Date:
October 29th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15392 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 413)
---------------------------------------
Vector Time (GMT): 2010/299/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3693177
80 A = 6727295
54 meter
Y = -2617360
51 meter E =
0020657
Z = -4995312
26 I = 51
29109
XDOT = 2444
495677 Wp = 111
94309
YDOT = -7035
996051 meter/sec RA = 277
50162 deg
ZDOT = 1877
941738 TA = 176
32223
MA = 176
30702
Ha = 195
994 n
mi
Hp = 184
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12116725
07 X = -3639368
54
Y = -8587140
78 feet Y = -2658358
88 meter
Z = -16388819
77 Z = -5013123
54
XDOT = 8019
998939 XDOT = 2513
868866
YDOT = -23083
976544 feet/sec YDOT = -7008
272383 meter/sec
ZDOT = 6161
226175 ZDOT = 1889
985776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12486928
89 X = 3806015
93
Y = -7892152
48 feet Y = -2405528
08 meter
Z = -16460193
27 Z = -5017066
91
XDOT = 17791
937041 XDOT = 5422
982410
YDOT = 15190
046347 feet/sec YDOT = 4629
926126 meter/sec
ZDOT = 6209
555389 ZDOT = 1892
672483
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 10299
60650684
00016717 00000-0 10270-3 0 9003
2 25544 51
6446 278
1944 0007833 125
2987 234
8909 15
71897499 4142
Satellite: ISS
Catalog Number: 25544
Epoch time: 10299
60650684 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 278
1944 deg
Eccentricity:
0007833
Arg of perigee: 125
2987 deg
Mean anomaly: 234
8909 deg
Mean motion: 15
71897499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 414
Checksum: 349
Coasting Arc #2 (Orbit 429)
---------------------------------------
Vector Time (GMT): 2010/300/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1092816
55 A = 6737570
69 meter
Y = 6562239
03 meter E =
0017485
Z = -1023070
72 I = 51
32411
XDOT = -4654
696941 Wp = 136
12279
YDOT = -1683
267254 meter/sec RA = 272
38379 deg
ZDOT = -5897
457847 TA = 55
10418
MA = 54
93997
Ha = 195
853 n
mi
Hp = 184
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3585356
13 X = -1161145
50
Y = 21529655
60 feet Y = 6549636
48 meter
Z = -3356531
23 Z = -1028545
53
XDOT = -15271
315423 XDOT = -4606
878964
YDOT = -5522
530361 feet/sec YDOT = -1735
051343 meter/sec
ZDOT = -19348
614984 ZDOT = -5919
954761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18788161
70 X = -5726631
69
Y = -11101248
35 feet Y = -3383660
50 meter
Z = -3378522
71 Z = -1029773
72
XDOT = 9815
289025 XDOT = 2991
700095
YDOT = -10767
799976 feet/sec YDOT = -3282
025433 meter/sec
ZDOT = -19438
784216 ZDOT = -5924
941429
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 10300
62367892
00016717 00000-0 10270-3 0 9015
2 25544 51
6454 272
9873 0007845 129
2112 230
9748 15
71944843 4303
Satellite: ISS
Catalog Number: 25544
Epoch time: 10300
62367892 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 272
9873 deg
Eccentricity:
0007845
Arg of perigee: 129
2112 deg
Mean anomaly: 230
9748 deg
Mean motion: 15
71944843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 430
Checksum: 312
Coasting Arc #3 (Orbit 445)
---------------------------------------
Vector Time (GMT): 2010/301/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4210581
16 A = 6725807
52 meter
Y = 259870
59 meter E =
0009289
Z = 5231033
86 I = 51
28510
XDOT = 38
122873 Wp = 118
79111
YDOT = 7693
454346 meter/sec RA = 267
22752 deg
ZDOT = -416
745072 TA = 335
16154
MA = 335
20622
Ha = 195
558 n
mi
Hp = 184
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13814242
66 X = 4181950
43
Y = 852593
81 feet Y = 306795
63 meter
Z = 17162184
57 Z = 5251419
69
XDOT = 125
075044 XDOT = -45
885085
YDOT = 25240
991949 feet/sec YDOT = 7693
