Date:
July 18th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 2806)
---------------------------------------
Vector Time (GMT): 2010/197/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2790626
11 A = 6731867
13 meter
Y = -4248105
09 meter E =
0016093
Z = -4427904
91 I = 51
97133
XDOT = 3652
461781 Wp = 89
53365
YDOT = 5875
425885 meter/sec RA = 80
35335 deg
ZDOT = -3345
210658 TA = 146
96808
MA = 146
86745
Ha = 197
342 n
mi
Hp = 185
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9155597
47 X = 2859431
48
Y = -13937352
67 feet Y = -4216513
57 meter
Z = -14527247
08 Z = -4414181
44
XDOT = 11983
142325 XDOT = 3602
740468
YDOT = 19276
331643 feet/sec YDOT = 5915
992162 meter/sec
ZDOT = -10975
100583 ZDOT = -3327
587503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11310611
90 X = -3447474
51
Y = -12318119
00 feet Y = -3754562
67 meter
Z = -14472376
27 Z = -4411180
29
XDOT = 20706
931695 XDOT = 6311
472781
YDOT = -6241
355603 feet/sec YDOT = -1902
365188 meter/sec
ZDOT = -10904
643248 ZDOT = -3323
735262
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 10197
41843322
00016717 00000-0 10270-3 0 9002
2 25544 51
6447 80
9500 0008050 113
3232 246
8777 15
71157114 28070
Satellite: ISS
Catalog Number: 25544
Epoch time: 10197
41843322 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 80
9500 deg
Eccentricity:
0008050
Arg of perigee: 113
3232 deg
Mean anomaly: 246
8777 deg
Mean motion: 15
71157114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2807
Checksum: 286
Coasting Arc #2 (Orbit 2822)
---------------------------------------
Vector Time (GMT): 2010/198/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4004318
98 A = 6734572
40 meter
Y = -3980930
65 meter E =
0019242
Z = 3651739
89 I = 51
97383
XDOT = 1963
275785 Wp = 98
05386
YDOT = -6018
777423 meter/sec RA = 75
21389 deg
ZDOT = -4391
597074 TA = 38
36379
MA = 38
22709
Ha = 197
379 n
mi
Hp = 185
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13137529
46 X = -3977245
23
Y = -13060796
09 feet Y = -4025558
28 meter
Z = 11980773
93 Z = 3632352
48
XDOT = 6441
193521 XDOT = 2051
766350
YDOT = -19746
645087 feet/sec YDOT = -5996
327738 meter/sec
ZDOT = -14408
126884 ZDOT = -4381
845140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15681218
47 X = -4779635
39
Y = 9956387
14 feet Y = 3034706
80 meter
Z = 11903266
82 Z = 3628115
73
XDOT = -17063
834852 XDOT = -5201
056863
YDOT = -9629
714218 feet/sec YDOT = -2935
136894 meter/sec
ZDOT = -14369
125535 ZDOT = -4379
709463
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 10198
43610761
00016717 00000-0 10270-3 0 9015
2 25544 51
6445 75
7463 0008016 117
4063 242
7915 15
71154390 28237
Satellite: ISS
Catalog Number: 25544
Epoch time: 10198
43610761 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 75
7463 deg
Eccentricity:
0008016
Arg of perigee: 117
4063 deg
Mean anomaly: 242
7915 deg
Mean motion: 15
71154390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2823
Checksum: 296
Coasting Arc #3 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2010/199/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -455131
49 A = 6736005
20 meter
Y = 5942907
73 meter E =
0020059
Z = 3124704
69 I = 51
97068
XDOT = -5143
138365 Wp = 98
47962
YDOT = -2982
012103 meter/sec RA = 70
17313 deg
ZDOT = 4892
950951 TA = 297
63903
MA = 297
84251
Ha = 197
208 n
mi
Hp = 185
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1493213
54 X = -536731
51
Y = 19497728
76 feet Y = 5937361
61 meter
Z = 10251655
80 Z = 3122296
07
XDOT = -16873
813535 XDOT = -5133
179666
YDOT = -9783
504274 feet/sec YDOT = -3039
470565 meter/sec
