Date:
August 3rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 3075)
---------------------------------------
Vector Time (GMT): 2010/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6090674
75 A = 6736621
21 meter
Y = -1301916
76 meter E =
0011469
Z = -2554440
41 I = 51
61615
XDOT = 3191
313839 Wp = 157
97660
YDOT = -4600
646429 meter/sec RA = 353
10729 deg
ZDOT = -5282
461969 TA = 50
97615
MA = 50
87410
Ha = 195
530 n
mi
Hp = 187
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19982528
72 X = -6063254
85
Y = -4271380
43 feet Y = -1369872
86 meter
Z = -8380710
02 Z = -2583962
27
XDOT = 10470
189760 XDOT = 3268
183058
YDOT = -15093
984348 feet/sec YDOT = -4564
529133 meter/sec
ZDOT = -17330
911973 ZDOT = -5266
772193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9602016
49 X = 2926694
62
Y = 17982081
91 feet Y = 5480938
57 meter
Z = -8498732
56 Z = -2590413
68
XDOT = -17042
138501 XDOT = -5194
443815
YDOT = 966
422335 feet/sec YDOT = 294
565528 meter/sec
ZDOT = -17268
132359 ZDOT = -5263
326743
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 10214
52664878
00016717 00000-0 10270-3 0 9001
2 25544 51
6453 353
4582 0007560 178
6519 181
4659 15
71417884 30767
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214
52664878 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 353
4582 deg
Eccentricity:
0007560
Arg of perigee: 178
6519 deg
Mean anomaly: 181
4659 deg
Mean motion: 15
71417884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 332
Coasting Arc #2 (Orbit 3091)
---------------------------------------
Vector Time (GMT): 2010/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1398088
97 A = 6728957
80 meter
Y = 4322598
74 meter E =
0006428
Z = 4958302
64 I = 51
56045
XDOT = -7426
548307 Wp = 129
98033
YDOT = -67
976616 meter/sec RA = 347
94993 deg
ZDOT = -2037
119954 TA = 339
74469
MA = 339
77017
Ha = 195
579 n
mi
Hp = 187
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4586906
08 X = -1470407
60
Y = 14181754
40 feet Y = 4306559
74 meter
Z = 16267397
12 Z = 4951335
42
XDOT = -24365
315968 XDOT = -7415
340296
YDOT = -223
020395 feet/sec YDOT = -150
961898 meter/sec
ZDOT = -6683
464416 ZDOT = -2073
170780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13757458
08 X = 4193273
22
Y = -5813883
56 feet Y = -1772071
71 meter
Z = 16239494
43 Z = 4949797
90
XDOT = 15425
311854 XDOT = 4701
635053
YDOT = 17451
373724 feet/sec YDOT = 5319
178711 meter/sec
ZDOT = -6827
601755 ZDOT = -2081
053015
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 10215
54414994
00016717 00000-0 10270-3 0 9017
2 25544 51
6458 348
2537 0007552 181
6310 178
4828 15
71393832 30926
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215
54414994 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 348
2537 deg
Eccentricity:
0007552
Arg of perigee: 181
6310 deg
Mean anomaly: 178
4828 deg
Mean motion: 15
71393832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 317
Coasting Arc #3 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2010/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6555316
83 A = 6738974
93 meter
Y = -1212254
13 meter E =
0010587
Z = 975468
40 I = 51
56650
XDOT = 18
959958 Wp = 88
39679
YDOT = 4911
081268 meter/sec RA = 342
85490 deg
ZDOT = 5920
827169 TA = 282
25444
MA = 282
37297
Ha = 195
320 n
mi
Hp = 187
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21506944
97 X = 6563646
64
Y = -3977211
71 feet Y = -1138902
17 meter
Z = 3200355
64 Z = 1007334
10
XDOT = 62
204585 XDOT = -64
720227
YDOT = 16112
471353 feet/sec YDOT = 4910
824860 meter/sec
ZDOT = 19425
285989 ZDOT = 5920