410956 meter/sec
ZDOT = -1367
273859 ZDOT = -416
763733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5532986
70 X = -1686454
34
Y = 12575154
14 feet Y = 3832906
98 meter
Z = 17243907
68 Z = 5255943
06
XDOT = -22819
143286 XDOT = -6955
274873
YDOT = -8182
490167 feet/sec YDOT = -2494
023003 meter/sec
ZDOT = -1367
394060 ZDOT = -416
781710
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 10301
64082165
00016717 00000-0 10270-3 0 9026
2 25544 51
6453 267
7810 0007759 133
3573 226
8237 15
72014672 4469
Satellite: ISS
Catalog Number: 25544
Epoch time: 10301
64082165 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 267
7810 deg
Eccentricity:
0007759
Arg of perigee: 133
3573 deg
Mean anomaly: 226
8237 deg
Mean motion: 15
72014672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 446
Checksum: 299
Coasting Arc #4 (Orbit 460)
---------------------------------------
Vector Time (GMT): 2010/302/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1148373
61 A = 6737746
74 meter
Y = -6631773
62 meter E =
0013585
Z = -279982
20 I = 51
32767
XDOT = 4699
990772 Wp = 77
85371
YDOT = -1056
615843 meter/sec RA = 262
08392 deg
ZDOT = 5998
217528 TA = 279
09463
MA = 279
24832
Ha = 195
627 n
mi
Hp = 184
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3767629
97 X = -1072770
42
Y = -21757787
47 feet Y = -6644192
70 meter
Z = -918576
76 Z = -285377
52
XDOT = 15419
917230 XDOT = 4682
318052
YDOT = -3466
587411 feet/sec YDOT = -1004
156612 meter/sec
ZDOT = 19679
191366 ZDOT = 6021
007471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21784609
97 X = 6639949
12
Y = 3603743
86 feet Y = 1098421
13 meter
Z = -940177
14 Z = -286565
99
XDOT = -1497
501056 XDOT = -456
438322
YDOT = 14002
713305 feet/sec YDOT = 4268
027015 meter/sec
ZDOT = 19770
565486 ZDOT = 6026
068360
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 10302
59436820
00016717 00000-0 10270-3 0 9033
2 25544 51
6449 262
8987 0007788 136
6288 223
5488 15
72029555 4611
Satellite: ISS
Catalog Number: 25544
Epoch time: 10302
59436820 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 262
8987 deg
Eccentricity:
0007788
Arg of perigee: 136
6288 deg
Mean anomaly: 223
5488 deg
Mean motion: 15
72029555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 461
Checksum: 338
Coasting Arc #5 (Orbit 476)
---------------------------------------
Vector Time (GMT): 2010/303/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3795737
02 A = 6725897
12 meter
Y = 2026505
26 meter E =
0019789
Z = -5185566
28 I = 51
29423
XDOT = -2490
169710 Wp = 101
90553
YDOT = -7200
548469 meter/sec RA = 256
95075 deg
ZDOT = -998
436098 TA = 158
55134
MA = 158
46831
Ha = 195
473 n
mi
Hp = 184
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12453205
46 X = -3792924
81
Y = 6648639
29 feet Y = 1984074
73 meter
Z = -17013012
73 Z = -5203999
39
XDOT = -8169
848129 XDOT = -2404
616480
YDOT = -23623
846684 feet/sec YDOT = -7227
916697 meter/sec
ZDOT = -3275
708983 ZDOT = -1010
325635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2453309
39 X = -747768
70
Y = -13811139
25 feet Y = -4209635
24 meter
Z = -17086925
95 Z = -5208095
03
XDOT = 23980
696163 XDOT = 7309
316191
YDOT = -177
403765 feet/sec YDOT = -54
072668 meter/sec
ZDOT = -3323
357268 ZDOT = -1012
959295
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 10303
61145572
00016717 00000-0 10270-3 0 9049
2 25544 51
6455 257
6906 0007821 140
3616 219
8120 15
72087921 4775
Satellite: ISS
Catalog Number: 25544
Epoch time: 10303
61145572 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 257
6906 deg
Eccentricity:
0007821
Arg of perigee: 140
3616 deg
Mean anomaly: 219
8120 deg
Mean motion: 15
