Date:
April 3rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25295 19 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 1155)
---------------------------------------
Vector Time (GMT): 2010/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 734424
93 A = 6728952
63 meter
Y = -6212176
16 meter E =
0017693
Z = 2465048
81 I = 51
32201
XDOT = 4891
247348 Wp = 91
45670
YDOT = 2696
274638 meter/sec RA = 258
35400 deg
ZDOT = 5304
388286 TA = 296
55352
MA = 296
73478
Ha = 191
645 n
mi
Hp = 181
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2409530
60 X = 791861
15
Y = -20381155
37 feet Y = -6203642
16 meter
Z = 8087430
47 Z = 2468756
39
XDOT = 16047
399436 XDOT = 4834
965628
YDOT = 8846
045400 feet/sec YDOT = 2750
656962 meter/sec
ZDOT = 17402
848707 ZDOT = 5328
013352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1196056
61 X = -364558
05
Y = -20482466
65 feet Y = -6243055
83 meter
Z = 8101967
19 Z = 2469479
60
XDOT = 15740
095148 XDOT = 4797
581001
YDOT = 6044
865191 feet/sec YDOT = 1842
474910 meter/sec
ZDOT = 17496
762736 ZDOT = 5333
013282
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 10092
55855761
00016717 00000-0 10270-3 0 9001
2 25544 51
6412 258
8565 0005841 133
1718 226
9934 15
74203020 11564
Satellite: ISS
Catalog Number: 25544
Epoch time: 10092
55855761 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 258
8565 deg
Eccentricity:
0005841
Arg of perigee: 133
1718 deg
Mean anomaly: 226
9934 deg
Mean motion: 15
74203020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 299
Coasting Arc #2 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2010/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4468496
04 A = 6722254
61 meter
Y = -2080530
52 meter E =
0016041
Z = -4586690
59 I = 51
30813
XDOT = 300
156406 Wp = 119
22003
YDOT = -7101
874545 meter/sec RA = 253
14984 deg
ZDOT = 2928
999439 TA = 179
99664
MA = 179
99663
Ha = 191
560 n
mi
Hp = 181
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14660420
08 X = -4422617
65
Y = -6825887
53 feet Y = -2130243
45 meter
Z = -15048197
46 Z = -4608287
17
XDOT = 984
765111 XDOT = 365
319912
YDOT = -23300
113338 feet/sec YDOT = -7098
153623 meter/sec
ZDOT = 9609
578211 ZDOT = 2930
616000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15602144
03 X = -4755533
50
Y = -3937352
14 feet Y = -1200104
93 meter
Z = -15134043
21 Z = -4612856
37
XDOT = -3796
828933 XDOT = -1157
273459
YDOT = -21914
989448 feet/sec YDOT = -6679
688784 meter/sec
ZDOT = 9615
781323 ZDOT = 2930
890147
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 10093
51076516
00016717 00000-0 10270-3 0 9012
2 25544 51
6421 253
9651 0005867 135
9355 224
2277 15
74244198 11710
Satellite: ISS
Catalog Number: 25544
Epoch time: 10093
51076516 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 253
9651 deg
Eccentricity:
0005867
Arg of perigee: 135
9355 deg
Mean anomaly: 224
2277 deg
Mean motion: 15
74244198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 306
Coasting Arc #3 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2010/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 180411
60 A = 6728169
35 meter
Y = 6169254
31 meter E =
0010544
Z = -2675176
19 I = 51
33855
XDOT = -5304
919736 Wp = 132
31497
YDOT = -2080
908420 meter/sec RA = 248
03466 deg
ZDOT = -5176
548795 TA = 78
30279
MA = 78
18449
Ha = 191
350 n
mi
Hp = 181
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 591901
58 X = 124408
02
Y = 20240335
67 feet Y = 6170958
63 meter
Z = -8776824
78 Z = -2674435
84
XDOT = -17404
592310 XDOT = -5256
109609
YDOT = -6827
127363 feet/sec YDOT = -2139
958316 meter/sec
ZDOT = -16983
