[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 27th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 67 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
088/02:32:13
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 213
4
093/19:42:41
776 -0
9 2
2 2
3
N/A 2
0 -0
2 228
2
000/00:05:23
552 0
2 -0
1 214
6
Coasting Arc #1 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2013/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888996
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6328760
74 A = 6794112
73 meter
Y = 1944342
70 meter E =
0025481
Z = 1477204
34 I = 51
81992
XDOT = -176
638827 Wp = 68
37175
YDOT = -5028
481869 meter/sec RA = 152
81687 deg
ZDOT = 5790
971544 TA = 307
71120
MA = 307
94192
Ha = 228
390 n
mi
Hp = 213
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20763650
71 X = -6357208
32
Y = 6379077
10 feet Y = 1873411
67 meter
Z = 4846470
94 Z = 1446390
25
XDOT = -579
523712 XDOT = -148
527269
YDOT = -16497
643928 feet/sec YDOT = -5030
299124 meter/sec
ZDOT = 18999
250471 ZDOT = 5790
182465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20260483
44 X = -6175395
35
Y = 7909785
70 feet Y = 2410902
68 meter
Z = 4717859
37 Z = 1438003
53
XDOT = -1346
155764 XDOT = -410
308277
YDOT = -14921
242930 feet/sec YDOT = -4547
994845 meter/sec
ZDOT = 18996
468756 ZDOT = 5790
123677
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 13086
56158343
00016717 00000-0 10270-3 0 9000
2 25544 51
6457 153
5573 0011854 76
2828 283
9642 15
52187117 22030
Satellite: ISS
Catalog Number: 25544
Epoch time: 13086
56158343 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 153
5573 deg
Eccentricity:
0011854
Arg of perigee: 76
2828 deg
Mean anomaly: 283
9642 deg
Mean motion: 15
52187117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 314
Coasting Arc #2 (Orbit 2217)
---------------------------------------
Vector Time (GMT): 2013/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888996
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6128230
64 A = 6792254
90 meter
Y = -1510175
18 meter E =
0015822
Z = -2520883
91 I = 51
84021
XDOT = -829
593460 Wp = 95
52647
YDOT = 5450
434564 meter/sec RA = 147
86514 deg
ZDOT = -5312
060859 TA = 112
62011
MA = 112
45268
Ha = 228
368 n
mi
Hp = 213
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20105743
57 X = 6156908
16
Y = -4954642
97 feet Y = -1441485
43 meter
Z = -8270616
51 Z = -2491043
39
XDOT = -2721
763319 XDOT = -864
674929
YDOT = 17882
003164 feet/sec YDOT = 5440
960679 meter/sec
ZDOT = -17428
021192 ZDOT = -5316
176913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19617777
79 X = 5979498
67
Y = -6780591
85 feet Y = -2066724
40 meter
Z = -8146095
84 Z = -2482930
01
XDOT = -1459
896320 XDOT = -444
976398
YDOT = 16614
511770 feet/sec YDOT = 5064
103188 meter/sec
ZDOT = -17445
732360 ZDOT = -5317
459223
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 13087
52730346
00016717 00000-0 10270-3 0 9017
2 25544 51
6449 148
7566 0011907 79
8601 280
3893 15
52225048 22187
Satellite: ISS
Catalog Number: 25544
Epoch time: 13087
52730346 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 148
7566 deg
Eccentricity:
0011907
Arg of perigee: 79
8601 deg
Mean anomaly: 280
3893 deg
Mean motion: 15
52225048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2218
Checksum: 318
Coasting Arc #3 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2013/088/02:32:13
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5301587
05 A = 6794757
15 meter
Y = 4211736
80 meter E =
0021402
Z = -496412
58 I = 51
86232
XDOT = -3285
325609 Wp = 61
91687
YDOT = -3452
146276 meter/sec RA = 144
83536 deg
ZDOT = 6004
159450 TA = 292
74897
MA = 292
97501
Ha = 228
268 n
mi
Hp = 213
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17393658
31 X = -5345878
10
Y = 13818034
13 feet Y = 4152203
41 meter
Z = -1628650
19 Z = -522275
57
XDOT = -10778
627326 XDOT = -3275
645698
YDOT = -11325
939226 feet/sec YDOT = -3488
830022 meter/sec
ZDOT = 19698
685861 ZDOT = 5988
