Date:
November 26th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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 3121)
---------------------------------------
Vector Time (GMT): 2009/328/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1243135
65 A = 6714572
23 meter
Y = -3998519
93 meter E =
0008004
Z = 5245240
93 I = 51
49757
XDOT = 7228
621248 Wp = 30
04315
YDOT = 2657
190528 meter/sec RA = 202
07147 deg
ZDOT = 319
026735 TA = 56
96367
MA = 56
88680
Ha = 188
917 n
mi
Hp = 179
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4078529
05 X = 1262274
63
Y = -13118503
71 feet Y = -3984511
72 meter
Z = 17208795
70 Z = 5251326
44
XDOT = 23715
948978 XDOT = 7196
821033
YDOT = 8717
816692 feet/sec YDOT = 2737
847414 meter/sec
ZDOT = 1046
675641 ZDOT = 354
066756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10312196
25 X = 3143157
42
Y = 9031429
02 feet Y = 2752779
56 meter
Z = 17232645
95 Z = 5252510
49
XDOT = -17057
160045 XDOT = -5199
022382
YDOT = 17256
076295 feet/sec YDOT = 5259
652055 meter/sec
ZDOT = 1185
149240 ZDOT = 361
233488
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 09328
55608418
00016717 00000-0 10270-3 0 9006
2 25544 51
6457 202
8335 0007833 11
2964 348
8375 15
75951685 31225
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
55608418 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 202
8335 deg
Eccentricity:
0007833
Arg of perigee: 11
2964 deg
Mean anomaly: 348
8375 deg
Mean motion: 15
75951685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3122
Checksum: 325
Coasting Arc #2 (Orbit 3137)
---------------------------------------
Vector Time (GMT): 2009/329/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6321397
76 A = 6726479
55 meter
Y = -2234164
38 meter E =
0019868
Z = 376061
70 I = 51
56599
XDOT = 1925
981027 Wp = 36
03877
YDOT = -4411
073900 meter/sec RA = 196
91376 deg
ZDOT = 6024
263692 TA = 328
06096
MA = 328
18126
Ha = 188
969 n
mi
Hp = 179
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20739493
95 X = -6297771
99
Y = -7329935
64 feet Y = -2304721
90 meter
Z = 1233798
22 Z = 345409
14
XDOT = 6318
835392 XDOT = 1945
898026
YDOT = -14472
027232 feet/sec YDOT = -4389
425338 meter/sec
ZDOT = 19764
644658 ZDOT = 6033
668451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14954416
06 X = 4558106
02
Y = -16140144
36 feet Y = -4919516
00 meter
Z = 1112656
40 Z = 339137
67
XDOT = 9649
355576 XDOT = 2941
123580
YDOT = 10341
770796 feet/sec YDOT = 3152
171739 meter/sec
ZDOT = 19801
583439 ZDOT = 6035
522632
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 09329
57065440
00016717 00000-0 10270-3 0 9012
2 25544 51
6453 197
6080 0007850 14
2944 345
8441 15
75990185 31385
Satellite: ISS
Catalog Number: 25544
Epoch time: 09329
57065440 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 197
6080 deg
Eccentricity:
0007850
Arg of perigee: 14
2944 deg
Mean anomaly: 345
8441 deg
Mean motion: 15
75990185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3138
Checksum: 321
Coasting Arc #3 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2009/330/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2146998
88 A = 6714809
23 meter
Y = 3738631
18 meter E =
0017382
Z = -5161303
72 I = 51
55533
XDOT = -7184
398136 Wp = 72
67483
YDOT = -2471
785127 meter/sec RA = 191
74343 deg
ZDOT = 1206
522498 TA = 208
82850
MA = 208
92465
Ha = 189
028 n
mi
Hp = 179
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7043959
59 X = -2163572
17
Y = 12265850
32 feet Y = 3714529
69 meter
Z = -16933411
15 Z = -5171774
16
XDOT = -23570
860025 XDOT = -7162
085420
YDOT = -8109
531258 feet/sec YDOT = -2552
000595 meter/sec
ZDOT = 3958
