Date:
January 27th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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 99)
---------------------------------------
Vector Time (GMT): 2010/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4662189
93 A = 6724253
13 meter
Y = 3820244
26 meter E =
0007131
Z = 2970210
74 I = 51
35178
XDOT = -1509
862651 Wp = 157
14864
YDOT = 5698
007368 meter/sec RA = 242
53892 deg
ZDOT = -4961
245218 TA = 348
38124
MA = 348
39768
Ha = 187
570 n
mi
Hp = 183
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15295898
72 X = 4604696
17
Y = 12533609
77 feet Y = 3872057
92 meter
Z = 9744785
91 Z = 2992720
11
XDOT = -4953
617620 XDOT = -1549
365954
YDOT = 18694
249896 feet/sec YDOT = 5680
902722 meter/sec
ZDOT = -16277
051239 ZDOT = -4968
675548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1898500
19 X = -578662
86
Y = 19639333
25 feet Y = 5986068
77 meter
Z = 9834074
97 Z = 2997426
05
XDOT = -16791
703681 XDOT = -5118
111282
YDOT = 6537
821394 feet/sec YDOT = 1992
727961 meter/sec
ZDOT = -16306
311067 ZDOT = -4970
163613
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
53781759
00016717 00000-0 10270-3 0 9000
2 25544 51
6439 243
2603 0011547 244
2265 115
7708 15
75408922 1006
Satellite: ISS
Catalog Number: 25544
Epoch time: 10025
53781759 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 243
2603 deg
Eccentricity:
0011547
Arg of perigee: 244
2265 deg
Mean anomaly: 115
7708 deg
Mean motion: 15
75408922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 100
Checksum: 290
Coasting Arc #2 (Orbit 115)
---------------------------------------
Vector Time (GMT): 2010/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1319444
61 A = 6719150
38 meter
Y = -4740414
62 meter E =
0008487
Z = 4581866
06 I = 51
34750
XDOT = 5594
656731 Wp = 201
09291
YDOT = 4398
052817 meter/sec RA = 237
41801 deg
ZDOT = 2933
018235 TA = 219
67092
MA = 219
73304
Ha = 187
478 n
mi
Hp = 183
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4328886
53 X = 1350097
13
Y = -15552541
41 feet Y = -4725488
87 meter
Z = 15032368
95 Z = 4588349
82
XDOT = 18355
173003 XDOT = 5530
813243
YDOT = 14429
307143 feet/sec YDOT = 4460
258323 meter/sec
ZDOT = 9622
763237 ZDOT = 2960
042069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15181185
80 X = 4627225
43
Y = -5420692
19 feet Y = -1652226
98 meter
Z = 15057908
65 Z = 4589650
56
XDOT = -1759
590252 XDOT = -536
323109
YDOT = 22156
272328 feet/sec YDOT = 6753
231806 meter/sec
ZDOT = 9729
969410 ZDOT = 2965
694676
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
55275967
00016717 00000-0 10270-3 0 9013
2 25544 51
6425 238
0367 0011490 247
9328 112
0616 15
75358475 1169
Satellite: ISS
Catalog Number: 25544
Epoch time: 10026
55275967 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 238
0367 deg
Eccentricity:
0011490
Arg of perigee: 247
9328 deg
Mean anomaly: 112
0616 deg
Mean motion: 15
75358475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 116
Checksum: 306
Coasting Arc #3 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2010/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5108311
81 A = 6726142
18 meter
Y = -3822278
64 meter E =
0006954
Z = -2121990
98 I = 51
38775
XDOT = 1564
831075 Wp = 278
29943
YDOT = -5154
571629 meter/sec RA = 232
20977 deg
ZDOT = 5503
360783 TA = 57
87846
MA = 57
81100
Ha = 187
138 n
mi
Hp = 183
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16759553
17 X = -5054882
70
Y = -12540284
24 feet Y = -3879103
84 meter
Z = -6961912
65 Z = -2146677
29
XDOT = 5133
960221 XDOT = 1595
620299
YDOT = -16911
324243 feet/sec YDOT = -5136
901185 meter/sec
