[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 20th 2011
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) : 104 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 593)
---------------------------------------
Vector Time (GMT): 2011/200/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6768165
90 A = 6772079
72 meter
Y = 270120
95 meter E =
0005208
Z = 59254
40 I = 51
65003
XDOT = -245
839043 Wp = 59
89289
YDOT = -4753
127122 meter/sec RA = 358
11106 deg
ZDOT = -6014
701395 TA = 119
46800
MA = 119
41603
Ha = 213
813 n
mi
Hp = 205
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22205268
69 X = -6770971
26
Y = 886223
60 feet Y = 194419
51 meter
Z = 194404
19 Z = 26368
51
XDOT = -806
558540 XDOT = -163
452635
YDOT = -15594
249089 feet/sec YDOT = -4755
415176 meter/sec
ZDOT = -19733
272293 ZDOT = -6015
695877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4842143
69 X = -1475885
40
Y = 21689792
30 feet Y = 6611048
69 meter
Z = 60805
74 Z = 18533
59
XDOT = -13667
812679 XDOT = -4165
949305
YDOT = -2984
250019 feet/sec YDOT = -909
599406 meter/sec
ZDOT = -19737
004807 ZDOT = -6015
839065
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 11200
41846008
00016717 00000-0 10270-3 0 9002
2 25544 51
6393 358
4657 0011862 339
4212 20
6465 15
60078652 5940
Satellite: ISS
Catalog Number: 25544
Epoch time: 11200
41846008 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 358
4657 deg
Eccentricity:
0011862
Arg of perigee: 339
4212 deg
Mean anomaly: 20
6465 deg
Mean motion: 15
60078652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 594
Checksum: 296
Coasting Arc #2 (Orbit 609)
---------------------------------------
Vector Time (GMT): 2011/201/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5506718
87 A = 6767107
86 meter
Y = 2014912
87 meter E =
0014350
Z = 3358368
90 I = 51
60268
XDOT = -4395
175843 Wp = 37
77311
YDOT = 4249
762559 meter/sec RA = 353
10356 deg
ZDOT = 4657
663622 TA = 1
58325
MA = 1
57871
Ha = 213
790 n
mi
Hp = 204
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18066662
95 X = 5467464
37
Y = 6610606
54 feet Y = 2076272
66 meter
Z = 11018270
66 Z = 3385024
88
XDOT = -14419
868252 XDOT = -4464
996566
YDOT = 13942
790549 feet/sec YDOT = 4200
222339 meter/sec
ZDOT = 15281
048627 ZDOT = 4636
142888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10737363
85 X = 3272748
50
Y = -15887690
22 feet Y = -4842567
98 meter
Z = 11126411
56 Z = 3391330
24
XDOT = 8895
322692 XDOT = 2711
294356
YDOT = 16650
488045 feet/sec YDOT = 5075
068756 meter/sec
ZDOT = 15193
363218 ZDOT = 4630
937109
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 11201
44336826
00016717 00000-0 10270-3 0 9019
2 25544 51
6385 353
3088 0011808 342
4756 17
5991 15
60098221 6102
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
44336826 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 353
3088 deg
Eccentricity:
0011808
Arg of perigee: 342
4756 deg
Mean anomaly: 17
5991 deg
Mean motion: 15
60098221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 610
Checksum: 295
Coasting Arc #3 (Orbit 624)
---------------------------------------
Vector Time (GMT): 2011/202/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2086536
26 A = 6760401
79 meter
Y = -3786485
28 meter E =
0017751
Z = -5209378
71 I = 51
54945
XDOT = 7190
707676 Wp = 40
08824
YDOT = -2421
435540 meter/sec RA = 348
05320 deg
ZDOT = -1108
887467 TA = 219
20641
MA = 219
33512
Ha = 214
015 n
mi
Hp = 204
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6845591
41 X = -2018734
09
Y = -12422851
98 feet Y = -3809438
76 meter
Z = -17091137
51 Z = -5219350
53
XDOT = 23591
560616 XDOT = 7222
636911
YDOT = -7944
342324 feet/sec YDOT = -2340
