Date:
January 16th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 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
022/09:06:27
025 1
5 3
3 3
3
N/A 2
8 0
0 185
3
000/00:00:54
049 1
1 0
0 179
5
024/09:02:55
218 -4
3 8
5 8
5
N/A -7
1 0
0 187
5
000/00:02:20
436 -1
8 0
1 183
4
Coasting Arc #1 (Orbit 3941)
---------------------------------------
Vector Time (GMT): 2010/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203350
79 A = 6719807
86 meter
Y = 4665933
97 meter E =
0011171
Z = -2375203
61 I = 51
35172
XDOT = -2468
946996 Wp = 165
04795
YDOT = -4949
058520 meter/sec RA = 294
40982 deg
ZDOT = -5369
096774 TA = 41
88565
MA = 41
80024
Ha = 185
761 n
mi
Hp = 178
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13790520
96 X = -4243675
65
Y = 15308182
31 feet Y = 4618704
39 meter
Z = -7792662
76 Z = -2395720
48
XDOT = -8100
219803 XDOT = -2387
340776
YDOT = -16237
068636 feet/sec YDOT = -4976
210919 meter/sec
ZDOT = -17615
146897 ZDOT = -5380
892917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19581594
92 X = -5968470
13
Y = -6309407
39 feet Y = -1923107
37 meter
Z = -7873819
01 Z = -2399940
03
XDOT = 11106
436965 XDOT = 3385
241987
YDOT = -12494
021654 feet/sec YDOT = -3808
177800 meter/sec
ZDOT = -17661
952923 ZDOT = -5383
363251
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 10015
52694026
00016717 00000-0 10270-3 0 9008
2 25544 51
6455 294
9075 0007095 189
8134 170
2894 15
77467326 39426
Satellite: ISS
Catalog Number: 25544
Epoch time: 10015
52694026 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 294
9075 deg
Eccentricity:
0007095
Arg of perigee: 189
8134 deg
Mean anomaly: 170
2894 deg
Mean motion: 15
77467326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 328
Coasting Arc #2 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2010/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1640804
52 A = 6715082
95 meter
Y = 5105083
54 meter E =
0009901
Z = 4031281
61 I = 51
32388
XDOT = -4855
542914 Wp = 116
74138
YDOT = 4597
067281 meter/sec RA = 289
17964 deg
ZDOT = -3842
441771 TA = 12
93001
MA = 12
90464
Ha = 185
601 n
mi
Hp = 178
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5383216
94 X = 1564013
88
Y = 16748961
74 feet Y = 5123002
29 meter
Z = 13225989
55 Z = 4039066
34
XDOT = -15930
258905 XDOT = -4887
921837
YDOT = 15082
241736 feet/sec YDOT = 4542
589004 meter/sec
ZDOT = -12606
436258 ZDOT = -3866
107682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12928299
10 X = -3940545
57
Y = 11897335
23 feet Y = 3626307
78 meter
Z = 13256924
24 Z = 4040710
51
XDOT = -19508
726060 XDOT = -5946
259703
YDOT = -7037
514386 feet/sec YDOT = -2145
034385 meter/sec
ZDOT = -12700
059135 ZDOT = -3870
978024
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 10016
54052319
00016717 00000-0 10270-3 0 9015
2 25544 51
6447 289
6765 0007069 193
4255 166
6723 15
77501994 39587
Satellite: ISS
Catalog Number: 25544
Epoch time: 10016
54052319 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 289
6765 deg
Eccentricity:
0007069
Arg of perigee: 193
4255 deg
Mean anomaly: 166
6723 deg
Mean motion: 15
77501994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 336
Coasting Arc #3 (Orbit 3973)
---------------------------------------
Vector Time (GMT): 2010/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222666
09 A = 6714462
25 meter
Y = -3153546
35 meter E =
0012253
Z = 4159926
03 I = 51
31367
XDOT = 1351
767067 Wp = 140
91721