ZDOT = 16052
988686 ZDOT = 4867
989589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18756276
93 X = 5716913
21
Y = 5548961
76 feet Y = 1691323
54 meter
Z = 10242004
66 Z = 3121763
02
XDOT = -12673
242567 XDOT = -3862
804334
YDOT = 13213
269939 feet/sec YDOT = 4027
404677 meter/sec
ZDOT = 15953
197802 ZDOT = 4862
534690
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 10199
45376820
00016717 00000-0 10270-3 0 9024
2 25544 51
6450 70
5422 0007936 120
8506 239
3438 15
71176308 28393
Satellite: ISS
Catalog Number: 25544
Epoch time: 10199
45376820 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 70
5422 deg
Eccentricity:
0007936
Arg of perigee: 120
8506 deg
Mean anomaly: 239
3438 deg
Mean motion: 15
71176308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 311
Coasting Arc #4 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2010/200/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4640154
89 A = 6730484
76 meter
Y = 1141019
71 meter E =
0018887
Z = -4757908
86 I = 51
94175
XDOT = 999
580732 Wp = 115
06656
YDOT = 7127
018108 meter/sec RA = 65
03615 deg
ZDOT = 2684
471232 TA = 181
28145
MA = 181
28630
Ha = 197
066 n
mi
Hp = 185
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15223605
29 X = 4650163
91
Y = 3743502
97 feet Y = 1192965
23 meter
Z = -15609937
19 Z = -4735342
62
XDOT = 3279
464345 XDOT = 906
770202
YDOT = 23382
605341 feet/sec YDOT = 7137
676760 meter/sec
ZDOT = 8807
320316 ZDOT = 2689
102605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6581251
83 X = 2005965
56
Y = -14327164
51 feet Y = -4366919
74 meter
Z = -15519716
27 Z = -4730409
52
XDOT = 22525
702437 XDOT = 6865
834103
YDOT = 788
502076 feet/sec YDOT = 240
335433 meter/sec
ZDOT = 8825
800213 ZDOT = 2690
103905
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 10200
40781242
00016717 00000-0 10270-3 0 9031
2 25544 51
6459 65
6634 0007816 124
5077 235
6823 15
71204376 28544
Satellite: ISS
Catalog Number: 25544
Epoch time: 10200
40781242 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 65
6634 deg
Eccentricity:
0007816
Arg of perigee: 124
5077 deg
Mean anomaly: 235
6823 deg
Mean motion: 15
71204376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2854
Checksum: 299
Coasting Arc #5 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2010/201/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2195638
24 A = 6739146
04 meter
Y = -6181068
61 meter E =
0015919
Z = -1522733
68 I = 51
95757
XDOT = 5036
007648 Wp = 135
99690
YDOT = -369
507836 meter/sec RA = 59
97823 deg
ZDOT = -5808
755066 TA = 60
68929
MA = 60
53031
Ha = 197
014 n
mi
Hp = 185
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7203537
52 X = -2118960
09
Y = -20279096
50 feet Y = -6205192
61 meter
Z = -4995845
40 Z = -1533214
65
XDOT = 16522
334804 XDOT = 5067
983002
YDOT = -1212
296051 feet/sec YDOT = -313
012599 meter/sec
ZDOT = -19057
595362 ZDOT = -5784
212643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21213988
66 X = -6466023
74
Y = 3560806
74 feet Y = 1085333
90 meter
Z = -5037709
73 Z = -1535493
93
XDOT = 1940
157524 XDOT = 591
360013
YDOT = -15047
144034 feet/sec YDOT = -4586
369502 meter/sec
ZDOT = -18959
461107 ZDOT = -5778
843745
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 10201
42544775
00016717 00000-0 10270-3 0 9043
2 25544 51
6463 60
4593 0007802 129
5317 230
6536 15
71194939 28700
Satellite: ISS
Catalog Number: 25544
Epoch time: 10201
42544775 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 60
4593 deg
Eccentricity:
0007802
Arg of perigee: 129
5317 deg
Mean anomaly: 230
6536 deg
Mean motion: 15
71194939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 307