ZDOT = 18055
645614 ZDOT = 5511
036832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 359639
79 X = 109618
21
Y = -20895900
75 feet Y = -6369070
55 meter
Z = -7059856
23 Z = -2151844
18
XDOT = 15124
241108 XDOT = 4609
868690
YDOT = -5865
870465 feet/sec YDOT = -1787
917318 meter/sec
ZDOT = 18085
895224 ZDOT = 5512
580864
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
50425067
00016717 00000-0 10270-3 0 9028
2 25544 51
6412 233
1395 0011672 251
4440 108
5457 15
75412069 1319
Satellite: ISS
Catalog Number: 25544
Epoch time: 10027
50425067 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 233
1395 deg
Eccentricity:
0011672
Arg of perigee: 251
4440 deg
Mean anomaly: 108
5457 deg
Mean motion: 15
75412069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 131
Checksum: 271
Coasting Arc #4 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2010/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1464822
63 A = 6717235
53 meter
Y = 4266269
66 meter E =
0001521
Z = -4978765
95 I = 51
37592
XDOT = -6089
737448 Wp = 78
78778
YDOT = -4313
746216 meter/sec RA = 227
08009 deg
ZDOT = -1904
932266 TA = 172
75739
MA = 172
75520
Ha = 186
695 n
mi
Hp = 183
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4805848
53 X = -1488234
63
Y = 13996947
72 feet Y = 4249758
72 meter
Z = -16334533
95 Z = -4985938
34
XDOT = -19979
453571 XDOT = -6031
794201
YDOT = -14152
710681 feet/sec YDOT = -4381
521106 meter/sec
ZDOT = -6249
777777 ZDOT = -1934
375107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14022893
73 X = -4274178
01
Y = 4630817
52 feet Y = 1411473
18 meter
Z = -16362814
72 Z = -4987385
93
XDOT = -306
853039 XDOT = -93
528806
YDOT = -23423
055575 feet/sec YDOT = -7139
347339 meter/sec
ZDOT = -6366
607072 ZDOT = -1940
541835
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
51916154
00016717 00000-0 10270-3 0 9033
2 25544 51
6398 227
9163 0011582 255
2250 104
7630 15
75440622 1471
Satellite: ISS
Catalog Number: 25544
Epoch time: 10028
51916154 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 227
9163 deg
Eccentricity:
0011582
Arg of perigee: 255
2250 deg
Mean anomaly: 104
7630 deg
Mean motion: 15
75440622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 288
Coasting Arc #5 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2010/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5505002
45 A = 6727248
52 meter
Y = 3669781
16 meter E =
0009313
Z = 1183577
88 I = 51
43243
XDOT = -1834
068758 Wp = 178
11222
YDOT = 4641
748574 meter/sec RA = 221
88934 deg
ZDOT = -5869
446912 TA = 348
87157
MA = 348
89216
Ha = 186
150 n
mi
Hp = 183
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18061031
65 X = 5457807
74
Y = 12039964
44 feet Y = 3731077
40 meter
Z = 3883129
53 Z = 1210205
97
XDOT = -6017
285950 XDOT = -1857
325481
YDOT = 15228
833904 feet/sec YDOT = 4621
109299 meter/sec
ZDOT = -19256
715592 ZDOT = -5878
412710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1564233
29 X = 476778
31
Y = 21630601
80 feet Y = 6593007
43 meter
Z = 3988802
17 Z = 1215786
90
XDOT = -14069
319574 XDOT = -4288
328606
YDOT = 4570
373294 feet/sec YDOT = 1393
049780 meter/sec
ZDOT = -19292
087667 ZDOT = -5880
228321
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
53405572
00016717 00000-0 10270-3 0 9044
2 25544 51
6403 222
6931 0011650 260
2906 99
6942 15
75506917 1639
Satellite: ISS
Catalog Number: 25544
Epoch time: 10029
53405572 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 222
6931 deg
Eccentricity:
0011650
Arg of perigee: 260
2906 deg
Mean anomaly: 99
6942 deg
Mean motion: 15
75506917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 297