716474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17372587
84 X = -5295164
77
Y = -13256254
45 feet Y = -4040506
36 meter
Z = 3327774
12 Z = 1014305
55
XDOT = 11011
452453 XDOT = 3356
290708
YDOT = -9510
911112 feet/sec YDOT = -2898
925707 meter/sec
ZDOT = 19424
789419 ZDOT = 5920
675815
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 10216
56163722
00016717 00000-0 10270-3 0 9021
2 25544 51
6467 343
0488 0007506 186
1980 173
9090 15
71457876 31084
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216
56163722 = yrday
fracday
Element set: 902
Inclination: 51
6467 deg
RA of node: 343
0488 deg
Eccentricity:
0007506
Arg of perigee: 186
1980 deg
Mean anomaly: 173
9090 deg
Mean motion: 15
71457876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 319
Coasting Arc #4 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2010/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1382918
96 A = 6727311
16 meter
Y = -3963090
55 meter E =
0015748
Z = -5269259
61 I = 51
49887
XDOT = 7167
836292 Wp = 118
99456
YDOT = -2769
388386 meter/sec RA = 337
72078 deg
ZDOT = 194
638469 TA = 152
90077
MA = 152
81848
Ha = 195
107 n
mi
Hp = 187
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4537135
70 X = -1312903
27
Y = -13002265
59 feet Y = -3978163
14 meter
Z = -17287597
14 Z = -5275808
13
XDOT = 23516
523269 XDOT = 7197
325858
YDOT = -9085
919901 feet/sec YDOT = -2689
068491 meter/sec
ZDOT = 638
577654 ZDOT = 229
530883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6452673
25 X = -1966774
81
Y = 12128605
23 feet Y = 3696798
88 meter
Z = -17313736
41 Z = -5277226
86
XDOT = -21825
395713 XDOT = -6652
380613
YDOT = -10467
784077 feet/sec YDOT = -3190
580587 meter/sec
ZDOT = 778
117038 ZDOT = 237
170073
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 10217
51552430
00016717 00000-0 10270-3 0 9036
2 25544 51
6468 338
1700 0007354 190
0754 170
0262 15
71480807 31237
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217
51552430 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 338
1700 deg
Eccentricity:
0007354
Arg of perigee: 190
0754 deg
Mean anomaly: 170
0262 deg
Mean motion: 15
71480807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 277
Coasting Arc #5 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2010/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5693467
33 A = 6739231
21 meter
Y = 3527248
00 meter E =
0017658
Z = 641817
92 I = 51
51155
XDOT = -3028
298738 Wp = 150
64012
YDOT = -3789
364719 meter/sec RA = 332
59057 deg
ZDOT = -5984
143892 TA = 22
35983
MA = 22
28294
Ha = 194
997 n
mi
Hp = 187
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18679354
76 X = -5735604
31
Y = 11572335
94 feet Y = 3463344
57 meter
Z = 2105701
84 Z = 614057
44
XDOT = -9935
363313 XDOT = -2956
630771
YDOT = -12432
298947 feet/sec YDOT = -3822
827574 meter/sec
ZDOT = -19633
018017 ZDOT = -5998
681535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21321791
53 X = 6498882
06
Y = 5354786
80 feet Y = 1632139
02 meter
Z = 1994667
43 Z = 607974
63
XDOT = -1694
013702 XDOT = -516
335376
YDOT = 14150
099671 feet/sec YDOT = 4312
950380 meter/sec
ZDOT = -19691
105110 ZDOT = -6001
848837
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 10218
53299395
00016717 00000-0 10270-3 0 9048
2 25544 51
6470 332
9646 0007400 194
2369 165
8586 15
71470612 31392
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218
53299395 = yrday
fracday
Element set: 904
Inclination: 51
6470 deg
RA of node: 332
9646 deg
Eccentricity:
0007400
Arg of perigee: 194
2369 deg
Mean anomaly: 165
8586 deg
Mean motion: 15
71470612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 324
