[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 13th 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) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 235 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
163/14:33:04
342 -8
7 8
8 8
8
N/A -1
2 -0
1 192
8
000/00:36:08
684 1
1 -0
0 190
3
163/18:40:07
203 0
8 8
3 8
3
N/A 5
6 -0
6 200
2
000/00:40:14
405 -6
1 0
5 194
7
166/15:05:14
161 8
6 9
5 9
5
N/A -3
7 0
3 203
3
000/00:30:28
323 1
7 0
6 197
7
166/19:08:40
031 -8
0 8
9 8
9
N/A -1
3 0
2 207
8
000/00:37:20
061 3
6 -0
4 205
2
Coasting Arc #1 (Orbit 3985)
---------------------------------------
Vector Time (GMT): 2011/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919843
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5089132
52 A = 6727467
16 meter
Y = 3466761
38 meter E =
0003629
Z = -2709568
25 I = 51
56935
XDOT = -4821
509143 Wp = 119
78583
YDOT = 3040
230515 meter/sec RA = 193
82805 deg
ZDOT = -5172
903559 TA = 91
15432
MA = 91
11274
Ha = 188
984 n
mi
Hp = 183
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16696629
00 X = 5063150
96
Y = 11373889
03 feet Y = 3523526
14 meter
Z = -8889659
61 Z = -2684907
87
XDOT = -15818
599550 XDOT = -4830
018065
YDOT = 9974
509564 feet/sec YDOT = 2986
266400 meter/sec
ZDOT = -16971
468369 ZDOT = -5196
346958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14678627
07 X = 4474045
53
Y = -13944366
49 feet Y = -4250242
90 meter
Z = -8789844
73 Z = -2679144
67
XDOT = 5382
285742 XDOT = 1640
520694
YDOT = 16409
121876 feet/sec YDOT = 5001
500348 meter/sec
ZDOT = -17066
569698 ZDOT = -5201
890444
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 11161
52638337
00016717 00000-0 10270-3 0 9004
2 25544 51
6452 194
7208 0001325 318
4435 41
6628 15
74556818 39868
Satellite: ISS
Catalog Number: 25544
Epoch time: 11161
52638337 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 194
7208 deg
Eccentricity:
0001325
Arg of perigee: 318
4435 deg
Mean anomaly: 41
6628 deg
Mean motion: 15
74556818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3986
Checksum: 316
Coasting Arc #2 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2011/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919843
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4164555
24 A = 6721887
33 meter
Y = -2900221
85 meter E =
0008939
Z = 4403642
03 I = 51
58016
XDOT = 5980
999229 Wp = 60
36573
YDOT = 3558
583973 meter/sec RA = 188
63742 deg
ZDOT = -3303
256149 TA = 62
86087
MA = 62
76974
Ha = 188
824 n
mi
Hp = 183
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13663238
99 X = 4175284
27
Y = -9515163
55 feet Y = -2853591
80 meter
Z = 14447644
47 Z = 4423899
34
XDOT = 19622
700884 XDOT = 5956
808697
YDOT = 11675
144268 feet/sec YDOT = 3625
332277 meter/sec
ZDOT = -10837
454558 ZDOT = -3274
258525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6668124
97 X = -2032444
49
Y = -15178166
58 feet Y = -4626305
17 meter
Z = 14529839
52 Z = 4428695
08
XDOT = 14201
051501 XDOT = 4328
480497
YDOT = -16530
202222 feet/sec YDOT = -5038
405637 meter/sec
ZDOT = -10720
058023 ZDOT = -3267
473685
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 11162
54184879
00016717 00000-0 10270-3 0 9015
2 25544 51
6438 189
5021 0001390 324
4580 35
6491 15
74613427 40028
Satellite: ISS
Catalog Number: 25544
Epoch time: 11162
54184879 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 189
5021 deg
Eccentricity:
0001390
Arg of perigee: 324
4580 deg
Mean anomaly: 35
6491 deg
Mean motion: 15
74613427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 297
Coasting Arc #3 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2011/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919843
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5311378
12 A = 6726452
30 meter
Y = -2755649
95 meter E =
0012811
Z = 3058762
27 I = 51
62540
XDOT = 4710
993230 Wp = 78
51056
YDOT = -3607