Coasting Arc #6 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2010/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1790071
52 A = 6716227
67 meter
Y = -3851398
92 meter E =
0009087
Z = 5210603
63 I = 51
41675
XDOT = 6486
990093 Wp = 250
87207
YDOT = 4069
166194 meter/sec RA = 216
74443 deg
ZDOT = 777
312650 TA = 191
69449
MA = 191
71561
Ha = 186
056 n
mi
Hp = 183
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5872938
05 X = 1807694
17
Y = -12635823
22 feet Y = -3831282
92 meter
Z = 17095156
26 Z = 5219342
18
XDOT = 21282
775897 XDOT = 6437
229914
YDOT = 13350
282790 feet/sec YDOT = 4141
429309 meter/sec
ZDOT = 2550
238354 ZDOT = 808
704675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13461648
01 X = 4103110
31
Y = -3429116
24 feet Y = -1045194
63 meter
Z = 17129652
41 Z = 5221118
06
XDOT = 2691
076242 XDOT = 820
240039
YDOT = 23955
990385 feet/sec YDOT = 7301
785869 meter/sec
ZDOT = 2674
828875 ZDOT = 815
287841
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
54893875
00016717 00000-0 10270-3 0 9055
2 25544 51
6393 217
4684 0011467 263
1214 96
8646 15
75437414 1796
Satellite: ISS
Catalog Number: 25544
Epoch time: 10030
54893875 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 217
4684 deg
Eccentricity:
0011467
Arg of perigee: 263
1214 deg
Mean anomaly: 96
8646 deg
Mean motion: 15
75437414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 179
Checksum: 325
Coasting Arc #7 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2010/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5791127
08 A = 6727880
61 meter
Y = -3410191
31 meter E =
0008563
Z = -159415
14 I = 51
48158
XDOT = 2309
816182 Wp = 337
38240
YDOT = -4208
736600 meter/sec RA = 211
57417 deg
ZDOT = 6024
306154 TA = 20
88078
MA = 20
84583
Ha = 185
749 n
mi
Hp = 183
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18999760
77 X = -5751788
93
Y = -11188291
69 feet Y = -3474731
17 meter
Z = -523015
54 Z = -187452
00
XDOT = 7578
137080 XDOT = 2327
443279
YDOT = -13808
190945 feet/sec YDOT = -4182
808315 meter/sec
ZDOT = 19764
783970 ZDOT = 6035
569699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3575344
39 X = -1089764
97
Y = -21754468
62 feet Y = -6630762
04 meter
Z = -634297
29 Z = -193333
81
XDOT = 13796
720150 XDOT = 4205
240302
YDOT = -2852
884268 feet/sec YDOT = -869
559125 meter/sec
ZDOT = 19809
272602 ZDOT = 6037
866289
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 10031
50037333
00016717 00000-0 10270-3 0 9062
2 25544 51
6391 212
5703 0011553 266
4441 93
5401 15
75504192 1944
Satellite: ISS
Catalog Number: 25544
Epoch time: 10031
50037333 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 212
5703 deg
Eccentricity:
0011553
Arg of perigee: 266
4441 deg
Mean anomaly: 93
5401 deg
Mean motion: 15
75504192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 270
Coasting Arc #8 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2010/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2273292
88 A = 6715759
46 meter
Y = 3532640
68 meter E =
0003680
Z = -5242792
81 I = 51
46776
XDOT = -6733
393455 Wp = 102
14830
YDOT = -3714
565183 meter/sec RA = 206
41368 deg
ZDOT = 416
198029 TA = 171
81616
MA = 171
81016
Ha = 185
454 n
mi
Hp = 183
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7458309
97 X = -2287158
68
Y = 11590028
48 feet Y = 3507141
74 meter
Z = -17200763
80 Z = -5253869
92
XDOT = -22091
185877 XDOT = -6693
377852
YDOT = -12186
893644 feet/sec YDOT = -3789
638231 meter/sec
ZDOT = 1365
479097 ZDOT = 383
585355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13580070
58 X = -4139205
51
Y = 2007237
91 feet Y = 611806
12 meter