Coasting Arc #6 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2010/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3730907
30 A = 6728029
50 meter
Y = 2401881
31 meter E =
0009979
Z = 5058291
45 I = 51
44905
XDOT = -5531
793839 Wp = 169
53931
YDOT = 5089
079464 meter/sec RA = 327
48287 deg
ZDOT = 1653
484080 TA = 264
45885
MA = 264
57268
Ha = 194
669 n
mi
Hp = 187
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12240509
51 X = 3679199
90
Y = 7880188
02 feet Y = 2443312
89 meter
Z = 16595444
41 Z = 5076290
55
XDOT = -18148
929918 XDOT = -5596
321905
YDOT = 16696
454933 feet/sec YDOT = 5026
858666 meter/sec
ZDOT = 5424
816535 ZDOT = 1626
454903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3044079
43 X = -927835
41
Y = -14151602
57 feet Y = -4313408
46 meter
Z = 16667391
41 Z = 5080220
90
XDOT = 23632
304728 XDOT = 7203
126481
YDOT = 1217
561490 feet/sec YDOT = 371
112742 meter/sec
ZDOT = 5316
690112 ZDOT = 1620
527146
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 10219
55045179
00016717 00000-0 10270-3 0 9051
2 25544 51
6479 327
7596 0007299 198
7386 161
3508 15
71526904 31550
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219
55045179 = yrday
fracday
Element set: 905
Inclination: 51
6479 deg
RA of node: 327
7596 deg
Eccentricity:
0007299
Arg of perigee: 198
7386 deg
Mean anomaly: 161
3508 deg
Mean motion: 15
71526904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 345
Coasting Arc #7 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2010/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3773638
59 A = 6737291
84 meter
Y = -5130756
40 meter E =
0002387
Z = -2201660
71 I = 51
45493
XDOT = 5203
336227 Wp = 143
53741
YDOT = 1482
550171 meter/sec RA = 322
32074 deg
ZDOT = 5464
707116 TA = 191
77151
MA = 191
77710
Ha = 194
617 n
mi
Hp = 188
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12380704
03 X = 3841426
21
Y = -16833190
30 feet Y = -5088178
11 meter
Z = -7223296
30 Z = -2183164
58
XDOT = 17071
313081 XDOT = 5159
825395
YDOT = 4864
009747 feet/sec YDOT = 1540
493232 meter/sec
ZDOT = 17928
829122 ZDOT = 5489
878802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20623270
26 X = -6285972
77
Y = 3518871
80 feet Y = 1072552
12 meter
Z = -7149293
84 Z = -2179104
76
XDOT = -8597
152495 XDOT = -2620
412080
YDOT = -13763
101275 feet/sec YDOT = -4194
993269 meter/sec
ZDOT = 18029
470502 ZDOT = 5495
382609
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 10220
50431173
00016717 00000-0 10270-3 0 9062
2 25544 51
6480 322
8806 0007084 202
9327 157
1520 15
71481124 31705
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220
50431173 = yrday
fracday
Element set: 906
Inclination: 51
6480 deg
RA of node: 322
8806 deg
Eccentricity:
0007084
Arg of perigee: 202
9327 deg
Mean anomaly: 157
1520 deg
Mean motion: 15
71481124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 271
Coasting Arc #8 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2010/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5096795
23 A = 6730770
27 meter
Y = -67281
17 meter E =
0006437
Z = -4398722
53 I = 51
41013
XDOT = 2928
730998 Wp = 118
72276
YDOT = -6300
163100 meter/sec RA = 317
23346 deg
ZDOT = -3303
848435 TA = 117
98186
MA = 117
91670
Ha = 194
388 n
mi
Hp = 188
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16721769
12 X = -5074296
41
Y = -220738
75 feet Y = -124150
54 meter
Z = -14431504
35 Z = -4423427
49
XDOT = 9608
697499 XDOT = 3015
011999
YDOT = -20669
826442 feet/sec YDOT = -6266
929668 meter/sec
ZDOT = -10839
397754 ZDOT = -3289
411802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12035258
