Date:
October 30th 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) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2010/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 440432
45 A = 6737711
78 meter
Y = 6693435
52 meter E =
0018883
Z = -534857
09 I = 51
32540
XDOT = -4847
944422 Wp = 137
75344
YDOT = -148
146550 meter/sec RA = 262
57611 deg
ZDOT = -5982
039468 TA = 48
08991
MA = 47
92903
Ha = 195
651 n
mi
Hp = 184
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1444988
34 X = 368150
75
Y = 21960090
29 feet Y = 6697956
56 meter
Z = -1754780
49 Z = -532892
92
XDOT = -15905
329468 XDOT = -4816
867413
YDOT = -486
045112 feet/sec YDOT = -202
185332 meter/sec
ZDOT = -19626
113740 ZDOT = -6005
515642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14358094
04 X = -4376347
06
Y = -16679513
08 feet Y = -5083915
59 meter
Z = -1746937
49 Z = -532466
55
XDOT = 11696
845528 XDOT = 3565
198517
YDOT = -8050
433166 feet/sec YDOT = -2453
772029 meter/sec
ZDOT = -19720
232894 ZDOT = -6010
726986
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10302
53082327
00016717 00000-0 10270-3 0 9003
2 25544 51
6434 263
2256 0007819 136
0044 224
1742 15
72014697 4608
Satellite: ISS
Catalog Number: 25544
Epoch time: 10302
53082327 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 263
2256 deg
Eccentricity:
0007819
Arg of perigee: 136
0044 deg
Mean anomaly: 224
1742 deg
Mean motion: 15
72014697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 460
Checksum: 275
Coasting Arc #2 (Orbit 475)
---------------------------------------
Vector Time (GMT): 2010/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4070349
07 A = 6725623
93 meter
Y = -1053458
23 meter E =
0009649
Z = 5243198
30 I = 51
29027
XDOT = 1772
986569 Wp = 130
30647
YDOT = 7496
199121 meter/sec RA = 257
42885 deg
ZDOT = 123
429394 TA = 318
48044
MA = 318
55370
Ha = 195
398 n
mi
Hp = 184
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13354163
60 X = 4056355
67
Y = -3456227
78 feet Y = -1008019
35 meter
Z = 17202094
15 Z = 5262938
32
XDOT = 5816
885069 XDOT = 1688
431300
YDOT = 24593
829136 feet/sec YDOT = 7515
552949 meter/sec
ZDOT = 404
952079 ZDOT = 131
837249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8330864
51 X = -2539247
50
Y = 10869523
40 feet Y = 3313030
73 meter
Z = 17281244
07 Z = 5267323
19
XDOT = -18907
611973 XDOT = -5763
040129
YDOT = -15221
751967 feet/sec YDOT = -4639
590000 meter/sec
ZDOT = 438
638491 ZDOT = 133
697012
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10303
54792423
00016717 00000-0 10270-3 0 9011
2 25544 51
6433 258
0188 0007763 140
2402 219
9331 15
72061952 4765
Satellite: ISS
Catalog Number: 25544
Epoch time: 10303
54792423 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 258
0188 deg
Eccentricity:
0007763
Arg of perigee: 140
2402 deg
Mean anomaly: 219
9331 deg
Mean motion: 15
72061952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 476
Checksum: 290
Coasting Arc #3 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2010/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2585097
24 A = 6737327
41 meter
Y = -6178917
72 meter E =
0011478
Z = -726624
22 I = 51
33749
XDOT = 4213
366588 Wp = 81
11138
YDOT = -2452
785118 meter/sec RA = 252
27620 deg
ZDOT = 5949
522141 TA = 270
94931
MA = 271
08082
Ha = 195
407 n
mi
Hp = 184
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8481290
17 X = -2512281
45
Y = -20272039
78 feet Y = -6207418
72 meter
Z = -2383937
73 Z = -739005
75
XDOT = 13823
381195 XDOT = 4211
578850
YDOT = -8047
195268 feet/sec YDOT = -2405
678556 meter/sec
ZDOT = 19519
429598 ZDOT = 5969