Coasting Arc #6 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2010/202/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3819626
09 A = 6728015
55 meter
Y = 1729623
06 meter E =
0009110
Z = 5254162
28 I = 51
90478
XDOT = -3949
021481 Wp = 113
72839
YDOT = -6576
585148 meter/sec RA = 54
86435 deg
ZDOT = -708
501086 TA = 342
96731
MA = 342
99786
Ha = 196
902 n
mi
Hp = 185
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12531581
67 X = -3864206
73
Y = 5674616
32 feet Y = 1686659
65 meter
Z = 17238065
21 Z = 5235498
66
XDOT = -12956
107222 XDOT = -3871
745665
YDOT = -21576
722928 feet/sec YDOT = -6620
313284 meter/sec
ZDOT = -2324
478627 ZDOT = -727
498581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3636626
07 X = 1108443
63
Y = 13363554
89 feet Y = 4073211
53 meter
Z = 17163421
96 Z = 5231411
01
XDOT = -22355
908482 XDOT = -6814
080905
YDOT = 9155
520768 feet/sec YDOT = 2790
602730 meter/sec
ZDOT = -2400
386556 ZDOT = -731
637822
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 10202
44306766
00016717 00000-0 10270-3 0 9053
2 25544 51
6463 55
2555 0007612 132
7732 227
4071 15
71283659 28869
Satellite: ISS
Catalog Number: 25544
Epoch time: 10202
44306766 = yrday
fracday
Element set: 905
Inclination: 51
6463 deg
RA of node: 55
2555 deg
Eccentricity:
0007612
Arg of perigee: 132
7732 deg
Mean anomaly: 227
4071 deg
Mean motion: 15
71283659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 306
Coasting Arc #7 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2010/203/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4518523
88 A = 6739891
12 meter
Y = 4990307
52 meter E =
0013609
Z = -289729
86 I = 51
92658
XDOT = -3351
769660 Wp = 76
71316
YDOT = 3372
052407 meter/sec RA = 49
77243 deg
ZDOT = 6046
819108 TA = 280
15581
MA = 280
30928
Ha = 196
737 n
mi
Hp = 185
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14824553
42 X = 4463792
96
Y = 16372400
00 feet Y = 5040530
38 meter
Z = -950557
30 Z = -267911
29
XDOT = -10996
619620 XDOT = -3418
601446
YDOT = 11063
164066 feet/sec YDOT = 3334
196291 meter/sec
ZDOT = 19838
645369 ZDOT = 6030
374605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18273017
34 X = 5569615
68
Y = -12412810
99 feet Y = -3783424
79 meter
Z = -863357
18 Z = -263151
27
XDOT = 8508
234728 XDOT = 2593
309945
YDOT = 11209
973426 feet/sec YDOT = 3416
799900 meter/sec
ZDOT = 19772
854702 ZDOT = 6026
766113
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 10203
39707692
00016717 00000-0 10270-3 0 9062
2 25544 51
6466 50
3765 0007598 136
1055 224
0711 15
71279956 29017
Satellite: ISS
Catalog Number: 25544
Epoch time: 10203
39707692 = yrday
fracday
Element set: 906
Inclination: 51
6466 deg
RA of node: 50
3765 deg
Eccentricity:
0007598
Arg of perigee: 136
1055 deg
Mean anomaly: 224
0711 deg
Mean motion: 15
71279956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 313
Coasting Arc #8 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2010/204/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1819008
73 A = 6728332
88 meter
Y = -3915779
23 meter E =
0019080
Z = -5175761
20 I = 51
86722
XDOT = 6057
042808 Wp = 99
57933
YDOT = 4540
821090 meter/sec RA = 44
68885 deg
ZDOT = -1313
868747 TA = 157
90547
MA = 157
82312
Ha = 196
594 n
mi
Hp = 185
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5967876
41 X = 1887802
99
Y = -12847044
72 feet Y = -3895052
55 meter
Z = -16980843
84 Z = -5166758
10
XDOT = 19872
187691 XDOT = 6012
198778
YDOT = 14897
706989 feet/sec YDOT = 4608
304024 meter/sec
ZDOT = -4310
593002 ZDOT = -1284
552341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12012814
