Date:
June 3rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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
156/03:22:07
080 -1
3 14
0 14
0
N/A -12
0 0
0 190
9
000/00:04:10
159 -7
0 0
1 187
6
158/23:59:56
477 -0
7 2
6 2
6
N/A -2
2 0
0 191
2
000/00:09:52
954 -1
2 0
2 188
8
159/01:30:56
389 -0
7 2
7 2
7
N/A -2
2 0
0 191
1
000/00:09:52
778 -1
3 0
2 190
2
Coasting Arc #1 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2010/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4235814
36 A = 6728720
35 meter
Y = -5178430
67 meter E =
0021374
Z = 590592
99 I = 51
39065
XDOT = 3399
210729 Wp = 35
83351
YDOT = 3473
684475 meter/sec RA = 305
23981 deg
ZDOT = 5986
552364 TA = 330
62787
MA = 330
74784
Ha = 190
683 n
mi
Hp = 180
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13897028
73 X = 4290536
70
Y = -16989601
92 feet Y = -5130757
37 meter
Z = 1937641
03 Z = 611302
79
XDOT = 11152
266171 XDOT = 3331
033201
YDOT = 11396
602608 feet/sec YDOT = 3511
314510 meter/sec
ZDOT = 19640
919829 ZDOT = 6002
900536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11240442
42 X = -3426086
85
Y = -18844094
35 feet Y = -5743679
96 meter
Z = 2020147
52 Z = 615740
96
XDOT = 13101
891815 XDOT = 3993
456625
YDOT = -5671
731210 feet/sec YDOT = -1728
743673 meter/sec
ZDOT = 19706
034344 ZDOT = 6006
399268
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 10153
56226467
00016717 00000-0 10270-3 0 9005
2 25544 51
6463 305
5315 0009247 13
9047 346
2370 15
75161414 21176
Satellite: ISS
Catalog Number: 25544
Epoch time: 10153
56226467 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 305
5315 deg
Eccentricity:
0009247
Arg of perigee: 13
9047 deg
Mean anomaly: 346
2370 deg
Mean motion: 15
75161414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2117
Checksum: 285
Coasting Arc #2 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2010/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2932560
90 A = 6717128
93 meter
Y = -3171426
07 meter E =
0018250
Z = -5157595
38 I = 51
33563
XDOT = 4574
957377 Wp = 68
37271
YDOT = -6076
022506 meter/sec RA = 300
06116 deg
ZDOT = 1144
761323 TA = 212
55955
MA = 212
67223
Ha = 190
746 n
mi
Hp = 180
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9621262
80 X = -2871824
84
Y = -10404941
16 feet Y = -3203879
54 meter
Z = -16921244
70 Z = -5171694
59
XDOT = 15009
702679 XDOT = 4636
999497
YDOT = -19934
457042 feet/sec YDOT = -6024
515840 meter/sec
ZDOT = 3755
778620 ZDOT = 1167
136471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12932461
04 X = -3941814
12
Y = 5628424
45 feet Y = 1715543
77 meter
Z = -16977405
87 Z = -5174713
31
XDOT = -13580
205441 XDOT = -4139
246619
YDOT = -19702
975089 feet/sec YDOT = -6005
466807 meter/sec
ZDOT = 3844
913758 ZDOT = 1171
929713
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 10154
51390013
00016717 00000-0 10270-3 0 9011
2 25544 51
6465 300
6377 0009333 17
5691 342
5794 15
75200834 21329
Satellite: ISS
Catalog Number: 25544
Epoch time: 10154
51390013 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 300
6377 deg
Eccentricity:
0009333
Arg of perigee: 17
5691 deg
Mean anomaly: 342
5794 deg
Mean motion: 15
75200834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 284
Coasting Arc #3 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2010/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3765824
91 A = 6727682
65 meter
Y = 5392029
88 meter E =
0008725
Z = -1430242
23 I = 51
35719
XDOT = -3314
283612 Wp = 75
90748
YDOT = -3841
638609 meter/sec RA = 294
91799 deg
ZDOT = -5783
922501 TA = 119
87977
MA = 119
79305
Ha = 190
819 n
mi
Hp = 179
