[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 7th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 1344)
---------------------------------------
Vector Time (GMT): 2011/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3653954
11 A = 6757923
51 meter
Y = 2030371
74 meter E =
0022490
Z = -5327042
75 I = 51
92897
XDOT = -3464
593039 Wp = 120
01720
YDOT = 6833
589312 meter/sec RA = 115
60852 deg
ZDOT = 217
861378 TA = 152
11232
MA = 151
99159
Ha = 214
025 n
mi
Hp = 201
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11988038
42 X = 3656856
10
Y = 6661324
60 feet Y = 2071248
69 meter
Z = -17477174
38 Z = -5309284
97
XDOT = -11366
775061 XDOT = -3541
808394
YDOT = 22419
912442 feet/sec YDOT = 6794
414382 meter/sec
ZDOT = 714
768301 ZDOT = 200
842958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9695972
94 X = -2955332
55
Y = -9828240
28 feet Y = -2995647
64 meter
Z = -17404934
26 Z = -5305023
96
XDOT = 16567
461802 XDOT = 5049
762357
YDOT = -17546
968995 feet/sec YDOT = -5348
316150 meter/sec
ZDOT = 645
180160 ZDOT = 196
650913
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 11248
51571325
00016717 00000-0 10270-3 0 9002
2 25544 51
6389 116
4411 0011722 156
9280 203
2405 15
60832800 13458
Satellite: ISS
Catalog Number: 25544
Epoch time: 11248
51571325 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 116
4411 deg
Eccentricity:
0011722
Arg of perigee: 156
9280 deg
Mean anomaly: 203
2405 deg
Mean motion: 15
60832800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 274
Coasting Arc #2 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2011/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1098674
26 A = 6763677
27 meter
Y = -5486418
39 meter E =
0017988
Z = 3778754
61 I = 51
96141
XDOT = 5041
151237 Wp = 122
08552
YDOT = -3947
184145 meter/sec RA = 110
57119 deg
ZDOT = -4259
851369 TA = 12
63071
MA = 12
58569
Ha = 213
843 n
mi
Hp = 201
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3604574
36 X = -1055598
67
Y = -18000060
34 feet Y = -5498463
55 meter
Z = 12397488
87 Z = 3773522
01
XDOT = 16539
210094 XDOT = 5105
608067
YDOT = -12950
079216 feet/sec YDOT = -3890
450560 meter/sec
ZDOT = -13975
890318 ZDOT = -4235
205172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1283309
63 X = -391152
77
Y = 18326772
77 feet Y = 5586000
34 meter
Z = 12376403
97 Z = 3772327
93
XDOT = -18151
222753 XDOT = -5532
492695
YDOT = 8111
227567 feet/sec YDOT = 2472
302162 meter/sec
ZDOT = -13875
340021 ZDOT = -4229
203638
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 11249
54012580
00016717 00000-0 10270-3 0 9010
2 25544 51
6394 111
2826 0011556 160
9202 199
2389 15
60877341 13613
Satellite: ISS
Catalog Number: 25544
Epoch time: 11249
54012580 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 111
2826 deg
Eccentricity:
0011556
Arg of perigee: 160
9202 deg
Mean anomaly: 199
2389 deg
Mean motion: 15
60877341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 297
Coasting Arc #3 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2011/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1629454
03 A = 6769776
39 meter
Y = 6568330
50 meter E =
0011363
Z = -248964
70 I = 51
99040
XDOT = -4639
209415 Wp = 104
23947
YDOT = -930
636101 meter/sec RA = 105
58013 deg
ZDOT = 6037
575320 TA = 253
08614
MA = 253
21074
Ha = 213
727 n
mi
Hp = 201
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5345977
80 X = -1701571
88
Y = 21549640
76 feet Y = 6549705
71 meter
Z = -816813
34 Z = -257055
80
XDOT = -15220
503331 XDOT = -4657
787040
YDOT = -3053
268048 feet/sec YDOT = -982
618295 meter/sec
ZDOT = 19808
317979 ZDOT = 6014
