[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 18th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 35520 9 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
There are no maneuvers
Coasting Arc #1 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2013/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3159942
30 A = 6791888
07 meter
Y = 3492590
81 meter E =
0004281
Z = 4894305
89 I = 51
29072
XDOT = -3521
780809 Wp = 10
99281
YDOT = 6404
734243 meter/sec RA = 284
24898 deg
ZDOT = -2292
187927 TA = 101
58026
MA = 101
53219
Ha = 226
075 n
mi
Hp = 223
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10367264
77 X = 3096877
22
Y = 11458631
27 feet Y = 3527574
17 meter
Z = 16057434
04 Z = 4909503
86
XDOT = -11554
398979 XDOT = -3582
003348
YDOT = 21012
907622 feet/sec YDOT = 6365
014964 meter/sec
ZDOT = -7520
301599 ZDOT = -2309
442099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12395838
61 X = -3778251
61
Y = 9115138
24 feet Y = 2778294
14 meter
Z = 16120764
16 Z = 4913608
92
XDOT = -19141
182136 XDOT = -5834
232315
YDOT = -12574
250413 feet/sec YDOT = -3832
631526 meter/sec
ZDOT = -7593
937391 ZDOT = -2314
632117
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 13350
54431474
00016717 00000-0 10270-3 0 9001
2 25544 51
6498 284
7934 0004935 278
5495 81
5096 15
49755134 22998
Satellite: ISS
Catalog Number: 25544
Epoch time: 13350
54431474 = yrday
fracday
Element set: 900
Inclination: 51
6498 deg
RA of node: 284
7934 deg
Eccentricity:
0004935
Arg of perigee: 278
5495 deg
Mean anomaly: 81
5096 deg
Mean motion: 15
49755134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 343
Coasting Arc #2 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2013/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3317426
83 A = 6792199
57 meter
Y = -3501396
71 meter E =
0006447
Z = -4788351
72 I = 51
28560
XDOT = 3144
822707 Wp = 112
79823
YDOT = -6490
522112 meter/sec RA = 279
27075 deg
ZDOT = 2567
632938 TA = 182
65716
MA = 182
66059
Ha = 226
129 n
mi
Hp = 223
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10883946
29 X = -3254766
35
Y = -11487522
00 feet Y = -3538143
41 meter
Z = -15709815
34 Z = -4804315
66
XDOT = 10317
659801 XDOT = 3204
694564
YDOT = -21294
363883 feet/sec YDOT = -6455
020216 meter/sec
ZDOT = 8423
992579 ZDOT = 2583
054937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12307079
57 X = 3751197
85
Y = -9841929
16 feet Y = -2999820
01 meter
Z = -15776373
78 Z = -4808638
73
XDOT = 19695
995609 XDOT = 6003
339462
YDOT = 11021
881370 feet/sec YDOT = 3359
469442 meter/sec
ZDOT = 8489
933156 ZDOT = 2587
731626
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 13351
51155360
00016717 00000-0 10270-3 0 9017
2 25544 51
6499 280
0032 0004975 282
3253 77
7334 15
49799907 23142
Satellite: ISS
Catalog Number: 25544
Epoch time: 13351
51155360 = yrday
fracday
Element set: 901
Inclination: 51
6499 deg
RA of node: 280
0032 deg
Eccentricity:
0004975
Arg of perigee: 282
3253 deg
Mean anomaly: 77
7334 deg
Mean motion: 15
49799907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2314
Checksum: 313
Coasting Arc #3 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2013/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3476395
49 A = 6792619
81 meter
Y = 3521554
20 meter E =
0005491
Z = 4653372
37 I = 51
28338
XDOT = -2788
336199 Wp = 27
59404
YDOT = 6537
347488 meter/sec RA = 274
29329 deg
ZDOT = -2858
077058 TA = 91
00423
MA = 90
94132
Ha = 226
143 n
mi
Hp = 223
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11405497