846068 meter/sec
ZDOT = -3638
082242 ZDOT = -1073
878071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13615354
38 X = -4149960
01
Y = 3799176
94 feet Y = 1157989
13 meter
Z = -17131396
15 Z = -5221649
55
XDOT = -2195
852097 XDOT = -669
295719
YDOT = -23797
767849 feet/sec YDOT = -7253
559640 meter/sec
ZDOT = -3495
733427 ZDOT = -1065
499549
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 11202
40421068
00016717 00000-0 10270-3 0 9020
2 25544 51
6377 348
4752 0011746 347
0378 13
0474 15
60101828 6259
Satellite: ISS
Catalog Number: 25544
Epoch time: 11202
40421068 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 348
4752 deg
Eccentricity:
0011746
Arg of perigee: 347
0378 deg
Mean anomaly: 13
0474 deg
Mean motion: 15
60101828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 625
Checksum: 283
Coasting Arc #4 (Orbit 640)
---------------------------------------
Vector Time (GMT): 2011/203/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2138877
38 A = 6763031
00 meter
Y = 4476227
50 meter E =
0016150
Z = 4598999
73 I = 51
52896
XDOT = -7069
758931 Wp = 20
44385
YDOT = -306
187506 meter/sec RA = 342
98506 deg
ZDOT = -2971
952163 TA = 99
28956
MA = 99
10689
Ha = 214
203 n
mi
Hp = 204
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7017314
24 X = -2211113
33
Y = 14685785
75 feet Y = 4451905
04 meter
Z = 15088581
79 Z = 4588434
04
XDOT = -23194
747148 XDOT = -7051
372586
YDOT = -1004
552185 feet/sec YDOT = -385
142835 meter/sec
ZDOT = -9750
499222 ZDOT = -3006
252059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12902898
48 X = 3932803
46
Y = 9986588
70 feet Y = 3043912
24 meter
Z = 15045383
33 Z = 4585832
84
XDOT = -5031
058685 XDOT = -1533
466687
YDOT = 21489
004184 feet/sec YDOT = 6549
848475 meter/sec
ZDOT = -9889
785955 ZDOT = -3014
406759
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 11203
42909665
00016717 00000-0 10270-3 0 9038
2 25544 51
6379 343
3189 0011773 350
3305 9
7622 15
60106199 6417
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
42909665 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 343
3189 deg
Eccentricity:
0011773
Arg of perigee: 350
3305 deg
Mean anomaly: 9
7622 deg
Mean motion: 15
60106199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 641
Checksum: 299
Coasting Arc #5 (Orbit 655)
---------------------------------------
Vector Time (GMT): 2011/204/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5326740
97 A = 6770539
20 meter
Y = -3734238
58 meter E =
0017752
Z = -1839062
23 I = 51
52562
XDOT = 4152
361442 Wp = 10
75771
YDOT = 3156
737693 meter/sec RA = 337
95137 deg
ZDOT = 5643
144225 TA = 328
90875
MA = 329
01368
Ha = 214
298 n
mi
Hp = 204
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17476184
30 X = 5377035
81
Y = -12251438
91 feet Y = -3674390
35 meter
Z = -6033668
73 Z = -1813063
30
XDOT = 13623
233077 XDOT = 4089
340439
YDOT = 10356
750960 feet/sec YDOT = 3202
819077 meter/sec
ZDOT = 18514
252708 ZDOT = 5663
163417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8709813
62 X = -2654751
19
Y = -19517166
60 feet Y = -5948832
38 meter
Z = -5927839
91 Z = -1806805
61
XDOT = 11308
019439 XDOT = 3446
684325
YDOT = -10668
002843 feet/sec YDOT = -3251
607266 meter/sec
ZDOT = 18595
354469 ZDOT = 5667
864042
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 11204
38991719
00016717 00000-0 10270-3 0 9046
2 25544 51
6377 338
4846 0011720 354
4677 5
6347 15
60131573 6568
Satellite: ISS
Catalog Number: 25544
Epoch time: 11204
38991719 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 338
4846 deg
Eccentricity:
0011720
Arg of perigee: 354
4677 deg
Mean anomaly: 5
6347 deg
Mean motion: 15