407145 ZDOT = 1171
674113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8699004
14 X = -2651456
46
Y = -11090511
52 feet Y = -3380387
91 meter
Z = -16974591
17 Z = -5173855
39
XDOT = 15670
404971 XDOT = 4776
339435
YDOT = -18096
899436 feet/sec YDOT = -5515
934948 meter/sec
ZDOT = 3820
675263 ZDOT = 1164
541820
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 09330
52179795
00016717 00000-0 10270-3 0 9029
2 25544 51
6445 192
7089 0007885 17
4480 342
6953 15
76014395 31530
Satellite: ISS
Catalog Number: 25544
Epoch time: 09330
52179795 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 192
7089 deg
Eccentricity:
0007885
Arg of perigee: 17
4480 deg
Mean anomaly: 342
6953 deg
Mean motion: 15
76014395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 333
Coasting Arc #4 (Orbit 3168)
---------------------------------------
Vector Time (GMT): 2009/331/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6153370
17 A = 6725214
82 meter
Y = 2095697
08 meter E =
0007568
Z = -1733261
65 I = 51
61960
XDOT = -3027
699885 Wp = 81
67071
YDOT = 4192
993400 meter/sec RA = 186
61584 deg
ZDOT = -5699
126147 TA = 117
51655
MA = 117
43962
Ha = 189
104 n
mi
Hp = 179
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20188222
33 X = 6137898
45
Y = 6875646
60 feet Y = 2164421
26 meter
Z = -5686553
96 Z = -1703405
37
XDOT = -9933
398574 XDOT = -3046
675669
YDOT = 13756
540026 feet/sec YDOT = 4159
030000 meter/sec
ZDOT = -18697
920430 ZDOT = -5713
880986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13775759
82 X = -4198851
59
Y = 16321626
12 feet Y = 4974831
64 meter
Z = -5568545
14 Z = -1697292
56
XDOT = -8036
449224 XDOT = -2449
509723
YDOT = -13159
085399 feet/sec YDOT = -4010
889230 meter/sec
ZDOT = -18756
004898 ZDOT = -5716
830293
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 09331
53633312
00016717 00000-0 10270-3 0 9032
2 25544 51
6442 187
4842 0007776 20
9157 339
2324 15
76004948 31698
Satellite: ISS
Catalog Number: 25544
Epoch time: 09331
53633312 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 187
4842 deg
Eccentricity:
0007776
Arg of perigee: 20
9157 deg
Mean anomaly: 339
2324 deg
Mean motion: 15
76004948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3169
Checksum: 314
Coasting Arc #5 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2009/332/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3121788
53 A = 6716564
79 meter
Y = -3643085
61 meter E =
0014678
Z = 4696566
04 I = 51
62110
XDOT = 6826
365477 Wp = 42
91885
YDOT = 2324
108888 meter/sec RA = 181
42583 deg
ZDOT = -2719
135624 TA = 73
91042
MA = 73
74886
Ha = 189
006 n
mi
Hp = 178
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10242088
37 X = 3139478
45
Y = -11952380
60 feet Y = -3608077
26 meter
Z = 15408681
22 Z = 4711774
87
XDOT = 22396
212194 XDOT = 6813
078954
YDOT = 7625
029161 feet/sec YDOT = 2400
371190 meter/sec
ZDOT = -8921
048635 ZDOT = -2686
004394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7663669
01 X = 2335886
31
Y = 13681305
04 feet Y = 4170061
78 meter
Z = 15468590
84 Z = 4714826
49
XDOT = -13973
864673 XDOT = -4259
233952
YDOT = 17823
333502 feet/sec YDOT = 5432
552051 meter/sec
ZDOT = -8790
086377 ZDOT = -2679
218328
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 09332
55084798
00016717 00000-0 10270-3 0 9044
2 25544 51
6439 182
2579 0007849 23
9849 336
1680 15
76078380 31856
Satellite: ISS
Catalog Number: 25544
Epoch time: 09332
55084798 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 182
2579 deg
Eccentricity:
0007849
Arg of perigee: 23
9849 deg
Mean anomaly: 336
1680 deg
Mean motion: 15
76078380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 354