223385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2941686
22 X = 896625
96
Y = -22010444
18 feet Y = -6708783
39 meter
Z = -1736878
62 Z = -529400
60
XDOT = 14101
466618 XDOT = 4298
127025
YDOT = 385
604710 feet/sec YDOT = 117
532315 meter/sec
ZDOT = 19632
622145 ZDOT = 5984
023230
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 13088
10672948
00016717 00000-0 10270-3 0 9026
2 25544 51
6431 145
8754 0011743 80
3078 279
9399 15
52221418 22270
Satellite: ISS
Catalog Number: 25544
Epoch time: 13088
10672948 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 145
8754 deg
Eccentricity:
0011743
Arg of perigee: 80
3078 deg
Mean anomaly: 279
9399 deg
Mean motion: 15
52221418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 320
Coasting Arc #4 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2013/089/02:32:13
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5479945
90 A = 6794594
19 meter
Y = -3960328
73 meter E =
0019997
Z = -639519
93 I = 51
88640
XDOT = 2335
884706 Wp = 110
39700
YDOT = 4173
458984 meter/sec RA = 139
88920 deg
ZDOT = -5987
118923 TA = 76
47688
MA = 76
25417
Ha = 228
277 n
mi
Hp = 213
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17978825
14 X = 5526930
51
Y = -12993204
50 feet Y = -3898785
88 meter
Z = -2098162
49 Z = -612784
04
XDOT = 7663
663733 XDOT = 2318
126730
YDOT = 13692
450736 feet/sec YDOT = 4199
480459 meter/sec
ZDOT = -19642
778619 ZDOT = -5975
814805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3575431
90 X = -1089791
64
Y = 21902846
40 feet Y = 6675987
58 meter
Z = -1986305
34 Z = -605425
87
XDOT = -13580
575815 XDOT = -4139
359508
YDOT = -3944
312004 feet/sec YDOT = -1202
226299 meter/sec
ZDOT = -19596
098405 ZDOT = -5972
890794
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 13089
13681406
00016717 00000-0 10270-3 0 9030
2 25544 51
6428 140
7543 0011810 83
8484 276
4013 15
52264233 22435
Satellite: ISS
Catalog Number: 25544
Epoch time: 13089
13681406 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 140
7543 deg
Eccentricity:
0011810
Arg of perigee: 83
8484 deg
Mean anomaly: 276
4013 deg
Mean motion: 15
52264233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 289
Coasting Arc #5 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2013/090/02:32:13
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5478469
12 A = 6793626
71 meter
Y = 3636706
66 meter E =
0025133
Z = 1669496
43 I = 51
90491
XDOT = -1474
418733 Wp = 75
15936
YDOT = -4881
585540 meter/sec RA = 134
94223 deg
ZDOT = 5729
797768 TA = 303
06203
MA = 303
30316
Ha = 228
286 n
mi
Hp = 213
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17973980
04 X = -5526838
42
Y = 11931452
30 feet Y = 3575172
64 meter
Z = 5477350
51 Z = 1642764
51
XDOT = -4837
331802 XDOT = -1447
556308
YDOT = -16015
700592 feet/sec YDOT = -4897
922807 meter/sec
ZDOT = 18798
549107 ZDOT = 5722
700705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3971296
81 X = 1210451
27
Y = -21233577
44 feet Y = -6471994
40 meter
Z = 5365526
25 Z = 1635412
40
XDOT = 13396
007838 XDOT = 4083
103189
YDOT = 7303
805051 feet/sec YDOT = 2226
199780 meter/sec
ZDOT = 18769
485489 ZDOT = 5720
939177
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 13090
16688836
00016717 00000-0 10270-3 0 9040
2 25544 51
6418 135
6325 0011808 88
4364 271
8140 15
52265563 22594
Satellite: ISS
Catalog Number: 25544
Epoch time: 13090
16688836 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 135
6325 deg
Eccentricity:
0011808
Arg of perigee: 88
4364 deg
Mean anomaly: 271
8140 deg
Mean motion: 15
52265563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 318
Coasting Arc #6 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2013/091/02:32:13
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5392739
42 A = 6791618
47 meter
Y = -3118163
47 meter E =
0016261
Z = -2714911
88 I = 51
91968
XDOT = 628
683031 Wp = 101
25502
YDOT = 5587
154158 meter/sec RA = 129
99514 deg
ZDOT = -5197
685685 TA = 109
24700
MA = 109
07101
Ha = 228
