546
40 A = 6723080
11 meter
Y = 4208781
83 meter E =
0011717
Z = 4681242
07 I = 51
70083
XDOT = -7137
687762 Wp = 75
69427
YDOT = 873
419526 meter/sec RA = 10
78367 deg
ZDOT = 2777
492044 TA = 346
96060
MA = 346
99087
Ha = 192
728 n
mi
Hp = 182
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7672396
34 X = 2268569
13
Y = 13808339
35 feet Y = 4234541
90 meter
Z = 15358405
76 Z = 4692432
22
XDOT = -23417
610768 XDOT = -7160
416261
YDOT = 2865
549627 feet/sec YDOT = 793
474767 meter/sec
ZDOT = 9112
506706 ZDOT = 2742
762672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15361986
40 X = 4682333
46
Y = 3489315
47 feet Y = 1063543
35 meter
Z = 15402940
63 Z = 4694816
30
XDOT = -13174
175798 XDOT = -4015
488783
YDOT = 18341
620608 feet/sec YDOT = 5590
525961 meter/sec
ZDOT = 8974
563903 ZDOT = 2735
447078
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
71906562
00016717 00000-0 10270-3 0 9034
2 25544 51
6493 11
0031 0007861 35
0501 325
1178 15
73818058 8126
Satellite: ISS
Catalog Number: 25544
Epoch time: 10070
71906562 = yrday
fracday
Element set: 903
Inclination: 51
6493 deg
RA of node: 11
0031 deg
Eccentricity:
0007861
Arg of perigee: 35
0501 deg
Mean anomaly: 325
1178 deg
Mean motion: 15
73818058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 812
Checksum: 274
Coasting Arc #5 (Orbit 826)
---------------------------------------
Vector Time (GMT): 2010/071/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6109723
10 A = 6730023
22 meter
Y = -1356839
95 meter E =
0013233
Z = -2465751
95 I = 51
69434
XDOT = 3158
186131 Wp = 40
91449
YDOT = 4553
317582 meter/sec RA = 5
61118 deg
ZDOT = 5345
781298 TA = 291
23791
MA = 291
37920
Ha = 192
788 n
mi
Hp = 182
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20045023
30 X = 6136419
37
Y = -4451574
65 feet Y = -1288368
34 meter
Z = -8089737
37 Z = -2436006
59
XDOT = 10361
503055 XDOT = 3081
067110
YDOT = 14938
705977 feet/sec YDOT = 4588
203554 meter/sec
ZDOT = 17538
652553 ZDOT = 5360
935733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9689492
84 X = 2953357
42
Y = -18155730
17 feet Y = -5533866
56 meter
Z = -7971606
93 Z = -2429745
79
XDOT = 16695
289911 XDOT = 5088
724365
YDOT = 1220
789683 feet/sec YDOT = 372
096695 meter/sec
ZDOT = 17598
942421 ZDOT = 5364
157650
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
67150478
00016717 00000-0 10270-3 0 9048
2 25544 51
6491 6
1136 0007803 37
0306 323
1395 15
73852144 8275
Satellite: ISS
Catalog Number: 25544
Epoch time: 10071
67150478 = yrday
fracday
Element set: 904
Inclination: 51
6491 deg
RA of node: 6
1136 deg
Eccentricity:
0007803
Arg of perigee: 37
0306 deg
Mean anomaly: 323
1395 deg
Mean motion: 15
73852144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 827
Checksum: 287
Coasting Arc #6 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2010/072/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3120438
55 A = 6722985
26 meter
Y = -3721617
91 meter E =
0018085
Z = -4666277
13 I = 51
64053
XDOT = 6811
628399 Wp = 57
85520
YDOT = -2171
393973 meter/sec RA =
52129 deg
ZDOT = -2821
792968 TA = 184
21967
MA = 184
23494
Ha = 192
692 n
mi
Hp = 181
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10237659
29 X = -3055923
33
Y = -12210032
50 feet Y = -3756152
25 meter
Z = -15309308
18 Z = -4681278
86
XDOT = 22347
862201 XDOT = 6849
110565
YDOT = -7123
995975 feet/sec YDOT = -2095
013004 meter/sec
ZDOT = -9257
850946 ZDOT = -2788
611442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15876484