986669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19319901
23 X = 5888705
89
Y = 10458975
99 feet Y = 3187895
88 meter
Z = -2433572
82 Z = -741753
00
XDOT = -4851
371480 XDOT = -1478
698027
YDOT = 13461
119098 feet/sec YDOT = 4102
949101 meter/sec
ZDOT = 19601
489767 ZDOT = 5974
534081
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10304
50143028
00016717 00000-0 10270-3 0 9020
2 25544 51
6429 253
1361 0007818 143
8779 216
2913 15
72104828 4919
Satellite: ISS
Catalog Number: 25544
Epoch time: 10304
50143028 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 253
1361 deg
Eccentricity:
0007818
Arg of perigee: 143
8779 deg
Mean anomaly: 216
2913 deg
Mean motion: 15
72104828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 293
Coasting Arc #4 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2010/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3120258
79 A = 6726144
51 meter
Y = 3108648
10 meter E =
0018109
Z = -5097844
13 I = 51
31125
XDOT = -3982
319661 Wp = 102
28904
YDOT = -6405
463032 meter/sec RA = 247
15158 deg
ZDOT = -1476
772893 TA = 153
50654
MA = 153
41386
Ha = 195
223 n
mi
Hp = 184
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10237069
53 X = -3130023
56
Y = 10198976
69 feet Y = 3073700
66 meter
Z = -16725210
39 Z = -5113026
44
XDOT = -13065
353220 XDOT = -3903
222595
YDOT = -21015
298663 feet/sec YDOT = -6449
553536 meter/sec
ZDOT = -4845
055422 ZDOT = -1495
926896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1238467
10 X = 377484
77
Y = -14326295
72 feet Y = -4366654
94 meter
Z = -16786090
40 Z = -5116400
35
XDOT = 22435
038929 XDOT = 6838
199866
YDOT = 7674
896858 feet/sec YDOT = 2339
308562 meter/sec
ZDOT = -4921
857430 ZDOT = -1500
182145
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10305
51847567
00016717 00000-0 10270-3 0 9032
2 25544 51
6437 247
9273 0007726 147
9379 212
2254 15
72142155 5077
Satellite: ISS
Catalog Number: 25544
Epoch time: 10305
51847567 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 247
9273 deg
Eccentricity:
0007726
Arg of perigee: 147
9379 deg
Mean anomaly: 212
2254 deg
Mean motion: 15
72142155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 313
Coasting Arc #5 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2010/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4258840
69 A = 6735843
65 meter
Y = 4866014
03 meter E =
0020757
Z = 1843129
21 I = 51
35787
XDOT = -2701
834856 Wp = 126
85016
YDOT = 4510
513726 meter/sec RA = 241
97901 deg
ZDOT = -5633
725981 TA = 32
60471
MA = 32
47671
Ha = 195
065 n
mi
Hp = 184
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13972574
43 X = 4195157
71
Y = 15964612
96 feet Y = 4913282
97 meter
Z = 6047011
85 Z = 1863664
15
XDOT = -8864
287585 XDOT = -2724
703260
YDOT = 14798
273378 feet/sec YDOT = 4480
172030 meter/sec
ZDOT = -18483
352955 ZDOT = -5646
907544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20985330
92 X = -6396328
86
Y = -2952099
94 feet Y = -899800
06 meter
Z = 6129359
48 Z = 1868228
77
XDOT = -3279
028563 XDOT = -999
447906
YDOT = -15387
798525 feet/sec YDOT = -4690
200990 meter/sec
ZDOT = -18536
208292 ZDOT = -5649
836287
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10306
53549262
00016717 00000-0 10270-3 0 9047
2 25544 51
6443 242
7191 0007738 151
5414 208
6172 15
72183149 5234
Satellite: ISS
Catalog Number: 25544
Epoch time: 10306
53549262 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 242
7191 deg
Eccentricity:
0007738
Arg of perigee: 151
5414 deg
Mean anomaly: 208
6172 deg
Mean motion: 15
72183149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 295
Coasting Arc #6 (Orbit 538)