286 n
mi
Hp = 213
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17692714
62 X = 5440394
98
Y = -10230195
12 feet Y = -3057592
16 meter
Z = -8907191
22 Z = -2688598
34
XDOT = 2062
608369 XDOT = 591
408676
YDOT = 18330
558260 feet/sec YDOT = 5593
975783 meter/sec
ZDOT = -17052
774558 ZDOT = -5194
722431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4668893
56 X = -1423078
76
Y = 19945894
19 feet Y = 6079508
55 meter
Z = -8797149
34 Z = -2681371
12
XDOT = -13403
092837 XDOT = -4085
262697
YDOT = -10610
193494 feet/sec YDOT = -3233
986977 meter/sec
ZDOT = -17041
027117 ZDOT = -5194
105065
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 13091
13257291
00016717 00000-0 10270-3 0 9056
2 25544 51
6420 130
8312 0011922 91
4567 268
7950 15
52294886 22747
Satellite: ISS
Catalog Number: 25544
Epoch time: 13091
13257291 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 130
8312 deg
Eccentricity:
0011922
Arg of perigee: 91
4567 deg
Mean anomaly: 268
7950 deg
Mean motion: 15
52294886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 307
Coasting Arc #7 (Orbit 2289)
---------------------------------------
Vector Time (GMT): 2013/092/02:32:13
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5182942
23 A = 6789300
74 meter
Y = 2516352
54 meter E =
0023948
Z = 3572788
13 I = 51
93074
XDOT = 83
010642 Wp = 94
44458
YDOT = -6229
252988 meter/sec RA = 125
04514 deg
ZDOT = 4480
155408 TA = 307
57754
MA = 307
79479
Ha = 228
279 n
mi
Hp = 213
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17004403
66 X = -5228051
10
Y = 8255749
79 feet Y = 2458141
57 meter
Z = 11721745
84 Z = 3547500
11
XDOT = 272
344627 XDOT = 130
897874
YDOT = -20437
181719 feet/sec YDOT = -6228
056733 meter/sec
ZDOT = 14698
672600 ZDOT = 4480
675297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5338514
68 X = 1627179
28
Y = -18200950
28 feet Y = -5547649
65 meter
Z = 11616029
59 Z = 3540565
82
XDOT = 13701
759583 XDOT = 4176
296321
YDOT = 13459
825674 feet/sec YDOT = 4102
554865 meter/sec
ZDOT = 14701
525979 ZDOT = 4481
025118
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 13092
16262553
00016717 00000-0 10270-3 0 9068
2 25544 51
6417 125
7097 0011840 96
2915 263
9585 15
52314090 22904
Satellite: ISS
Catalog Number: 25544
Epoch time: 13092
16262553 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 125
7097 deg
Eccentricity:
0011840
Arg of perigee: 96
2915 deg
Mean anomaly: 263
9585 deg
Mean motion: 15
52314090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2290
Checksum: 306
Coasting Arc #8 (Orbit 2304)
---------------------------------------
Vector Time (GMT): 2013/093/02:32:13
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4933356
25 A = 6786716
05 meter
Y = -1722979
50 meter E =
0019897
Z = -4348186
35 I = 51
93991
XDOT = -730
478932 Wp = 87
25183
YDOT = 6754
619212 meter/sec RA = 120
09251 deg
ZDOT = -3518
277633 TA = 147
07530
MA = 146
95121
Ha = 228
266 n
mi
Hp = 213
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16185552
01 X = 4973378
60
Y = -5652819
89 feet Y = -1667588
07 meter
Z = -14265703
25 Z = -4324123
28
XDOT = -2396
584421 XDOT = -788
865422
YDOT = 22160
824186 feet/sec YDOT = 6746
123881 meter/sec
ZDOT = -11542
905621 ZDOT = -3521
968428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6455371
33 X = -1967597
18
Y = 15972254
35 feet Y = 4868343
13 meter
Z = -14165169
53 Z = -4317543
67
XDOT = -13986
988673 XDOT = -4263
234148
YDOT = -15866
301431 feet/sec YDOT = -4836
048676 meter/sec
ZDOT = -11559
047903 ZDOT = -3523
197801
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 13093
12829161
00016717 00000-0 10270-3 0 9070
2 25544 51
6426 120
9088 0012071 99
2440 261
0078 15
52324699 23053
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
12829161 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 120
9088 deg
Eccentricity:
0012071
Arg of perigee: 99
2440 deg
Mean anomaly: 261
0078 deg
Mean motion: 15
52324699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2305
