Date:
April 22nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3686)
---------------------------------------
Vector Time (GMT): 2009/110/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4228443
05 A = 6735694
32 meter
Y = -4936047
08 meter E =
0006268
Z = -1752852
47 I = 51
36280
XDOT = 2784
619886 Wp = 318
72666
YDOT = -4400
657846 meter/sec RA = 241
86444 deg
ZDOT = 5668
014631 TA = 21
80110
MA = 21
77444
Ha = 191
089 n
mi
Hp = 190
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13872844
66 X = -4164418
00
Y = -16194380
20 feet Y = -4982974
08 meter
Z = -5750828
30 Z = -1773238
64
XDOT = 9135
892013 XDOT = 2806
087520
YDOT = -14437
853826 feet/sec YDOT = -4369
398382 meter/sec
ZDOT = 18595
848528 ZDOT = 5681
594658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18620682
51 X = -5675584
03
Y = -10346851
82 feet Y = -3153720
43 meter
Z = -5830834
88 Z = -1777238
47
XDOT = 2667
754311 XDOT = 813
131514
YDOT = -15322
714229 feet/sec YDOT = -4670
363297 meter/sec
ZDOT = 18648
563779 ZDOT = 5684
082240
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 09110
48264461
00010596 00000-0 82463-4 0 9006
2 25544 51
6400 242
7464 0008829 262
3492 97
6668 15
72282945 36873
Satellite: ISS
Catalog Number: 25544
Epoch time: 09110
48264461 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 242
7464 deg
Eccentricity:
0008829
Arg of perigee: 262
3492 deg
Mean anomaly: 97
6668 deg
Mean motion: 15
72282945 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3687
Checksum: 329
Coasting Arc #2 (Orbit 3702)
---------------------------------------
Vector Time (GMT): 2009/111/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1595487
99 A = 6727167
62 meter
Y = 4493347
74 meter E =
0003765
Z = -4748480
98 I = 51
34953
XDOT = -5533
374130 Wp = 33
09518
YDOT = -4687
257263 meter/sec RA = 236
75876 deg
ZDOT = -2574
054004 TA = 211
53248
MA = 211
55505
Ha = 190
694 n
mi
Hp = 190
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5234540
66 X = -1622547
34
Y = 14741954
54 feet Y = 4475354
57 meter
Z = -15579005
84 Z = -4756297
84
XDOT = -18154
114601 XDOT = -5468
044790
YDOT = -15378
140626 feet/sec YDOT = -4748
769515 meter/sec
ZDOT = -8445
059067 ZDOT = -2600
776461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 592011
89 X = 180445
22
Y = 15602355
65 feet Y = 4755598
00 meter
Z = -15609198
65 Z = -4757683
75
XDOT = -21331
465271 XDOT = -6501
830615
YDOT = -7751
195909 feet/sec YDOT = -2362
564513 meter/sec
ZDOT = -8549
806109 ZDOT = -2605
980902
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 09111
49957811
00010596 00000-0 82463-4 0 9017
2 25544 51
6402 237
5376 0008872 267
0396 92
9751 15
72310078 37031
Satellite: ISS
Catalog Number: 25544
Epoch time: 09111
49957811 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 237
5376 deg
Eccentricity:
0008872
Arg of perigee: 267
0396 deg
Mean anomaly: 92
9751 deg
Mean motion: 15
72310078 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3703
Checksum: 318
Coasting Arc #3 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2009/112/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5282179
84 A = 6733679
68 meter
Y = 3161915
67 meter E =
0005123
Z = 2720890
78 I = 51
38931
XDOT = -743
721297 Wp = 118
43578
YDOT = 5675
271176 meter/sec RA = 231
57311 deg
ZDOT = -5146
414311 TA = 30
41032
MA = 30
38062
Ha = 190
228 n
mi
Hp = 190
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17329986
35 X = 5233212
42
Y = 10373739
09 feet Y = 3220710
42 meter
Z = 8926807
02 Z = 2746432
86