76 X = 3668346
87
Y = 11487285
27 feet Y = 3501324
55 meter
Z = -14530293
52 Z = -4428833
46
XDOT = -20319
196479 XDOT = -6193
291087
YDOT = 7678
366968 feet/sec YDOT = 2340
366252 meter/sec
ZDOT = -10781
628183 ZDOT = -3286
240270
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 10221
52175162
00016717 00000-0 10270-3 0 9079
2 25544 51
6480 317
6760 0007206 206
4548 153
6247 15
71509438 31869
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221
52175162 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 317
6760 deg
Eccentricity:
0007206
Arg of perigee: 206
4548 deg
Mean anomaly: 153
6247 deg
Mean motion: 15
71509438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 302
Coasting Arc #9 (Orbit 3201)
---------------------------------------
Vector Time (GMT): 2010/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1260741
52 A = 6733854
83 meter
Y = 5592578
25 meter E =
0010443
Z = 3519562
58 I = 51
39878
XDOT = -6104
163199 Wp = 122
15549
YDOT = 1439
558302 meter/sec RA = 312
05159 deg
ZDOT = -4469
839950 TA = 15
81864
MA = 15
78605
Ha = 194
279 n
mi
Hp = 188
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4136291
09 X = -1340282
04
Y = 18348353
84 feet Y = 5578035
06 meter
Z = 11547121
33 Z = 3513244
99
XDOT = -20026
782150 XDOT = -6098
093789
YDOT = 4722
960309 feet/sec YDOT = 1371
331941 meter/sec
ZDOT = -14664
829233 ZDOT = -4499
478470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15386842
69 X = 4689909
65
Y = -10844327
44 feet Y = -3305351
00 meter
Z = 11521833
11 Z = 3511854
73
XDOT = 17201
203660 XDOT = 5242
926875
YDOT = 8684
936368 feet/sec YDOT = 2647
168605 meter/sec
ZDOT = -14783
353846 ZDOT = -4505
966252
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 10222
53918192
00016717 00000-0 10270-3 0 9080
2 25544 51
6476 312
4716 0006996 209
4817 150
5951 15
71532107 32021
Satellite: ISS
Catalog Number: 25544
Epoch time: 10222
53918192 = yrday
fracday
Element set: 908
Inclination: 51
6476 deg
RA of node: 312
4716 deg
Eccentricity:
0006996
Arg of perigee: 209
4817 deg
Mean anomaly: 150
5951 deg
Mean motion: 15
71532107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3202
Checksum: 305
Coasting Arc #10 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2010/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5260241
14 A = 6734205
42 meter
Y = -2564983
04 meter E =
0010380
Z = 3330190
06 I = 51
38091
XDOT = 35
153035 Wp = 123
18324
YDOT = 6130
213505 meter/sec RA = 306
96810 deg
ZDOT = 4650
038337 TA = 276
08883
MA = 276
20709
Ha = 194
039 n
mi
Hp = 188
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17258008
98 X = 5272355
17
Y = -8415298
69 feet Y = -2506092
14 meter
Z = 10925820
40 Z = 3355773
20
XDOT = 115
331480 XDOT = -55
987322
YDOT = 20112
249032 feet/sec YDOT = 6130
097016 meter/sec
ZDOT = 15256
031291 ZDOT = 4649
987730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18502210
13 X = -5639473
65
Y = -4906964
42 feet Y = -1495642
76 meter
Z = 11028127
59 Z = 3361373
29
XDOT = 12800
563493 XDOT = 3901
611753
YDOT = -13861
960229 feet/sec YDOT = -4225
125478 meter/sec
ZDOT = 15255
811585 ZDOT = 4649
971371
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 10223
55660033
00016717 00000-0 10270-3 0 9092
2 25544 51
6474 307
2661 0007023 214
2869 145
7840 15
71570960 32182
Satellite: ISS
Catalog Number: 25544
Epoch time: 10223
55660033 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 307
2661 deg
Eccentricity:
0007023
Arg of perigee: 214
2869 deg
Mean anomaly: 145
7840 deg
Mean motion: 15
71570960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 298