Coasting Arc #6 (Orbit 3200)
---------------------------------------
Vector Time (GMT): 2009/333/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5684121
00 A = 6722453
08 meter
Y = -1984034
79 meter E =
0018941
Z = 2965792
47 I = 51
66953
XDOT = 4088
374491 Wp = 63
18587
YDOT = -4221
000562 meter/sec RA = 176
31969 deg
ZDOT = 4995
932816 TA = 331
10123
MA = 331
20599
Ha = 189
167 n
mi
Hp = 178
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18648690
94 X = -5675920
42
Y = -6509300
48 feet Y = -2047552
36 meter
Z = 9730290
26 Z = 2938197
97
XDOT = 13413
302135 XDOT = 4111
000546
YDOT = -13848
427040 feet/sec YDOT = -4175
155816 meter/sec
ZDOT = 16390
855696 ZDOT = 5015
849365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12356699
40 X = 3766321
98
Y = -15477972
62 feet Y = -4717686
05 meter
Z = 9621203
60 Z = 2932542
86
XDOT = 7505
202015 XDOT = 2287
585574
YDOT = 16262
053742 feet/sec YDOT = 4956
673981 meter/sec
ZDOT = 16469
345658 ZDOT = 5019
856557
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 09333
56534573
00016717 00000-0 10270-3 0 9058
2 25544 51
6424 177
0316 0007788 27
6842 332
4735 15
76101164 32013
Satellite: ISS
Catalog Number: 25544
Epoch time: 09333
56534573 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 177
0316 deg
Eccentricity:
0007788
Arg of perigee: 27
6842 deg
Mean anomaly: 332
4735 deg
Mean motion: 15
76101164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3201
Checksum: 305
Coasting Arc #7 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2009/334/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3967609
50 A = 6719388
88 meter
Y = 3753999
17 meter E =
0011647
Z = -3919271
68 I = 51
68838
XDOT = -6139
397187 Wp = 67
36319
YDOT = -2277
498180 meter/sec RA = 171
12005 deg
ZDOT = 4047
563653 TA = 244
65003
MA = 244
77068
Ha = 189
127 n
mi
Hp = 178
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13017091
54 X = -3990252
81
Y = 12316270
23 feet Y = 3709504
82 meter
Z = -12858502
88 Z = -3938601
51
XDOT = -20142
379224 XDOT = -6133
136419
YDOT = -7472
106890 feet/sec YDOT = -2346
117962 meter/sec
ZDOT = 13279
408309 ZDOT = 4017
752542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7593041
99 X = -2314359
20
Y = -16171434
69 feet Y = -4929053
29 meter
Z = -12934708
90 Z = -3942499
27
XDOT = 12301
497377 XDOT = 3749
496401
YDOT = -16266
949400 feet/sec YDOT = -4958
166177 meter/sec
ZDOT = 13161
542984 ZDOT = 4011
638302
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 09334
51642119
00016717 00000-0 10270-3 0 9061
2 25544 51
6412 172
1315 0007818 32
0982 328
0656 15
76114502 32163
Satellite: ISS
Catalog Number: 25544
Epoch time: 09334
51642119 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 172
1315 deg
Eccentricity:
0007818
Arg of perigee: 32
0982 deg
Mean anomaly: 328
0656 deg
Mean motion: 15
76114502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 288
Coasting Arc #8 (Orbit 3231)
---------------------------------------
Vector Time (GMT): 2009/335/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4962994
20 A = 6719038
73 meter
Y = 2059204
01 meter E =
0014437
Z = -4050195
49 I = 51
71589
XDOT = -4984
155612 Wp = 53
33313
YDOT = 4392
464119 meter/sec RA = 166
02476 deg
ZDOT = -3875
273155 TA = 176
73744
MA = 176
72802
Ha = 189
218 n
mi
Hp = 178
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16282789
37 X = 4959274
60
Y = 6755918
67 feet Y = 2114682
89 meter
Z = -13288042
94 Z = -4026093
36
XDOT = -16352
216574 XDOT = -5014
076590
YDOT = 14410
971520 feet/sec YDOT = 4336
561577 meter/sec
ZDOT = -12714
150772 ZDOT = -3899
558933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11349203