72087921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 477
Checksum: 298
Coasting Arc #6 (Orbit 492)
---------------------------------------
Vector Time (GMT): 2010/304/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3125301
07 A = 6736618
24 meter
Y = 5774250
37 meter E =
0021378
Z = 1454527
11 I = 51
33860
XDOT = -3721
919459 Wp = 127
87685
YDOT = 3481
552356 meter/sec RA = 251
78439 deg
ZDOT = -5779
313014 TA = 36
04253
MA = 35
89857
Ha = 195
356 n
mi
Hp = 184
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10253612
44 X = 3053434
13
Y = 18944390
97 feet Y = 5808797
58 meter
Z = 4772070
58 Z = 1469535
29
XDOT = -12211
021848 XDOT = -3732
498965
YDOT = 11422
415866 feet/sec YDOT = 3439
872296 meter/sec
ZDOT = -18961
000702 ZDOT = -5797
420137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21123279
11 X = -6438375
47
Y = 4154000
05 feet Y = 1266139
22 meter
Z = 4832239
45 Z = 1472866
58
XDOT = -7022
210871 XDOT = -2140
369874
YDOT = -13398
354575 feet/sec YDOT = -4083
818475 meter/sec
ZDOT = -19033
610108 ZDOT = -5801
444361
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 10304
62851436
00016717 00000-0 10270-3 0 9055
2 25544 51
6455 252
4827 0007855 144
5250 215
6436 15
72113095 4931
Satellite: ISS
Catalog Number: 25544
Epoch time: 10304
62851436 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 252
4827 deg
Eccentricity:
0007855
Arg of perigee: 144
5250 deg
Mean anomaly: 215
6436 deg
Mean motion: 15
72113095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 493
Checksum: 300
Coasting Arc #7 (Orbit 508)
---------------------------------------
Vector Time (GMT): 2010/305/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2527817
15 A = 6727113
26 meter
Y = -3923666
65 meter E =
0014222
Z = 4839696
52 I = 51
31775
XDOT = 4518
655790 Wp = 136
18778
YDOT = 5789
342705 meter/sec RA = 246
67329 deg
ZDOT = 2319
239909 TA = 291
04476
MA = 291
19681
Ha = 195
158 n
mi
Hp = 184
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8293363
34 X = 2547993
68
Y = -12872922
08 feet Y = -3895286
05 meter
Z = 15878269
43 Z = 4852026
05
XDOT = 14824
986188 XDOT = 4442
315811
YDOT = 18993
906511 feet/sec YDOT = 5839
446297 meter/sec
ZDOT = 7609
054818 ZDOT = 2341
006200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10064581
59 X = 3067684
47
Y = 11472736
46 feet Y = 3496890
07 meter
Z = 15927710
26 Z = 4854766
09
XDOT = -21533
904875 XDOT = -6563
534206
YDOT = 8141
503421 feet/sec YDOT = 2481
530243 meter/sec
ZDOT = 7696
332882 ZDOT = 2345
842263
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 10305
64554237
00016717 00000-0 10270-3 0 9068
2 25544 51
6454 247
2745 0007823 148
7816 211
3812 15
72181863 5097
Satellite: ISS
Catalog Number: 25544
Epoch time: 10305
64554237 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 247
2745 deg
Eccentricity:
0007823
Arg of perigee: 148
7816 deg
Mean anomaly: 211
3812 deg
Mean motion: 15
72181863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 509
Checksum: 309
Coasting Arc #8 (Orbit 523)
---------------------------------------
Vector Time (GMT): 2010/306/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4605242
44 A = 6734340
38 meter
Y = -4208159
13 meter E =
0008507
Z = -2549069
75 I = 51
35648
XDOT = 1916
355977 Wp = 116
12610
YDOT = -5274
384747 meter/sec RA = 241
48894 deg
ZDOT = 5255
017496 TA = 214
90783
MA = 214
96364
Ha = 195
054 n
mi
Hp = 184
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15109063
13 X = -4545460
57
Y = -13806296
36 feet Y = -4259323
59 meter
Z = -8363089
73 Z = -2571297
06
XDOT = 6287
257142 XDOT = 1949
664231
YDOT = -17304
411901 feet/sec YDOT = -5252
768397 meter/sec
ZDOT = 17240
871051 ZDOT = 5264