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12355068
60 X = -3818891
81
Y = 17690386
74 feet Y = 5349621
61 meter
Z = -4692395
77 Z = -1448664
99
XDOT = -10873
633896 XDOT = -3242
982084
YDOT = -12603
801212 feet/sec YDOT = -3878
301642 meter/sec
ZDOT = -18976
123692 ZDOT = -5799
850527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13028880
49 X = 3971202
77
Y = 17179979
46 feet Y = 5236457
74 meter
Z = -4765780
12 Z = -1452609
78
XDOT = -14055
095290 XDOT = -4283
993044
YDOT = 5401
961683 feet/sec YDOT = 1646
517921 meter/sec
ZDOT = -19039
574019 ZDOT = -5803
262161
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 10155
52894974
00016717 00000-0 10270-3 0 9029
2 25544 51
6460 295
4150 0009470 20
7116 339
4429 15
75254287 21482
Satellite: ISS
Catalog Number: 25544
Epoch time: 10155
52894974 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 295
4150 deg
Eccentricity:
0009470
Arg of perigee: 20
7116 deg
Mean anomaly: 339
4429 deg
Mean motion: 15
75254287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2148
Checksum: 315
Coasting Arc #4 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2010/156/03:24:12
159
Vector Time (MET): N/A
Weight (LBS) : 814961
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4630779
60 A = 6727404
24 meter
Y = 2026610
01 meter E =
0006893
Z = -4445809
34 I = 51
32602
XDOT = 15
328751 Wp = 37
44274
YDOT = -6994
514573 meter/sec RA = 291
61746 deg
ZDOT = -3201
605823 TA = 200
32817
MA = 200
35563
Ha = 190
872 n
mi
Hp = 187
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15192846
45 X = -4631500
32
Y = 6648982
97 feet Y = 1974822
28 meter
Z = -14585988
65 Z = -4468307
31
XDOT = 50
291177 XDOT = 109
094424
YDOT = -22947
882458 feet/sec YDOT = -6993
818568 meter/sec
ZDOT = -10503
956111 ZDOT = -3201
304293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13917538
02 X = -4242065
59
Y = -8871940
61 feet Y = -2704167
50 meter
Z = -14675606
57 Z = -4473124
88
XDOT = 18500
775642 XDOT = 5639
036416
YDOT = -11634
126387 feet/sec YDOT = -3546
081723 meter/sec
ZDOT = -10502
762397 ZDOT = -3201
241979
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 10156
16336347
00016717 00000-0 10270-3 0 9036
2 25544 51
6488 292
1574 0005294 292
8655 67
1949 15
72629024 21581
Satellite: ISS
Catalog Number: 25544
Epoch time: 10156
16336347 = yrday
fracday
Element set: 903
Inclination: 51
6488 deg
RA of node: 292
1574 deg
Eccentricity:
0005294
Arg of perigee: 292
8655 deg
Mean anomaly: 67
1949 deg
Mean motion: 15
72629024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 331
Coasting Arc #5 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2010/157/03:24:12
159
Vector Time (MET): N/A
Weight (LBS) : 814961
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 896146
57 A = 6731748
77 meter
Y = 5878178
47 meter E =
0008372
Z = 3150604
50 I = 51
32995
XDOT = -4996
328398 Wp = 79
79980
YDOT = 3344
710077 meter/sec RA = 286
42200 deg
ZDOT = -4806
892036 TA = 63
35383
MA = 63
26811
Ha = 191
012 n
mi
Hp = 187
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2940113
43 X = 815043
93
Y = 19285362
44 feet Y = 5887745
93 meter
Z = 10336628
94 Z = 3154761
60
XDOT = -16392
153537 XDOT = -5010
007017
YDOT = 10973
458259 feet/sec YDOT = 3288
762155 meter/sec
ZDOT = -15770
643164 ZDOT = -4831
197283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14213188
82 X = -4332179
95
Y = 13349602
42 feet Y = 4068958
82 meter
Z = 10353199
90 Z = 3155655
33
XDOT = -17328
296032 XDOT = -5281
664630
YDOT = -6112
118706 feet/sec YDOT = -1862
973781 meter/sec
ZDOT = -15867
456237 ZDOT = -4836
400661