60131573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 656
Checksum: 318
Coasting Arc #6 (Orbit 671)
---------------------------------------
Vector Time (GMT): 2011/205/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6325663
92 A = 6770295
49 meter
Y = 1602841
73 meter E =
0007616
Z = -1822575
22 I = 51
49799
XDOT = 307
015056 Wp = 33
26195
YDOT = -5190
316371 meter/sec RA = 332
94420 deg
ZDOT = -5635
071542 TA = 166
84264
MA = 166
82277
Ha = 214
400 n
mi
Hp = 203
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20753490
55 X = -6334263
40
Y = 5258667
10 feet Y = 1532056
40 meter
Z = -5979577
50 Z = -1853325
78
XDOT = 1007
267243 XDOT = 392
405294
YDOT = -17028
597018 feet/sec YDOT = -5186
405140 meter/sec
ZDOT = -18487
767527 ZDOT = -5633
373179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1602558
39 X = 488459
80
Y = 21313901
13 feet Y = 6496477
06 meter
Z = -6104565
65 Z = -1860671
61
XDOT = -15026
435008 XDOT = -4580
057391
YDOT = -4158
690172 feet/sec YDOT = -1267
568764 meter/sec
ZDOT = -18480
537658 ZDOT = -5632
867878
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 11205
41478023
00016717 00000-0 10270-3 0 9050
2 25544 51
6378 333
3286 0011942 358
7710 1
3415 15
60185265 6726
Satellite: ISS
Catalog Number: 25544
Epoch time: 11205
41478023 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 333
3286 deg
Eccentricity:
0011942
Arg of perigee: 358
7710 deg
Mean anomaly: 1
3415 deg
Mean motion: 15
60185265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 672
Checksum: 290
Coasting Arc #7 (Orbit 687)
---------------------------------------
Vector Time (GMT): 2011/206/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4766731
68 A = 6762616
94 meter
Y = 1334957
06 meter E =
0011353
Z = 4596731
21 I = 51
44538
XDOT = -4409
607425 Wp = 43
38189
YDOT = 5553
575382 meter/sec RA = 327
90587 deg
ZDOT = 2963
614014 TA = 17
09349
MA = 17
05529
Ha = 214
329 n
mi
Hp = 203
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15638883
46 X = 4729119
77
Y = 4379780
39 feet Y = 1388050
74 meter
Z = 15081139
14 Z = 4619796
58
XDOT = -14467
215961 XDOT = -4485
777416
YDOT = 18220
391673 feet/sec YDOT = 5503
838240 meter/sec
ZDOT = 9723
143092 ZDOT = 2942
007952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6747653
79 X = 2056684
87
Y = -14676331
56 feet Y = -4473345
86 meter
Z = 15174728
01 Z = 4625257
10
XDOT = 14667
123660 XDOT = 4470
539292
YDOT = 16692
966617 feet/sec YDOT = 5088
016225 meter/sec
ZDOT = 9635
040830 ZDOT = 2936
760445
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 11206
43963226
00016717 00000-0 10270-3 0 9068
2 25544 51
6373 328
1716 0011749 2
0286 358
0915 15
60182795 6882
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
43963226 = yrday
fracday
Element set: 906
Inclination: 51
6373 deg
RA of node: 328
1716 deg
Eccentricity:
0011749
Arg of perigee: 2
0286 deg
Mean anomaly: 358
0915 deg
Mean motion: 15
60182795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 688
Checksum: 314
Coasting Arc #8 (Orbit 702)
---------------------------------------
Vector Time (GMT): 2011/207/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1506619
90 A = 6760201
83 meter
Y = -4064125
19 meter E =
0018079
Z = -5199516
52 I = 51
41314
XDOT = 6542
533437 Wp = 58
12404
YDOT = -3840
643619 meter/sec RA = 322
83050 deg
ZDOT = 1118
431919 TA = 222
55940
MA = 222
69966
Ha = 214
534 n
mi
Hp = 203
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4942978
66 X = -1435804
07
Y = -13333744
05 feet Y = -4080576
52 meter
Z = -17058781
23 Z = -5206664
09
XDOT = 21465
004715 XDOT = 6579
560927
YDOT = -12600
536807 feet/sec YDOT = -3767
274134 meter/sec
ZDOT = 3669
396060 ZDOT = 1150