XDOT = -2440
030501 XDOT = -782
127183
YDOT = 18619
656088 feet/sec YDOT = 5666
739493 meter/sec
ZDOT = -16884
561387 ZDOT = -5150
120885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19927269
33 X = 6073831
69
Y = 3008491
59 feet Y = 916988
24 meter
Z = 9026831
59 Z = 2751378
27
XDOT = 5147
759818 XDOT = 1569
037193
YDOT = 16654
393043 feet/sec YDOT = 5076
258999 meter/sec
ZDOT = -16898
604849 ZDOT = -5150
694758
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 09112
51649625
00010596 00000-0 82463-4 0 9023
2 25544 51
6405 232
3277 0008835 270
6315 89
3835 15
72318841 37193
Satellite: ISS
Catalog Number: 25544
Epoch time: 09112
51649625 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 232
3277 deg
Eccentricity:
0008835
Arg of perigee: 270
6315 deg
Mean anomaly: 89
3835 deg
Mean motion: 15
72318841 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3719
Checksum: 316
Coasting Arc #4 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2009/113/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -345274
41 A = 6729093
64 meter
Y = -5241219
02 meter E =
0002239
Z = 4206670
98 I = 51
39499
XDOT = 6328
877563 Wp = 157
32733
YDOT = 2481
115781 meter/sec RA = 226
48042 deg
ZDOT = 3608
085911 TA = 255
79541
MA = 255
82028
Ha = 190
709 n
mi
Hp = 190
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1132790
08 X = -307076
18
Y = -17195600
47 feet Y = -5244866
37 meter
Z = 13801413
98 Z = 4205086
56
XDOT = 20764
034000 XDOT = 6283
135183
YDOT = 8140
143637 feet/sec YDOT = 2551
633340 meter/sec
ZDOT = 11837
552203 ZDOT = 3638
720962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7937010
60 X = -2419200
83
Y = -15302212
37 feet Y = -4664114
33 meter
Z = 13794820
63 Z = 4204661
33
XDOT = 21110
382885 XDOT = 6434
444703
YDOT = -162
186148 feet/sec YDOT = -49
434338 meter/sec
ZDOT = 11957
425123 ZDOT = 3644
623178
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 09113
53339633
00010596 00000-0 82463-4 0 9032
2 25544 51
6418 227
1181 0008906 275
1416 84
8730 15
72388938 37350
Satellite: ISS
Catalog Number: 25544
Epoch time: 09113
53339633 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 227
1181 deg
Eccentricity:
0008906
Arg of perigee: 275
1416 deg
Mean anomaly: 84
8730 deg
Mean motion: 15
72388938 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3735
Checksum: 322
Coasting Arc #5 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2009/114/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5598477
22 A = 6731253
78 meter
Y = -1143951
27 meter E =
0003542
Z = -3554113
90 I = 51
42367
XDOT = -1573
402395 Wp = 283
09927
YDOT = -6090
795155 meter/sec RA = 221
29092 deg
ZDOT = 4435
949224 TA = 34
40129
MA = 34
37836
Ha = 190
993 n
mi
Hp = 189
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18367707
41 X = -5568003
64
Y = -3753120
97 feet Y = -1206386
36 meter
Z = -11660478
69 Z = -3581237
88
XDOT = -5162
081350 XDOT = -1526
726681
YDOT = -19982
923736 feet/sec YDOT = -6108
128833 meter/sec
ZDOT = 14553
639186 ZDOT = 4428
418909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18218322
70 X = -5552944
76
Y = 4131183
73 feet Y = 1259184
80 meter
Z = -11766537
07 Z = -3586440
50
XDOT = -12722
062018 XDOT = -3877
684503
YDOT = -14709
787190 feet/sec YDOT = -4483
543135 meter/sec
ZDOT = 14523
752088 ZDOT = 4426
839636
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 09114
48672843
00010596 00000-0 82463-4 0 9041
2 25544 51
6419 222
2350 0008960 280
0532 79
9619 15
72362891 37507
Satellite: ISS
Catalog Number: 25544