427806 ZDOT = -5202
201541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4811395
80 X = 1466513
44
Y = 19670460
21 feet Y = 5995556
27 meter
Z = -8773691
04 Z = -2674221
03
XDOT = -16907
206279 XDOT = -5153
316474
YDOT = -3455
907758 feet/sec YDOT = -1053
360685 meter/sec
ZDOT = -17085
394458 ZDOT = -5207
628231
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 10094
52642033
00016717 00000-0 10270-3 0 9028
2 25544 51
6421 248
7472 0005712 138
7730 221
3865 15
74313298 11876
Satellite: ISS
Catalog Number: 25544
Epoch time: 10094
52642033 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 248
7472 deg
Eccentricity:
0005712
Arg of perigee: 138
7730 deg
Mean anomaly: 221
3865 deg
Mean motion: 15
74313298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 298
Coasting Arc #4 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2010/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4790042
80 A = 6722521
16 meter
Y = 1535038
84 meter E =
0011787
Z = 4449233
62 I = 51
33175
XDOT = 722
818322 Wp = 95
97506
YDOT = 6983
808321 meter/sec RA = 242
82874 deg
ZDOT = -3181
684507 TA = 25
96866
MA = 25
90956
Ha = 191
184 n
mi
Hp = 181
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15715363
50 X = 4750908
20
Y = 5036216
68 feet Y = 1588385
18 meter
Z = 14597223
15 Z = 4472408
50
XDOT = 2371
451187 XDOT = 660
126411
YDOT = 22912
756958 feet/sec YDOT = 6991
540743 meter/sec
ZDOT = -10438
597463 ZDOT = -3178
325416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16359360
48 X = 4986333
07
Y = 1417633
53 feet Y = 432094
70 meter
Z = 14689339
40 Z = 4477310
65
XDOT = 7593
521732 XDOT = 2314
505424
YDOT = 20596
939984 feet/sec YDOT = 6277
947307 meter/sec
ZDOT = -10425
028540 ZDOT = -3177
548699
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 10095
54204382
00016717 00000-0 10270-3 0 9033
2 25544 51
6417 243
5292 0005784 143
2016 216
9546 15
74320022 12039
Satellite: ISS
Catalog Number: 25544
Epoch time: 10095
54204382 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 243
5292 deg
Eccentricity:
0005784
Arg of perigee: 143
2016 deg
Mean anomaly: 216
9546 deg
Mean motion: 15
74320022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 276
Coasting Arc #5 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2010/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1047845
58 A = 6727351
72 meter
Y = -5980079
71 meter E =
0016569
Z = 2887635
94 I = 51
36483
XDOT = 5659
840249 Wp = 100
06799
YDOT = 1445
690237 meter/sec RA = 237
71727 deg
ZDOT = 5020
447681 TA = 293
28979
MA = 293
46410
Ha = 191
055 n
mi
Hp = 181
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3437813
58 X = -994924
91
Y = -19619684
09 feet Y = -5991501
39 meter
Z = 9473871
19 Z = 2882674
20
XDOT = 18569
029688 XDOT = 5618
865335
YDOT = 4743
078204 feet/sec YDOT = 1508
752939 meter/sec
ZDOT = 16471
285042 ZDOT = 5047
843474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8102694
38 X = -2469701
25
Y = -18206421
79 feet Y = -5549317
36 meter
Z = 9453959
53 Z = 2881566
86
XDOT = 17742
711950 XDOT = 5407
978602
YDOT = 759
747480 feet/sec YDOT = 231
571032 meter/sec
ZDOT = 16580
177801 ZDOT = 5053
638194
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 10096
55763070
00016717 00000-0 10270-3 0 9040
2 25544 51
6427 238
3112 0005688 147
9362 212
2149 15
74427985 12192
Satellite: ISS
Catalog Number: 25544
Epoch time: 10096
55763070 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 238
3112 deg
Eccentricity:
0005688
Arg of perigee: 147
9362 deg
Mean anomaly: 212
2149 deg
Mean motion: 15
74427985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1219
Checksum: 316