Checksum: 297
Coasting Arc #9 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/093/19:45:23
552
Vector Time (MET): N/A
Weight (LBS) : 903996
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2747518
02 A = 6784760
60 meter
Y = 3505676
26 meter E =
0023521
Z = -5139125
52 I = 51
94354
XDOT = -4461
114574 Wp = 102
26790
YDOT = 5975
531254 meter/sec RA = 116
50641 deg
ZDOT = 1692
884975 TA = 184
05176
MA = 184
07084
Ha = 228
178 n
mi
Hp = 214
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9014166
73 X = 2733076
99
Y = 11501562
54 feet Y = 3536319
65 meter
Z = -16860648
02 Z = -5125813
68
XDOT = -14636
202671 XDOT = -4535
826229
YDOT = 19604
761333 feet/sec YDOT = 5925
226639 meter/sec
ZDOT = 5554
084564 ZDOT = 1671
031493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3489697
19 X = 1063659
70
Y = -14255484
94 feet Y = -4345071
81 meter
Z = -16805527
57 Z = -5122324
80
XDOT = 23442
776279 XDOT = 7145
358210
YDOT = -694
124175 feet/sec YDOT = -211
569048 meter/sec
ZDOT = 5462
281045 ZDOT = 1664
903262
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 13093
83644090
00016717 00000-0 10270-3 0 9085
2 25544 51
6461 117
3917 0010108 101
4369 258
7919 15
51905700 23164
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
83644090 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 117
3917 deg
Eccentricity:
0010108
Arg of perigee: 101
4369 deg
Mean anomaly: 258
7919 deg
Mean motion: 15
51905700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 303
Coasting Arc #10 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/094/19:45:23
552
Vector Time (MET): N/A
Weight (LBS) : 903996
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2331725
06 A = 6786132
85 meter
Y = -4226193
77 meter E =
0016549
Z = 4756308
10 I = 51
96111
XDOT = 4505
907185 Wp = 86
60688
YDOT = -5577
410926 meter/sec RA = 111
55315 deg
ZDOT = -2737
675388 TA = 30
37087
MA = 30
27509
Ha = 228
164 n
mi
Hp = 214
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7650016
61 X = -2307398
31
Y = -13865465
13 feet Y = -4252132
16 meter
Z = 15604685
36 Z = 4745040
30
XDOT = 14783
160057 XDOT = 4581
238920
YDOT = -18298
592276 feet/sec YDOT = -5526
602066 meter/sec
ZDOT = -8981
874632 ZDOT = -2715
602749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5945782
10 X = -1812274
38
Y = 14726543
85 feet Y = 4488650
57 meter
Z = 15558170
33 Z = 4742130
32
XDOT = -22485
171973 XDOT = -6853
480417
YDOT = 344
639089 feet/sec YDOT = 105
045994 meter/sec
ZDOT = -8889
189872 ZDOT = -2709
425073
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 13094
86674318
00016717 00000-0 10270-3 0 9096
2 25544 51
6458 112
2728 0010041 104
8183 255
4082 15
51947017 23321
Satellite: ISS
Catalog Number: 25544
Epoch time: 13094
86674318 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 112
2728 deg
Eccentricity:
0010041
Arg of perigee: 104
8183 deg
Mean anomaly: 255
4082 deg
Mean motion: 15
51947017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 301
Coasting Arc #11 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2013/095/19:45:23
552
Vector Time (MET): N/A
Weight (LBS) : 903996
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2007012
23 A = 6788120
10 meter
Y = 4910213
24 meter E =
0018098
Z = -4254274
89 I = 51
97852
XDOT = -4481
148849 Wp = 109
24851
YDOT = 5000
798624 meter/sec RA = 106
60301 deg
ZDOT = 3664
708598 TA = 198
17255
MA = 198
23731
Ha = 228
064 n
mi
Hp = 214
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6584685
81 X = 1972622
05
Y = 16109623
50 feet Y = 4932464
19 meter
Z = -13957594
77 Z = -4244609
09
XDOT = -14701
931918 XDOT = -4554
537895
YDOT = 16406
819633 feet/sec YDOT = 4950
277637 meter/sec
ZDOT = 12023
322172 ZDOT = 3642
760886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8104172
60 X = 2470151
81
Y = -15437247
07 feet Y = -4705272
91 meter
Z = -13917840
98 Z = -4242157
93
XDOT = 20938
297903 XDOT = 6381
993201
YDOT = 255
707100 feet/sec YDOT = 77
939524 meter/sec
ZDOT = 11931
214091 ZDOT = 3636
634055