Z = -17244538
32 Z = -5256135
28
XDOT = -5074
776280 XDOT = -1546
791810
YDOT = -23700
154137 feet/sec YDOT = -7223
806981 meter/sec
ZDOT = 1236
031247 ZDOT = 376
742324
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 10032
51522408
00016717 00000-0 10270-3 0 9077
2 25544 51
6395 207
3467 0011377 270
1276 89
8584 15
75538228 2105
Satellite: ISS
Catalog Number: 25544
Epoch time: 10032
51522408 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 207
3467 deg
Eccentricity:
0011377
Arg of perigee: 270
1276 deg
Mean anomaly: 89
8584 deg
Mean motion: 15
75538228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 306
Coasting Arc #9 (Orbit 225)
---------------------------------------
Vector Time (GMT): 2010/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5917345
71 A = 6727311
62 meter
Y = 3062589
36 meter E =
0008516
Z = -890644
05 I = 51
53527
XDOT = -2930
379228 Wp = 216
12771
YDOT = 3926
820509 meter/sec RA = 201
26843 deg
ZDOT = -5944
287662 TA = 333
61444
MA = 333
65778
Ha = 185
673 n
mi
Hp = 183
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19413863
87 X = 5886986
00
Y = 10047865
35 feet Y = 3128590
85 meter
Z = -2922060
52 Z = -861972
02
XDOT = -9614
105080 XDOT = -2945
196183
YDOT = 12883
269386 feet/sec YDOT = 3893
968271 meter/sec
ZDOT = -19502
256108 ZDOT = -5958
559229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5461233
90 X = 1664584
09
Y = 21182180
87 feet Y = 6456328
73 meter
Z = -2808252
84 Z = -855955
47
XDOT = -14390
834412 XDOT = -4386
326329
YDOT = 1107
307834 feet/sec YDOT = 337
507428 meter/sec
ZDOT = -19558
680232 ZDOT = -5961
485735
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 10033
53005760
00016717 00000-0 10270-3 0 9088
2 25544 51
6400 202
1228 0011457 275
4237 84
5620 15
75598849 2269
Satellite: ISS
Catalog Number: 25544
Epoch time: 10033
53005760 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 202
1228 deg
Eccentricity:
0011457
Arg of perigee: 275
4237 deg
Mean anomaly: 84
5620 deg
Mean motion: 15
75598849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 226
Checksum: 291
Coasting Arc #10 (Orbit 241)
---------------------------------------
Vector Time (GMT): 2010/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2862891
83 A = 6716556
86 meter
Y = -3364491
68 meter E =
0008425
Z = 5066473
51 I = 51
52693
XDOT = 6761
908097 Wp = 302
01503
YDOT = 3297
593825 meter/sec RA = 196
09094 deg
ZDOT = -1628
672150 TA = 163
67831
MA = 163
65117
Ha = 185
909 n
mi
Hp = 183
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9392689
75 X = 2875689
80
Y = -11038358
54 feet Y = -3332405
48 meter
Z = 16622288
42 Z = 5080412
35
XDOT = 22184
737851 XDOT = 6732
442921
YDOT = 10818
877379 feet/sec YDOT = 3373
044711 meter/sec
ZDOT = -5343
412566 ZDOT = -1595
894989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14414390
71 X = 4393506
29
Y = -676366
32 feet Y = -206156
45 meter
Z = 16677419
51 Z = 5083277
47
XDOT = 7101
477196 XDOT = 2164
530249
YDOT = 22601
586591 feet/sec YDOT = 6888
963593 meter/sec
ZDOT = -5213
309378 ZDOT = -1589
016699
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 10034
54487897
00016717 00000-0 10270-3 0 9096
2 25544 51
6398 196
8986 0011284 278
0565 81
9319 15
75538253 2423
Satellite: ISS
Catalog Number: 25544
Epoch time: 10034
54487897 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 196
8986 deg
Eccentricity:
0011284
Arg of perigee: 278
0565 deg
Mean anomaly: 81
9319 deg
Mean motion: 15
75538253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 242
Checksum: 353
Coasting Arc #11 (Orbit 257)
---------------------------------------