Coasting Arc #6 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2010/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5088889
91 A = 6722813
39 meter
Y = -997518
83 meter E =
0013545
Z = -4292654
42 I = 51
36729
XDOT = -1619
882998 Wp = 126
02206
YDOT = -6668
383257 meter/sec RA = 232
51117 deg
ZDOT = 3469
727413 TA = 179
26278
MA = 179
26078
Ha = 190
926 n
mi
Hp = 181
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16695833
02 X = -5056504
45
Y = -3272699
57 feet Y = -1054244
90 meter
Z = -14083511
88 Z = -4317297
38
XDOT = -5314
576765 XDOT = -1562
050745
YDOT = -21877
897826 feet/sec YDOT = -6686
174269 meter/sec
ZDOT = 11383
620123 ZDOT = 3461
998792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16896050
43 X = -5149916
17
Y = 1102873
21 feet Y = 336155
75 meter
Z = -14181461
85 Z = -4322509
57
XDOT = -10738
808611 XDOT = -3273
188865
YDOT = -18529
873628 feet/sec YDOT = -5647
905482 meter/sec
ZDOT = 11352
682019 ZDOT = 3460
297479
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 10097
50971541
00016717 00000-0 10270-3 0 9051
2 25544 51
6430 233
4197 0005518 150
4195 209
7281 15
74440975 12349
Satellite: ISS
Catalog Number: 25544
Epoch time: 10097
50971541 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 233
4197 deg
Eccentricity:
0005518
Arg of perigee: 150
4195 deg
Mean anomaly: 209
7281 deg
Mean motion: 15
74440975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 304
Coasting Arc #7 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2010/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1739955
10 A = 6726349
19 meter
Y = 5658415
16 meter E =
0008952
Z = -3192968
71 I = 51
39906
XDOT = -5971
831464 Wp = 129
91297
YDOT = -854
166297 meter/sec RA = 227
40289 deg
ZDOT = -4782
462774 TA = 87
49111
MA = 87
38862
Ha = 190
763 n
mi
Hp = 181
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5708514
10 X = 1692063
14
Y = 18564354
21 feet Y = 5677604
43 meter
Z = -10475619
14 Z = -3184632
69
XDOT = -19592
622913 XDOT = -5938
603989
YDOT = -2802
382864 feet/sec YDOT = -920
761334 meter/sec
ZDOT = -15690
494664 ZDOT = -4811
392991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10625468
93 X = 3238642
93
Y = 16279401
21 feet Y = 4961961
49 meter
Z = -10442293
01 Z = -3182810
91
XDOT = -18336
181345 XDOT = -5588
868074
YDOT = 1860
233344 feet/sec YDOT = 566
999123 meter/sec
ZDOT = -15805
483916 ZDOT = -4817
511498
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 10098
52523856
00016717 00000-0 10270-3 0 9067
2 25544 51
6431 228
2004 0005470 154
2353 205
9084 15
74497624 12504
Satellite: ISS
Catalog Number: 25544
Epoch time: 10098
52523856 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 228
2004 deg
Eccentricity:
0005470
Arg of perigee: 154
2353 deg
Mean anomaly: 205
9084 deg
Mean motion: 15
74497624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1250
Checksum: 295
Coasting Arc #8 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2010/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5335245
74 A = 6723405
91 meter
Y = 473367
82 meter E =
0012676
Z = 4051400
71 I = 51
41149
XDOT = 2357
516974 Wp = 101
75536
YDOT = 6261
192239 meter/sec RA = 222
19650 deg
ZDOT = -3828
621141 TA = 27
73061
MA = 27
66308
Ha = 190
537 n
mi
Hp = 181
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17504087
06 X = 5309875
04
Y = 1553044
01 feet Y = 532888
12 meter
Z = 13291997
07 Z = 4077257
56
XDOT = 7734
635741 XDOT = 2305
926653
YDOT = 20541
969289 feet/sec YDOT = 6287
266688 meter/sec
ZDOT = -12561
092982 ZDOT = -3817
294100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17127579
16 X = 5220486
13
Y = -3564889