58 X = -3661505
88
Y = -7587963
82 feet Y = -2312811
37 meter
Z = -16944800
25 Z = -5164775
12
XDOT = 16656
879866 XDOT = 5077
016983
YDOT = -17058
643125 feet/sec YDOT = -5199
474424 meter/sec
ZDOT = -4193
404482 ZDOT = -1278
149686
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 10204
41467213
00016717 00000-0 10270-3 0 9079
2 25544 51
6463 45
1718 0007451 139
7774 220
3940 15
71305474 29174
Satellite: ISS
Catalog Number: 25544
Epoch time: 10204
41467213 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 45
1718 deg
Eccentricity:
0007451
Arg of perigee: 139
7774 deg
Mean anomaly: 220
3940 deg
Mean motion: 15
71305474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 297
Coasting Arc #9 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2010/205/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5799442
06 A = 6738257
29 meter
Y = -2769694
34 meter E =
0020926
Z = 1986051
67 I = 51
87796
XDOT = 570
722944 Wp = 122
59953
YDOT = -5244
129601 meter/sec RA = 39
56214 deg
ZDOT = -5615
217197 TA = 35
35767
MA = 35
21908
Ha = 196
641 n
mi
Hp = 186
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19027040
87 X = -5777687
49
Y = -9086923
70 feet Y = -2834425
81 meter
Z = 6515917
56 Z = 1957930
99
XDOT = 1872
450605 XDOT = 656
598500
YDOT = -17205
149610 feet/sec YDOT = -5237
266486 meter/sec
ZDOT = -18422
628598 ZDOT = -5612
236834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11033117
27 X = -3362894
14
Y = 18008978
15 feet Y = 5489136
54 meter
Z = 6403489
45 Z = 1951783
58
XDOT = -15590
455451 XDOT = -4751
970821
YDOT = -2967
660805 feet/sec YDOT = -904
543013 meter/sec
ZDOT = -18410
653635 ZDOT = -5611
567228
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 10205
43225570
00016717 00000-0 10270-3 0 9081
2 25544 51
6462 39
9677 0007546 143
3385 216
8295 15
71289029 29330
Satellite: ISS
Catalog Number: 25544
Epoch time: 10205
43225570 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 39
9677 deg
Eccentricity:
0007546
Arg of perigee: 143
3385 deg
Mean anomaly: 216
8295 deg
Mean motion: 15
71289029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 325
Coasting Arc #10 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2010/206/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 919042
32 A = 6731072
11 meter
Y = 4919788
15 meter E =
0015502
Z = 4495481
29 I = 51
82962
XDOT = -6814
705254 Wp = 127
85968
YDOT = -1649
336019 meter/sec RA = 34
50228 deg
ZDOT = 3181
448514 TA = 290
34946
MA = 290
51594
Ha = 196
419 n
mi
Hp = 186
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3015230
71 X = 842122
30
Y = 16141037
22 feet Y = 4929634
78 meter
Z = 14748954
35 Z = 4499759
67
XDOT = -22357
956870 XDOT = -6811
210148
YDOT = -5411
207412 feet/sec YDOT = -1725
522977 meter/sec
ZDOT = 10437
823210 ZDOT = 3148
351701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16335937
58 X = 4979193
77
Y = -1502796
36 feet Y = -458052
33 meter
Z = 14766011
64 Z = 4500680
35
XDOT = -7463
357763 XDOT = -2274
831446
YDOT = 20668
011420 feet/sec YDOT = 6299
609881 meter/sec
ZDOT = 10305
480066 ZDOT = 3141
110324
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 10206
44982437
00016717 00000-0 10270-3 0 9096
2 25544 51
6458 34
7625 0007342 146
9501 213
2121 15
71303992 29496
Satellite: ISS
Catalog Number: 25544
Epoch time: 10206
44982437 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 34
7625 deg
Eccentricity:
0007342
Arg of perigee: 146
9501 deg
Mean anomaly: 213
2121 deg
Mean motion: 15
71303992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2949
Checksum: 306