YDOT = 6648
329402 meter/sec RA = 284
04524 deg
ZDOT = 3652
563537 TA = 271
61827
MA = 271
75861
Ha = 185
420 n
mi
Hp = 178
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13853891
38 X = 4237408
10
Y = -10346280
68 feet Y = -3106243
83 meter
Z = 13648051
28 Z = 4180474
85
XDOT = 4434
931323 XDOT = 1259
580751
YDOT = 21812
104336 feet/sec YDOT = 6662
929991 meter/sec
ZDOT = 11983
476171 ZDOT = 3658
906762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15341103
96 X = 4675968
49
Y = 7835841
81 feet Y = 2388364
58 meter
Z = 13729357
11 Z = 4184708
05
XDOT = -17112
775740 XDOT = -5215
974046
YDOT = 12375
758587 feet/sec YDOT = 3772
131217 meter/sec
ZDOT = 12008
747706 ZDOT = 3660
266301
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 10017
55407921
00016717 00000-0 10270-3 0 9021
2 25544 51
6449 284
4442 0007039 197
6844 162
4078 15
77544985 39743
Satellite: ISS
Catalog Number: 25544
Epoch time: 10017
55407921 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 284
4442 deg
Eccentricity:
0007039
Arg of perigee: 197
6844 deg
Mean anomaly: 162
4078 deg
Mean motion: 15
77544985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 338
Coasting Arc #4 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2010/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -764779
51 A = 6719898
33 meter
Y = -6320771
86 meter E =
0002423
Z = -2154323
50 I = 51
32666
XDOT = 4819
982040 Wp = 140
59034
YDOT = -2451
013558 meter/sec RA = 278
81429 deg
ZDOT = 5481
700545 TA = 195
17119
MA = 195
17845
Ha = 185
229 n
mi
Hp = 178
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2509119
12 X = -683577
60
Y = -20737440
48 feet Y = -6328869
96 meter
Z = -7067990
50 Z = -2157841
76
XDOT = 15813
589371 XDOT = 4820
402969
YDOT = -8041
383065 feet/sec YDOT = -2397
111556 meter/sec
ZDOT = 17984
581841 ZDOT = 5505
116402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17353632
17 X = 5289387
09
Y = -11618485
93 feet Y = -3541314
51 meter
Z = -7082078
88 Z = -2158617
64
XDOT = 13451
554353 XDOT = 4100
033767
YDOT = 9075
546397 feet/sec YDOT = 2766
226542 meter/sec
ZDOT = 18077
255401 ZDOT = 5509
947446
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 10018
50426399
00016717 00000-0 10270-3 0 9038
2 25544 51
6451 279
5390 0007057 201
9774 158
1090 15
77604493 39897
Satellite: ISS
Catalog Number: 25544
Epoch time: 10018
50426399 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 279
5390 deg
Eccentricity:
0007057
Arg of perigee: 201
9774 deg
Mean anomaly: 158
1090 deg
Mean motion: 15
77604493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 329
Coasting Arc #5 (Orbit 4004)
---------------------------------------
Vector Time (GMT): 2010/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4197669
49 A = 6710131
62 meter
Y = 999836
38 meter E =
0011853
Z = -5147563
41 I = 51
29067
XDOT = -425
989896 Wp = 109
99389
YDOT = -7603
360720 meter/sec RA = 273
65683 deg
ZDOT = -1135
570519 TA = 149
14621
MA = 149
07650
Ha = 184
908 n
mi
Hp = 178
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13771881
54 X = -4183532
42
Y = 3280303
08 feet Y = 952974
76 meter
Z = -16888331
41 Z = -5167920
92
XDOT = -1397
604647 XDOT = -335
419827
YDOT = -24945
409186 feet/sec YDOT = -7607
617953 meter/sec
ZDOT = -3725
625063 ZDOT = -1137
420177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9315324
42 X = -2839310
88
Y = -10531905
89 feet Y = -3210124
91 meter
Z = -16968928
57 Z = -5172129
43
XDOT = 20611