Epoch time: 09114
48672843 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 222
2350 deg
Eccentricity:
0008960
Arg of perigee: 280
0532 deg
Mean anomaly: 79
9619 deg
Mean motion: 15
72362891 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3750
Checksum: 318
Coasting Arc #6 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2009/115/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2384904
30 A = 6731408
12 meter
Y = 5219877
94 meter E =
0004302
Z = -3517559
52 I = 51
44765
XDOT = -6258
101643 Wp = 306
45570
YDOT = -160
938912 meter/sec RA = 216
20517 deg
ZDOT = -4475
510153 TA = 275
47479
MA = 275
52386
Ha = 191
248 n
mi
Hp = 189
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7824489
16 X = 2343445
57
Y = 17125583
78 feet Y = 5246315
58 meter
Z = -11540549
59 Z = -3506073
98
XDOT = -20531
829539 XDOT = -6234
095131
YDOT = -528
014804 feet/sec YDOT = -230
786347 meter/sec
ZDOT = -14683
432261 ZDOT = -4505
854437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14464009
88 X = 4408630
21
Y = 12097254
45 feet Y = 3687243
16 meter
Z = -11495276
77 Z = -3503760
36
XDOT = -17821
350828 XDOT = -5431
947732
YDOT = 7222
819569 feet/sec YDOT = 2201
515405 meter/sec
ZDOT = -14802
005247 ZDOT = -4511
651199
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 09115
50359990
00010596 00000-0 82463-4 0 9051
2 25544 51
6422 217
0258 0008871 283
6294 76
3880 15
72399588 37666
Satellite: ISS
Catalog Number: 25544
Epoch time: 09115
50359990 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 217
0258 deg
Eccentricity:
0008871
Arg of perigee: 283
6294 deg
Mean anomaly: 76
3880 deg
Mean motion: 15
72399588 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3766
Checksum: 347
Coasting Arc #7 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2009/116/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5170089
56 A = 6728814
22 meter
Y = -822404
04 meter E =
0005868
Z = 4229990
71 I = 51
46384
XDOT = 3830
793778 Wp = 11
98822
YDOT = 5631
348397 meter/sec RA = 211
01883 deg
ZDOT = -3580
776702 TA = 114
54916
MA = 114
48798
Ha = 191
429 n
mi
Hp = 189
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16962236
08 X = 5158352
55
Y = -2698176
00 feet Y = -764654
92 meter
Z = 13877922
29 Z = 4255079
04
XDOT = 12568
221055 XDOT = 3784
933547
YDOT = 18475
552485 feet/sec YDOT = 5673
930326 meter/sec
ZDOT = -11747
955058 ZDOT = -3562
277393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13932177
29 X = 4246527
64
Y = -9907730
84 feet Y = -3019876
36 meter
Z = 13975894
94 Z = 4259852
78
XDOT = 18798
711748 XDOT = 5729
847341
YDOT = 9935
410085 feet/sec YDOT = 3028
312994 meter/sec
ZDOT = -11675
243962 ZDOT = -3558
614360
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 09116
52045630
00010596 00000-0 82463-4 0 9068
2 25544 51
6420 211
8167 0008751 288
6983 71
3229 15
72416964 37820
Satellite: ISS
Catalog Number: 25544
Epoch time: 09116
52045630 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 211
8167 deg
Eccentricity:
0008751
Arg of perigee: 288
6983 deg
Mean anomaly: 71
3229 deg
Mean motion: 15
72416964 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3782
Checksum: 318
Coasting Arc #8 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2009/117/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4232925
03 A = 6733390
37 meter
Y = -4465408
35 meter E =
0008028
Z = 2722006
06 I = 51
50532
XDOT = 5374
400230 Wp = 40
95135
YDOT = -1948
477058 meter/sec RA = 205
93159 deg
ZDOT = 5158
546788 TA = 350
17446
MA = 350