945026 meter/sec RA = 183
54316 deg
ZDOT = 4915
196477 TA = 316
98137
MA = 317
08145
Ha = 189
071 n
mi
Hp = 183
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17425781
22 X = -5295028
21
Y = -9040846
30 feet Y = -2814954
04 meter
Z = 10035309
28 Z = 3032998
64
XDOT = 15456
014534 XDOT = 4727
110458
YDOT = -11837
089979 feet/sec YDOT = -3555
174442 meter/sec
ZDOT = 16125
972692 ZDOT = 4938
121335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12026798
41 X = -3665768
16
Y = 15583128
29 feet Y = 4749737
50 meter
Z = 9930982
72 Z = 3026963
53
XDOT = -7756
778239 XDOT = -2364
266007
YDOT = -16354
012124 feet/sec YDOT = -4984
702895 meter/sec
ZDOT = 16219
015989 ZDOT = 4943
556073
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 11163
55729055
00016717 00000-0 10270-3 0 9029
2 25544 51
6434 184
2829 0001390 334
2845 25
8249 15
74610944 40185
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
55729055 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 184
2829 deg
Eccentricity:
0001390
Arg of perigee: 334
2845 deg
Mean anomaly: 25
8249 deg
Mean motion: 15
74610944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 308
Coasting Arc #4 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2011/163/14:51:08
684
Vector Time (MET): N/A
Weight (LBS) : 918279
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6651125
30 A = 6739114
62 meter
Y = 416572
45 meter E =
0011478
Z = -950524
09 I = 51
63920
XDOT = -1149
162857 Wp = 335
75212
YDOT = -4764
120273 meter/sec RA = 182
89809 deg
ZDOT = 5938
172480 TA = 13
87352
MA = 13
84200
Ha = 192
794 n
mi
Hp = 190
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21821277
23 X = -6650671
64
Y = 1366707
50 feet Y = 342198
20 meter
Z = -3118517
35 Z = -982834
42
XDOT = -3770
219348 XDOT = -1124
650991
YDOT = -15630
315855 feet/sec YDOT = -4776
834747 meter/sec
ZDOT = 19482
193176 ZDOT = 5932
648616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12892270
55 X = 3929564
06
Y = 17634946
71 feet Y = 5375131
76 meter
Z = -3249491
41 Z = -990444
98
XDOT = -9790
350046 XDOT = -2984
098694
YDOT = 10751
845642 feet/sec YDOT = 3277
162552 meter/sec
ZDOT = 19459
971183 ZDOT = 5931
399217
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 11163
62076304
00016717 00000-0 10270-3 0 9030
2 25544 51
6413 183
9567 0011235 283
9183 76
0729 15
71416265 40190
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
62076304 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 183
9567 deg
Eccentricity:
0011235
Arg of perigee: 283
9183 deg
Mean anomaly: 76
0729 deg
Mean motion: 15
71416265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 304
Coasting Arc #5 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2011/163/19:00:14
405
Vector Time (MET): N/A
Weight (LBS) : 916539
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2305202
27 A = 6739198
53 meter
Y = 3984677
30 meter E =
0004945
Z = -4922896
38 I = 51
61287
XDOT = -7221
637398 Wp = 146
19604
YDOT = 1478
598165 meter/sec RA = 182
04125 deg
ZDOT = -2189
893854 TA = 102
52782
MA = 102
47249
Ha = 200
224 n
mi
Hp = 194
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7562999
57 X = 2284388
28
Y = 13073088
26 feet Y = 4010339
86 meter
Z = -16151234
83 Z = -4911747
53
XDOT = -23693
036082 XDOT = -7226
996422
YDOT = 4851
043848 feet/sec YDOT = 1397
811804 meter/sec
ZDOT = -7184
691123 ZDOT = -2224
989709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8775784
58 X = -2674859
14
Y = -12350844
28 feet Y = -3764537
34 meter
Z = -16106186
27 Z = -4909165
58
XDOT = 22232
849056 XDOT = 6776
572392
YDOT = -6264
354603 feet/sec YDOT = -1909
375283 meter/sec
ZDOT = -7326
995966 ZDOT = -2233
268370
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 11163
81162665
00016717 00000-0 10270-3 0 9048
2 25544 51
6435 182
9821 0011861 230
3949 129
6164 15
67895060 40228
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