117478 XDOT = 6282
268607
YDOT = -12247
587388 feet/sec YDOT = -3733
064636 meter/sec
ZDOT = -3733
149199 ZDOT = -1137
863876
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 10019
51776925
00016717 00000-0 10270-3 0 9044
2 25544 51
6451 274
3065 0006981 206
5761 153
5047 15
77651994 40050
Satellite: ISS
Catalog Number: 25544
Epoch time: 10019
51776925 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 274
3065 deg
Eccentricity:
0006981
Arg of perigee: 206
5761 deg
Mean anomaly: 153
5047 deg
Mean motion: 15
77651994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 318
Coasting Arc #6 (Orbit 4020)
---------------------------------------
Vector Time (GMT): 2010/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6028
87 A = 6721845
77 meter
Y = 6708010
59 meter E =
0015461
Z = -232434
41 I = 51
32912
XDOT = -4821
420482 Wp = 163
17993
YDOT = -208
812608 meter/sec RA = 268
46241 deg
ZDOT = -6015
219515 TA = 19
36222
MA = 19
30354
Ha = 184
879 n
mi
Hp = 179
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19779
77 X = -79909
48
Y = 22007908
76 feet Y = 6707530
09 meter
Z = -762580
10 Z = -232643
00
XDOT = -15818
308667 XDOT = -4789
506786
YDOT = -685
080734 feet/sec YDOT = -262
550009 meter/sec
ZDOT = -19734
972163 ZDOT = -6038
564086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19258141
65 X = -5869881
58
Y = 10652297
43 feet Y = 3246820
26 meter
Z = -763221
57 Z = -232629
94
XDOT = -6233
320673 XDOT = -1899
916141
YDOT = -12662
968963 feet/sec YDOT = -3859
672940 meter/sec
ZDOT = -19827
432680 ZDOT = -6043
401481
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 10020
53124997
00016717 00000-0 10270-3 0 9055
2 25544 51
6449 269
0740 0007173 210
3358 149
7393 15
77630783 40219
Satellite: ISS
Catalog Number: 25544
Epoch time: 10020
53124997 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 269
0740 deg
Eccentricity:
0007173
Arg of perigee: 210
3358 deg
Mean anomaly: 149
7393 deg
Mean motion: 15
77630783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4021
Checksum: 308
Coasting Arc #7 (Orbit 4036)
---------------------------------------
Vector Time (GMT): 2010/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222530
47 A = 6710335
04 meter
Y = 1363654
06 meter E =
0002709
Z = 5033155
72 I = 51
29347
XDOT = -451
191326 Wp = 180
26336
YDOT = 7513
405009 meter/sec RA = 263
25862 deg
ZDOT = -1659
793639 TA = 285
74035
MA = 285
77023
Ha = 184
364 n
mi
Hp = 179
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13853446
42 X = 4182518
16
Y = 4473930
65 feet Y = 1410649
06 meter
Z = 16512978
07 Z = 5053571
36
XDOT = -1480
286502 XDOT = -527
111136
YDOT = 24650
278902 feet/sec YDOT = 7507
935069 meter/sec
ZDOT = -5445
517187 ZDOT = -1662
169733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2996808
18 X = 913427
13
Y = 14151853
83 feet Y = 4313485
05 meter
Z = 16593873
93 Z = 5057812
77
XDOT = -21044
887047 XDOT = -6414
481572
YDOT = 10842
195739 feet/sec YDOT = 3304
701261 meter/sec
ZDOT = -5454
712834 ZDOT = -1662
596472
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 10021
54470154
00016717 00000-0 10270-3 0 9067
2 25544 51
6449 263
8410 0007025 216
3312 143
7377 15
77749963 40371
Satellite: ISS
Catalog Number: 25544
Epoch time: 10021
54470154 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 263
8410 deg
Eccentricity:
0007025
Arg of perigee: 216
3312 deg
Mean anomaly: 143
7377 deg
Mean motion: 15