53 X = -3459237
24
Y = 13582753
42 feet Y = 4140023
24 meter
Z = -13192730
60 Z = -4021144
29
XDOT = -7877
990373 XDOT = -2401
211466
YDOT = -19021
254016 feet/sec YDOT = -5797
678224 meter/sec
ZDOT = -12809
927436 ZDOT = -3904
465882
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 09335
53088319
00016717 00000-0 10270-3 0 9071
2 25544 51
6403 166
9055 0007913 36
1173 324
0524 15
76148530 32324
Satellite: ISS
Catalog Number: 25544
Epoch time: 09335
53088319 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 166
9055 deg
Eccentricity:
0007913
Arg of perigee: 36
1173 deg
Mean anomaly: 324
0524 deg
Mean motion: 15
76148530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3232
Checksum: 299
Coasting Arc #9 (Orbit 3247)
---------------------------------------
Vector Time (GMT): 2009/336/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4673664
09 A = 6722493
38 meter
Y = -3944688
60 meter E =
0018576
Z = 2780318
42 I = 51
75751
XDOT = 5175
380893 Wp = 78
33379
YDOT = 2487
683574 meter/sec RA = 160
82987 deg
ZDOT = -5137
768176 TA = 69
86791
MA = 69
66815
Ha = 189
106 n
mi
Hp = 178
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15333543
60 X = 4703920
35
Y = -12941891
75 feet Y = -3892256
20 meter
Z = 9121779
58 Z = 2803096
46
XDOT = 16979
596106 XDOT = 5172
137425
YDOT = 8161
691516 feet/sec YDOT = 2545
540401 meter/sec
ZDOT = -16856
194802 ZDOT = -5112
633108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8082413
45 X = 2463519
62
Y = 18320407
85 feet Y = 5584060
31 meter
Z = 9211635
74 Z = 2807706
57
XDOT = -11329
353935 XDOT = -3453
187079
YDOT = 13476
608088 feet/sec YDOT = 4107
670145 meter/sec
ZDOT = -16756
771844 ZDOT = -5107
464058
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 09336
54532513
00016717 00000-0 10270-3 0 9084
2 25544 51
6406 161
6784 0007809 38
2115 321
9602 15
76198983 32488
Satellite: ISS
Catalog Number: 25544
Epoch time: 09336
54532513 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 161
6784 deg
Eccentricity:
0007809
Arg of perigee: 38
2115 deg
Mean anomaly: 321
9602 deg
Mean motion: 15
76198983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3248
Checksum: 326
Coasting Arc #10 (Orbit 3263)
---------------------------------------
Vector Time (GMT): 2009/337/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4039308
68 A = 6715933
48 meter
Y = -2342056
02 meter E =
0011764
Z = 4816594
00 I = 51
76221
XDOT = 5633
164797 Wp = 80
01476
YDOT = -4661
624003 meter/sec RA = 155
72864 deg
ZDOT = 2454
363029 TA = 346
06889
MA = 346
10132
Ha = 189
387 n
mi
Hp = 178
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13252325
08 X = -4036217
69
Y = -7683910
83 feet Y = -2387209
46 meter
Z = 15802473
77 Z = 4796977
86
XDOT = 18481
511801 XDOT = 5672
950187
YDOT = -15294
042005 feet/sec YDOT = -4598
408583 meter/sec
ZDOT = 8052
372144 ZDOT = 2481
825244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10965060
94 X = 3342150
57
Y = -10811158
83 feet Y = -3295241
21 meter
Z = 15724855
04 Z = 4792935
82
XDOT = 9033
467955 XDOT = 2753
401033
YDOT = 21046
439943 feet/sec YDOT = 6414
954894 meter/sec
ZDOT = 8160
732182 ZDOT = 2487
391169
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 09337
55975235
00016717 00000-0 10270-3 0 9099
2 25544 51
6398 156
4513 0007882 43
4696 316
7089 15
76178130 32644
Satellite: ISS
Catalog Number: 25544
Epoch time: 09337
55975235 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 156
4513 deg
Eccentricity:
0007882
Arg of perigee: 43
4696 deg
Mean anomaly: 316
7089 deg
Mean motion: 15
76178130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3264
Checksum: 347