---------------------------------------
Vector Time (GMT): 2010/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1466444
59 A = 6727586
06 meter
Y = -4601691
77 meter E =
0014720
Z = 4679492
28 I = 51
34630
XDOT = 5575
554902 Wp = 137
07735
YDOT = 4560
762720 meter/sec RA = 236
87532 deg
ZDOT = 2722
028874 TA = 285
92778
MA = 286
08993
Ha = 194
891 n
mi
Hp = 184
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4811169
92 X = 1495059
86
Y = -15097413
93 feet Y = -4585132
90 meter
Z = 15352664
95 Z = 4686686
16
XDOT = 18292
502960 XDOT = 5510
917746
YDOT = 14963
132285 feet/sec YDOT = 4622
750644 meter/sec
ZDOT = 8930
540926 ZDOT = 2748
958410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6558821
11 X = 1999128
67
Y = 14393562
51 feet Y = 4387157
85 meter
Z = 15381508
66 Z = 4688283
84
XDOT = -22519
814108 XDOT = -6864
039340
YDOT = 548
053441 feet/sec YDOT = 167
046689 meter/sec
ZDOT = 9038
536770 ZDOT = 2754
946008
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10307
55247890
00016717 00000-0 10270-3 0 9053
2 25544 51
6446 237
5110 0007757 156
6463 203
5053 15
72259859 5392
Satellite: ISS
Catalog Number: 25544
Epoch time: 10307
55247890 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 237
5110 deg
Eccentricity:
0007757
Arg of perigee: 156
6463 deg
Mean anomaly: 203
5053 deg
Mean motion: 15
72259859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 539
Checksum: 319
Coasting Arc #7 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2010/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5300550
77 A = 6733461
17 meter
Y = -3019694
52 meter E =
0008591
Z = -2863330
28 I = 51
38414
XDOT = 569
398916 Wp = 127
78318
YDOT = -5775
455482 meter/sec RA = 231
68846 deg
ZDOT = 5041
921350 TA = 199
27433
MA = 199
30684
Ha = 194
789 n
mi
Hp = 184
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17390258
44 X = -5252480
07
Y = -9907134
27 feet Y = -3078699
76 meter
Z = -9394128
23 Z = -2888964
30
XDOT = 1868
106679 XDOT = 609
445326
YDOT = -18948
344757 feet/sec YDOT = -5768
864086 meter/sec
ZDOT = 16541
736713 ZDOT = 5044
784991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19446606
48 X = 5927325
66
Y = -4523253
08 feet Y = -1378687
54 meter
Z = -9496932
20 Z = -2894664
93
XDOT = 11257
246031 XDOT = 3431
208590
YDOT = 13677
928591 feet/sec YDOT = 4169
032635 meter/sec
ZDOT = 16553
214853 ZDOT = 5045
419887
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10308
50587979
00016717 00000-0 10270-3 0 9065
2 25544 51
6447 232
6276 0007653 159
7451 200
4017 15
72272757 5543
Satellite: ISS
Catalog Number: 25544
Epoch time: 10308
50587979 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 232
6276 deg
Eccentricity:
0007653
Arg of perigee: 159
7451 deg
Mean anomaly: 200
4017 deg
Mean motion: 15
72272757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 554
Checksum: 322
Coasting Arc #8 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2010/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 504543
73 A = 6729604
18 meter
Y = 5308999
93 meter E =
0010572
Z = -4109366
00 I = 51
39227
XDOT = -6305
910572 Wp = 117
04084
YDOT = -2300
266274 meter/sec RA = 226
59710 deg
ZDOT = -3758
156410 TA = 114
31997
MA = 114
20953
Ha = 194
604 n
mi
Hp = 185
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1655327
20 X = 465103
22
Y = 17417978
77 feet Y = 5314421
53 meter
Z = -13482171
92 Z = -4107010
64
XDOT = -20688
682979 XDOT = -6261
462851
YDOT = -7546
805361 feet/sec YDOT = -2370
534229 meter/sec
ZDOT = -12329
909483 ZDOT = -3788
683560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13313934
53 X = -4058087
25
Y = -11363096