304632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13876950
74 X = -4229694
58
Y = 2944418
19 feet Y = 897458
67 meter
Z = -17087551
76 Z = -5208285
78
XDOT = -9290
507446 XDOT = -2831
746670
YDOT = -21970
727008 feet/sec YDOT = -6696
677592 meter/sec
ZDOT = 3799
084790 ZDOT = 1157
961044
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 11207
40042127
00016717 00000-0 10270-3 0 9075
2 25544 51
6383 323
3386 0011720 6
6210 353
5098 15
60189512 7033
Satellite: ISS
Catalog Number: 25544
Epoch time: 11207
40042127 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 323
3386 deg
Eccentricity:
0011720
Arg of perigee: 6
6210 deg
Mean anomaly: 353
5098 deg
Mean motion: 15
60189512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 703
Checksum: 272
Coasting Arc #9 (Orbit 718)
---------------------------------------
Vector Time (GMT): 2011/208/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2155471
95 A = 6767186
38 meter
Y = 5504937
15 meter E =
0018437
Z = 3292493
41 I = 51
41244
XDOT = -6060
083665 Wp = 52
72306
YDOT = 448
672057 meter/sec RA = 317
76737 deg
ZDOT = -4688
398295 TA = 88
78007
MA = 88
56885
Ha = 214
698 n
mi
Hp = 203
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7071758
35 X = -2232863
11
Y = 18060817
42 feet Y = 5480400
20 meter
Z = 10802143
75 Z = 3281835
03
XDOT = -19882
164255 XDOT = -6041
875371
YDOT = 1472
021183 feet/sec YDOT = 381
006931 meter/sec
ZDOT = -15381
884171 ZDOT = -4717
793439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17059388
26 X = 5199701
54
Y = 9280136
61 feet Y = 2828585
64 meter
Z = 10758510
04 Z = 3279193
86
XDOT = -269
567633 XDOT = -82
164215
YDOT = 18577
310232 feet/sec YDOT = 5662
364159 meter/sec
ZDOT = -15501
298439 ZDOT = -4724
795764
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 11208
42525063
00016717 00000-0 10270-3 0 9084
2 25544 51
6378 318
1812 0011741 10
1077 350
0312 15
60187807 7190
Satellite: ISS
Catalog Number: 25544
Epoch time: 11208
42525063 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 318
1812 deg
Eccentricity:
0011741
Arg of perigee: 10
1077 deg
Mean anomaly: 350
0312 deg
Mean motion: 15
60187807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 719
Checksum: 278
Coasting Arc #10 (Orbit 734)
---------------------------------------
Vector Time (GMT): 2011/209/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4678183
63 A = 6771657
38 meter
Y = -4874240
83 meter E =
0023270
Z = 159236
03 I = 51
40784
XDOT = 3356
697917 Wp = 30
84654
YDOT = 3429
933095 meter/sec RA = 312
74641 deg
ZDOT = 6005
928822 TA = 330
88101
MA = 331
01057
Ha = 214
713 n
mi
Hp = 202
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15348371
50 X = 4731567
12
Y = -15991603
78 feet Y = -4821628
07 meter
Z = 522427
92 Z = 182091
24
XDOT = 11012
788441 XDOT = 3288
919134
YDOT = 11253
061335 feet/sec YDOT = 3467
090006 meter/sec
ZDOT = 19704
490885 ZDOT = 6022
071136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14300115
07 X = -4358675
07
Y = -16932354
51 feet Y = -5160981
65 meter
Z = 615556
55 Z = 187621
64
XDOT = 11096
320643 XDOT = 3382
158532
YDOT = -8615
296353 feet/sec YDOT = -2625
942329 meter/sec
ZDOT = 19769
842527 ZDOT = 6025
848002
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 11209
45006828
00016717 00000-0 10270-3 0 9092
2 25544 51
6394 313
0253 0011772 14
2646 345
8840 15
60226726 7352
Satellite: ISS
Catalog Number: 25544
Epoch time: 11209
45006828 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 313
0253 deg
Eccentricity:
0011772
Arg of perigee: 14
2646 deg
Mean anomaly: 345
8840 deg
Mean motion: 15
60226726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 735
Checksum: 298
Coasting Arc #11 (Orbit 749)