Vector Time (GMT): 2010/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5837232
00 A = 6725972
61 meter
Y = -2703086
35 meter E =
0007968
Z = 1946101
64 I = 51
58959
XDOT = 3640
693904 Wp = 14
16629
YDOT = -3825
123555 meter/sec RA = 190
96872 deg
ZDOT = 5609
846579 TA = 7
52140
MA = 7
50946
Ha = 186
222 n
mi
Hp = 183
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19151023
61 X = -5816025
45
Y = -8868393
53 feet Y = -2768243
16 meter
Z = 6384847
90 Z = 1917796
29
XDOT = 11944
533805 XDOT = 3655
945294
YDOT = -12549
617961 feet/sec YDOT = -3784
325869 meter/sec
ZDOT = 18405
008462 ZDOT = 5627
569873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6870605
72 X = -2094160
62
Y = -19990673
02 feet Y = -6093157
14 meter
Z = 6272492
42 Z = 1911855
69
XDOT = 15792
198785 XDOT = 4813
462190
YDOT = 366
424782 feet/sec YDOT = 111
686274 meter/sec
ZDOT = 18475
132840 ZDOT = 5631
220490
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 10035
55968024
00016717 00000-0 10270-3 0 9106
2 25544 51
6407 191
6746 0011363 281
7400 78
2489 15
75622531 2585
Satellite: ISS
Catalog Number: 25544
Epoch time: 10035
55968024 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 191
6746 deg
Eccentricity:
0011363
Arg of perigee: 281
7400 deg
Mean anomaly: 78
2489 deg
Mean motion: 15
75622531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 258
Checksum: 305
Coasting Arc #12 (Orbit 272)
---------------------------------------
Vector Time (GMT): 2010/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3481011
23 A = 6717990
73 meter
Y = 3360991
31 meter E =
0000705
Z = -4660103
89 I = 51
59338
XDOT = -6560
308712 Wp = 217
94336
YDOT = -2900
978070 meter/sec RA = 185
77920 deg
ZDOT = 2807
396070 TA = 79
77704
MA = 79
76910
Ha = 186
474 n
mi
Hp = 183
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11420640
53 X = -3495698
08
Y = 11026874
37 feet Y = 3321982
53 meter
Z = -15289054
75 Z = -4677050
03
XDOT = -21523
322546 XDOT = -6541
019523
YDOT = -9517
644586 feet/sec YDOT = -2974
231521 meter/sec
ZDOT = 9210
617028 ZDOT = 2775
573329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15807852
45 X = -4818233
43
Y = -281831
89 feet Y = -85902
36 meter
Z = -15356124
35 Z = -4680546
70
XDOT = -8455
057308 XDOT = -2577
101468
YDOT = -20870
196366 feet/sec YDOT = -6361
235852 meter/sec
ZDOT = 9084
294408 ZDOT = 2768
892936
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 10036
51104416
00016717 00000-0 10270-3 0 9111
2 25544 51
6412 186
7781 0011309 285
8400 74
1517 15
75628698 2734
Satellite: ISS
Catalog Number: 25544
Epoch time: 10036
51104416 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 186
7781 deg
Eccentricity:
0011309
Arg of perigee: 285
8400 deg
Mean anomaly: 74
1517 deg
Mean motion: 15
75628698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 273
Checksum: 299
Coasting Arc #13 (Orbit 288)
---------------------------------------
Vector Time (GMT): 2010/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5556314
72 A = 6723778
42 meter
Y = 2388407
02 meter E =
0006790
Z = -2935130
01 I = 51
64292
XDOT = -4338
441965 Wp = 287
71098
YDOT = 3917
031903 meter/sec RA = 180
67507 deg
ZDOT = -5013
923959 TA = 286
12318
MA = 286
19792
Ha = 186
848 n
mi
Hp = 183
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18229378
99 X = 5543452
29
Y = 7835981
04 feet Y = 2450469
20 meter
Z = -9629691
64 Z = -2908169
00
XDOT = -14233
733480 XDOT = -4357
564091
YDOT = 12851
154539 feet/sec YDOT = 3868
410115 meter/sec
ZDOT = -16449
881755 ZDOT = -5035
046123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7628274
39 X = 2325098
03
Y = 18373137
82 feet Y = 5600132
41 meter
Z = -9522660