993306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10591107
32 X = 3228169
51
Y = -19512548
29 feet Y = -5947424
72 meter
Z = -850049
74 Z = -259095
16
XDOT = 12655
284255 XDOT = 3857
330641
YDOT = 6041
324312 feet/sec YDOT = 1841
395650 meter/sec
ZDOT = 19716
371362 ZDOT = 6009
549991
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 11250
50050149
00016717 00000-0 10270-3 0 9022
2 25544 51
6385 106
4455 0011643 164
8295 195
3212 15
60865717 13761
Satellite: ISS
Catalog Number: 25544
Epoch time: 11250
50050149 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 106
4455 deg
Eccentricity:
0011643
Arg of perigee: 164
8295 deg
Mean anomaly: 195
3212 deg
Mean motion: 15
60865717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 297
Coasting Arc #4 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2011/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3602270
89 A = 6764762
34 meter
Y = -4561124
34 meter E =
0013341
Z = -3456230
19 I = 51
97970
XDOT = 2627
116324 Wp = 147
66231
YDOT = 5552
460784 meter/sec RA = 100
59442 deg
ZDOT = -4608
497727 TA = 72
78883
MA = 72
64284
Ha = 213
670 n
mi
Hp = 202
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11818474
03 X = 3669795
99
Y = -14964318
69 feet Y = -4520464
14 meter
Z = -11339337
88 Z = -3438566
44
XDOT = 8619
148046 XDOT = 2587
219226
YDOT = 18216
734857 feet/sec YDOT = 5581
615520 meter/sec
ZDOT = -15119
743200 ZDOT = -4595
832581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15069483
98 X = -4593178
72
Y = 11753676
93 feet Y = 3582520
73 meter
Z = -11267185
85 Z = -3434238
25
XDOT = -3329
990957 XDOT = -1014
981244
YDOT = -18653
528324 feet/sec YDOT = -5685
595433 meter/sec
ZDOT = -15068
388036 ZDOT = -4592
844673
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 11251
52488800
00016717 00000-0 10270-3 0 9035
2 25544 51
6375 101
2861 0011603 169
1297 191
0112 15
60866330 13922
Satellite: ISS
Catalog Number: 25544
Epoch time: 11251
52488800 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 101
2861 deg
Eccentricity:
0011603
Arg of perigee: 169
1297 deg
Mean anomaly: 191
0112 deg
Mean motion: 15
60866330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 281
Coasting Arc #5 (Orbit 1407)
---------------------------------------
Vector Time (GMT): 2011/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4192296
83 A = 6757962
68 meter
Y = 414215
45 meter E =
0013621
Z = 5281895
92 I = 51
96134
XDOT = 174
602549 Wp = 161
66107
YDOT = -7645
789004 meter/sec RA = 95
56199 deg
ZDOT = 725
062165 TA = 281
37970
MA = 281
53269
Ha = 213
600 n
mi
Hp = 202
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13754254
70 X = -4222275
15
Y = 1358974
59 feet Y = 367167
36 meter
Z = 17329054
86 Z = 5261457
25
XDOT = 572
843007 XDOT = 256
564119
YDOT = -25084
609593 feet/sec YDOT = -7643
378171 meter/sec
ZDOT = 2378
812877 ZDOT = 726
109958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13821290
97 X = 4212729
49
Y = 1696378
46 feet Y = 517056
16 meter
Z = 17245773
18 Z = 5256511
67
XDOT = -5893
877573 XDOT = -1796
453884
YDOT = 23350
555294 feet/sec YDOT = 7117
249254 meter/sec
ZDOT = 2383
414219 ZDOT = 726
464654
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 11252
54926133
00016717 00000-0 10270-3 0 9045
2 25544 51
6374 96
1263 0011586 172
5068 187
6264 15
60871159 14085
Satellite: ISS
Catalog Number: 25544
Epoch time: 11252
54926133 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 96
1263 deg
Eccentricity:
0011586
Arg of perigee: 172
5068 deg
Mean anomaly: 187
6264 deg
Mean motion: 15
60871159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 314