58 X = -4839152
50
Y = 36752
11 feet Y = 11202
04 meter
Z = -15368974
10 Z = -4684463
31
XDOT = 8791
255935 XDOT = 2679
574809
YDOT = -20645
052828 feet/sec YDOT = -6292
612102 meter/sec
ZDOT = -9126
094171 ZDOT = -2781
633503
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
68742080
00016717 00000-0 10270-3 0 9057
2 25544 51
6486
8978 0007714 40
4919 319
6817 15
73889526 8434
Satellite: ISS
Catalog Number: 25544
Epoch time: 10072
68742080 = yrday
fracday
Element set: 905
Inclination: 51
6486 deg
RA of node:
8978 deg
Eccentricity:
0007714
Arg of perigee: 40
4919 deg
Mean anomaly: 319
6817 deg
Mean motion: 15
73889526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 335
Coasting Arc #7 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2010/073/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5766808
96 A = 6729781
61 meter
Y = 2427568
83 meter E =
0018960
Z = 2465135
99 I = 51
63396
XDOT = -3943
299644 Wp = 83
87323
YDOT = -3914
510462 meter/sec RA = 355
34416 deg
ZDOT = -5332
916136 TA = 68
25361
MA = 68
05191
Ha = 192
745 n
mi
Hp = 181
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18919976
90 X = -5805500
87
Y = 7964464
67 feet Y = 2362864
88 meter
Z = 8087716
51 Z = 2437027
00
XDOT = -12937
334791 XDOT = -3873
327855
YDOT = -12842
882094 feet/sec YDOT = -3958
216145 meter/sec
ZDOT = -17496
444016 ZDOT = -5351
902002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5612193
97 X = -1710596
72
Y = 19791264
60 feet Y = 6032377
45 meter
Z = 7976121
00 Z = 2431121
68
XDOT = -16601
441082 XDOT = -5060
119242
YDOT = 2423
619977 feet/sec YDOT = 738
719369 meter/sec
ZDOT = -17571
937071 ZDOT = -5355
926419
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
70331694
00016717 00000-0 10270-3 0 9067
2 25544 51
6491 355
6825 0007811 44
5357 315
6432 15
73940294 8597
Satellite: ISS
Catalog Number: 25544
Epoch time: 10073
70331694 = yrday
fracday
Element set: 906
Inclination: 51
6491 deg
RA of node: 355
6825 deg
Eccentricity:
0007811
Arg of perigee: 44
5357 deg
Mean anomaly: 315
6432 deg
Mean motion: 15
73940294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 318
Coasting Arc #8 (Orbit 874)
---------------------------------------
Vector Time (GMT): 2010/074/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3740454
70 A = 6722920
02 meter
Y = 3092012
70 meter E =
0012991
Z = 4640728
30 I = 51
58007
XDOT = -6322
177728 Wp = 82
67773
YDOT = 3374
032627 meter/sec RA = 350
24947 deg
ZDOT = 2842
536419 TA = 339
22194
MA = 339
27470
Ha = 192
700 n
mi
Hp = 181
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12271833
02 X = 3683057
68
Y = 10144398
62 feet Y = 3133520
31 meter
Z = 15225486
55 Z = 4658759
46
XDOT = -20742
052914 XDOT = -6373
245272
YDOT = 11069
660850 feet/sec YDOT = 3303
049078 meter/sec
ZDOT = 9325
906888 ZDOT = 2811
699161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15471886
63 X = 4715831
04
Y = -3455366
83 feet Y = -1053195
81 meter
Z = 15297166
86 Z = 4662576
46
XDOT = -4180
241053 XDOT = -1274
137473
YDOT = 22101
212564 feet/sec YDOT = 6736
449589 meter/sec
ZDOT = 9203
503241 ZDOT = 2805
227788
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
71919381
00016717 00000-0 10270-3 0 9075
2 25544 51
6482 350
4662 0007785 48
3978 311
7851 15
73919911 8752
Satellite: ISS
Catalog Number: 25544
Epoch time: 10074
71919381 = yrday
fracday
Element set: 907
Inclination: 51
6482 deg
RA of node: 350
4662 deg
Eccentricity:
0007785
Arg of perigee: 48