77749963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4037
Checksum: 302
Coasting Arc #8 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/022/09:06:54
049
Vector Time (MET): N/A
Weight (LBS) : 751544
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3247995
79 A = 6713103
59 meter
Y = -3384633
77 meter E =
0008948
Z = 4801696
90 I = 51
29940
XDOT = 3266
943469 Wp = 153
46269
YDOT = 6553
556477 meter/sec RA = 258
72715 deg
ZDOT = 2400
016042 TA = 272
96568
MA = 273
06807
Ha = 185
298 n
mi
Hp = 179
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10656154
17 X = 3262276
41
Y = -11104441
51 feet Y = -3348233
05 meter
Z = 15753598
74 Z = 4817510
10
XDOT = 10718
318469 XDOT = 3181
758905
YDOT = 21501
169544 feet/sec YDOT = 6589
613011 meter/sec
ZDOT = 7874
068378 ZDOT = 2415
679980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8569161
06 X = 2611880
29
Y = 12706597
74 feet Y = 3872970
99 meter
Z = 15816130
02 Z = 4820756
43
XDOT = -22368
269152 XDOT = -6817
848437
YDOT = 5167
255625 feet/sec YDOT = 1574
979515 meter/sec
ZDOT = 7936
299862 ZDOT = 2418
984198
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 10022
43147916
00016717 00000-0 10270-3 0 9074
2 25544 51
6433 259
2616 0004825 204
5256 155
5680 15
77140228 40515
Satellite: ISS
Catalog Number: 25544
Epoch time: 10022
43147916 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 259
2616 deg
Eccentricity:
0004825
Arg of perigee: 204
5256 deg
Mean anomaly: 155
5680 deg
Mean motion: 15
77140228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 293
Coasting Arc #9 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2010/023/09:06:54
049
Vector Time (MET): N/A
Weight (LBS) : 751544
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2699657
84 A = 6722674
17 meter
Y = -6058151
71 meter E =
0004957
Z = -1086871
31 I = 51
33930
XDOT = 4062
410887 Wp = 46
12776
YDOT = -2862
417275 meter/sec RA = 253
51436 deg
ZDOT = 5884
426261 TA = 301
91986
MA = 301
96807
Ha = 185
176 n
mi
Hp = 179
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8857145
13 X = -2626434
08
Y = -19875825
81 feet Y = -6087931
42 meter
Z = -3565850
76 Z = -1099808
54
XDOT = 13328
119708 XDOT = 4065
531752
YDOT = -9391
132793 feet/sec YDOT = -2816
971789 meter/sec
ZDOT = 19305
860435 ZDOT = 5904
168765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21234274
46 X = 6472206
85
Y = -4715260
17 feet Y = -1437211
30 meter
Z = -3617274
22 Z = -1102545
18
XDOT = 6237
121738 XDOT = 1901
074706
YDOT = 13267
136914 feet/sec YDOT = 4043
823331 meter/sec
ZDOT = 19383
971593 ZDOT = 5908
234542
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 10023
38192280
00016717 00000-0 10270-3 0 9084
2 25544 51
6435 254
3579 0004708 209
1720 150
9183 15
77155577 40664
Satellite: ISS
Catalog Number: 25544
Epoch time: 10023
38192280 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 254
3579 deg
Eccentricity:
0004708
Arg of perigee: 209
1720 deg
Mean anomaly: 150
9183 deg
Mean motion: 15
77155577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 312
Coasting Arc #10 (Orbit 4081)
---------------------------------------
Vector Time (GMT): 2010/024/09:04:05
436
Vector Time (MET): N/A
Weight (LBS) : 750857
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3348347
02 A = 6715940
64 meter
Y = 2732129
88 meter E =
0006208
Z = -5144636
27 I = 51
31224
XDOT = -3656
089832 Wp = 124
09893
YDOT = -6675
595678 meter/sec RA = 248
36280 deg
ZDOT = -1170
068823 TA = 134
70150