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 10157
18008411
00016717 00000-0 10270-3 0 9048
2 25544 51
6481 286
9474 0005279 296
7740 63
2883 15
72632846 21743
Satellite: ISS
Catalog Number: 25544
Epoch time: 10157
18008411 = yrday
fracday
Element set: 904
Inclination: 51
6481 deg
RA of node: 286
9474 deg
Eccentricity:
0005279
Arg of perigee: 296
7740 deg
Mean anomaly: 63
2883 deg
Mean motion: 15
72632846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 325
Coasting Arc #6 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2010/158/03:24:12
159
Vector Time (MET): N/A
Weight (LBS) : 814961
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3962715
75 A = 6729156
05 meter
Y = -3750225
95 meter E =
0006263
Z = 3932887
60 I = 51
31482
XDOT = 1991
939406 Wp = 83
22741
YDOT = 6283
793502 meter/sec RA = 281
32427 deg
ZDOT = 3980
203527 TA = 325
28666
MA = 325
32752
Ha = 191
024 n
mi
Hp = 187
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13001035
92 X = 3985251
46
Y = -12303890
92 feet Y = -3705786
92 meter
Z = 12903174
56 Z = 3952193
03
XDOT = 6535
234271 XDOT = 1902
189518
YDOT = 20616
120415 feet/sec YDOT = 6305
566310 meter/sec
ZDOT = 13058
410521 ZDOT = 3989
663149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17533545
56 X = 5344224
69
Y = 3316199
22 feet Y = 1010777
52 meter
Z = 12980068
70 Z = 3956324
94
XDOT = -12731
879131 XDOT = -3880
676759
YDOT = 15996
584387 feet/sec YDOT = 4875
758921 meter/sec
ZDOT = 13096
108741 ZDOT = 3991
693944
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 10158
19678008
00016717 00000-0 10270-3 0 9056
2 25544 51
6487 281
7367 0005398 301
7779 58
2857 15
72672791 21900
Satellite: ISS
Catalog Number: 25544
Epoch time: 10158
19678008 = yrday
fracday
Element set: 905
Inclination: 51
6487 deg
RA of node: 281
7367 deg
Eccentricity:
0005398
Arg of perigee: 301
7779 deg
Mean anomaly: 58
2857 deg
Mean motion: 15
72672791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 350
Coasting Arc #7 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2010/159/00:04:52
954
Vector Time (MET): N/A
Weight (LBS) : 814706
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4201123
65 A = 6726612
28 meter
Y = 1827774
36 meter E =
0008121
Z = -4932146
79 I = 51
29581
XDOT = -777
871100 Wp = 49
58714
YDOT = -7368
653058 meter/sec RA = 276
87840 deg
ZDOT = -2065
169733 TA = 200
27361
MA = 200
30588
Ha = 191
202 n
mi
Hp = 188
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13783214
06 X = -4197290
11
Y = 5996635
05 feet Y = 1780816
92 meter
Z = -16181583
97 Z = -4952546
60
XDOT = -2552
070537 XDOT = -685
383317
YDOT = -24175
370924 feet/sec YDOT = -7376
834301 meter/sec
ZDOT = -6775
491251 ZDOT = -2068
724912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2691510
30 X = -820372
34
Y = -14698842
94 feet Y = -4480207
33 meter
Z = -16262843
24 Z = -4956914
62
XDOT = 23034
265624 XDOT = 7020
844162
YDOT = 3304
981760 feet/sec YDOT = 1007
358440 meter/sec
ZDOT = -6789
674339 ZDOT = -2069
492739
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 10159
02283231
00016717 00000-0 10270-3 0 9060
2 25544 51
6469 277
5025 0006437 287
0302 73
0154 15
72214414 22031
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
02283231 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 277
5025 deg
Eccentricity:
0006437
Arg of perigee: 287
0302 deg
Mean anomaly: 73
0154 deg
Mean motion: 15
72214414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 275
Coasting Arc #8 (Orbit 2203)
---------------------------------------
Vector Time (GMT): 2010/159/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4161732
78 A = 6728357