---------------------------------------
Vector Time (GMT): 2011/210/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5317428
63 A = 6766080
95 meter
Y = 2206547
62 meter E =
0014999
Z = -3573869
09 I = 51
36967
XDOT = 374
888034 Wp = 36
13561
YDOT = -6252
675942 meter/sec RA = 307
72098 deg
ZDOT = -4415
849227 TA = 186
32989
MA = 186
34886
Ha = 214
846 n
mi
Hp = 202
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17445631
98 X = -5324346
68
Y = 7239329
47 feet Y = 2147046
61 meter
Z = -11725292
30 Z = -3599717
10
XDOT = 1229
947618 XDOT = 466
229684
YDOT = -20514
028680 feet/sec YDOT = -6247
972507 meter/sec
ZDOT = -14487
694315 ZDOT = -4413
806894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5692524
16 X = 1735081
36
Y = 17940929
57 feet Y = 5468395
33 meter
Z = -11830412
54 Z = -3605909
74
XDOT = -19012
853704 XDOT = -5795
117809
YDOT = -3520
121937 feet/sec YDOT = -1072
933166 meter/sec
ZDOT = -14479
022841 ZDOT = -4413
206162
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 11210
41082467
00016717 00000-0 10270-3 0 9105
2 25544 51
6393 308
1917 0011869 17
5600 342
5964 15
60240583 7501
Satellite: ISS
Catalog Number: 25544
Epoch time: 11210
41082467 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 308
1917 deg
Eccentricity:
0011869
Arg of perigee: 17
5600 deg
Mean anomaly: 342
5964 deg
Mean motion: 15
60240583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 750
Checksum: 290
Coasting Arc #12 (Orbit 765)
---------------------------------------
Vector Time (GMT): 2011/211/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3957662
52 A = 6759665
46 meter
Y = 1591369
19 meter E =
0011980
Z = 5236848
29 I = 51
33115
XDOT = -3637
274111 Wp = 34
99076
YDOT = 6732
407296 meter/sec RA = 302
64992 deg
ZDOT = 711
823714 TA = 48
24734
MA = 48
14499
Ha = 214
789 n
mi
Hp = 202
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12984457
07 X = 3914134
40
Y = 5221027
51 feet Y = 1635382
34 meter
Z = 17181260
80 Z = 5255968
51
XDOT = -11933
314013 XDOT = -3715
744685
YDOT = 22087
950445 feet/sec YDOT = 6691
294265 meter/sec
ZDOT = 2335
379640 ZDOT = 693
964298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6113847
27 X = 1863500
65
Y = -12482170
41 feet Y = -3804565
54 meter
Z = 17258831
65 Z = 5260491
89
XDOT = 20283
991059 XDOT = 6182
560475
YDOT = 13023
489734 feet/sec YDOT = 3969
559671 meter/sec
ZDOT = 2262
444858 ZDOT = 689
593193
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 11211
43562006
00016717 00000-0 10270-3 0 9111
2 25544 51
6397 303
0351 0011913 20
8882 339
2758 15
60271706 7662
Satellite: ISS
Catalog Number: 25544
Epoch time: 11211
43562006 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 303
0351 deg
Eccentricity:
0011913
Arg of perigee: 20
8882 deg
Mean anomaly: 339
2758 deg
Mean motion: 15
60271706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 766
Checksum: 287
Coasting Arc #13 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2011/212/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1382188
63 A = 6763268
72 meter
Y = -4956061
83 meter E =
0015501
Z = -4396823
02 I = 51
32786
XDOT = 5313
455236 Wp = 60
24019
YDOT = -4420
512337 meter/sec RA = 297
56925 deg
ZDOT = 3328
807097 TA = 243
44405
MA = 243
60302
Ha = 214
968 n
mi
Hp = 202
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4534739
59 X = -1305307
87
Y = -16260045
37 feet Y = -4971088
18 meter
Z = -14425272
38 Z = -4403351
07
XDOT = 17432
595920 XDOT = 5346
321058
YDOT = -14502
993230 feet/sec YDOT = -4360
910480 meter/sec
ZDOT = 10921
283127 ZDOT = 3354
698718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16473919
26 X = -5021250
59
Y = 3578443
89 feet Y = 1090709