81162665 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 182
9821 deg
Eccentricity:
0011861
Arg of perigee: 230
3949 deg
Mean anomaly: 129
6164 deg
Mean motion: 15
67895060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 310
Coasting Arc #6 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2011/164/19:00:14
405
Vector Time (MET): N/A
Weight (LBS) : 916539
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4751213
55 A = 6743869
94 meter
Y = -3123150
42 meter E =
0006405
Z = 3619129
82 I = 51
65858
XDOT = 5445
016134 Wp = 159
87346
YDOT = 3190
232680 meter/sec RA = 176
90965 deg
ZDOT = -4398
810733 TA = 336
92036
MA = 336
94912
Ha = 199
912 n
mi
Hp = 194
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15587970
98 X = 4768202
89
Y = -10246556
51 feet Y = -3069925
12 meter
Z = 11873785
50 Z = 3642252
10
XDOT = 17864
226162 XDOT = 5430
306433
YDOT = 10466
642651 feet/sec YDOT = 3251
040698 meter/sec
ZDOT = -14431
793743 ZDOT = -4372
393800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14357838
72 X = -4376269
24
Y = 11814896
78 feet Y = 3601180
54 meter
Z = 11967632
32 Z = 3647734
33
XDOT = -18086
492378 XDOT = -5512
762877
YDOT = -7481
130796 feet/sec YDOT = -2280
248666 meter/sec
ZDOT = -14324
820283 ZDOT = -4366
205222
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 11164
83142108
00016717 00000-0 10270-3 0 9052
2 25544 51
6427 177
7930 0011882 234
1911 125
8145 15
67890925 40385
Satellite: ISS
Catalog Number: 25544
Epoch time: 11164
83142108 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 177
7930 deg
Eccentricity:
0011882
Arg of perigee: 234
1911 deg
Mean anomaly: 125
8145 deg
Mean motion: 15
67890925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 311
Coasting Arc #7 (Orbit 4053)
---------------------------------------
Vector Time (GMT): 2011/165/19:00:14
405
Vector Time (MET): N/A
Weight (LBS) : 916539
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6299651
09 A = 6747429
55 meter
Y = -892201
42 meter E =
0003597
Z = 2246874
79 I = 51
70124
XDOT = 2620
713316 Wp = 119
09810
YDOT = -4730
908959 meter/sec RA = 171
86749 deg
ZDOT = 5460
939664 TA = 266
00847
MA = 266
04959
Ha = 199
672 n
mi
Hp = 195
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20668146
63 X = -6300121
06
Y = -2927170
01 feet Y = -962651
01 meter
Z = 7371636
44 Z = 2216269
67
XDOT = 8598
140801 XDOT = 2646
892139
YDOT = -15521
354854 feet/sec YDOT = -4701
457243 meter/sec
ZDOT = 17916
468713 ZDOT = 5473
733797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20914316
09 X = 6374683
54
Y = 381510
37 feet Y = 116284
36 meter
Z = 7247583
44 Z = 2209063
43
XDOT = -6508
391237 XDOT = -1983
757649
YDOT = 14914
205960 feet/sec YDOT = 4545
849977 meter/sec
ZDOT = 17968
517578 ZDOT = 5476
804158
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 11165
85119712
00016717 00000-0 10270-3 0 9061
2 25544 51
6430 172
6024 0011852 238
5961 121
4040 15
67920340 40546
Satellite: ISS
Catalog Number: 25544
Epoch time: 11165
85119712 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 172
6024 deg
Eccentricity:
0011852
Arg of perigee: 238
5961 deg
Mean anomaly: 121
4040 deg
Mean motion: 15
67920340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4054
Checksum: 281
Coasting Arc #8 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2011/166/15:20:28
323
Vector Time (MET): N/A
Weight (LBS) : 915220
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3677904
72 A = 6750299
69 meter
Y = -4025572
64 meter E =
0009274
Z = 3970781
99 I = 51
70784
XDOT = 6315
192874 Wp = 94
08657
YDOT = 1827
437429 meter/sec RA = 167
51215 deg
ZDOT = -3989
403494 TA = 37
32015
MA = 37
25575
Ha = 203
348 n
mi
Hp = 197
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12066616
55 X = 3703356
79
Y = -13207259
31 feet Y = -3984302
56 meter
Z = 13027499
96 Z = 3988710
24
XDOT = 20719
136726 XDOT = 6313
668523
YDOT = 5995
529624 feet/sec YDOT = 1898