Coasting Arc #6 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2011/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3329190
13 A = 6761829
00 meter
Y = 4032228
27 meter E =
0016864
Z = -4303708
53 I = 51
97528
XDOT = -2843
706022 Wp = 149
29911
YDOT = 6161
798808 meter/sec RA = 90
51669 deg
ZDOT = 3565
337261 TA = 156
92473
MA = 156
84890
Ha = 213
287 n
mi
Hp = 202
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10922539
80 X = 3304759
86
Y = 13229095
37 feet Y = 4069320
34 meter
Z = -14119778
65 Z = -4287595
25
XDOT = -9329
744168 XDOT = -2929
716619
YDOT = 20215
875353 feet/sec YDOT = 6129
518139 meter/sec
ZDOT = 11697
300726 ZDOT = 3551
313304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8118543
75 X = -2474532
14
Y = -15173810
63 feet Y = -4624977
48 meter
Z = -14054312
76 Z = -4283754
53
XDOT = 12171
552840 XDOT = 3709
889306
YDOT = -17317
730738 feet/sec YDOT = -5278
444329 meter/sec
ZDOT = 11639
895966 ZDOT = 3547
840290
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 11253
50959654
00016717 00000-0 10270-3 0 9057
2 25544 51
6360 91
2876 0011593 176
4771 183
6469 15
60923259 14237
Satellite: ISS
Catalog Number: 25544
Epoch time: 11253
50959654 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 91
2876 deg
Eccentricity:
0011593
Arg of perigee: 176
4771 deg
Mean anomaly: 183
6469 deg
Mean motion: 15
60923259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 328
Coasting Arc #7 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2011/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1288083
29 A = 6769102
42 meter
Y = -6557086
41 meter E =
0022052
Z = 987896
41 I = 51
99962
XDOT = 4525
205758 Wp = 149
73443
YDOT = -1791
719921 meter/sec RA = 85
51891 deg
ZDOT = -5953
388605 TA = 19
57005
MA = 19
48554
Ha = 213
027 n
mi
Hp = 202
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4225995
06 X = -1219463
90
Y = -21512750
68 feet Y = -6571106
77 meter
Z = 3241129
95 Z = 981806
30
XDOT = 14846
475583 XDOT = 4573
824951
YDOT = -5878
346196 feet/sec YDOT = -1740
845048 meter/sec
ZDOT = -19532
114847 ZDOT = -5931
287141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 204253
76 X = 62256
55
Y = 21926560
85 feet Y = 6683215
75 meter
Z = 3216614
58 Z = 980424
12
XDOT = -14192
753699 XDOT = -4325
951328
YDOT = 3003
137034 feet/sec YDOT = 915
356168 meter/sec
ZDOT = -19441
994325 ZDOT = -5925
919870
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 11254
53394033
00016717 00000-0 10270-3 0 9066
2 25544 51
6364 86
1283 0011367 180
6791 179
4352 15
60973925 14390
Satellite: ISS
Catalog Number: 25544
Epoch time: 11254
53394033 = yrday
fracday
Element set: 906
Inclination: 51
6364 deg
RA of node: 86
1283 deg
Eccentricity:
0011367
Arg of perigee: 180
6791 deg
Mean anomaly: 179
4352 deg
Mean motion: 15
60973925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 320
Coasting Arc #8 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2011/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1249708
90 A = 6766050
87 meter
Y = 6012902
29 meter E =
0015495
Z = 2841629
19 I = 51
98481
XDOT = -4615
019562 Wp = 127
22114
YDOT = -3387
823086 meter/sec RA = 80
53651 deg
ZDOT = 5110
816012 TA = 264
98765
MA = 265
16456
Ha = 212
948 n
mi
Hp = 202
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4100094
80 X = -1330657
49
Y = 19727369
70 feet Y = 5998474
97 meter
Z = 9322930
41 Z = 2835360
88
XDOT = -15141
140294 XDOT = -4601
620499
YDOT = -11114
905138 feet/sec YDOT = -3439
355591 meter/sec
ZDOT = 16767
769069 ZDOT = 5088
429328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7402524
52 X = 2256289
47
Y = -18752684
43 feet Y = -5715818
21 meter
Z = 9297116