93 meter
Y = 2085134
66 meter E =
0005741
Z = -4863221
03 I = 51
29779
XDOT = -993
695046 Wp = 44
96856
YDOT = -7282
834745 meter/sec RA = 276
55526 deg
ZDOT = -2269
826702 TA = 202
80369
MA = 202
82920
Ha = 191
120 n
mi
Hp = 190
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13653978
92 X = -4161114
84
Y = 6840992
98 feet Y = 2038599
73 meter
Z = -15955449
57 Z = -4883437
26
XDOT = -3260
154350 XDOT = -901
156657
YDOT = -23893
814779 feet/sec YDOT = -7293
429150 meter/sec
ZDOT = -7446
938000 ZDOT = -2274
430244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8991287
48 X = -2740544
42
Y = -12239725
93 feet Y = -3730668
46 meter
Z = -16035976
90 Z = -4887765
76
XDOT = 22139
143595 XDOT = 6748
010968
YDOT = -6472
528397 feet/sec YDOT = -1972
826655 meter/sec
ZDOT = -7465
297242 ZDOT = -2275
422599
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 10159
08639845
00016717 00000-0 10270-3 0 9073
2 25544 51
6481 277
1777 0007775 274
0264 86
0009 15
71706171 22043
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
08639845 = yrday
fracday
Element set: 907
Inclination: 51
6481 deg
RA of node: 277
1777 deg
Eccentricity:
0007775
Arg of perigee: 274
0264 deg
Mean anomaly: 86
0009 deg
Mean motion: 15
71706171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2204
Checksum: 320
Coasting Arc #9 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2010/160/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1977173
46 A = 6735652
70 meter
Y = 5867355
83 meter E =
0005926
Z = 2644600
01 I = 51
31986
XDOT = -4247
320559 Wp = 107
88982
YDOT = 3774
395392 meter/sec RA = 271
37325 deg
ZDOT = -5190
778800 TA = 41
90004
MA = 41
85470
Ha = 191
609 n
mi
Hp = 190
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6486789
55 X = 1898569
49
Y = 19249855
09 feet Y = 5889025
89 meter
Z = 8676509
23 Z = 2654015
17
XDOT = -13934
778737 XDOT = -4263
994609
YDOT = 12383
186982 feet/sec YDOT = 3726
806832 meter/sec
ZDOT = -17030
114174 ZDOT = -5211
452568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17752151
97 X = -5410855
92
Y = 9840928
56 feet Y = 2999515
03 meter
Z = 8714034
52 Z = 2656037
72
XDOT = -13982
034865 XDOT = -4261
724227
YDOT = -10047
018435 feet/sec YDOT = -3062
331219 meter/sec
ZDOT = -17112
461726 ZDOT = -5215
878334
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 10160
10371707
00016717 00000-0 10270-3 0 9089
2 25544 51
6479 271
9719 0007811 277
7873 82
2402 15
71706658 22208
Satellite: ISS
Catalog Number: 25544
Epoch time: 10160
10371707 = yrday
fracday
Element set: 908
Inclination: 51
6479 deg
RA of node: 271
9719 deg
Eccentricity:
0007811
Arg of perigee: 277
7873 deg
Mean anomaly: 82
2402 deg
Mean motion: 15
71706658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 311
Coasting Arc #10 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2010/161/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3032617
16 A = 6731128
04 meter
Y = -4362345
96 meter E =
0002541
Z = 4131595
40 I = 51
30601
XDOT = 3357
106058 Wp = 112
83331
YDOT = 5848
813480 meter/sec RA = 266
27916 deg
ZDOT = 3708
549309 TA = 299
02868
MA = 299
05413
Ha = 191
822 n
mi
Hp = 190
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9949531
37 X = 3061101
47
Y = -14312158
65 feet Y = -4328274
85 meter
Z = 13555103
01 Z = 4146396
53
XDOT = 11014
127486 XDOT = 3273
438330
YDOT = 19189
020603 feet/sec YDOT = 5885
886209 meter/sec
ZDOT = 12167
156525 ZDOT = 3724
656121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15992313
86 X = 4874457
26
Y = 6817274
37 feet Y = 2077905
23 meter
Z = 13614056
89 Z = 4149564
54
XDOT = -16124
966425 XDOT = -4914