19015
Ha = 191
645 n
mi
Hp = 189
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13887549
30 X = -4195900
75
Y = -14650289
86 feet Y = -4512536
58 meter
Z = 8930466
06 Z = 2701531
70
XDOT = 17632
546686 XDOT = 5370
729215
YDOT = -6392
641265 feet/sec YDOT = -1888
398295 meter/sec
ZDOT = 16924
366101 ZDOT = 5184
647067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19108468
37 X = -5824261
16
Y = -6617407
98 feet Y = -2016985
95 meter
Z = 8850118
13 Z = 2697516
00
XDOT = 12161
184654 XDOT = 3706
729082
YDOT = -12334
315641 feet/sec YDOT = -3759
499407 meter/sec
ZDOT = 17026
222102 ZDOT = 5189
592497
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 09117
53729541
00010596 00000-0 82463-4 0 9071
2 25544 51
6419 206
6067 0008833 292
8662 67
1567 15
72464841 37983
Satellite: ISS
Catalog Number: 25544
Epoch time: 09117
53729541 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 206
6067 deg
Eccentricity:
0008833
Arg of perigee: 292
8662 deg
Mean anomaly: 67
1567 deg
Mean motion: 15
72464841 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3798
Checksum: 344
Coasting Arc #9 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2009/118/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4073376
56 A = 6726572
71 meter
Y = 2488493
52 meter E =
0003126
Z = -4741894
26 I = 51
50959
XDOT = -5740
442096 Wp = 82
99587
YDOT = -4404
762553 meter/sec RA = 200
75662 deg
ZDOT = 2621
426362 TA = 212
79172
MA = 212
81112
Ha = 191
687 n
mi
Hp = 188
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13364096
32 X = -4077864
99
Y = 8164348
81 feet Y = 2442917
98 meter
Z = -15557395
88 Z = -4761693
68
XDOT = -18833
471443 XDOT = -5703
495245
YDOT = -14451
320713 feet/sec YDOT = -4468
749182 meter/sec
ZDOT = 8600
480191 ZDOT = 2593
628255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7814598
17 X = -2381889
52
Y = 13482566
16 feet Y = 4109486
17 meter
Z = -15634599
25 Z = -4765425
85
XDOT = -22494
593516 XDOT = -6856
352104
YDOT = -3198
156749 feet/sec YDOT = -974
798177 meter/sec
ZDOT = 8491
501382 ZDOT = 2588
209621
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 09118
49056982
00010596 00000-0 82463-4 0 9080
2 25544 51
6413 201
7236 0008837 297
1961 62
8300 15
72505574 38139
Satellite: ISS
Catalog Number: 25544
Epoch time: 09118
49056982 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 201
7236 deg
Eccentricity:
0008837
Arg of perigee: 297
1961 deg
Mean anomaly: 62
8300 deg
Mean motion: 15
72505574 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3813
Checksum: 319
Coasting Arc #10 (Orbit 3828)
---------------------------------------
Vector Time (GMT): 2009/119/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5671907
74 A = 6735031
06 meter
Y = 3119218
67 meter E =
0003291
Z = -1855020
03 I = 51
56487
XDOT = -3816
183846 Wp = 249
87045
YDOT = 3579
908662 meter/sec RA = 195
66275 deg
ZDOT = -5641
773974 TA = 310
72063
MA = 310
74921
Ha = 191
998 n
mi
Hp = 188
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18608621
20 X = 5645617
98
Y = 10233657
06 feet Y = 3182498
43 meter
Z = -6086023
73 Z = -1827529
26
XDOT = -12520
288209 XDOT = -3828
524430
YDOT = 11745
107158 feet/sec YDOT = 3537
165386 meter/sec
ZDOT = -18509
757134 ZDOT = -5660
342788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21266612
62 X = 6482063
53
Y = -197514
63 feet Y = -60202
46 meter
Z = -5978325
87 Z = -1822193
72
XDOT = -5093
070416 XDOT = -1552
367863
YDOT = 14765
761316 feet/sec YDOT = 4500
604049 meter/sec
ZDOT = -18582
079888 ZDOT = -5663