15 feet Y = -1086578
21 meter
Z = 13394767
38 Z = 4082725
10
XDOT = 13168
086992 XDOT = 4013
632915
YDOT = 16146
994014 feet/sec YDOT = 4921
603775 meter/sec
ZDOT = -12515
850038 ZDOT = -3814
831091
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 10099
54072866
00016717 00000-0 10270-3 0 9071
2 25544 51
6436 222
9820 0005464 156
9913 203
1497 15
74527579 12668
Satellite: ISS
Catalog Number: 25544
Epoch time: 10099
54072866 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 222
9820 deg
Eccentricity:
0005464
Arg of perigee: 156
9913 deg
Mean anomaly: 203
1497 deg
Mean motion: 15
74527579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1266
Checksum: 333
Coasting Arc #9 (Orbit 1281)
---------------------------------------
Vector Time (GMT): 2010/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2327313
69 A = 6725087
73 meter
Y = -5250053
29 meter E =
0015047
Z = 3492890
58 I = 51
44218
XDOT = 6250
549028 Wp = 111
48806
YDOT = 233
892173 meter/sec RA = 217
09285 deg
ZDOT = 4495
371572 TA = 290
15860
MA = 290
32039
Ha = 190
386 n
mi
Hp = 181
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7635543
60 X = -2285401
49
Y = -17224584
27 feet Y = -5275844
08 meter
Z = 11459614
78 Z = 3481686
71
XDOT = 20507
050616 XDOT = 6225
631368
YDOT = 767
362772 feet/sec YDOT = 303
650551 meter/sec
ZDOT = 14748
594395 ZDOT = 4525
676156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12608638
98 X = -3843113
16
Y = -14036847
35 feet Y = -4278431
07 meter
Z = 11414891
15 Z = 3479258
82
XDOT = 18649
887072 XDOT = 5684
485579
YDOT = -4604
628909 feet/sec YDOT = -1403
490891 meter/sec
ZDOT = 14869
037676 ZDOT = 4532
082684
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 10100
55618153
00016717 00000-0 10270-3 0 9081
2 25544 51
6446 217
7629 0005321 161
6432 198
4924 15
74641159 12829
Satellite: ISS
Catalog Number: 25544
Epoch time: 10100
55618153 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 217
7629 deg
Eccentricity:
0005321
Arg of perigee: 161
6432 deg
Mean anomaly: 198
4924 deg
Mean motion: 15
74641159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1282
Checksum: 304
Coasting Arc #10 (Orbit 1296)
---------------------------------------
Vector Time (GMT): 2010/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5576104
09 A = 6724056
67 meter
Y = 66030
34 meter E =
0009773
Z = -3768815
70 I = 51
46410
XDOT = -2907
335818 Wp = 131
80822
YDOT = -5749
795552 meter/sec RA = 211
88810 deg
ZDOT = 4201
356038 TA = 182
47889
MA = 182
48374
Ha = 190
200 n
mi
Hp = 181
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18294304
77 X = -5558119
74
Y = 216634
97 feet Y = 3775
28 meter
Z = -12364880
90 Z = -3795860
81
XDOT = -9538
503340 XDOT = -2863
233984
YDOT = -18864
158635 feet/sec YDOT = -5782
060184 meter/sec
ZDOT = 13783
976503 ZDOT = 4187
339750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17176946
83 X = -5235533
39
Y = 6083700
59 feet Y = 1854311
94 meter
Z = -12472364
73 Z = -3801576
77
XDOT = -14747
685350 XDOT = -4495
094495
YDOT = -13498
779125 feet/sec YDOT = -4114
427877 meter/sec
ZDOT = 13728
050574 ZDOT = 4184
309815
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 10101
50814113
00016717 00000-0 10270-3 0 9092
2 25544 51
6448 212
8706 0005073 165
2189 194
9124 15
74646954 12973
Satellite: ISS
Catalog Number: 25544
Epoch time: 10101
50814113 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 212
8706 deg
Eccentricity:
0005073
Arg of perigee: 165
2189 deg
Mean anomaly: 194
9124 deg
Mean motion: 15
74646954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1297
Checksum: 309