70 meter
Z = -14451510
14 Z = -4404820
29
XDOT = -13299
239516 XDOT = -4053
608205
YDOT = -16910
574632 feet/sec YDOT = -5154
343148 meter/sec
ZDOT = 11026
701894 ZDOT = 3360
938737
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 11212
39635626
00016717 00000-0 10270-3 0 9127
2 25544 51
6399 298
2026 0011932 24
5727 335
5995 15
60263110 7817
Satellite: ISS
Catalog Number: 25544
Epoch time: 11212
39635626 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 298
2026 deg
Eccentricity:
0011932
Arg of perigee: 24
5727 deg
Mean anomaly: 335
5995 deg
Mean motion: 15
60263110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 308
Coasting Arc #14 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2011/213/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1482808
57 A = 6770688
21 meter
Y = 6459517
56 meter E =
0018099
Z = 1381190
45 I = 51
33965
XDOT = -5045
323495 Wp = 78
35932
YDOT = 92
481384 meter/sec RA = 292
52595 deg
ZDOT = -5781
096963 TA = 86
49504
MA = 86
28804
Ha = 215
066 n
mi
Hp = 202
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4864857
51 X = -1561639
35
Y = 21192642
92 feet Y = 6442495
08 meter
Z = 4531464
72 Z = 1373795
91
XDOT = -16552
898605 XDOT = -5017
899853
YDOT = 303
416615 feet/sec YDOT = 36
215044 meter/sec
ZDOT = -18966
853552 ZDOT = -5805
539906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21003599
86 X = 6401897
24
Y = 5649620
81 feet Y = 1722004
42 meter
Z = 4501077
98 Z = 1371928
57
XDOT = 124
205374 XDOT = 37
857798
YDOT = 14907
108448 feet/sec YDOT = 4543
686655 meter/sec
ZDOT = -19066
144860 ZDOT = -5811
360953
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 11213
42113011
00016717 00000-0 10270-3 0 9132
2 25544 51
6397 293
0455 0011938 28
5955 331
5853 15
60285007 7972
Satellite: ISS
Catalog Number: 25544
Epoch time: 11213
42113011 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 293
0455 deg
Eccentricity:
0011938
Arg of perigee: 28
5955 deg
Mean anomaly: 331
5853 deg
Mean motion: 15
60285007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 298
Coasting Arc #15 (Orbit 812)
---------------------------------------
Vector Time (GMT): 2011/214/09:16:22
796
Vector Time (MET): N/A
Weight (LBS) : 901814
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3561961
51 A = 6769166
82 meter
Y = -5274586
86 meter E =
0024377
Z = 2261896
07 I = 51
32488
XDOT = 3143
232118 Wp = 53
69997
YDOT = 4458
426538 meter/sec RA = 287
50465 deg
ZDOT = 5420
400566 TA = 331
69967
MA = 331
83189
Ha = 215
050 n
mi
Hp = 201
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11686225
44 X = 3609690
59
Y = -17305074
99 feet Y = -5234488
01 meter
Z = 7420918
88 Z = 2279315
54
XDOT = 10312
441331 XDOT = 3066
812756
YDOT = 14627
383654 feet/sec YDOT = 4493
148687 meter/sec
ZDOT = 17783
466425 ZDOT = 5435
484526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17083992
48 X = -5207200
91
Y = -11962916
45 feet Y = -3646296
93 meter
Z = 7491952
59 Z = 2283547
15
XDOT = 13944
176758 XDOT = 4250
185076
YDOT = -8684
107057 feet/sec YDOT = -2646
915831 meter/sec
ZDOT = 17844
502735 ZDOT = 5439
004434
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 11214
44589205
00016717 00000-0 10270-3 0 9148
2 25544 51
6402 287
8892 0012038 32
5950 327
5947 15
60320332 8136
Satellite: ISS
Catalog Number: 25544
Epoch time: 11214
44589205 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 287
8892 deg
Eccentricity:
0012038
Arg of perigee: 32
5950 deg
Mean anomaly: 327
5947 deg
Mean motion: 15
60320332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 813
Checksum: 298
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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