07 Z = -2902506
79
XDOT = -17753
545169 XDOT = -5411
280568
YDOT = -1217
942735 feet/sec YDOT = -371
228946 meter/sec
ZDOT = -16533
501414 ZDOT = -5039
411231
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 10037
52581563
00016717 00000-0 10270-3 0 9126
2 25544 51
6410 181
5540 0011349 290
2631 69
7312 15
75663032 2899
Satellite: ISS
Catalog Number: 25544
Epoch time: 10037
52581563 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 181
5540 deg
Eccentricity:
0011349
Arg of perigee: 290
2631 deg
Mean anomaly: 69
7312 deg
Mean motion: 15
75663032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 289
Checksum: 289
Coasting Arc #14 (Orbit 304)
---------------------------------------
Vector Time (GMT): 2010/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4072288
28 A = 6720312
56 meter
Y = -3518710
41 meter E =
0006955
Z = 4029538
03 I = 51
66179
XDOT = 6109
323647 Wp = 1
27441
YDOT = 2604
835714 meter/sec RA = 175
47817 deg
ZDOT = -3892
564342 TA = 128
89719
MA = 128
83514
Ha = 187
086 n
mi
Hp = 183
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13360525
84 X = 4091758
04
Y = -11544325
51 feet Y = -3473062
98 meter
Z = 13220269
13 Z = 4049368
00
XDOT = 20043
712753 XDOT = 6098
650895
YDOT = 8546
048929 feet/sec YDOT = 2673
094280 meter/sec
ZDOT = -12770
880388 ZDOT = -3862
911585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17584198
77 X = 5359663
79
Y = 699097
63 feet Y = 213084
96 meter
Z = 13298790
70 Z = 4053471
41
XDOT = 8841
977112 XDOT = 2695
034624
YDOT = 18730
158632 feet/sec YDOT = 5708
952351 meter/sec
ZDOT = -12653
150239 ZDOT = -3856
680193
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 10038
54057196
00016717 00000-0 10270-3 0 9130
2 25544 51
6411 176
3299 0011283 293
8994 66
0987 15
75657505 3056
Satellite: ISS
Catalog Number: 25544
Epoch time: 10038
54057196 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 176
3299 deg
Eccentricity:
0011283
Arg of perigee: 293
8994 deg
Mean anomaly: 66
0987 deg
Mean motion: 15
75657505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 305
Checksum: 330
Coasting Arc #15 (Orbit 320)
---------------------------------------
Vector Time (GMT): 2010/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5063978
35 A = 6720959
88 meter
Y = -2206162
85 meter E =
0003954
Z = 3824702
58 I = 51
69560
XDOT = 4960
105115 Wp = 19
83949
YDOT = -4174
459003 meter/sec RA = 170
38434 deg
ZDOT = 4161
764203 TA = 26
66581
MA = 26
64548
Ha = 187
366 n
mi
Hp = 183
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16614102
21 X = -5057511
60
Y = -7238067
08 feet Y = -2262755
27 meter
Z = 12548236
82 Z = 3800117
91
XDOT = 16273
310746 XDOT = 4986
199347
YDOT = -13695
731637 feet/sec YDOT = -4118
846459 meter/sec
ZDOT = 13654
082030 ZDOT = 4185
923067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7475806
20 X = -2278625
73
Y = -16582242
83 feet Y = -5054267
61 meter
Z = 12450614
39 Z = 3794947
27
XDOT = 19984
897607 XDOT = 6091
396790
YDOT = 1308
082471 feet/sec YDOT = 398
703537 meter/sec
ZDOT = 13749
762735 ZDOT = 4190
927682
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 10039
55530923
00016717 00000-0 10270-3 0 9147
2 25544 51
6423 171
1056 0011405 297
8791 62
1217 15
75736490 3210
Satellite: ISS
Catalog Number: 25544
Epoch time: 10039
55530923 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 171
1056 deg
Eccentricity:
0011405
Arg of perigee: 297
8791 deg
Mean anomaly: 62
1217 deg
Mean motion: 15
75736490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 321
Checksum: 291
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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