Coasting Arc #11 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2010/207/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5771260
39 A = 6734581
44 meter
Y = 102598
02 meter E =
0010669
Z = -3483051
43 I = 51
81537
XDOT = 2646
696258 Wp = 127
87693
YDOT = 5596
894418 meter/sec RA = 29
35071 deg
ZDOT = 4553
360677 TA = 191
02925
MA = 191
05265
Ha = 196
221 n
mi
Hp = 186
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18934581
32 X = 5786603
82
Y = 336607
67 feet Y = 167221
85 meter
Z = -11427334
08 Z = -3454978
02
XDOT = 8683
386673 XDOT = 2561
795174
YDOT = 18362
514495 feet/sec YDOT = 5626
016173 meter/sec
ZDOT = 14938
847366 ZDOT = 4566
012393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1673921
05 X = 510211
14
Y = -18931005
55 feet Y = -5770170
49 meter
Z = -11315063
23 Z = -3448831
27
XDOT = 17542
348879 XDOT = 5346
907938
YDOT = -7402
004572 feet/sec YDOT = -2256
130993 meter/sec
ZDOT = 14989
385262 ZDOT = 4568
764628
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 10207
40378154
00016717 00000-0 10270-3 0 9100
2 25544 51
6451 29
8823 0007215 152
1589 207
9960 15
71349785 29646
Satellite: ISS
Catalog Number: 25544
Epoch time: 10207
40378154 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 29
8823 deg
Eccentricity:
0007215
Arg of perigee: 152
1589 deg
Mean anomaly: 207
9960 deg
Mean motion: 15
71349785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 320
Coasting Arc #12 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2010/208/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3621902
22 A = 6734680
34 meter
Y = -4558733
51 meter E =
0010159
Z = -3384695
32 I = 51
78844
XDOT = 5985
876814 Wp = 129
41341
YDOT = -1314
487863 meter/sec RA = 24
29758 deg
ZDOT = -4650
490469 TA = 90
35050
MA = 90
23410
Ha = 196
083 n
mi
Hp = 186
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11882881
31 X = -3554214
58
Y = -14956474
78 feet Y = -4598857
04 meter
Z = -11104643
44 Z = -3402126
10
XDOT = 19638
703457 XDOT = 6022
721497
YDOT = -4312
624222 feet/sec YDOT = -1247
343808 meter/sec
ZDOT = -15257
514663 ZDOT = -4621
322361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15565115
31 X = -4744247
15
Y = 11003371
89 feet Y = 3353827
75 meter
Z = -11174305
53 Z = -3405928
33
XDOT = -2453
620722 XDOT = -747
863596
YDOT = -18795
408222 feet/sec YDOT = -5728
840426 meter/sec
ZDOT = -15140
852356 ZDOT = -4614
931798
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 10208
42132415
00016717 00000-0 10270-3 0 9112
2 25544 51
6444 24
6775 0007184 156
4200 203
7292 15
71355825 29801
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208
42132415 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 24
6775 deg
Eccentricity:
0007184
Arg of perigee: 156
4200 deg
Mean anomaly: 203
7292 deg
Mean motion: 15
71355825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 287
Coasting Arc #13 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2010/209/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4390383
84 A = 6730635
42 meter
Y = 2277162
03 meter E =
0010817
Z = 4554706
33 I = 51
74756
XDOT = -5488
205856 Wp = 106
66782
YDOT = -4457
657482 meter/sec RA = 19
14280 deg
ZDOT = -3058
649339 TA = 13
71765
MA = 13
68828
Ha = 196
021 n
mi
Hp = 186
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14404146
45 X = -4437646
65
Y = 7471004
04 feet Y = 2227801
57 meter
Z = 14943262
22 Z = 4533263
64
XDOT = -18005
924726 XDOT = -5423
093568
YDOT = -14624
860504 feet/sec YDOT = -4518
665615 meter/sec
ZDOT = -10034
938777 ZDOT = -3085
152629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6943623
92 X = 2116416
57
Y = 14752543
83 feet Y = 4496575