52 feet Y = -3463471
82 meter
Z = -13472721
97 Z = -4106485
66
XDOT = 19269
647861 XDOT = 5873
388668
YDOT = -7860
990673 feet/sec YDOT = -2396
029957 meter/sec
ZDOT = -12452
343248 ZDOT = -3795
474222
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10309
52281158
00016717 00000-0 10270-3 0 9079
2 25544 51
6457 227
4186 0007640 163
1530 196
9887 15
72334405 5700
Satellite: ISS
Catalog Number: 25544
Epoch time: 10309
52281158 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 227
4186 deg
Eccentricity:
0007640
Arg of perigee: 163
1530 deg
Mean anomaly: 196
9887 deg
Mean motion: 15
72334405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 313
Coasting Arc #9 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5540008
52 A = 6730868
50 meter
Y = 970749
10 meter E =
0014749
Z = 3680382
42 I = 51
41817
XDOT = 1783
093156 Wp = 115
30024
YDOT = 6143
158819 meter/sec RA = 221
40713 deg
ZDOT = -4297
224022 TA = 20
23716
MA = 20
17876
Ha = 194
378 n
mi
Hp = 185
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18175880
97 X = 5510862
47
Y = 3184872
36 feet Y = 1032537
73 meter
Z = 12074745
46 Z = 3707225
87
XDOT = 5850
043162 XDOT = 1735
142494
YDOT = 20154
720535 feet/sec YDOT = 6162
830460 meter/sec
ZDOT = -14098
504009 ZDOT = -4288
677771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15087522
42 X = -4598676
83
Y = 10500523
55 feet Y = 3200559
58 meter
Z = 12182414
02 Z = 3713199
79
XDOT = -17648
813970 XDOT = -5379
358498
YDOT = -9014
466874 feet/sec YDOT = -2747
609503 meter/sec
ZDOT = -14064
224159 ZDOT = -4286
775524
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10310
53971518
00016717 00000-0 10270-3 0 9089
2 25544 51
6452 222
2103 0007679 167
3403 192
7954 15
72353793 5861
Satellite: ISS
Catalog Number: 25544
Epoch time: 10310
53971518 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 222
2103 deg
Eccentricity:
0007679
Arg of perigee: 167
3403 deg
Mean anomaly: 192
7954 deg
Mean motion: 15
72353793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 314
Coasting Arc #10 (Orbit 601)
---------------------------------------
Vector Time (GMT): 2010/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2577816
48 A = 6731859
96 meter
Y = -5225670
30 meter E =
0015634
Z = 3367101
92 I = 51
44542
XDOT = 6156
194498 Wp = 118
55035
YDOT = -44
642153 meter/sec RA = 216
32060 deg
ZDOT = 4620
246842 TA = 281
22603
MA = 281
40171
Ha = 194
332 n
mi
Hp = 185
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8457403
14 X = -2535547
72
Y = -17144587
60 feet Y = -5254260
83 meter
Z = 11046922
31 Z = 3354680
92
XDOT = 20197
488509 XDOT = 6133
791171
YDOT = -146
463757 feet/sec YDOT = 24
074609 meter/sec
ZDOT = 15158
290163 ZDOT = 4650
100083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18232858
95 X = 5557375
41
Y = 5841724
12 feet Y = 1780557
51 meter
Z = 10997097
73 Z = 3351915
39
XDOT = -13486
995017 XDOT = -4110
836081
YDOT = 13187
466639 feet/sec YDOT = 4019
539831 meter/sec
ZDOT = 15278
044411 ZDOT = 4656
747936
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10311
55658929
00016717 00000-0 10270-3 0 9091
2 25544 51
6453 217
0010 0007605 171
4401 188
6893 15
72401427 6027
Satellite: ISS
Catalog Number: 25544
Epoch time: 10311
55658929 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 217
0010 deg
Eccentricity:
0007605
Arg of perigee: 171
4401 deg
Mean anomaly: 188
6893 deg
Mean motion: 15
72401427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 602
Checksum: 292
Coasting Arc #11 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2010/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5057430