3978 deg
Mean anomaly: 311
7851 deg
Mean motion: 15
73919911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 875
Checksum: 341
Coasting Arc #9 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2010/075/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5224968
39 A = 6729620
35 meter
Y = -3433574
60 meter E =
0012995
Z = -2484530
20 I = 51
57247
XDOT = 4586
245047 Wp = 49
59766
YDOT = 3146
977679 meter/sec RA = 345
06663 deg
ZDOT = 5322
273779 TA = 282
27684
MA = 282
42232
Ha = 192
703 n
mi
Hp = 181
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17142284
74 X = 5275044
23
Y = -11265008
53 feet Y = -3374866
20 meter
Z = -8151345
80 Z = -2459025
41
XDOT = 15046
735718 XDOT = 4524
859615
YDOT = 10324
729919 feet/sec YDOT = 3197
921199 meter/sec
ZDOT = 17461
528145 ZDOT = 5344
404157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1219070
30 X = 371572
63
Y = -20516141
79 feet Y = -6253320
02 meter
Z = -8050128
91 Z = -2453679
29
XDOT = 15706
940197 XDOT = 4787
475372
YDOT = -5918
269578 feet/sec YDOT = -1803
888567 meter/sec
ZDOT = 17549
485273 ZDOT = 5349
083111
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
67155720
00016717 00000-0 10270-3 0 9081
2 25544 51
6472 345
5759 0007578 51
3717 308
8123 15
73975688 8907
Satellite: ISS
Catalog Number: 25544
Epoch time: 10075
67155720 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 345
5759 deg
Eccentricity:
0007578
Arg of perigee: 51
3717 deg
Mean anomaly: 308
8123 deg
Mean motion: 15
73975688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 342
Coasting Arc #10 (Orbit 905)
---------------------------------------
Vector Time (GMT): 2010/076/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213715
23 A = 6722614
97 meter
Y = -2412583
27 meter E =
0018469
Z = -4667396
76 I = 51
51933
XDOT = 5630
228963 Wp = 64
20757
YDOT = -4420
681376 meter/sec RA = 339
96740 deg
ZDOT = -2798
590827 TA = 178
07694
MA = 178
06983
Ha = 192
657 n
mi
Hp = 181
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13824525
03 X = -4163750
77
Y = -7915299
44 feet Y = -2459424
68 meter
Z = -15312981
50 Z = -4687745
34
XDOT = 18471
879800 XDOT = 5692
838392
YDOT = -14503
547823 feet/sec YDOT = -4357
371045 meter/sec
ZDOT = -9181
728434 ZDOT = -2771
086653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14437315
92 X = -4400493
89
Y = 6546021
96 feet Y = 1995227
49 meter
Z = -15393841
80 Z = -4692042
98
XDOT = -509
688022 XDOT = -155
352909
YDOT = -22454
258244 feet/sec YDOT = -6844
057913 meter/sec
ZDOT = -9072
597954 ZDOT = -2765
327857
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
68739319
00016717 00000-0 10270-3 0 9096
2 25544 51
6460 340
3596 0007576 55
6688 304
5191 15
74008429 9065
Satellite: ISS
Catalog Number: 25544
Epoch time: 10076
68739319 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 340
3596 deg
Eccentricity:
0007576
Arg of perigee: 55
6688 deg
Mean anomaly: 304
5191 deg
Mean motion: 15
74008429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 906
Checksum: 335
Coasting Arc #11 (Orbit 921)
---------------------------------------
Vector Time (GMT): 2010/077/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4593711
53 A = 6729459
98 meter
Y = 4278889
34 meter E =
0019749
Z = 2407230
75 I = 51
51563
XDOT = -5013
036343 Wp = 89
18570
YDOT = -2346
613406 meter/sec RA = 334
78063 deg
ZDOT = -5357
197410 TA = 63
59581
MA = 63
39324
Ha = 192
565 n
mi
Hp = 181
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15071232