050027 meter/sec
ZDOT = -13088
594141 ZDOT = -3958
727664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17835057
85 X = -5436125
63
Y = 205458
09 feet Y = 62623
63 meter
Z = 13100350
65 Z = 3992986
88
XDOT = -9747
762673 XDOT = -2971
118063
YDOT = -18016
711980 feet/sec YDOT = -5491
493812 meter/sec
ZDOT = -12964
273443 ZDOT = -3951
510545
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 11166
67985797
00016717 00000-0 10270-3 0 9077
2 25544 51
6398 168
3849 0003099 207
4956 152
6039 15
65259689 40676
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
67985797 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 168
3849 deg
Eccentricity:
0003099
Arg of perigee: 207
4956 deg
Mean anomaly: 152
6039 deg
Mean motion: 15
65259689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 377
Coasting Arc #9 (Orbit 4069)
---------------------------------------
Vector Time (GMT): 2011/166/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6555507
91 A = 6765568
21 meter
Y = 230407
18 meter E =
0009778
Z = 1629697
18 I = 51
73437
XDOT = 1252
680770 Wp = 13
67236
YDOT = -4949
958839 meter/sec RA = 166
68570 deg
ZDOT = 5741
060789 TA = 4
21198
MA = 4
20375
Ha = 207
802 n
mi
Hp = 205
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21507571
90 X = -6565513
90
Y = 755929
08 feet Y = 157043
24 meter
Z = 5346775
53 Z = 1597826
34
XDOT = 4109
845047 XDOT = 1280
050100
YDOT = -16240
022437 feet/sec YDOT = -4935
798724 meter/sec
ZDOT = 18835
501275 ZDOT = 5747
211785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20634139
30 X = 6289285
66
Y = -6224530
91 feet Y = -1897237
02 meter
Z = 5217527
84 Z = 1590302
48
XDOT = -176
830989 XDOT = -53
898086
YDOT = 15216
730616 feet/sec YDOT = 4638
059492 meter/sec
ZDOT = 18860
631437 ZDOT = 5748
720462
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 11166
87152924
00016717 00000-0 10270-3 0 9088
2 25544 51
6421 167
4160 0010688 287
4137 72
5851 15
61963750 40703
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
87152924 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 167
4160 deg
Eccentricity:
0010688
Arg of perigee: 287
4137 deg
Mean anomaly: 72
5851 deg
Mean motion: 15
61963750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4070
Checksum: 315
Coasting Arc #10 (Orbit 4084)
---------------------------------------
Vector Time (GMT): 2011/167/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3933321
03 A = 6756753
99 meter
Y = 2682789
11 meter E =
0007479
Z = -4797995
84 I = 51
73471
XDOT = -5951
497200 Wp = 5
96494
YDOT = 4111
807619 meter/sec RA = 161
65303 deg
ZDOT = -2572
917937 TA = 238
73275
MA = 238
80602
Ha = 207
985 n
mi
Hp = 204
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12904596
56 X = 3926336
85
Y = 8801801
55 feet Y = 2726735
79 meter
Z = -15741456
17 Z = -4778904
35
XDOT = -19525
909450 XDOT = -5984
535222
YDOT = 13490
182477 feet/sec YDOT = 4045
070142 meter/sec
ZDOT = -8441
331815 ZDOT = -2601
909540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14900779
34 X = -4541757
54
Y = -4939190
61 feet Y = -1505465
30 meter
Z = -15664128
96 Z = -4774426
51
XDOT = 14718
194137 XDOT = 4486
105573
YDOT = -17186
005283 feet/sec YDOT = -5238
294410 meter/sec
ZDOT = -8559
070690 ZDOT = -2608
804746
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 11167
83120408
00016717 00000-0 10270-3 0 9098
2 25544 51
6424 162
5753 0010798 290
9247 69
0754 15
62011061 40852
Satellite: ISS
Catalog Number: 25544
Epoch time: 11167
83120408 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 162
5753 deg
Eccentricity:
0010798
Arg of perigee: 290
9247 deg
Mean anomaly: 69
0754 deg
Mean motion: 15
62011061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4085
Checksum: 304
Coasting Arc #11 (Orbit 4100)
---------------------------------------
Vector Time (GMT): 2011/168/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 755013