MA = 134
65092
Ha = 187
522 n
mi
Hp = 183
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10985390
49 X = -3353657
79
Y = 8963680
72 feet Y = 2694657
30 meter
Z = -16878727
92 Z = -5160915
16
XDOT = -11995
045380 XDOT = -3575
486471
YDOT = -21901
560623 feet/sec YDOT = -6716
029492 meter/sec
ZDOT = -3838
808474 ZDOT = -1187
634593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6685229
83 X = -2037658
05
Y = -12415956
10 feet Y = -3784383
42 meter
Z = -16943127
47 Z = -5164265
25
XDOT = 22900
282835 XDOT = 6980
006208
YDOT = -7016
436267 feet/sec YDOT = -2138
609774 meter/sec
ZDOT = -3908
590886 ZDOT = -1191
338502
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 10024
39571018
00016717 00000-0 10270-3 0 9097
2 25544 51
6442 249
1275 0010679 237
5531 122
4601 15
75621930 40822
Satellite: ISS
Catalog Number: 25544
Epoch time: 10024
39571018 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 249
1275 deg
Eccentricity:
0010679
Arg of perigee: 237
5531 deg
Mean anomaly: 122
4601 deg
Mean motion: 15
75621930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 293
Coasting Arc #11 (Orbit 4097)
---------------------------------------
Vector Time (GMT): 2010/025/09:04:05
436
Vector Time (MET): N/A
Weight (LBS) : 750857
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3356668
92 A = 6727501
78 meter
Y = 5800405
80 meter E =
0013645
Z = 473345
57 I = 51
36327
XDOT = -3963
933406 Wp = 177
52166
YDOT = 2782
666743 meter/sec RA = 243
17878 deg
ZDOT = -5996
262027 TA = 357
30332
MA = 357
31067
Ha = 187
389 n
mi
Hp = 183
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11012693
32 X = 3289258
88
Y = 19030202
77 feet Y = 5837565
12 meter
Z = 1552971
04 Z = 489488
85
XDOT = -13005
030861 XDOT = -3965
626576
YDOT = 9129
484064 feet/sec YDOT = 2738
330703 meter/sec
ZDOT = -19672
775678 ZDOT = -6015
522535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20675598
39 X = -6301922
39
Y = 7466215
08 feet Y = 2275702
36 meter
Z = 1617100
54 Z = 492892
24
XDOT = -6162
389276 XDOT = -1878
296251
YDOT = -12792
387716 feet/sec YDOT = -3899
119776 meter/sec
ZDOT = -19748
989992 ZDOT = -6019
492150
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 10025
41049798
00016717 00000-0 10270-3 0 9108
2 25544 51
6441 243
9041 0010783 241
1981 118
8101 15
75608525 40986
Satellite: ISS
Catalog Number: 25544
Epoch time: 10025
41049798 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 243
9041 deg
Eccentricity:
0010783
Arg of perigee: 241
1981 deg
Mean anomaly: 118
8101 deg
Mean motion: 15
75608525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 298
Coasting Arc #12 (Orbit 4113)
---------------------------------------
Vector Time (GMT): 2010/026/09:04:05
436
Vector Time (MET): N/A
Weight (LBS) : 750857
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3622810
29 A = 6715258
22 meter
Y = -2123667
82 meter E =
0008621
Z = 5246637
24 I = 51
33747
XDOT = 4004
128047 Wp = 240
83585
YDOT = 6574
523650 meter/sec RA = 238
01401 deg
ZDOT = -107
978381 TA = 210
16853
MA = 210
21820
Ha = 186
920 n
mi
Hp = 183
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11885860
53 X = 3620801
38
Y = -6967414
09 feet Y = -2083167
15 meter
Z = 17213376
78 Z = 5264231
54
XDOT = 13136
903042 XDOT = 3930
837499
YDOT = 21569
959480 feet/sec YDOT = 6618
890400 meter/sec
ZDOT = -354
259780 ZDOT = -88
703962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4994144
36 X = 1522215
20
Y = 12746556