408527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17283460
81 X = 5267998
85
Y = -10894070
41 feet Y = -3320512
66 meter
Z = -8452223
98 Z = -2576237
87
XDOT = 14271
362444 XDOT = 4349
911273
YDOT = 9260
839886 feet/sec YDOT = 2822
703997 meter/sec
ZDOT = 17278
525732 ZDOT = 5266
494643
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 10306
59898048
00016717 00000-0 10270-3 0 9075
2 25544 51
6461 242
3913 0007786 152
2771 207
8807 15
72228308 5243
Satellite: ISS
Catalog Number: 25544
Epoch time: 10306
59898048 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 242
3913 deg
Eccentricity:
0007786
Arg of perigee: 152
2771 deg
Mean anomaly: 207
8807 deg
Mean motion: 15
72228308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 524
Checksum: 322
Coasting Arc #9 (Orbit 539)
---------------------------------------
Vector Time (GMT): 2010/307/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -743681
72 A = 6729002
68 meter
Y = 5115236
61 meter E =
0011983
Z = -4315577
76 I = 51
35501
XDOT = -5780
298530 Wp = 109
32285
YDOT = -3731
116054 meter/sec RA = 236
39292 deg
ZDOT = -3438
055414 TA = 125
81917
MA = 125
70777
Ha = 194
844 n
mi
Hp = 184
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2439900
66 X = -779861
12
Y = 16782272
35 feet Y = 5106717
84 meter
Z = -14158719
67 Z = -4319278
76
XDOT = -18964
234022 XDOT = -5721
444994
YDOT = -12241
194402 feet/sec YDOT = -3795
425908 meter/sec
ZDOT = -11279
709363 ZDOT = -3465
993723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15682740
29 X = -4780099
24
Y = -6420988
58 feet Y = -1957117
32 meter
Z = -14173555
86 Z = -4320099
83
XDOT = 16054
914145 XDOT = 4893
537831
YDOT = -14151
321418 feet/sec YDOT = -4313
322768 meter/sec
ZDOT = -11391
750165 ZDOT = -3472
205450
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 10307
61595181
00016717 00000-0 10270-3 0 9082
2 25544 51
6468 237
1826 0007674 156
3870 203
7646 15
72273291 5401
Satellite: ISS
Catalog Number: 25544
Epoch time: 10307
61595181 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 237
1826 deg
Eccentricity:
0007674
Arg of perigee: 156
3870 deg
Mean anomaly: 203
7646 deg
Mean motion: 15
72273291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 540
Checksum: 317
Coasting Arc #10 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2010/308/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5324174
15 A = 6731783
06 meter
Y = 2240646
50 meter E =
0016523
Z = 3437008
22 I = 51
38238
XDOT = 329
989446 Wp = 114
94015
YDOT = 6211
118649 meter/sec RA = 231
20141 deg
ZDOT = -4550
130000 TA = 24
18239
MA = 24
10492
Ha = 194
648 n
mi
Hp = 184
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17467762
95 X = 5282026
23
Y = 7351202
43 feet Y = 2299949
03 meter
Z = 11276273
68 Z = 3462771
42
XDOT = 1082
642540 XDOT = 282
615425
YDOT = 20377
685855 feet/sec YDOT = 6214
543806 meter/sec
ZDOT = -14928
248031 ZDOT = -4548
642075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11154577
28 X = -3399915
16
Y = 15244588
58 feet Y = 4646550
60 meter
Z = 11379595
44 Z = 3468500
69
XDOT = -18989
082994 XDOT = -5787
872497
YDOT = -2730
734173 feet/sec YDOT = -832
327776 meter/sec
ZDOT = -14922
274610 ZDOT = -4548
309301
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 10308
63289484
00016717 00000-0 10270-3 0 9092
2 25544 51
6465 231
9741 0007714 159
8920 200
2548 15
72301803 5566
Satellite: ISS
Catalog Number: 25544
Epoch time: 10308
63289484 = yrday
fracday
Element set: 909
Inclination: 51
6465 deg
RA of node: 231
9741 deg
Eccentricity:
0007714
Arg of perigee: 159
8920 deg
Mean anomaly: 200
2548 deg
Mean motion: 15
72301803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 312