Coasting Arc #11 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2009/338/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5068277
99 A = 6724905
10 meter
Y = 4167523
39 meter E =
0016188
Z = -1446590
80 I = 51
82059
XDOT = -4081
612409 Wp = 42
88503
YDOT = -2958
129364 meter/sec RA = 150
55341 deg
ZDOT = 5827
691800 TA = 301
21975
MA = 301
37829
Ha = 189
226 n
mi
Hp = 178
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16628208
62 X = -5107475
94
Y = 13672976
99 feet Y = 4110627
97 meter
Z = -4746032
80 Z = -1471307
27
XDOT = -13391
116829 XDOT = -4076
540848
YDOT = -9705
148833 feet/sec YDOT = -3003
744914 meter/sec
ZDOT = 19119
723752 ZDOT = 5807
875009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9085482
83 X = -2769255
17
Y = -19492721
88 feet Y = -5941381
63 meter
Z = -4843577
67 Z = -1476322
47
XDOT = 11352
512697 XDOT = 3460
245870
YDOT = -9983
220238 feet/sec YDOT = -3042
885529 meter/sec
ZDOT = 19041
277175 ZDOT = 5803
781283
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 09338
51075874
00016717 00000-0 10270-3 0 9108
2 25544 51
6404 151
5510 0007838 48
2358 311
9475 15
76221975 32792
Satellite: ISS
Catalog Number: 25544
Epoch time: 09338
51075874 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 151
5510 deg
Eccentricity:
0007838
Arg of perigee: 48
2358 deg
Mean anomaly: 311
9475 deg
Mean motion: 15
76221975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 324
Coasting Arc #12 (Orbit 3294)
---------------------------------------
Vector Time (GMT): 2009/339/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3061761
45 A = 6713896
85 meter
Y = 2899259
49 meter E =
0021923
Z = -5243240
44 I = 51
80990
XDOT = -5927
345313 Wp = 73
22142
YDOT = 4833
581988 meter/sec RA = 145
43476 deg
ZDOT = -785
001743 TA = 189
29415
MA = 189
33479
Ha = 189
300 n
mi
Hp = 177
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10045149
12 X = 3054584
68
Y = 9512006
21 feet Y = 2933458
50 meter
Z = -17202232
42 Z = -5228383
38
XDOT = -19446
670973 XDOT = -5977
141326
YDOT = 15858
208621 feet/sec YDOT = 4767
020598 meter/sec
ZDOT = -2575
465036 ZDOT = -813
917201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11617401
14 X = -3540983
87
Y = 7644632
45 feet Y = 2330083
97 meter
Z = -17143385
57 Z = -5225303
92
XDOT = -10325
909111 XDOT = -3147
337097
YDOT = -21749
465790 feet/sec YDOT = -6629
237173 meter/sec
ZDOT = -2689
600642 ZDOT = -819
790276
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 09339
52514853
00016717 00000-0 10270-3 0 9116
2 25544 51
6410 146
3250 0007955 52
7034 307
4855 15
76260136 32955
Satellite: ISS
Catalog Number: 25544
Epoch time: 09339
52514853 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 146
3250 deg
Eccentricity:
0007955
Arg of perigee: 52
7034 deg
Mean anomaly: 307
4855 deg
Mean motion: 15
76260136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3295
Checksum: 305
Coasting Arc #13 (Orbit 3310)
---------------------------------------
Vector Time (GMT): 2009/340/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5221838
09 A = 6725572
76 meter
Y = -4233334
25 meter E =
0015532
Z = -101492
93 I = 51
87400
XDOT = 2932
628094 Wp = 105
15222
YDOT = 3744
214164 meter/sec RA = 140
28944 deg
ZDOT = -6057
389181 TA = 75
94738
MA = 75
77478
Ha = 189
244 n
mi
Hp = 177
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17132014
75 X = 5269280
91
Y = -13888891
91 feet Y = -4174675
30 meter
Z = -332982
04 Z = -76010
41
XDOT = 9621
483248 XDOT = 2919
967429
YDOT = 12284
167204 feet/sec YDOT = 3776
938416 meter/sec
ZDOT = -19873
324085 ZDOT = -6043
172788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9845896
82 X = 3001029
35