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 13095
83264265
00016717 00000-0 10270-3 0 9102
2 25544 51
6463 107
4735 0010024 108
4252 251
7991 15
51938144 23474
Satellite: ISS
Catalog Number: 25544
Epoch time: 13095
83264265 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 107
4735 deg
Eccentricity:
0010024
Arg of perigee: 108
4252 deg
Mean anomaly: 251
7991 deg
Mean motion: 15
51938144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 300
Coasting Arc #12 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/096/19:45:23
552
Vector Time (MET): N/A
Weight (LBS) : 903996
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1696577
47 A = 6790331
80 meter
Y = -5518356
02 meter E =
0021706
Z = 3552995
23 I = 51
99351
XDOT = 4484
520541 Wp = 98
67117
YDOT = -4295
325924 meter/sec RA = 101
65667 deg
ZDOT = -4509
685472 TA = 39
63291
MA = 39
47446
Ha = 228
084 n
mi
Hp = 214
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5566199
05 X = -1652003
41
Y = -18104842
59 feet Y = -5537078
57 meter
Z = 11656808
51 Z = 3544862
34
XDOT = 14712
993900 XDOT = 4554
125309
YDOT = -14092
276655 feet/sec YDOT = -4244
788538 meter/sec
ZDOT = -14795
556012 ZDOT = -4487
730526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10022758
53 X = -3054936
80
Y = 16096183
19 feet Y = 4906116
63 meter
Z = 11623522
70 Z = 3542849
72
XDOT = -19167
803013 XDOT = -5842
346358
YDOT = -1269
485478 feet/sec YDOT = -386
939174 meter/sec
ZDOT = -14703
490509 ZDOT = -4481
623907
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 13096
86292478
00016717 00000-0 10270-3 0 9114
2 25544 51
6459 102
3541 0010081 111
9106 248
3118 15
51956987 23634
Satellite: ISS
Catalog Number: 25544
Epoch time: 13096
86292478 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 102
3541 deg
Eccentricity:
0010081
Arg of perigee: 111
9106 deg
Mean anomaly: 248
3118 deg
Mean motion: 15
51956987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 312
Coasting Arc #13 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2013/097/19:45:23
552
Vector Time (MET): N/A
Weight (LBS) : 903996
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1476401
30 A = 6792356
35 meter
Y = 6025780
17 meter E =
0013149
Z = -2779007
71 I = 52
00586
XDOT = -4466
515113 Wp = 97
92015
YDOT = 3465
372219 meter/sec RA = 96
71371 deg
ZDOT = 5160
220391 TA = 230
83267
MA = 230
94956
Ha = 227
923 n
mi
Hp = 214
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4843836
29 X = 1422409
72
Y = 19769619
98 feet Y = 6041987
99 meter
Z = -9117479
36 Z = -2771967
35
XDOT = -14653
920976 XDOT = -4530
000722
YDOT = 11369
331427 feet/sec YDOT = 3415
070499 meter/sec
ZDOT = 16929
856925 ZDOT = 5138
367766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11477711
41 X = 3498406
44
Y = -16825118
18 feet Y = -5128296
02 meter
Z = -9088816
91 Z = -2770271
39
XDOT = 17084
995148 XDOT = 5207
506521
YDOT = 2593
016114 feet/sec YDOT = 790
351311 meter/sec
ZDOT = 16838
307577 ZDOT = 5132
316150
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 13097
82880317
00016717 00000-0 10270-3 0 9127
2 25544 51
6461 97
5544 0009920 115
5755 244
6423 15
51972460 23783
Satellite: ISS
Catalog Number: 25544
Epoch time: 13097
82880317 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 97
5544 deg
Eccentricity:
0009920
Arg of perigee: 115
5755 deg
Mean anomaly: 244
6423 deg
Mean motion: 15
51972460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 324
Coasting Arc #14 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2013/098/19:49:23
552
Vector Time (MET): N/A
Weight (LBS) : 903996
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -126117
22 A = 6795612
53 meter
Y = -6770735
80 meter E =
0022792
Z = 429771
82 I = 52
01889
XDOT = 4721
467892 Wp = 125
88586
YDOT = -483
701531 meter/sec RA = 91
77304 deg
ZDOT = -6025
246970 TA = 49
50520
MA = 49
30680
Ha = 227
979 n
mi
Hp = 214
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -413770
40 X = -52483
76
Y = -22213700
15 feet Y = -6771734
37 meter
Z = 1410012