Coasting Arc #11 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2010/309/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1336191
21 A = 6731330
61 meter
Y = -5528750
20 meter E =
0016318
Z = 3595102
82 I = 51
40141
XDOT = 6176
758371 Wp = 120
09885
YDOT = 1373
007072 meter/sec RA = 226
11241 deg
ZDOT = 4384
303911 TA = 283
02927
MA = 283
21140
Ha = 194
604 n
mi
Hp = 185
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4383829
44 X = -1291733
32
Y = -18138944
22 feet Y = -5543443
73 meter
Z = 11794956
77 Z = 3588719
36
XDOT = 20264
955287 XDOT = 6139
647222
YDOT = 4504
616377 feet/sec YDOT = 1441
871777 meter/sec
ZDOT = 14384
199184 ZDOT = 4414
221444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18670997
07 X = 5690919
91
Y = -486307
14 feet Y = -148226
42 meter
Z = 11769351
59 Z = 3587298
36
XDOT = -8737
192348 XDOT = -2663
096228
YDOT = 17394
117385 feet/sec YDOT = 5301
726979 meter/sec
ZDOT = 14504
188244 ZDOT = 4420
876577
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 10309
64980745
00016717 00000-0 10270-3 0 9104
2 25544 51
6470 226
7650 0007625 164
1842 195
9560 15
72338140 5722
Satellite: ISS
Catalog Number: 25544
Epoch time: 10309
64980745 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 226
7650 deg
Eccentricity:
0007625
Arg of perigee: 164
1842 deg
Mean anomaly: 195
9560 deg
Mean motion: 15
72338140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 310
Coasting Arc #12 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2010/310/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5290407
89 A = 6729102
02 meter
Y = -184436
98 meter E =
0013653
Z = -4168900
78 I = 51
41650
XDOT = -2679
223840 Wp = 138
89379
YDOT = -6198
634371 meter/sec RA = 220
92205 deg
ZDOT = 3670
912504 TA = 168
78164
MA = 168
75117
Ha = 194
345 n
mi
Hp = 185
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17356981
27 X = -5267699
87
Y = -605108
22 feet Y = -243470
40 meter
Z = -13677495
99 Z = -4194547
24
XDOT = -8790
104463 XDOT = -2627
543628
YDOT = -20336
726939 feet/sec YDOT = -6228
306221 meter/sec
ZDOT = 12043
676193 ZDOT = 3658
021755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3984251
05 X = 1214399
72
Y = -16820587
19 feet Y = -5126914
98 meter
Z = -13780364
34 Z = -4200255
05
XDOT = 20453
360319 XDOT = 6234
184225
YDOT = -4988
569361 feet/sec YDOT = -1520
515941 meter/sec
ZDOT = 11991
970450 ZDOT = 3655
152593
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 10310
60313535
00016717 00000-0 10270-3 0 9110
2 25544 51
6468 221
8815 0007567 169
3293 190
8032 15
72398583 5871
Satellite: ISS
Catalog Number: 25544
Epoch time: 10310
60313535 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 221
8815 deg
Eccentricity:
0007567
Arg of perigee: 169
3293 deg
Mean anomaly: 190
8032 deg
Mean motion: 15
72398583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 587
Checksum: 315
Coasting Arc #13 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2010/311/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3296989
91 A = 6733301
76 meter
Y = 5146965
09 meter E =
0011071
Z = -2814741
61 I = 51
45386
XDOT = -5707
514865 Wp = 154
28227
YDOT = 881
548773 meter/sec RA = 215
83293 deg
ZDOT = -5090
682806 TA = 58
04876
MA = 57
94115
Ha = 194
251 n
mi
Hp = 185
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10816896
03 X = 3252864
45
Y = 16886368
41 feet Y = 5183587
45 meter
Z = -9234716
57 Z = -2798831
28
XDOT = -18725
442469 XDOT = -5692
217981
YDOT = 2892
220383 feet/sec YDOT = 817
809715 meter/sec
ZDOT = -16701
715242 ZDOT = -5118
373504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18562137
86 X = -5657739
62
Y = 7666577
25 feet Y = 2336772