Coasting Arc #11 (Orbit 3232)
---------------------------------------
Vector Time (GMT): 2010/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1249610
53 A = 6730172
84 meter
Y = -4839767
64 meter E =
0010292
Z = -4515757
35 I = 51
34925
XDOT = 5569
843639 Wp = 149
66627
YDOT = -4315
336329 meter/sec RA = 301
78435 deg
ZDOT = 3077
974298 TA = 151
19848
MA = 151
14162
Ha = 193
845 n
mi
Hp = 188
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4099772
09 X = -1173462
10
Y = -15878502
76 feet Y = -4853315
82 meter
Z = -14815476
88 Z = -4521642
85
XDOT = 18273
765219 XDOT = 5602
732543
YDOT = -14157
927588 feet/sec YDOT = -4252
867077 meter/sec
ZDOT = 10098
340873 ZDOT = 3105
112115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7119807
04 X = -2170117
18
Y = 14749428
79 feet Y = 4495625
90 meter
Z = -14839003
81 Z = -4522928
36
XDOT = -21978
023185 XDOT = -6698
901467
YDOT = -321
568507 feet/sec YDOT = -98
014081 meter/sec
ZDOT = 10206
860941 ZDOT = 3111
051215
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 10224
51042300
00016717 00000-0 10270-3 0 9102
2 25544 51
6465 302
3869 0006861 217
7415 142
3267 15
71595895 32339
Satellite: ISS
Catalog Number: 25544
Epoch time: 10224
51042300 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 302
3869 deg
Eccentricity:
0006861
Arg of perigee: 217
7415 deg
Mean anomaly: 142
3267 deg
Mean motion: 15
71595895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 295
Coasting Arc #12 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2010/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4226003
49 A = 6737304
05 meter
Y = 4840762
28 meter E =
0010170
Z = -2003259
58 I = 51
35733
XDOT = -2655
613653 Wp = 181
34122
YDOT = -4615
584080 meter/sec RA = 296
68821 deg
ZDOT = -5560
553055 TA = 21
05750
MA = 21
01565
Ha = 193
619 n
mi
Hp = 188
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13864840
86 X = -4270088
32
Y = 15881766
01 feet Y = 4793258
07 meter
Z = -6572373
95 Z = -2023896
41
XDOT = -8712
643217 XDOT = -2576
792086
YDOT = -15142
992387 feet/sec YDOT = -4644
840068 meter/sec
ZDOT = -18243
284300 ZDOT = -5573
262405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20736677
68 X = 6320539
36
Y = -3655543
26 feet Y = -1114209
59 meter
Z = -6654893
31 Z = -2028411
48
XDOT = -3098
210085 XDOT = -944
334434
YDOT = 15673
475585 feet/sec YDOT = 4777
275358 meter/sec
ZDOT = -18294
100701 ZDOT = -5576
041894
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 10225
52782428
00016717 00000-0 10270-3 0 9117
2 25544 51
6456 297
1814 0006828 222
0945 137
9693 15
71574054 32494
Satellite: ISS
Catalog Number: 25544
Epoch time: 10225
52782428 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 297
1814 deg
Eccentricity:
0006828
Arg of perigee: 222
0945 deg
Mean anomaly: 137
9693 deg
Mean motion: 15
71574054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 325
Coasting Arc #13 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2010/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3206237
29 A = 6727566
76 meter
Y = 2998824
84 meter E =
0002335
Z = 5098462
90 I = 51
31299
XDOT = -3815
080121 Wp = 213
45419
YDOT = 6527
222038 meter/sec RA = 291
51877 deg
ZDOT = -1442
265294 TA = 250
42349
MA = 250
44870
Ha = 193
299 n
mi
Hp = 189
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10519151
21 X = 3147698
33
Y = 9838664
19 feet Y = 3034351
57 meter
Z = 16727240
50 Z = 5113896
53
XDOT = -12516
667065 XDOT = -3880
778948
YDOT = 21414
770467 feet/sec YDOT = 6484
192196 meter/sec
ZDOT = -4731
841516 ZDOT = -1460
958374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2159384