05 X = -4652911
33
Y = 14038350
85 feet Y = 4227188
95 meter
Z = 7897738
68 Z = 2384770
27
XDOT = -16446
969630 XDOT = -4960
399160
YDOT = -7698
862880 feet/sec YDOT = -2402
378345 meter/sec
ZDOT = -17576
106989 ZDOT = -5381
422712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2947205
85 X = 898308
34
Y = 20418882
50 feet Y = 6223675
38 meter
Z = 7808637
64 Z = 2380072
75
XDOT = -14139
732025 XDOT = -4309
790321
YDOT = 8847
447189 feet/sec YDOT = 2696
701903 meter/sec
ZDOT = -17672
356237 ZDOT = -5386
534181
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
70320686
00016717 00000-0 10270-3 0 9105
2 25544 51
6466 335
1430 0007529 57
7814 302
4078 15
74090682 9223
Satellite: ISS
Catalog Number: 25544
Epoch time: 10077
70320686 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 335
1430 deg
Eccentricity:
0007529
Arg of perigee: 57
7814 deg
Mean anomaly: 302
4078 deg
Mean motion: 15
74090682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 922
Checksum: 302
Coasting Arc #12 (Orbit 937)
---------------------------------------
Vector Time (GMT): 2010/078/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4513326
48 A = 6722380
74 meter
Y = 1677830
16 meter E =
0013540
Z = 4679378
09 I = 51
46338
XDOT = -4831
274276 Wp = 90
42168
YDOT = 5349
457863 meter/sec RA = 329
67553 deg
ZDOT = 2734
848744 TA = 332
57396
MA = 332
64536
Ha = 192
552 n
mi
Hp = 181
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14807501
59 X = 4471497
59
Y = 5504692
12 feet Y = 1728067
32 meter
Z = 15352290
32 Z = 4701202
18
XDOT = -15850
637389 XDOT = -4904
019245
YDOT = 17550
714773 feet/sec YDOT = 5295
025141 meter/sec
ZDOT = 8972
600867 ZDOT = 2711
201248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12742678
54 X = 3883968
42
Y = -9193387
47 feet Y = -2802144
50 meter
Z = 15438987
24 Z = 4705803
31
XDOT = 5114
626118 XDOT = 1558
938041
YDOT = 22037
681922 feet/sec YDOT = 6717
085450 meter/sec
ZDOT = 8878
809651 ZDOT = 2706
261182
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
71900396
00016717 00000-0 10270-3 0 9110
2 25544 51
6452 329
9257 0007570 63
0621 297
1315 15
74046819 9382
Satellite: ISS
Catalog Number: 25544
Epoch time: 10078
71900396 = yrday
fracday
Element set: 911
Inclination: 51
6452 deg
RA of node: 329
9257 deg
Eccentricity:
0007570
Arg of perigee: 63
0621 deg
Mean anomaly: 297
1315 deg
Mean motion: 15
74046819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 938
Checksum: 316
Coasting Arc #13 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2010/079/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3810942
92 A = 6729507
54 meter
Y = -5021749
77 meter E =
0012996
Z = -2352242
01 I = 51
46182
XDOT = 5286
680172 Wp = 57
68895
YDOT = 1500
867087 meter/sec RA = 324
48439 deg
ZDOT = 5389
419528 TA = 275
76399
MA = 275
91215
Ha = 192
608 n
mi
Hp = 181
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12503093
57 X = 3878240
59
Y = -16475556
98 feet Y = -4978757
38 meter
Z = -7717329
43 Z = -2333564
67
XDOT = 17344
751219 XDOT = 5243
323378
YDOT = 4924
104616 feet/sec YDOT = 1559
743743 meter/sec
ZDOT = 17681
822600 ZDOT = 5414
996908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7086662
86 X = -2160014
84
Y = -19459912
12 feet Y = -5931381
22 meter
Z = -7643266
96 Z = -2329667
77
XDOT = 12038
236664 XDOT = 3669
254535
YDOT = -11331
683826 feet/sec YDOT = -3453
897230 meter/sec
ZDOT = 17783
418579 ZDOT = 5420
385983
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
67129162