889766
YDOT = 13382
690230 feet/sec YDOT = 4079
043982 meter/sec
ZDOT = 12231
343977 ZDOT = 3728
113644
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 10161
12101320
00016717 00000-0 10270-3 0 9095
2 25544 51
6484 266
7654 0007846 282
6482 77
3803 15
71747063 22365
Satellite: ISS
Catalog Number: 25544
Epoch time: 10161
12101320 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 266
7654 deg
Eccentricity:
0007846
Arg of perigee: 282
6482 deg
Mean anomaly: 77
3803 deg
Mean motion: 15
71747063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 304
Coasting Arc #11 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2010/162/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3711812
62 A = 6732216
21 meter
Y = -4156775
74 meter E =
0001789
Z = -3775058
38 I = 51
31377
XDOT = 2448
376771 Wp = 295
05040
YDOT = -5981
406202 meter/sec RA = 261
08625 deg
ZDOT = 4178
062121 TA = 19
01957
MA = 19
01289
Ha = 192
023 n
mi
Hp = 190
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12177862
94 X = -3646716
16
Y = -13637715
68 feet Y = -4197918
75 meter
Z = -12385362
12 Z = -3792933
25
XDOT = 8032
732187 XDOT = 2494
783451
YDOT = -19624
036096 feet/sec YDOT = -5953
768315 meter/sec
ZDOT = 13707
552890 ZDOT = 4190
068070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10698056
14 X = 3260767
51
Y = -14767182
05 feet Y = -4501037
09 meter
Z = -12456595
00 Z = -3796770
16
XDOT = 19801
908223 XDOT = 6035
621626
YDOT = 2740
154693 feet/sec YDOT = 835
199151 meter/sec
ZDOT = 13755
368612 ZDOT = 4192
636353
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 10162
07470838
00016717 00000-0 10270-3 0 9105
2 25544 51
6489 261
8848 0007971 286
7862 73
2425 15
71790673 22514
Satellite: ISS
Catalog Number: 25544
Epoch time: 10162
07470838 = yrday
fracday
Element set: 910
Inclination: 51
6489 deg
RA of node: 261
8848 deg
Eccentricity:
0007971
Arg of perigee: 286
7862 deg
Mean anomaly: 73
2425 deg
Mean motion: 15
71790673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2251
Checksum: 333
Coasting Arc #12 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2010/163/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1111374
72 A = 6734195
85 meter
Y = 5863122
76 meter E =
0003648
Z = -3119915
03 I = 51
32642
XDOT = -4859
088445 Wp = 299
19610
YDOT = -3496
222324 meter/sec RA = 255
99596 deg
ZDOT = -4833
389486 TA = 277
20595
MA = 277
24741
Ha = 192
351 n
mi
Hp = 190
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3646242
51 X = -1161698
52
Y = 19235967
07 feet Y = 5850413
98 meter
Z = -10235941
69 Z = -3125435
16
XDOT = -15941
891225 XDOT = -4796
152009
YDOT = -11470
545684 feet/sec YDOT = -3550
206653 meter/sec
ZDOT = -15857
577054 ZDOT = -4856
842968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19541689
10 X = -5956306
84
Y = 994765
52 feet Y = 303204
53 meter
Z = -10257916
17 Z = -3126612
85
XDOT = 7535
375737 XDOT = 2296
782525
YDOT = -16659
528881 feet/sec YDOT = -5077
824403 meter/sec
ZDOT = -15951
045873 ZDOT = -4861
878782
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 10163
09196306
00016717 00000-0 10270-3 0 9114
2 25544 51
6490 256
6789 0008103 290
2807 69
7483 15
71803765 22677
Satellite: ISS
Catalog Number: 25544
Epoch time: 10163
09196306 = yrday
fracday
Element set: 911
Inclination: 51
6490 deg
RA of node: 256
6789 deg
Eccentricity:
0008103
Arg of perigee: 290
2807 deg
Mean anomaly: 69
7483 deg
Mean motion: 15
71803765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 325
Coasting Arc #13 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2010/164/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4547791