23 A = 6728309
84 meter
Y = 985005
25 meter E =
0014058
Z = -4341075
63 I = 51
45964
XDOT = -4018
148516 Wp = 140
20413
YDOT = -5597
480740 meter/sec RA = 211
13425 deg
ZDOT = 3406
591388 TA = 164
33243
MA = 164
28888
Ha = 194
088 n
mi
Hp = 185
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16592618
86 X = -5046980
18
Y = 3231644
53 feet Y = 928508
75 meter
Z = -14242374
11 Z = -4365619
78
XDOT = -13182
901954 XDOT = -3971
806815
YDOT = -18364
438123 feet/sec YDOT = -5642
155207 meter/sec
ZDOT = 11176
480932 ZDOT = 3387
182938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8948133
29 X = 2727391
03
Y = -14243413
66 feet Y = -4341392
48 meter
Z = -14340844
66 Z = -4371089
45
XDOT = 21417
119443 XDOT = 6527
938006
YDOT = 2265
452559 feet/sec YDOT = 690
509940 meter/sec
ZDOT = 11098
617725 ZDOT = 3382
858683
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10312
50988220
00016717 00000-0 10270-3 0 9109
2 25544 51
6455 212
1173 0007554 175
6967 184
4262 15
72454150 6172
Satellite: ISS
Catalog Number: 25544
Epoch time: 10312
50988220 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 212
1173 deg
Eccentricity:
0007554
Arg of perigee: 175
6967 deg
Mean anomaly: 184
4262 deg
Mean motion: 15
72454150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 295
Coasting Arc #12 (Orbit 632)
---------------------------------------
Vector Time (GMT): 2010/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4366348
21 A = 6733682
24 meter
Y = 4420180
88 meter E =
0011561
Z = -2582736
11 I = 51
50429
XDOT = -5222
343640 Wp = 160
46475
YDOT = 2098
861864 meter/sec RA = 206
04560 deg
ZDOT = -5254
243766 TA = 48
90489
MA = 48
80510
Ha = 193
989 n
mi
Hp = 185
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14325289
40 X = 4329143
12
Y = 14501905
78 feet Y = 4468800
17 meter
Z = -8473543
66 Z = -2561614
03
XDOT = -17133
673360 XDOT = -5219
900695
YDOT = 6886
029736 feet/sec YDOT = 2040
476509 meter/sec
ZDOT = -17238
332566 ZDOT = -5279
608331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20399529
56 X = -6217776
61
Y = 898595
99 feet Y = 273892
06 meter
Z = -8388793
04 Z = -2556904
12
XDOT = 6413
052728 XDOT = 1954
698471
YDOT = -15751
056960 feet/sec YDOT = -4800
922161 meter/sec
ZDOT = -17340
108797 ZDOT = -5285
265161
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10313
52670093
00016717 00000-0 10270-3 0 9119
2 25544 51
6455 206
9077 0007638 180
7581 179
3571 15
72473351 6336
Satellite: ISS
Catalog Number: 25544
Epoch time: 10313
52670093 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 206
9077 deg
Eccentricity:
0007638
Arg of perigee: 180
7581 deg
Mean anomaly: 179
3571 deg
Mean motion: 15
72473351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 633
Checksum: 309
Coasting Arc #13 (Orbit 648)
---------------------------------------
Vector Time (GMT): 2010/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3925859
62 A = 6726091
25 meter
Y = -2590110
11 meter E =
0006604
Z = 4802164
09 I = 51
50738
XDOT = 5871
637698 Wp = 125
87243
YDOT = 4335
235143 meter/sec RA = 200
87094 deg
ZDOT = -2463
359480 TA = 348
23513
MA = 348
25055
Ha = 193
521 n
mi
Hp = 185
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12880116
87 X = 3931202
52
Y = -8497736
58 feet Y = -2546179
23 meter
Z = 15755131
52 Z = 4821249
02
XDOT = 19263
903209 XDOT = 5834
690636
YDOT = 14223
212410 feet/sec YDOT = 4400
688903 meter/sec
ZDOT = -8081
888059 ZDOT = -2434
924082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2039872
07 X = -621753
01
Y = 15216065
69 feet Y = 4637856
82 meter
Z = 15831720
48 Z = 4825508
40
XDOT = -22316
063457 XDOT = -6801
936142