26 A = 6755963
45 meter
Y = -4562325
70 meter E =
0009137
Z = 4931832
64 I = 51
76152
XDOT = 7241
969599 Wp = 330
77914
YDOT = -1220
508800 meter/sec RA = 156
57926 deg
ZDOT = -2231
679470 TA = 140
97992
MA = 140
91397
Ha = 208
125 n
mi
Hp = 204
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2477077
62 X = 782016
27
Y = -14968260
18 feet Y = -4553732
61 meter
Z = 16180553
28 Z = 4935565
21
XDOT = 23759
742780 XDOT = 7265
920293
YDOT = -4004
293964 feet/sec YDOT = -1139
390374 meter/sec
ZDOT = -7321
783039 ZDOT = -2196
440425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2033903
40 X = 619933
76
Y = 15018392
25 feet Y = 4577605
96 meter
Z = 16195868
67 Z = 4936500
77
XDOT = -20544
592955 XDOT = -6261
991933
YDOT = 10545
342604 feet/sec YDOT = 3214
220426 meter/sec
ZDOT = -7178
795786 ZDOT = -2188
096956
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 11168
85484499
00016717 00000-0 10270-3 0 9106
2 25544 51
6429 157
4113 0010877 294
6142 65
3881 15
62054067 41015
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
85484499 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 157
4113 deg
Eccentricity:
0010877
Arg of perigee: 294
6142 deg
Mean anomaly: 65
3881 deg
Mean motion: 15
62054067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4101
Checksum: 315
Coasting Arc #12 (Orbit 4115)
---------------------------------------
Vector Time (GMT): 2011/169/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4813878
71 A = 6764818
73 meter
Y = 4332409
26 meter E =
0011714
Z = -1926860
03 I = 51
81825
XDOT = -4561
066340 Wp = 333
96071
YDOT = -2563
202948 meter/sec RA = 151
54444 deg
ZDOT = 5629
119630 TA = 4
76798
MA = 4
75683
Ha = 208
404 n
mi
Hp = 204
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15793565
32 X = -4852606
56
Y = 14213941
15 feet Y = 4278361
32 meter
Z = -6321719
24 Z = -1950338
90
XDOT = -14964
128413 XDOT = -4559
409994
YDOT = -8409
458490 feet/sec YDOT = -2614
199221 meter/sec
ZDOT = 18468
240255 ZDOT = 5606
965869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10677604
96 X = 3254533
99
Y = -18337014
18 feet Y = -5589121
92 meter
Z = -6417135
33 Z = -1955942
85
XDOT = 15582
415524 XDOT = 4749
520252
YDOT = 2639
002250 feet/sec YDOT = 804
367886 meter/sec
ZDOT = 18378
464528 ZDOT = 5601
755988
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 11169
81449816
00016717 00000-0 10270-3 0 9118
2 25544 51
6428 152
5697 0010906 298
4020 61
6037 15
62030128 41167
Satellite: ISS
Catalog Number: 25544
Epoch time: 11169
81449816 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 152
5697 deg
Eccentricity:
0010906
Arg of perigee: 298
4020 deg
Mean anomaly: 61
6037 deg
Mean motion: 15
62030128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4116
Checksum: 299
Coasting Arc #13 (Orbit 4131)
---------------------------------------
Vector Time (GMT): 2011/170/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6083387
95 A = 6764239
39 meter
Y = -1840606
19 meter E =
0005406
Z = -2313106
97 I = 51
84204
XDOT = -435
428442 Wp = 285
29372
YDOT = 5405
294353 meter/sec RA = 146
54989 deg
ZDOT = -5434
377951 TA = 280
48752
MA = 280
54843
Ha = 208
616 n
mi
Hp = 204
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19958621
89 X = 6114754
33
Y = -6038734
22 feet Y = -1772402
34 meter
Z = -7588933
63 Z = -2283478
34
XDOT = -1428
571004 XDOT = -469
440263
YDOT = 17733
905357 feet/sec YDOT = 5400
235725 meter/sec
ZDOT = -17829
323987 ZDOT = -5436
575083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17007739
98 X = -5183959
14
Y = 12139227
36 feet Y = 3700036
50 meter
Z = -7468651
31 Z = -2276444
92
XDOT = -3554
024312 XDOT = -1083
266610
YDOT = -15978
953508 feet/sec YDOT = -4870
385029 meter/sec
ZDOT = -17838
446262 ZDOT = -5437
158421
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 11170
83811469
00016717 00000-0 10270-3 0 9120
2 25544 51
6426 147
4063 0010905 301