Coasting Arc #11 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2010/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2701142
49 A = 6723760
23 meter
Y = 4802124
77 meter E =
0007898
Z = -3857366
51 I = 51
49010
XDOT = -6503
294129 Wp = 114
96749
YDOT = 371
959655 meter/sec RA = 206
78808 deg
ZDOT = -4100
726249 TA = 112
16544
MA = 112
08160
Ha = 190
074 n
mi
Hp = 182
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8862016
03 X = 2665982
04
Y = 15755002
51 feet Y = 4832133
65 meter
Z = -12655401
93 Z = -3844330
05
XDOT = -21336
266828 XDOT = -6487
049365
YDOT = 1220
340074 feet/sec YDOT = 299
326451 meter/sec
ZDOT = -13453
826277 ZDOT = -4132
280060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13746500
36 X = 4189933
31
Y = 11794176
49 feet Y = 3594865
00 meter
Z = -12603402
68 Z = -3841517
14
XDOT = -18725
481063 XDOT = -5707
526628
YDOT = 7348
805717 feet/sec YDOT = 2239
915982 meter/sec
ZDOT = -13579
223488 ZDOT = -4138
947319
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 10102
52353081
00016717 00000-0 10270-3 0 9109
2 25544 51
6452 207
6513 0005101 168
7474 191
3804 15
74700746 13138
Satellite: ISS
Catalog Number: 25544
Epoch time: 10102
52353081 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 207
6513 deg
Eccentricity:
0005101
Arg of perigee: 168
7474 deg
Mean anomaly: 191
3804 deg
Mean motion: 15
74700746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1313
Checksum: 271
Coasting Arc #12 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2010/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5771725
23 A = 6724970
19 meter
Y = -606559
02 meter E =
0014156
Z = 3381336
49 I = 51
52229
XDOT = 3262
570726 Wp = 110
15627
YDOT = 5238
557575 meter/sec RA = 201
58676 deg
ZDOT = -4618
517619 TA = 29
82316
MA = 29
74256
Ha = 189
817 n
mi
Hp = 182
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18936106
40 X = 5761652
79
Y = -1990023
05 feet Y = -542072
24 meter
Z = 11093623
67 Z = 3409351
45
XDOT = 10703
972198 XDOT = 3226
185950
YDOT = 17186
868685 feet/sec YDOT = 5274
837816 meter/sec
ZDOT = -15152
616859 ZDOT = -4602
756612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16934918
34 X = 5161763
11
Y = -8559344
68 feet Y = -2608888
26 meter
Z = 11204952
60 Z = 3415269
55
XDOT = 15567
178087 XDOT = 4744
875881
YDOT = 11000
477550 feet/sec YDOT = 3352
945557 meter/sec
ZDOT = -15089
769147 ZDOT = -4599
361636
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 10103
53888731
00016717 00000-0 10270-3 0 9117
2 25544 51
6451 202
4324 0005001 170
4320 189
6940 15
74746166 13293
Satellite: ISS
Catalog Number: 25544
Epoch time: 10103
53888731 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 202
4324 deg
Eccentricity:
0005001
Arg of perigee: 170
4320 deg
Mean anomaly: 189
6940 deg
Mean motion: 15
74746166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 284
Coasting Arc #13 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2010/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2942718
45 A = 6722188
33 meter
Y = -4346431
96 meter E =
0012781
Z = 4195867
18 I = 51
54230
XDOT = 6714
392293 Wp = 127
14798
YDOT = -1022
862774 meter/sec RA = 196
48840 deg
ZDOT = 3634
314667 TA = 285
73225
MA = 285
87320
Ha = 189
688 n
mi
Hp = 182
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9654588
08 X = -2914280
24
Y = -14259947
39 feet Y = -4379179
96 meter
Z = 13765968
42 Z = 4181640
54
XDOT = 22028
846107 XDOT = 6707
675973
YDOT = -3355
848997 feet/sec YDOT = -947
815798 meter/sec
ZDOT = 11923
604551 ZDOT = 3666
917435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14331377
36 X = -4368203
82
Y = -9629490
08 feet Y = -2935068