74 meter
Z = -9170894
13 Z = -2795288
53
XDOT = 1055
101258 XDOT = 321
594863
YDOT = -17488
886267 feet/sec YDOT = -5330
612534 meter/sec
ZDOT = -16812
796140 ZDOT = -5124
540264
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 10311
61999114
00016717 00000-0 10270-3 0 9126
2 25544 51
6464 216
6726 0007664 174
3565 185
7685 15
72412396 6031
Satellite: ISS
Catalog Number: 25544
Epoch time: 10311
61999114 = yrday
fracday
Element set: 912
Inclination: 51
6464 deg
RA of node: 216
6726 deg
Eccentricity:
0007664
Arg of perigee: 174
3565 deg
Mean anomaly: 185
7685 deg
Mean motion: 15
72412396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 321
Coasting Arc #14 (Orbit 618)
---------------------------------------
Vector Time (GMT): 2010/312/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4518429
49 A = 6726694
66 meter
Y = -1664592
63 meter E =
0007992
Z = 4689254
20 I = 51
45801
XDOT = 4805
211243 Wp = 119
12587
YDOT = 5370
305093 meter/sec RA = 210
65206 deg
ZDOT = -2724
156260 TA = 357
75027
MA = 357
75386
Ha = 193
781 n
mi
Hp = 185
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14824243
73 X = 4513927
35
Y = -5461261
90 feet Y = -1614090
32 meter
Z = 15384692
25 Z = 4711194
21
XDOT = 15765
128750 XDOT = 4758
036132
YDOT = 17619
111199 feet/sec YDOT = 5423
776267 meter/sec
ZDOT = -8937
520539 ZDOT = -2700
926211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2995441
79 X = 913010
66
Y = 15423835
78 feet Y = 4701185
15 meter
Z = 15472716
56 Z = 4716084
01
XDOT = -18829
169943 XDOT = -5739
130999
YDOT = 12528
007360 feet/sec YDOT = 3818
536643 meter/sec
ZDOT = -8844
323983 ZDOT = -2695
749950
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 10312
63681590
00016717 00000-0 10270-3 0 9136
2 25544 51
6461 211
4630 0007485 178
3020 181
8169 15
72526191 6196
Satellite: ISS
Catalog Number: 25544
Epoch time: 10312
63681590 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 211
4630 deg
Eccentricity:
0007485
Arg of perigee: 178
3020 deg
Mean anomaly: 181
8169 deg
Mean motion: 15
72526191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 619
Checksum: 296
Coasting Arc #15 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2010/313/14:15:05
655
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4980871
05 A = 6734730
47 meter
Y = -4093012
75 meter E =
0012870
Z = 1941774
24 I = 51
51056
XDOT = 4485
813317 Wp = 99
68879
YDOT = -2787
794823 meter/sec RA = 205
55493 deg
ZDOT = 5596
713798 TA = 281
93170
MA = 282
07596
Ha = 193
777 n
mi
Hp = 185
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16341440
47 X = -4944165
00
Y = -13428519
52 feet Y = -4148506
75 meter
Z = 6370650
41 Z = 1917665
58
XDOT = 14717
235292 XDOT = 4489
465211
YDOT = -9146
308475 feet/sec YDOT = -2737
611738 meter/sec
ZDOT = 18361
921910 ZDOT = 5618
514975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15667315
23 X = 4775397
68
Y = -14252235
91 feet Y = -4344081
51 meter
Z = 6273914
62 Z = 1912289
17
XDOT = 5884
920212 XDOT = 1793
723681
YDOT = 14640
013496 feet/sec YDOT = 4462
276114 meter/sec
ZDOT = 18449
401378 ZDOT = 5623
377540
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 10313
65361324
00016717 00000-0 10270-3 0 9140
2 25544 51
6449 206
2527 0007551 182
5609 177
5516 15
72547341 6359
Satellite: ISS
Catalog Number: 25544
Epoch time: 10313
65361324 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 206
2527 deg
Eccentricity:
0007551
Arg of perigee: 182
5609 deg
Mean anomaly: 177
5516 deg
Mean motion: 15
72547341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 303
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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