86 X = -658180
50
Y = -14167588
87 feet Y = -4318281
09 meter
Z = 16788952
10 Z = 5117272
60
XDOT = 21988
135564 XDOT = 6701
983720
YDOT = -9038
640337 feet/sec YDOT = -2754
977575 meter/sec
ZDOT = -4806
584831 ZDOT = -1465
047056
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 10226
54521346
00016717 00000-0 10270-3 0 9121
2 25544 51
6461 291
9755 0006851 227
6468 132
4115 15
71629764 32659
Satellite: ISS
Catalog Number: 25544
Epoch time: 10226
54521346 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 291
9755 deg
Eccentricity:
0006851
Arg of perigee: 227
6468 deg
Mean anomaly: 132
4115 deg
Mean motion: 15
71629764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 314
Coasting Arc #14 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2010/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2278901
96 A = 6738973
54 meter
Y = -6318512
60 meter E =
0006621
Z = 503315
99 I = 51
34013
XDOT = 4381
047164 Wp = 49
24705
YDOT = 2060
263418 meter/sec RA = 286
39616 deg
ZDOT = 5980
545966 TA = 316
24412
MA = 316
29656
Ha = 193
258 n
mi
Hp = 189
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7476712
48 X = 2346942
35
Y = -20730028
20 feet Y = -6292648
13 meter
Z = 1651299
17 Z = 514551
96
XDOT = 14373
514316 XDOT = 4328
631039
YDOT = 6759
394417 feet/sec YDOT = 2108
961691 meter/sec
ZDOT = 19621
213799 ZDOT = 6001
701723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18436759
04 X = -5619524
16
Y = 12065273
78 feet Y = 3677495
45 meter
Z = 1696223
03 Z = 517008
78
XDOT = -6440
502522 XDOT = -1963
065169
YDOT = -12633
177532 feet/sec YDOT = -3850
592512 meter/sec
ZDOT = 19705
806879 ZDOT = 6006
329937
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 10227
56259751
00016717 00000-0 10270-3 0 9133
2 25544 51
6454 286
7695 0006509 231
7454 128
3123 15
71574106 32817
Satellite: ISS
Catalog Number: 25544
Epoch time: 10227
56259751 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 286
7695 deg
Eccentricity:
0006509
Arg of perigee: 231
7454 deg
Mean anomaly: 128
3123 deg
Mean motion: 15
71574106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 314
Coasting Arc #15 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2010/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187761
03 A = 6726956
45 meter
Y = -505113
67 meter E =
0010098
Z = -5248303
77 I = 51
29244
XDOT = 1271
830173 Wp = 108
45860
YDOT = -7579
030970 meter/sec RA = 281
25294 deg
ZDOT = -289
002544 TA = 158
80206
MA = 158
76019
Ha = 192
996 n
mi
Hp = 189
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13739373
46 X = -4156306
33
Y = -1657197
07 feet Y = -551767
63 meter
Z = -17218844
38 Z = -5268571
42
XDOT = 4172
671172 XDOT = 1357
889675
YDOT = -24865
587173 feet/sec YDOT = -7564
327408 meter/sec
ZDOT = -948
171075 ZDOT = -282
615297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10057540
10 X = 3065538
22
Y = 9357619
02 feet Y = 2852202
28 meter
Z = -17299888
44 Z = -5273006
00
XDOT = -17314
880108 XDOT = -5277
575457
YDOT = 16926
021369 feet/sec YDOT = 5159
051313 meter/sec
ZDOT = -922
638451 ZDOT = -281
220200
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 10228
51638244
00016717 00000-0 10270-3 0 9148
2 25544 51
6452 281
8889 0006605 235
1331 124
9210 15
71605959 32961
Satellite: ISS
Catalog Number: 25544
Epoch time: 10228
51638244 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 281
8889 deg
Eccentricity:
0006605
Arg of perigee: 235
1331 deg
Mean anomaly: 124
9210 deg
Mean motion: 15
71605959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 313
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list