38 A = 6728906
69 meter
Y = 1864343
78 meter E =
0007086
Z = 4598987
74 I = 51
31768
XDOT = 20
347604 Wp =
32795
YDOT = 7125
750197 meter/sec RA = 250
80790 deg
ZDOT = -2901
758310 TA = 118
59819
MA = 118
52687
Ha = 192
460 n
mi
Hp = 189
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14920575
41 X = 4504264
87
Y = 6116613
46 feet Y = 1914955
55 meter
Z = 15088542
47 Z = 4620975
62
XDOT = 66
757231 XDOT = -45
239098
YDOT = 23378
445529 feet/sec YDOT = 7125
611633 meter/sec
ZDOT = -9520
204430 ZDOT = -2901
817270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2220155
22 X = -676703
31
Y = 15888838
87 feet Y = 4842918
09 meter
Z = 15176177
20 Z = 4625698
81
XDOT = -21448
319188 XDOT = -6537
447688
YDOT = 6118
241445 feet/sec YDOT = 1864
839992 meter/sec
ZDOT = -9520
407303 ZDOT = -2901
820146
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 10164
10919544
00016717 00000-0 10270-3 0 9125
2 25544 51
6487 251
4726 0008167 295
4960 64
5357 15
71892183 22837
Satellite: ISS
Catalog Number: 25544
Epoch time: 10164
10919544 = yrday
fracday
Element set: 912
Inclination: 51
6487 deg
RA of node: 251
4726 deg
Eccentricity:
0008167
Arg of perigee: 295
4960 deg
Mean anomaly: 64
5357 deg
Mean motion: 15
71892183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 326
Coasting Arc #14 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2010/165/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1177285
73 A = 6736634
47 meter
Y = -6340970
38 meter E =
0011163
Z = 1920618
76 I = 51
35394
XDOT = 5238
096761 Wp = 31
97016
YDOT = 724
688448 meter/sec RA = 245
70621 deg
ZDOT = 5597
883125 TA = 349
46437
MA = 349
48774
Ha = 192
688 n
mi
Hp = 189
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3862486
01 X = -1115622
34
Y = -20803708
59 feet Y = -6353791
10 meter
Z = 6301242
66 Z = 1915048
02
XDOT = 17185
356827 XDOT = 5202
410465
YDOT = 2377
586773 feet/sec YDOT = 783
063297 meter/sec
ZDOT = 18365
758285 ZDOT = 5623
243169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19013736
14 X = 5795386
77
Y = -9298962
54 feet Y = -2834323
78 meter
Z = 6279003
28 Z = 1913840
20
XDOT = 1577
255385 XDOT = 480
747441
YDOT = 15706
761781 feet/sec YDOT = 4787
420991 meter/sec
ZDOT = 18466
839980 ZDOT = 5628
692826
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 10165
12640880
00016717 00000-0 10270-3 0 9133
2 25544 51
6481 246
2655 0008182 299
7515 60
2833 15
71878883 22994
Satellite: ISS
Catalog Number: 25544
Epoch time: 10165
12640880 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 246
2655 deg
Eccentricity:
0008182
Arg of perigee: 299
7515 deg
Mean anomaly: 60
2833 deg
Mean motion: 15
71878883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 331
Coasting Arc #15 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2010/166/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4356675
01 A = 6726684
83 meter
Y = 581075
77 meter E =
0007029
Z = -5097612
92 I = 51
33384
XDOT = -2650
932176 Wp = 75
06169
YDOT = -7072
216382 meter/sec RA = 240
53584 deg
ZDOT = 1462
924221 TA = 209
01468
MA = 209
05377
Ha = 192
716 n
mi
Hp = 189
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14293553
17 X = -4338085
83
Y = 1906416
57 feet Y = 532461
71 meter
Z = -16724451
85 Z = -5118732
23
XDOT = -8697
284042 XDOT = -2578
758911
YDOT = -23202
809653 feet/sec YDOT = -7101
457412 meter/sec
ZDOT = 4799
620149 ZDOT = 1450
220099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5842963
66 X = -1780935
32
Y = -13075817
89 feet Y = -3985509
29 meter
Z = -16808632
85 Z = -5123271
29
XDOT = 18833
655080 XDOT = 5740
498068
YDOT = -14505