58 meter
Z = 13709252
39 Z = 4178580
13
XDOT = 18443
606907 XDOT = 5621
611385
YDOT = -10218
320545 feet/sec YDOT = -3114
544102 meter/sec
ZDOT = 12053
161491 ZDOT = 3673
803622
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 10104
55420765
00016717 00000-0 10270-3 0 9120
2 25544 51
6454 197
2124 0004882 175
6333 184
4874 15
74838872 13455
Satellite: ISS
Catalog Number: 25544
Epoch time: 10104
55420765 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 197
2124 deg
Eccentricity:
0004882
Arg of perigee: 175
6333 deg
Mean anomaly: 184
4874 deg
Mean motion: 15
74838872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 319
Coasting Arc #14 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2010/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5939873
04 A = 6725920
68 meter
Y = 1184881
40 meter E =
0005208
Z = -2931922
46 I = 51
58421
XDOT = -3416
532695 Wp = 125
88689
YDOT = -4734
907293 meter/sec RA = 191
29305 deg
ZDOT = 5011
333023 TA = 200
32797
MA = 200
34872
Ha = 189
460 n
mi
Hp = 182
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19487772
43 X = -5938438
12
Y = 3887406
17 feet Y = 1118466
13 meter
Z = -9619168
17 Z = -2960775
42
XDOT = -11209
096768 XDOT = -3387
676769
YDOT = -15534
472745 feet/sec YDOT = -4772
951490 meter/sec
ZDOT = 16441
381310 ZDOT = 4994
805460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16412941
35 X = -5002664
52
Y = 11103226
32 feet Y = 3384263
38 meter
Z = -9733823
44 Z = -2966869
38
XDOT = -15626
304660 XDOT = -4762
897660
YDOT = -8752
254184 feet/sec YDOT = -2667
687075 meter/sec
ZDOT = 16375
502791 ZDOT = 4991
253251
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 10105
50604258
00016717 00000-0 10270-3 0 9138
2 25544 51
6449 192
3197 0004673 179
8805 180
2361 15
74852118 13604
Satellite: ISS
Catalog Number: 25544
Epoch time: 10105
50604258 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 192
3197 deg
Eccentricity:
0004673
Arg of perigee: 179
8805 deg
Mean anomaly: 180
2361 deg
Mean motion: 15
74852118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1360
Checksum: 306
Coasting Arc #15 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2010/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2975884
58 A = 6720666
99 meter
Y = 3954400
16 meter E =
0009306
Z = -4554196
99 I = 51
59550
XDOT = -6868
606196 Wp = 97
47219
YDOT = 1677
198367 meter/sec RA = 186
19463 deg
ZDOT = -3038
370297 TA = 142
30715
MA = 142
24191
Ha = 189
334 n
mi
Hp = 182
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9763400
85 X = 2953568
45
Y = 12973753
80 feet Y = 3987553
46 meter
Z = -14941591
16 Z = -4539794
12
XDOT = -22534
797232 XDOT = -6872
090316
YDOT = 5502
619313 feet/sec YDOT = 1600
370022 meter/sec
ZDOT = -9968
406485 ZDOT = -3071
747058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14242018
13 X = 4340967
13
Y = 7906917
68 feet Y = 2410028
51 meter
Z = -14884186
32 Z = -4536699
99
XDOT = -17779
426782 XDOT = -5419
169283
YDOT = 13050
137581 feet/sec YDOT = 3977
681935 meter/sec
ZDOT = -10101
041184 ZDOT = -3078
797353
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 10106
52130029
00016717 00000-0 10270-3 0 9142
2 25544 51
6439 187
0997 0004666 183
2976 176
8158 15
74899111 13768
Satellite: ISS
Catalog Number: 25544
Epoch time: 10106
52130029 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 187
0997 deg
Eccentricity:
0004666
Arg of perigee: 183
2976 deg
Mean anomaly: 176
8158 deg
Mean motion: 15
74899111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 334
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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