60 feet Y = 3885150
45 meter
Z = 17283017
58 Z = 5267863
76
XDOT = -22462
937492 XDOT = -6846
703348
YDOT = 9158
632281 feet/sec YDOT = 2791
551119 meter/sec
ZDOT = -277
690026 ZDOT = -84
639920
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 10026
42526095
00016717 00000-0 10270-3 0 9111
2 25544 51
6440 238
6803 0010821 246
1965 113
8065 15
75700148 41149
Satellite: ISS
Catalog Number: 25544
Epoch time: 10026
42526095 = yrday
fracday
Element set: 911
Inclination: 51
6440 deg
RA of node: 238
6803 deg
Eccentricity:
0010821
Arg of perigee: 246
1965 deg
Mean anomaly: 113
8065 deg
Mean motion: 15
75700148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4114
Checksum: 284
Coasting Arc #13 (Orbit 4129)
---------------------------------------
Vector Time (GMT): 2010/027/09:04:05
436
Vector Time (MET): N/A
Weight (LBS) : 750857
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3595612
52 A = 6727134
38 meter
Y = -5641402
71 meter E =
0004656
Z = 677057
19 I = 51
39445
XDOT = 4397
350247 Wp = 4
58896
YDOT = -2086
657755 meter/sec RA = 232
85310 deg
ZDOT = 5967
995117 TA = 2
81428
MA = 2
81166
Ha = 186
656 n
mi
Hp = 183
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11796629
01 X = -3535551
09
Y = -18508539
06 feet Y = -5681275
22 meter
Z = 2221316
25 Z = 659735
33
XDOT = 14427
002124 XDOT = 4391
365909
YDOT = -6845
990009 feet/sec YDOT = -2037
518065 meter/sec
ZDOT = 19580
036473 ZDOT = 5989
342292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20005245
02 X = 6097598
68
Y = -9045310
74 feet Y = -2757010
71 meter
Z = 2152497
50 Z = 656081
24
XDOT = 4071
932125 XDOT = 1241
124912
YDOT = 13683
905010 feet/sec YDOT = 4170
854247 meter/sec
ZDOT = 19664
556241 ZDOT = 5993
756742
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 10027
44000399
00016717 00000-0 10270-3 0 9129
2 25544 51
6438 233
4559 0010773 250
7059 109
2940 15
75707651 41303
Satellite: ISS
Catalog Number: 25544
Epoch time: 10027
44000399 = yrday
fracday
Element set: 912
Inclination: 51
6438 deg
RA of node: 233
4559 deg
Eccentricity:
0010773
Arg of perigee: 250
7059 deg
Mean anomaly: 109
2940 deg
Mean motion: 15
75707651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4130
Checksum: 296
Coasting Arc #14 (Orbit 4144)
---------------------------------------
Vector Time (GMT): 2010/028/09:04:05
436
Vector Time (MET): N/A
Weight (LBS) : 750857
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4096640
57 A = 6715757
69 meter
Y = 1548321
87 meter E =
0006426
Z = -5095344
31 I = 51
37551
XDOT = -4182
353881 Wp = 149
01621
YDOT = -6302
832389 meter/sec RA = 227
66749 deg
ZDOT = 1442
732606 TA = 134
88528
MA = 134
83309
Ha = 186
191 n
mi
Hp = 183
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13440421
81 X = -4088898
07
Y = 5079796
15 feet Y = 1502554
59 meter
Z = -16717008
89 Z = -5115226
33
XDOT = -13721
633467 XDOT = -4118
572010
YDOT = -20678
583953 feet/sec YDOT = -6349
245461 meter/sec
ZDOT = 4733
374693 ZDOT = 1422
569559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3361160
65 X = -1024481
76
Y = -13874907
41 feet Y = -4229071
78 meter
Z = -16795749
38 Z = -5119344
41
XDOT = 21231
612327 XDOT = 6471
395437
YDOT = -10794
413305 feet/sec YDOT = -3290
137175 meter/sec
ZDOT = 4653
257192 ZDOT = 1418
312792
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 10028
39130390
00016717 00000-0 10270-3 0 9130
2 25544 51
6435 228
5582 0010820 254
7084 105
2885 15
75757292 41452
Satellite: ISS