817950
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 09119
50738149
00010596 00000-0 82463-4 0 9096
2 25544 51
6403 196
5137 0008892 301
1628 58
8662 15
72491010 38298
Satellite: ISS
Catalog Number: 25544
Epoch time: 09119
50738149 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 196
5137 deg
Eccentricity:
0008892
Arg of perigee: 301
1628 deg
Mean anomaly: 58
8662 deg
Mean motion: 15
72491010 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3829
Checksum: 324
Coasting Arc #11 (Orbit 3844)
---------------------------------------
Vector Time (GMT): 2009/120/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2506451
43 A = 6725040
47 meter
Y = -3634257
60 meter E =
0008774
Z = 5077893
50 I = 51
56149
XDOT = 7057
799051 Wp = 337
41646
YDOT = 2608
087346 meter/sec RA = 190
50261 deg
ZDOT = -1610
078968 TA = 128
11752
MA = 128
03838
Ha = 192
098 n
mi
Hp = 188
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8223265
85 X = 2522236
46
Y = -11923417
32 feet Y = -3606141
14 meter
Z = 16659755
57 Z = 5090107
93
XDOT = 23155
508699 XDOT = 7035
931922
YDOT = 8556
717016 feet/sec YDOT = 2686
889632 meter/sec
ZDOT = -5282
411313 ZDOT = -1575
844989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1005861
84 X = 306586
69
Y = -14394229
34 feet Y = -4387361
10 meter
Z = 16707239
19 Z = 5092366
50
XDOT = 23287
325758 XDOT = 7097
976891
YDOT = -4375
097467 feet/sec YDOT = -1333
529708 meter/sec
ZDOT = -5148
371493 ZDOT = -1569
223631
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 09120
52417650
00010596 00000-0 82463-4 0 9103
2 25544 51
6409 191
3029 0009066 305
4839 54
5477 15
72555079 38453
Satellite: ISS
Catalog Number: 25544
Epoch time: 09120
52417650 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 191
3029 deg
Eccentricity:
0009066
Arg of perigee: 305
4839 deg
Mean anomaly: 54
5477 deg
Mean motion: 15
72555079 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3845
Checksum: 316
Coasting Arc #12 (Orbit 3860)
---------------------------------------
Vector Time (GMT): 2009/121/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6515966
54 A = 6736040
97 meter
Y = -1372064
93 meter E =
0014391
Z = 951022
38 I = 51
62696
XDOT = 1826
949841 Wp = 17
77748
YDOT = -4551
912047 meter/sec RA = 185
39763 deg
ZDOT = 5940
186603 TA = 352
61223
MA = 352
63341
Ha = 192
460 n
mi
Hp = 187
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21377842
99 X = -6504759
50
Y = -4501525
37 feet Y = -1444867
66 meter
Z = 3120152
16 Z = 919394
95
XDOT = 5993
929926 XDOT = 1848
857941
YDOT = -14934
094641 feet/sec YDOT = -4531
359862 meter/sec
ZDOT = 19488
801192 ZDOT = 5949
114892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20624527
85 X = -6286356
09
Y = 7256845
81 feet Y = 2211886
60 meter
Z = 2996379
65 Z = 913296
52
XDOT = -2194
808126 XDOT = -668
977517
YDOT = -14313
294535 feet/sec YDOT = -4362
692174 meter/sec
ZDOT = 19523
369970 ZDOT = 5950
723167
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 09121
54096071
00010596 00000-0 82463-4 0 9117
2 25544 51
6405 186
0929 0009012 310
8837 49
1544 15
72518190 38614
Satellite: ISS
Catalog Number: 25544
Epoch time: 09121
54096071 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 186
0929 deg
Eccentricity:
0009012
Arg of perigee: 310
8837 deg
Mean anomaly: 49
1544 deg
Mean motion: 15
72518190 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3861
Checksum: 301
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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