53 Z = 429338
82
XDOT = 15490
380224 XDOT = 4755
795076
YDOT = -1586
947281 feet/sec YDOT = -430
711899 meter/sec
ZDOT = -19767
870638 ZDOT = -6002
226898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15749661
00 X = -4800496
67
Y = 15670695
33 feet Y = 4776427
94 meter
Z = 1409007
37 Z = 429465
44
XDOT = -10803
507272 XDOT = -3292
909017
YDOT = -9027
315031 feet/sec YDOT = -2751
525622 meter/sec
ZDOT = -19671
798282 ZDOT = -5995
964116
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 13098
85906443
00016717 00000-0 10270-3 0 9131
2 25544 51
6460 92
4346 0010044 120
3256 239
8890 15
51944755 23943
Satellite: ISS
Catalog Number: 25544
Epoch time: 13098
85906443 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 92
4346 deg
Eccentricity:
0010044
Arg of perigee: 120
3256 deg
Mean anomaly: 239
8890 deg
Mean motion: 15
51944755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 318
Coasting Arc #15 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2013/099/19:49:23
552
Vector Time (MET): N/A
Weight (LBS) : 903996
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -51276
48 A = 6795329
58 meter
Y = 6770128
22 meter E =
0018521
Z = 544080
73 I = 52
01848
XDOT = -4726
818823 Wp = 81
29762
YDOT = -532
346145 meter/sec RA = 86
83659 deg
ZDOT = 6007
225221 TA = 284
53533
MA = 284
74069
Ha = 227
740 n
mi
Hp = 214
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -168229
94 X = -129620
72
Y = 22211706
76 feet Y = 6769116
83 meter
Z = 1785041
78 Z = 543640
57
XDOT = -15507
935771 XDOT = -4749
696510
YDOT = -1746
542472 feet/sec YDOT = -585
331647 meter/sec
ZDOT = 19708
744163 ZDOT = 5984
206997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15900143
52 X = 4846363
74
Y = -15510741
74 feet Y = -4727674
08 meter
Z = 1782391
53 Z = 543272
94
XDOT = 8633
233067 XDOT = 2631
409439
YDOT = 11168
466093 feet/sec YDOT = 3404
148465 meter/sec
ZDOT = 19612
800801 ZDOT = 5977
981684
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 13099
88931113
00016717 00000-0 10270-3 0 9148
2 25544 51
6457 87
3146 0009841 123
5690 236
6403 15
52023630 24105
Satellite: ISS
Catalog Number: 25544
Epoch time: 13099
88931113 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 87
3146 deg
Eccentricity:
0009841
Arg of perigee: 123
5690 deg
Mean anomaly: 236
6403 deg
Mean motion: 15
52023630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 297
Coasting Arc #16 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2013/100/19:49:23
552
Vector Time (MET): N/A
Weight (LBS) : 903996
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 303864
03 A = 6794514
43 meter
Y = -6596699
37 meter E =
0017747
Z = -1575412
79 I = 52
01263
XDOT = 4782
450199 Wp = 134
17655
YDOT = 1587
381875 meter/sec RA = 81
90024 deg
ZDOT = -5776
549834 TA = 62
94675
MA = 62
76575
Ha = 227
754 n
mi
Hp = 214
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 996929
24 X = 385260
19
Y = -21642714
46 feet Y = -6592846
41 meter
Z = -5168677
15 Z = -1573738
26
XDOT = 15690
453409 XDOT = 4792
405622
YDOT = 5207
945785 feet/sec YDOT = 1640
917333 meter/sec
ZDOT = -18951
935151 ZDOT = -5753
292777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15842445
13 X = -4828777
28
Y = 14781690
78 feet Y = 4505459
35 meter
Z = -5160884
67 Z = -1573037
65
XDOT = -6608
471437 XDOT = -2014
262094
YDOT = -13605
943830 feet/sec YDOT = -4147
091679 meter/sec
ZDOT = -18855
125983 ZDOT = -5747
042400
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 13100
85516048
00016717 00000-0 10270-3 0 9155
2 25544 51
6456 82
5149 0009830 127
8128 232
3915 15
51985864 24257
Satellite: ISS
Catalog Number: 25544
Epoch time: 13100
85516048 = yrday
fracday
Element set: 915
Inclination: 51
6456 deg
RA of node: 82
5149 deg
Eccentricity:
0009830
Arg of perigee: 127
8128 deg
Mean anomaly: 232
3915 deg
Mean motion: 15
51985864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 316
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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