2940 58
7149 15
62029812 41325
Satellite: ISS
Catalog Number: 25544
Epoch time: 11170
83811469 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 147
4063 deg
Eccentricity:
0010905
Arg of perigee: 301
2940 deg
Mean anomaly: 58
7149 deg
Mean motion: 15
62029812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4132
Checksum: 289
Coasting Arc #14 (Orbit 4147)
---------------------------------------
Vector Time (GMT): 2011/171/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4027679
46 A = 6755436
99 meter
Y = -1900389
84 meter E =
0005442
Z = 5082440
44 I = 51
83738
XDOT = 4886
774572 Wp = 307
37334
YDOT = -5655
044760 meter/sec RA = 141
51252 deg
ZDOT = 1762
640990 TA = 125
67788
MA = 125
62722
Ha = 208
916 n
mi
Hp = 204
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13214171
45 X = -4030818
86
Y = -6234874
81 feet Y = -1945447
98 meter
Z = 16674673
37 Z = 5062866
36
XDOT = 16032
724975 XDOT = 4941
084691
YDOT = -18553
296458 feet/sec YDOT = -5600
094427 meter/sec
ZDOT = 5782
942882 ZDOT = 1786
511881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14636372
52 X = 4461166
34
Y = 1380073
64 feet Y = 420646
45 meter
Z = 16595322
21 Z = 5058254
21
XDOT = -8705
028943 XDOT = -2653
292822
YDOT = 21793
169267 feet/sec YDOT = 6642
557993 meter/sec
ZDOT = 5880
021760 ZDOT = 1792
230633
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 11171
86171802
00016717 00000-0 10270-3 0 9135
2 25544 51
6426 142
2415 0010836 306
1493 53
8660 15
62051002 41486
Satellite: ISS
Catalog Number: 25544
Epoch time: 11171
86171802 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 142
2415 deg
Eccentricity:
0010836
Arg of perigee: 306
1493 deg
Mean anomaly: 53
8660 deg
Mean motion: 15
62051002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4148
Checksum: 275
Coasting Arc #15 (Orbit 4162)
---------------------------------------
Vector Time (GMT): 2011/172/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 25315
20 A = 6757190
38 meter
Y = 4953610
06 meter E =
0003569
Z = -4595080
20 I = 51
86593
XDOT = -6454
937930 Wp = 19
63459
YDOT = 2846
881382 meter/sec RA = 136
44547 deg
ZDOT = 3037
410180 TA = 280
52748
MA = 280
56769
Ha = 208
975 n
mi
Hp = 203
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 83055
11 X = -7757
05
Y = 16252001
50 feet Y = 4953708
73 meter
Z = -15075722
45 Z = -4595037
01
XDOT = -21177
617879 XDOT = -6501
047606
YDOT = 9340
162015 feet/sec YDOT = 2774
440197 meter/sec
ZDOT = 9965
256495 ZDOT = 3005
940701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5904038
04 X = -1799550
79
Y = -15141869
09 feet Y = -4615241
70 meter
Z = -15075741
89 Z = -4595086
13
XDOT = 15463
217891 XDOT = 4713
188813
YDOT = -15810
871422 feet/sec YDOT = -4819
153609 meter/sec
ZDOT = 9837
442383 ZDOT = 2998
452438
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 11172
82133197
00016717 00000-0 10270-3 0 9148
2 25544 51
6415 137
3993 0010933 309
0903 50
9281 15
62104565 41633
Satellite: ISS
Catalog Number: 25544
Epoch time: 11172
82133197 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 137
3993 deg
Eccentricity:
0010933
Arg of perigee: 309
0903 deg
Mean anomaly: 50
9281 deg
Mean motion: 15
62104565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4163
Checksum: 295
Coasting Arc #16 (Orbit 4178)
---------------------------------------
Vector Time (GMT): 2011/173/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3697250
67 A = 6765572
37 meter
Y = -5548094
14 meter E =
0003641
Z = 1147241
81 I = 51
91563
XDOT = 4562
501459 Wp = 87
54994
YDOT = 1817
175024 meter/sec RA = 131
42927 deg
ZDOT = -5899
571241 TA = 80
00814
MA = 79
96705
Ha = 209
133 n
mi
Hp = 203
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12130087
51 X = 3753442
69
Y = -18202408
60 feet Y = -5506435
17 meter
Z = 3763916
69 Z = 1165338
85
XDOT = 14968
836807 XDOT = 4570
501226
YDOT = 5961
860315 feet/sec YDOT = 1868