84 Z = 2833761
21
XDOT = 11797
068284 XDOT = 3595
746413
YDOT = 12970
757920 feet/sec YDOT = 3953
487014 meter/sec
ZDOT = 16676
724352 ZDOT = 5083
065582
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 11255
55827021
00016717 00000-0 10270-3 0 9078
2 25544 51
6351 80
9672 0011635 184
6812 175
4238 15
60982862 14553
Satellite: ISS
Catalog Number: 25544
Epoch time: 11255
55827021 = yrday
fracday
Element set: 907
Inclination: 51
6351 deg
RA of node: 80
9672 deg
Eccentricity:
0011635
Arg of perigee: 184
6812 deg
Mean anomaly: 175
4238 deg
Mean motion: 15
60982862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 315
Coasting Arc #9 (Orbit 1469)
---------------------------------------
Vector Time (GMT): 2011/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3494612
05 A = 6758171
64 meter
Y = -2625867
85 meter E =
0014951
Z = -5162642
98 I = 51
95212
XDOT = 2993
837213 Wp = 125
84188
YDOT = 6903
980299 meter/sec RA = 75
51082 deg
ZDOT = -1496
567373 TA = 129
88303
MA = 129
75147
Ha = 212
875 n
mi
Hp = 202
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11465262
65 X = 3548794
41
Y = -8615052
00 feet Y = -2586486
57 meter
Z = -16937805
05 Z = -5145534
31
XDOT = 9822
300566 XDOT = 2923
683075
YDOT = 22650
853999 feet/sec YDOT = 6937
066802 meter/sec
ZDOT = -4909
997944 ZDOT = -1482
194519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12732423
78 X = -3880842
77
Y = 6776218
82 feet Y = 2065391
50 meter
Z = -16867983
03 Z = -5141361
23
XDOT = -5835
259759 XDOT = -1778
587174
YDOT = -22947
172784 feet/sec YDOT = -6994
298264 meter/sec
ZDOT = -4851
772894 ZDOT = -1478
820378
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 11256
51856725
00016717 00000-0 10270-3 0 9089
2 25544 51
6348 76
1292 0011552 187
2302 172
8689 15
60987424 14702
Satellite: ISS
Catalog Number: 25544
Epoch time: 11256
51856725 = yrday
fracday
Element set: 908
Inclination: 51
6348 deg
RA of node: 76
1292 deg
Eccentricity:
0011552
Arg of perigee: 187
2302 deg
Mean anomaly: 172
8689 deg
Mean motion: 15
60987424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1470
Checksum: 325
Coasting Arc #10 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2011/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4526463
77 A = 6760260
02 meter
Y = -1848450
39 meter E =
0009318
Z = 4660473
75 I = 51
95053
XDOT = -98
013178 Wp = 146
42505
YDOT = -7108
291660 meter/sec RA = 70
46194 deg
ZDOT = -2919
311549 TA = 332
39164
MA = 332
44109
Ha = 212
790 n
mi
Hp = 203
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14850602
92 X = -4528097
38
Y = -6064469
79 feet Y = -1899076
72 meter
Z = 15290268
21 Z = 4638480
40
XDOT = -321
565543 XDOT = -4
338082
YDOT = -23321
166862 feet/sec YDOT = -7108
864244 meter/sec
ZDOT = -9577
793796 ZDOT = -2919
559413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13999054
70 X = 4266911
87
Y = 8004608
29 feet Y = 2439804
61 meter
Z = 15200763
68 Z = 4633192
77
XDOT = -2268
779061 XDOT = -691
523858
YDOT = 22127
193972 feet/sec YDOT = 6744
368723 meter/sec
ZDOT = -9578
455605 ZDOT = -2919
513268
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 11257
54286805
00016717 00000-0 10270-3 0 9090
2 25544 51
6349 70
9688 0011557 191
6029 168
4863 15
60986798 14869
Satellite: ISS
Catalog Number: 25544
Epoch time: 11257
54286805 = yrday
fracday
Element set: 909
Inclination: 51
6349 deg
RA of node: 70
9688 deg
Eccentricity:
0011557
Arg of perigee: 191
6029 deg
Mean anomaly: 168
4863 deg
Mean motion: 15
60986798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 363
Coasting Arc #11 (Orbit 1500)
---------------------------------------