Catalog Number: 25544
Epoch time: 10028
39130390 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 228
5582 deg
Eccentricity:
0010820
Arg of perigee: 254
7084 deg
Mean anomaly: 105
2885 deg
Mean motion: 15
75757292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4145
Checksum: 306
Coasting Arc #15 (Orbit 4160)
---------------------------------------
Vector Time (GMT): 2010/029/09:04:05
436
Vector Time (MET): N/A
Weight (LBS) : 750857
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3651844
45 A = 6725794
23 meter
Y = 5333984
81 meter E =
0010133
Z = -1833453
02 I = 51
43005
XDOT = -5026
530727 Wp = 217
94028
YDOT = 1497
933850 meter/sec RA = 222
53115 deg
ZDOT = -5645
291769 TA = 342
48581
MA = 342
52073
Ha = 185
962 n
mi
Hp = 183
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11981116
97 X = 3600833
79
Y = 17499950
16 feet Y = 5374536
81 meter
Z = -6015265
80 Z = -1815836
42
XDOT = -16491
242543 XDOT = -5015
484347
YDOT = 4914
481135 feet/sec YDOT = 1441
786380 meter/sec
ZDOT = -18521
298454 ZDOT = -5669
682965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18702032
01 X = -5700379
36
Y = 10043246
17 feet Y = 3061181
43 meter
Z = -5945254
16 Z = -1812113
47
XDOT = -2372
195002 XDOT = -723
045036
YDOT = -15455
454555 feet/sec YDOT = -4710
822548 meter/sec
ZDOT = -18617
920647 ZDOT = -5674
742213
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 10029
40600269
00016717 00000-0 10270-3 0 9141
2 25544 51
6432 223
3343 0010964 258
2706 101
7228 15
75741822 41618
Satellite: ISS
Catalog Number: 25544
Epoch time: 10029
40600269 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 223
3343 deg
Eccentricity:
0010964
Arg of perigee: 258
2706 deg
Mean anomaly: 101
7228 deg
Mean motion: 15
75741822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4161
Checksum: 283
Coasting Arc #16 (Orbit 4176)
---------------------------------------
Vector Time (GMT): 2010/030/09:04:05
436
Vector Time (MET): N/A
Weight (LBS) : 750857
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4699178
74 A = 6717274
48 meter
Y = -1105873
34 meter E =
0004683
Z = 4675329
30 I = 51
42564
XDOT = 4120
197682 Wp = 301
14180
YDOT = 5896
332533 meter/sec RA = 217
32806 deg
ZDOT = -2746
172040 TA = 176
00275
MA = 175
99900
Ha = 185
179 n
mi
Hp = 183
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15417253
09 X = 4688484
41
Y = -3628193
36 feet Y = -1053384
31 meter
Z = 15339006
89 Z = 4698131
14
XDOT = 13517
708932 XDOT = 4067
297593
YDOT = 19344
923010 feet/sec YDOT = 5942
111349 meter/sec
ZDOT = -9009
750787 ZDOT = -2726
285049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2209235
65 X = 673375
03
Y = 15594710
43 feet Y = 4753267
74 meter
Z = 15429351
79 Z = 4702866
43
XDOT = -19368
774557 XDOT = -5903
602485
YDOT = 11581
061272 feet/sec YDOT = 3529
907476 meter/sec
ZDOT = -8930
700561 ZDOT = -2722
077531
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 10030
42067616
00016717 00000-0 10270-3 0 9159
2 25544 51
6432 218
1090 0010952 263
6297 96
3620 15
75852735 41779
Satellite: ISS
Catalog Number: 25544
Epoch time: 10030
42067616 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 218
1090 deg
Eccentricity:
0010952
Arg of perigee: 263
6297 deg
Mean anomaly: 96
3620 deg
Mean motion: 15
75852735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4177
Checksum: 302
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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