241040 meter/sec
ZDOT = -19355
548692 ZDOT = -5877
387125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4528310
30 X = -1380228
98
Y = 21386938
59 feet Y = 6518738
88 meter
Z = 3837581
84 Z = 1169694
94
XDOT = -14660
273952 XDOT = -4468
451501
YDOT = 362
250551 feet/sec YDOT = 110
413968 meter/sec
ZDOT = -19265
592977 ZDOT = -5872
152739
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 11173
84490790
00016717 00000-0 10270-3 0 9157
2 25544 51
6417 132
2358 0010979 313
3220 46
7021 15
62132745 41797
Satellite: ISS
Catalog Number: 25544
Epoch time: 11173
84490790 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 132
2358 deg
Eccentricity:
0010979
Arg of perigee: 313
3220 deg
Mean anomaly: 46
7021 deg
Mean motion: 15
62132745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4179
Checksum: 298
Coasting Arc #17 (Orbit 4194)
---------------------------------------
Vector Time (GMT): 2011/174/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5208256
81 A = 6762211
65 meter
Y = 3038064
23 meter E =
0010834
Z = 3045163
98 I = 51
92240
XDOT = -512
516081 Wp = 30
32089
YDOT = -5848
767143 meter/sec RA = 126
43577 deg
ZDOT = 4960
040855 TA = 4
61710
MA = 4
60711
Ha = 209
348 n
mi
Hp = 203
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17087456
74 X = -5256634
75
Y = 9967402
33 feet Y = 2979551
51 meter
Z = 9990695
47 Z = 3019745
17
XDOT = -1681
483206 XDOT = -471
170851
YDOT = -19188
868580 feet/sec YDOT = -5854
267778 meter/sec
ZDOT = 16273
099917 ZDOT = 4957
650847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11983053
67 X = 3652434
76
Y = -15804742
42 feet Y = -4817285
49 meter
Z = 9887407
39 Z = 3013681
77
XDOT = 7882
011503 XDOT = 2402
437106
YDOT = 16147
503716 feet/sec YDOT = 4921
759133 meter/sec
ZDOT = 16263
641975 ZDOT = 4957
158074
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 11174
86846927
00016717 00000-0 10270-3 0 9168
2 25544 51
6405 127
0700 0010985 316
0587 43
9696 15
62152216 41950
Satellite: ISS
Catalog Number: 25544
Epoch time: 11174
86846927 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 127
0700 deg
Eccentricity:
0010985
Arg of perigee: 316
0587 deg
Mean anomaly: 43
9696 deg
Mean motion: 15
62152216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4195
Checksum: 322
Coasting Arc #18 (Orbit 4209)
---------------------------------------
Vector Time (GMT): 2011/175/19:27:20
061
Vector Time (MET): N/A
Weight (LBS) : 913605
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4001274
36 A = 6754298
86 meter
Y = 1375941
61 meter E =
0012494
Z = -5272366
60 I = 51
91190
XDOT = -3421
778093 Wp = 37
36511
YDOT = 6822
704266 meter/sec RA = 121
39206 deg
ZDOT = -807
612673 TA = 224
90144
MA = 225
00257
Ha = 209
469 n
mi
Hp = 203
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13127540
56 X = 4011203
12
Y = 4514244
14 feet Y = 1420742
44 meter
Z = -17297790
68 Z = -5252904
13
XDOT = -11226
306079 XDOT = -3493
893339
YDOT = 22384
200347 feet/sec YDOT = 6784
036741 meter/sec
ZDOT = -2649
647876 ZDOT = -824
410021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13930563
98 X = -4246035
90
Y = 1172460
42 feet Y = 357365
93 meter
Z = -17218856
16 Z = -5248307
36
XDOT = 1376
414451 XDOT = 419
531125
YDOT = -23985
134834 feet/sec YDOT = -7310
669097 meter/sec
ZDOT = -2718
116781 ZDOT = -828
481995
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 11175
82804657
00016717 00000-0 10270-3 0 9170
2 25544 51
6393 122
2277 0010849 320
2029 39
8331 15
62159569 42105
Satellite: ISS
Catalog Number: 25544
Epoch time: 11175
82804657 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 122
2277 deg
Eccentricity:
0010849
Arg of perigee: 320
2029 deg
Mean anomaly: 39
8331 deg
Mean motion: 15
62159569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4210
Checksum: 309
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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