Vector Time (GMT): 2011/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3836408
57 A = 6768226
48 meter
Y = 5338032
79 meter E =
0005249
Z = -1626109
09 I = 51
96716
XDOT = -3122
607948 Wp = 157
95305
YDOT = 3996
616509 meter/sec RA = 65
45220 deg
ZDOT = 5753
927473 TA = 184
29681
MA = 184
30131
Ha = 212
469 n
mi
Hp = 203
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12586642
28 X = 3784331
88
Y = 17513230
94 feet Y = 5380642
53 meter
Z = -5335003
58 Z = -1607598
75
XDOT = -10244
776732 XDOT = -3195
018468
YDOT = 13112
258889 feet/sec YDOT = 3961
293277 meter/sec
ZDOT = 18877
714807 ZDOT = 5738
581519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10493239
89 X = -3198339
52
Y = -18863318
34 feet Y = -5749539
43 meter
Z = -5259869
12 Z = -1603208
11
XDOT = 10439
457139 XDOT = 3181
946536
YDOT = -11052
464616 feet/sec YDOT = -3368
791215 meter/sec
ZDOT = 18814
998252 ZDOT = 5734
811467
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 11258
50313599
00016717 00000-0 10270-3 0 9100
2 25544 51
6356 66
1302 0011574 194
6386 165
4436 15
61033018 15015
Satellite: ISS
Catalog Number: 25544
Epoch time: 11258
50313599 = yrday
fracday
Element set: 910
Inclination: 51
6356 deg
RA of node: 66
1302 deg
Eccentricity:
0011574
Arg of perigee: 194
6386 deg
Mean anomaly: 165
4436 deg
Mean motion: 15
61033018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1501
Checksum: 289
Coasting Arc #12 (Orbit 1516)
---------------------------------------
Vector Time (GMT): 2011/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1418537
69 A = 6766893
39 meter
Y = -6187101
96 meter E =
0014839
Z = -2319113
39 I = 51
95008
XDOT = 5358
928091 Wp = 177
94574
YDOT = 807
866730 meter/sec RA = 60
47077 deg
ZDOT = -5448
718965 TA = 27
88915
MA = 27
80968
Ha = 212
190 n
mi
Hp = 203
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4653995
05 X = -1337980
98
Y = -20298890
95 feet Y = -6202514
69 meter
Z = -7608639
72 Z = -2325808
50
XDOT = 17581
785077 XDOT = 5375
965125
YDOT = 2650
481396 feet/sec YDOT = 867
888353 meter/sec
ZDOT = -17876
374557 ZDOT = -5422
643828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2568446
46 X = 782862
48
Y = 20656643
23 feet Y = 6296144
86 meter
Z = -7635588
75 Z = -2327327
45
XDOT = -15832
140717 XDOT = -4825
636491
YDOT = -4581
305433 feet/sec YDOT = -1396
381896 meter/sec
ZDOT = -17770
197178 ZDOT = -5416
356100
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 11259
52740623
00016717 00000-0 10270-3 0 9116
2 25544 51
6361 60
9702 0011349 198
6287 161
4455 15
61074490 15174
Satellite: ISS
Catalog Number: 25544
Epoch time: 11259
52740623 = yrday
fracday
Element set: 911
Inclination: 51
6361 deg
RA of node: 60
9702 deg
Eccentricity:
0011349
Arg of perigee: 198
6287 deg
Mean anomaly: 161
4455 deg
Mean motion: 15
61074490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 304
Coasting Arc #13 (Orbit 1532)
---------------------------------------
Vector Time (GMT): 2011/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1846297
26 A = 6758664
90 meter
Y = 4192591
24 meter E =
0013974
Z = 4973008
37 I = 51
90660
XDOT = -5453
797874 Wp = 176
49574
YDOT = -4959
247059 meter/sec RA = 55
44957 deg
ZDOT = 2142
265267 TA = 252
65898
MA = 252
81187
Ha = 212
054 n
mi
Hp = 203
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6057405
70 X = -1917200
54
Y = 13755220
60 feet Y = 4171548
71 meter
Z = 16315644
25 Z = 4963866
49
XDOT = -17893
037644 XDOT = -5408
344065
YDOT = -16270
495600 feet/sec YDOT = -5019
980473 meter/sec
ZDOT = 7028
429354 ZDOT = 2115
881293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7265855
29 X = 2214632
69
Y = -13203287
39 feet Y = -4024362