36 meter
Z = 14857488
33 Z = 4528562
44
XDOT = -14187
523535 XDOT = -4324
357174
YDOT = 16900
390055 feet/sec YDOT = 5151
238889 meter/sec
ZDOT = -10140
883214 ZDOT = -3090
941204
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 10209
43885212
00016717 00000-0 10270-3 0 9125
2 25544 51
6449 19
4721 0007079 160
5899 199
5533 15
71412492 29963
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209
43885212 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 19
4721 deg
Eccentricity:
0007079
Arg of perigee: 160
5899 deg
Mean anomaly: 199
5533 deg
Mean motion: 15
71412492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 332
Coasting Arc #14 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2010/210/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5732545
43 A = 6737875
65 meter
Y = 2981663
23 meter E =
0015018
Z = 1899889
69 I = 51
74231
XDOT = -3771
927981 Wp = 95
39138
YDOT = 3635
853735 meter/sec RA = 14
07386 deg
ZDOT = 5635
562952 TA = 285
66208
MA = 285
82774
Ha = 195
809 n
mi
Hp = 186
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18807563
75 X = 5689548
72
Y = 9782359
69 feet Y = 3045527
48 meter
Z = 6233233
90 Z = 1927633
62
XDOT = -12375
091801 XDOT = -3839
680482
YDOT = 11928
653985 feet/sec YDOT = 3593
294666 meter/sec
ZDOT = 18489
379765 ZDOT = 5617
074870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10135428
24 X = 3089278
53
Y = -18582170
54 feet Y = -5663845
58 meter
Z = 6344151
07 Z = 1933697
25
XDOT = 10336
228967 XDOT = 3150
482589
YDOT = 11968
385216 feet/sec YDOT = 3647
963814 meter/sec
ZDOT = 18415
411527 ZDOT = 5613
017434
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 10210
45636725
00016717 00000-0 10270-3 0 9133
2 25544 51
6439 14
2663 0007177 164
7454 195
3926 15
71433031 30124
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210
45636725 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 14
2663 deg
Eccentricity:
0007177
Arg of perigee: 164
7454 deg
Mean anomaly: 195
3926 deg
Mean motion: 15
71433031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 291
Coasting Arc #15 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2010/211/09:31:03
569
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2037668
50 A = 6727999
17 meter
Y = -3814986
77 meter E =
0018139
Z = -5168692
67 I = 51
67848
XDOT = 7265
536102 Wp = 120
89460
YDOT = 2155
959606 meter/sec RA = 8
93378 deg
ZDOT = 1267
164843 TA = 161
27299
MA = 161
20616
Ha = 195
753 n
mi
Hp = 186
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6685264
11 X = 2105285
16
Y = -12516360
80 feet Y = -3791822
06 meter
Z = -16957653
10 Z = -5158629
74
XDOT = 23837
060701 XDOT = 7234
732205
YDOT = 7073
358289 feet/sec YDOT = 2237
034888 meter/sec
ZDOT = 4157
364970 ZDOT = 1302
385595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12505411
03 X = -3811649
28
Y = -6806694
78 feet Y = -2074680
57 meter
Z = -16917376
98 Z = -5156416
50
XDOT = 6617
400471 XDOT = 2016
983664
YDOT = -22888
126501 feet/sec YDOT = -6976
300958 meter/sec
ZDOT = 4298
183432 ZDOT = 1310
086310
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 10211
41027645
00016717 00000-0 10270-3 0 9146
2 25544 51
6431 9
3854 0007145 167
2492 192
8851 15
71434949 30272
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211
41027645 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 9
3854 deg
Eccentricity:
0007145
Arg of perigee: 167
2492 deg
Mean anomaly: 192
8851 deg
Mean motion: 15
71434949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 302
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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