953881 feet/sec YDOT = -4421
414743 meter/sec
ZDOT = 4748
928412 ZDOT = 1447
473380
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 10166
08002550
00016717 00000-0 10270-3 0 9146
2 25544 51
6474 241
3840 0008246 303
1181 56
9189 15
71932743 23148
Satellite: ISS
Catalog Number: 25544
Epoch time: 10166
08002550 = yrday
fracday
Element set: 914
Inclination: 51
6474 deg
RA of node: 241
3840 deg
Eccentricity:
0008246
Arg of perigee: 303
1181 deg
Mean anomaly: 56
9189 deg
Mean motion: 15
71932743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2314
Checksum: 288
Coasting Arc #16 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2010/167/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3377577
29 A = 6737961
79 meter
Y = 5792899
83 meter E =
0003474
Z = -635415
91 I = 51
38706
XDOT = -4451
028346 Wp = 173
33243
YDOT = 1941
300289 meter/sec RA = 235
41521 deg
ZDOT = -5968
008019 TA = 13
60179
MA = 13
59243
Ha = 192
975 n
mi
Hp = 189
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11081290
31 X = 3315635
71
Y = 19005576
87 feet Y = 5830323
68 meter
Z = -2084697
88 Z = -619157
33
XDOT = -14603
111373 XDOT = -4443
414288
YDOT = 6369
095435 feet/sec YDOT = 1891
569760 meter/sec
ZDOT = -19580
078802 ZDOT = -5989
612105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14813908
33 X = -4515279
26
Y = 16273331
47 feet Y = 4960111
43 meter
Z = -2019830
50 Z = -615644
34
XDOT = -9225
962510 XDOT = -2812
073373
YDOT = -10836
709405 feet/sec YDOT = -3303
029027 meter/sec
ZDOT = -19666
188017 ZDOT = -5994
254108
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 10167
09719815
00016717 00000-0 10270-3 0 9158
2 25544 51
6470 236
1776 0008190 306
1256 53
9148 15
71910427 23303
Satellite: ISS
Catalog Number: 25544
Epoch time: 10167
09719815 = yrday
fracday
Element set: 915
Inclination: 51
6470 deg
RA of node: 236
1776 deg
Eccentricity:
0008190
Arg of perigee: 306
1256 deg
Mean anomaly: 53
9148 deg
Mean motion: 15
71910427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 305
Coasting Arc #17 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2010/168/01:35:52
778
Vector Time (MET): N/A
Weight (LBS) : 814451
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3222516
58 A = 6725878
70 meter
Y = -2695141
76 meter E =
0006597
Z = 5255826
77 I = 51
36467
XDOT = 4927
760829 Wp = 324
35317
YDOT = 5910
607655 meter/sec RA = 230
26979 deg
ZDOT = 14
829709 TA = 125
53624
MA = 125
47471
Ha = 193
042 n
mi
Hp = 188
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10572560
96 X = 3226883
01
Y = -8842328
60 feet Y = -2659081
95 meter
Z = 17243526
16 Z = 5271491
87
XDOT = 16167
194320 XDOT = 4861
229061
YDOT = 19391
757398 feet/sec YDOT = 5965
340813 meter/sec
ZDOT = 48
653902 ZDOT = 38
607760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11694956
20 X = 3564622
65
Y = 7144017
07 feet Y = 2177496
40 meter
Z = 17305953
73 Z = 5274854
70
XDOT = -12775
855342 XDOT = -3894
080708
YDOT = 20608
671320 feet/sec YDOT = 6281
523018 meter/sec
ZDOT = 143
516529 ZDOT = 43
743838
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 10168
11434846
00016717 00000-0 10270-3 0 9161
2 25544 51
6466 230
9695 0008276 311
1744 48
8704 15
71973461 23468
Satellite: ISS
Catalog Number: 25544
Epoch time: 10168
11434846 = yrday
fracday
Element set: 916
Inclination: 51
6466 deg
RA of node: 230
9695 deg
Eccentricity:
0008276
Arg of perigee: 311
1744 deg
Mean anomaly: 48
8704 deg
Mean motion: 15
71973461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 323
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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