00016717 00000-0 10270-3 0 9121
2 25544 51
6446 325
0343 0007496 68
0002 292
1957 15
74105805 9538
Satellite: ISS
Catalog Number: 25544
Epoch time: 10079
67129162 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 325
0343 deg
Eccentricity:
0007496
Arg of perigee: 68
0002 deg
Mean anomaly: 292
1957 deg
Mean motion: 15
74105805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 953
Checksum: 303
Coasting Arc #14 (Orbit 968)
---------------------------------------
Vector Time (GMT): 2010/080/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4678125
65 A = 6721888
81 meter
Y = -975719
28 meter E =
0019203
Z = -4745445
55 I = 51
41266
XDOT = 3906
199790 Wp = 71
46812
YDOT = -6086
449033 meter/sec RA = 319
37477 deg
ZDOT = -2601
940972 TA = 172
88130
MA = 172
85400
Ha = 192
593 n
mi
Hp = 180
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15348181
28 X = -4643814
76
Y = -3201178
74 feet Y = -1027841
18 meter
Z = -15569047
09 Z = -4768088
53
XDOT = 12815
616108 XDOT = 3986
608999
YDOT = -19968
664806 feet/sec YDOT = -6042
318082 meter/sec
ZDOT = -8536
551747 ZDOT = -2582
769121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10742808
90 X = -3274408
15
Y = 11295920
05 feet Y = 3442996
43 meter
Z = -15658981
07 Z = -4772857
43
XDOT = -9401
484389 XDOT = -2865
572442
YDOT = -20657
816657 feet/sec YDOT = -6296
502517 meter/sec
ZDOT = -8460
546498 ZDOT = -2578
774573
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
68704624
00016717 00000-0 10270-3 0 9137
2 25544 51
6444 319
8174 0007630 72
0513 288
1481 15
74146795 9698
Satellite: ISS
Catalog Number: 25544
Epoch time: 10080
68704624 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 319
8174 deg
Eccentricity:
0007630
Arg of perigee: 72
0513 deg
Mean anomaly: 288
1481 deg
Mean motion: 15
74146795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 969
Checksum: 319
Coasting Arc #15 (Orbit 984)
---------------------------------------
Vector Time (GMT): 2010/081/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 798335
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2999609
32 A = 6729569
44 meter
Y = 5600697
04 meter E =
0020565
Z = 2196221
83 I = 51
41665
XDOT = -5380
595470 Wp = 97
04970
YDOT = -721
777313 meter/sec RA = 314
18140 deg
ZDOT = -5467
007144 TA = 58
24537
MA = 58
04515
Ha = 192
461 n
mi
Hp = 180
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9841237
94 X = -3072683
19
Y = 18374990
30 feet Y = 5566745
10 meter
Z = 7205452
20 Z = 2181472
15
XDOT = -17652
872278 XDOT = -5345
566881
YDOT = -2368
035805 feet/sec YDOT = -781
750603 meter/sec
ZDOT = -17936
375145 ZDOT = -5493
060889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10746149
18 X = 3275426
27
Y = 17884336
16 feet Y = 5451145
66 meter
Z = 7146997
43 Z = 2178404
82
XDOT = -9697
000545 XDOT = -2955
645766
YDOT = 13090
224175 feet/sec YDOT = 3989
900329 meter/sec
ZDOT = -18039
850803 ZDOT = -5498
546525
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
70277822
00016717 00000-0 10270-3 0 9147
2 25544 51
6444 314
5995 0007381 74
7162 285
4817 15
74192747 9852
Satellite: ISS
Catalog Number: 25544
Epoch time: 10081
70277822 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 314
5995 deg
Eccentricity:
0007381
Arg of perigee: 74
7162 deg
Mean anomaly: 285
4817 deg
Mean motion: 15
74192747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 985
Checksum: 333
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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