YDOT = 5293
529255 feet/sec YDOT = 1613
467717 meter/sec
ZDOT = -7967
775876 ZDOT = -2428
578087
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 10314
54348987
00016717 00000-0 10270-3 0 9127
2 25544 51
6451 201
6980 0007449 184
9527 175
1563 15
72579009 6492
Satellite: ISS
Catalog Number: 25544
Epoch time: 10314
54348987 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 201
6980 deg
Eccentricity:
0007449
Arg of perigee: 184
9527 deg
Mean anomaly: 175
1563 deg
Mean motion: 15
72579009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 649
Checksum: 333
Coasting Arc #14 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2010/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5752607
73 A = 6734993
39 meter
Y = -3045665
24 meter E =
0011658
Z = 1722855
86 I = 51
56590
XDOT = 3655
384728 Wp = 96
38467
YDOT = -3663
469499 meter/sec RA = 195
77374 deg
ZDOT = 5694
833665 TA = 282
68088
MA = 282
81119
Ha = 193
505 n
mi
Hp = 185
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18873384
93 X = -5726492
41
Y = -9992340
01 feet Y = -3109848
43 meter
Z = 5652414
23 Z = 1694972
61
XDOT = 11992
732048 XDOT = 3668
413822
YDOT = -12019
256886 feet/sec YDOT = -3622
520238 meter/sec
ZDOT = 18683
837483 ZDOT = 5712
623207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19843215
46 X = 6048212
07
Y = -7971884
37 feet Y = -2429830
36 meter
Z = 5540502
15 Z = 1688745
05
XDOT = 912
935946 XDOT = 278
262876
YDOT = 15386
972332 feet/sec YDOT = 4689
949167 meter/sec
ZDOT = 18755
235310 ZDOT = 5716
595722
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 10315
56025290
00016717 00000-0 10270-3 0 9130
2 25544 51
6450 196
4874 0007423 188
7907 171
3127 15
72577294 6656
Satellite: ISS
Catalog Number: 25544
Epoch time: 10315
56025290 = yrday
fracday
Element set: 913
Inclination: 51
6450 deg
RA of node: 196
4874 deg
Eccentricity:
0007423
Arg of perigee: 188
7907 deg
Mean anomaly: 171
3127 deg
Mean motion: 15
72577294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 320
Coasting Arc #15 (Orbit 679)
---------------------------------------
Vector Time (GMT): 2010/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814740
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2397622
46 A = 6724690
08 meter
Y = 3675357
53 meter E =
0015547
Z = -5107973
13 I = 51
56147
XDOT = -7100
077864 Wp = 130
11184
YDOT = -2540
320673 meter/sec RA = 190
61502 deg
ZDOT = 1498
011860 TA = 154
33079
MA = 154
25354
Ha = 193
235 n
mi
Hp = 185
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7866215
42 X = -2413728
90
Y = 12058259
63 feet Y = 3648456
00 meter
Z = -16758442
04 Z = -5119659
91
XDOT = -23294
218715 XDOT = -7078
420983
YDOT = -8334
385411 feet/sec YDOT = -2619
596977 meter/sec
ZDOT = 4914
737073 ZDOT = 1463
571795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4418578
23 X = -1346782
65
Y = -13644806
23 feet Y = -4158936
94 meter
Z = -16805349
72 Z = -5122270
59
XDOT = 20220
135093 XDOT = 6163
097176
YDOT = -12458
270570 feet/sec YDOT = -3797
280870 meter/sec
ZDOT = 4776
491857 ZDOT = 1455
874718
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 10316
51344093
00016717 00000-0 10270-3 0 9142
2 25544 51
6449 191
6025 0007444 193
2889 166
8079 15
72639298 6807
Satellite: ISS
Catalog Number: 25544
Epoch time: 10316
51344093 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 191
6025 deg
Eccentricity:
0007444
Arg of perigee: 193
2889 deg
Mean anomaly: 166
8079 deg
Mean motion: 15
72639298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 333
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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