Y = 19736322
82 feet Y = 6015631
20 meter
Z = -232383
35 Z = -70830
44
XDOT = -12662
795178 XDOT = -3859
619970
YDOT = 6126
309551 feet/sec YDOT = 1867
299151 meter/sec
ZDOT = -19816
971438 ZDOT = -6040
212894
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 09340
53951804
00016717 00000-0 10270-3 0 9121
2 25544 51
6410 141
0973 0007982 54
3943 305
7964 15
76321506 33116
Satellite: ISS
Catalog Number: 25544
Epoch time: 09340
53951804 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 141
0973 deg
Eccentricity:
0007982
Arg of perigee: 54
3943 deg
Mean anomaly: 305
7964 deg
Mean motion: 15
76321506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3311
Checksum: 301
Coasting Arc #14 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2009/341/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2099529
10 A = 6713943
88 meter
Y = -3675733
71 meter E =
0011552
Z = 5203651
12 I = 51
85692
XDOT = 5943
534611 Wp = 59
66735
YDOT = -4812
566546 meter/sec RA = 135
14346 deg
ZDOT = -994
083506 TA = 39
80823
MA = 39
72354
Ha = 189
467 n
mi
Hp = 177
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6888218
84 X = -2083548
82
Y = -12059493
81 feet Y = -3699122
98 meter
Z = 17072346
20 Z = 5193490
08
XDOT = 19499
785470 XDOT = 6001
736925
YDOT = -15789
260320 feet/sec YDOT = -4745
776923 meter/sec
ZDOT = -3261
428827 ZDOT = -965
068773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13212508
56 X = 4027172
61
Y = -4436620
62 feet Y = -1352281
96 meter
Z = 17032027
76 Z = 5191362
06
XDOT = 11245
805542 XDOT = 3427
721529
YDOT = 21317
172851 feet/sec YDOT = 6497
474285 meter/sec
ZDOT = -3146
873566 ZDOT = -959
167063
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 09341
55387333
00016717 00000-0 10270-3 0 9135
2 25544 51
6412 135
8705 0008038 60
2666 299
9298 15
76265361 33270
Satellite: ISS
Catalog Number: 25544
Epoch time: 09341
55387333 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 135
8705 deg
Eccentricity:
0008038
Arg of perigee: 60
2666 deg
Mean anomaly: 299
9298 deg
Mean motion: 15
76265361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 329
Coasting Arc #15 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2009/342/12:11:21
825
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5081294
35 A = 6724384
53 meter
Y = 4080220
04 meter E =
0022008
Z = 1615760
09 I = 51
91457
XDOT = -1941
880777 Wp = 63
58589
YDOT = -4725
462120 meter/sec RA = 130
03162 deg
ZDOT = 5775
684920 TA = 314
21743
MA = 314
39797
Ha = 189
272 n
mi
Hp = 177
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16670913
23 X = -5134391
55
Y = 13386548
69 feet Y = 4023101
01 meter
Z = 5301050
15 Z = 1590946
32
XDOT = -6370
999923 XDOT = -1916
952894
YDOT = -15503
484646 feet/sec YDOT = -4747
038394 meter/sec
ZDOT = 18949
097507 ZDOT = 5766
311437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10104265
30 X = -3079780
06
Y = -18869341
46 feet Y = -5751375
28 meter
Z = 5203070
47 Z = 1585895
88
XDOT = 15051
417894 XDOT = 4587
672174
YDOT = -2798
516573 feet/sec YDOT = -852
987851 meter/sec
ZDOT = 18911
853364 ZDOT = 5764
332905
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 09342
56820488
00016717 00000-0 10270-3 0 9141
2 25544 51
6424 130
6440 0007895 64
2128 295
9850 15
76359037 33431
Satellite: ISS
Catalog Number: 25544
Epoch time: 09342
56820488 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 130
6440 deg
Eccentricity:
0007895
Arg of perigee: 64
2128 deg
Mean anomaly: 295
9850 deg
Mean motion: 15
76359037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 326
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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