00 meter
Z = 16278177
22 Z = 4961588
42
XDOT = 15573
777797 XDOT = 4746
887472
YDOT = 17159
907538 feet/sec YDOT = 5230
339818 meter/sec
ZDOT = 6921
220867 ZDOT = 2109
588120
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 11260
55166126
00016717 00000-0 10270-3 0 9122
2 25544 51
6360 55
8096 0011450 202
8193 157
2456 15
61082898 15332
Satellite: ISS
Catalog Number: 25544
Epoch time: 11260
55166126 = yrday
fracday
Element set: 912
Inclination: 51
6360 deg
RA of node: 55
8096 deg
Eccentricity:
0011450
Arg of perigee: 202
8193 deg
Mean anomaly: 157
2456 deg
Mean motion: 15
61082898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 298
Coasting Arc #14 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2011/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4649142
06 A = 6759010
87 meter
Y = -409507
50 meter E =
0015286
Z = -4899639
05 I = 51
89098
XDOT = 3077
769170 Wp = 154
60933
YDOT = 6619
150822 meter/sec RA = 50
39564 deg
ZDOT = 2356
436614 TA = 138
42989
MA = 138
31357
Ha = 211
908 n
mi
Hp = 203
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15253090
75 X = 4677177
41
Y = -1343528
54 feet Y = -357361
46 meter
Z = -16074931
27 Z = -4876985
27
XDOT = 10097
667880 XDOT = 2992
076572
YDOT = 21716
374087 feet/sec YDOT = 6653
089313 meter/sec
ZDOT = 7731
091254 ZDOT = 2371
179994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15404657
55 X = -4695339
62
Y = 342681
28 feet Y = 104449
25 meter
Z = -15982626
72 Z = -4871504
62
XDOT = -8591
542402 XDOT = -2618
702124
YDOT = -21201
385254 feet/sec YDOT = -6462
182225 meter/sec
ZDOT = 7790
780406 ZDOT = 2374
629868
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 11261
51188565
00016717 00000-0 10270-3 0 9131
2 25544 51
6373 50
9724 0011436 205
7522 154
3066 15
61100122 15484
Satellite: ISS
Catalog Number: 25544
Epoch time: 11261
51188565 = yrday
fracday
Element set: 913
Inclination: 51
6373 deg
RA of node: 50
9724 deg
Eccentricity:
0011436
Arg of perigee: 205
7522 deg
Mean anomaly: 154
3066 deg
Mean motion: 15
61100122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 279
Coasting Arc #15 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2011/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5532879
44 A = 6767264
31 meter
Y = -3255720
50 meter E =
0016576
Z = 2105225
82 I = 51
89811
XDOT = 961
147600 Wp = 153
21342
YDOT = -5226
748791 meter/sec RA = 45
37487 deg
ZDOT = -5554
621887 TA = 3
45925
MA = 3
44781
Ha = 211
742 n
mi
Hp = 204
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18152491
61 X = -5506288
96
Y = -10681497
69 feet Y = -3317443
77 meter
Z = 6906908
87 Z = 2078411
73
XDOT = 3153
371391 XDOT = 1046
506141
YDOT = -17148
125956 feet/sec YDOT = -5215
523632 meter/sec
ZDOT = -18223
825089 ZDOT = -5549
745047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17661370
92 X = 5383185
86
Y = 11540266
09 feet Y = 3517473
10 meter
Z = 6797865
16 Z = 2071989
30
XDOT = -3239
214868 XDOT = -987
312692
YDOT = 15685
151627 feet/sec YDOT = 4780
834216 meter/sec
ZDOT = -18203
660180 ZDOT = -5548
475623
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 11262
53610859
00016717 00000-0 10270-3 0 9141
2 25544 51
6368 45
8117 0011421 210
0070 150
0433 15
61114133 15644
Satellite: ISS
Catalog Number: 25544
Epoch time: 11262
53610859 = yrday
fracday
Element set: 914
Inclination: 51
6368 deg
RA of node: 45
8117 deg
Eccentricity:
0011421
Arg of perigee: 210
0070 deg
Mean anomaly: 150
0433 deg
Mean motion: 15
61114133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 259
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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