03 X = 3414153
57
Y = 11553655
52 feet Y = 3560080
97 meter
Z = 15266969
72 Z = 4670109
53
XDOT = -9148
084641 XDOT = -2847
347311
YDOT = 21447
990447 feet/sec YDOT = 6505
836888 meter/sec
ZDOT = -9376
893236 ZDOT = -2871
765151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12234465
28 X = -3729065
02
Y = 10571353
59 feet Y = 3222148
57 meter
Z = 15336786
67 Z = 4674652
58
XDOT = -20071
001953 XDOT = -6117
641395
YDOT = -9510
567351 feet/sec YDOT = -2898
820929 meter/sec
ZDOT = -9435
543010 ZDOT = -2875
953509
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 13352
54324960
00016717 00000-0 10270-3 0 9026
2 25544 51
6500 274
8948 0004943 285
8185 74
2420 15
49835538 23306
Satellite: ISS
Catalog Number: 25544
Epoch time: 13352
54324960 = yrday
fracday
Element set: 902
Inclination: 51
6500 deg
RA of node: 274
8948 deg
Eccentricity:
0004943
Arg of perigee: 285
8185 deg
Mean anomaly: 74
2420 deg
Mean motion: 15
49835538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 316
Coasting Arc #4 (Orbit 2344)
---------------------------------------
Vector Time (GMT): 2013/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3657350
57 A = 6793044
69 meter
Y = -3532274
84 meter E =
0004725
Z = -4509452
32 I = 51
28405
XDOT = 2441
901899 Wp = 111
22297
YDOT = -6540
460174 meter/sec RA = 269
31426 deg
ZDOT = 3143
686354 TA = 190
52245
MA = 190
53235
Ha = 226
194 n
mi
Hp = 222
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11999181
67 X = -3595674
50
Y = -11588828
22 feet Y = -3572828
38 meter
Z = -14794791
07 Z = -4527069
83
XDOT = 8011
489169 XDOT = 2499
586202
YDOT = -21458
202672 feet/sec YDOT = -6512
831045 meter/sec
ZDOT = 10313
931607 ZDOT = 3155
688302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12112681
48 X = 3691945
31
Y = -11374671
22 feet Y = -3466999
79 meter
Z = -14868320
18 Z = -4531863
99
XDOT = 20249
665938 XDOT = 6172
098178
YDOT = 8018
587997 feet/sec YDOT = 2444
065622 meter/sec
ZDOT = 10365
481914 ZDOT = 3159
398888
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 13353
51043936
00016717 00000-0 10270-3 0 9036
2 25544 51
6502 270
1043 0004969 289
5391 70
5222 15
49882292 23455
Satellite: ISS
Catalog Number: 25544
Epoch time: 13353
51043936 = yrday
fracday
Element set: 903
Inclination: 51
6502 deg
RA of node: 270
1043 deg
Eccentricity:
0004969
Arg of perigee: 289
5391 deg
Mean anomaly: 70
5222 deg
Mean motion: 15
49882292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2345
Checksum: 305
Coasting Arc #5 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2013/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3841410
63 A = 6793606
42 meter
Y = 3553112
44 meter E =
0006740
Z = 4331763
43 I = 51
28710
XDOT = -2126
877501 Wp = 42
42124
YDOT = 6504
999340 meter/sec RA = 264
33623 deg
ZDOT = -3441
553341 TA = 82
77006
MA = 82
69345
Ha = 226
270 n
mi
Hp = 223
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12603053
26 X = 3780351
07
Y = 11657193
03 feet Y = 3595727
77 meter
Z = 14211822
26 Z = 4350276
50
XDOT = -6977
944557 XDOT = -2182
741772
YDOT = 21341
861351 feet/sec YDOT = 6480
903176 meter/sec
ZDOT = -11291
185502 ZDOT = -3452
020581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12000334
01 X = -3657701
81
Y = 12186707
11 feet Y = 3714508
33 meter
Z = 14289126
86 Z = 4355325
87
XDOT = -20252
856249 XDOT = -6173
070585
YDOT = -6620
429852 feet/sec YDOT = -2017
907019 meter/sec
ZDOT = -11336
265163 ZDOT = -3455
293622
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 13354
54208319
00016717 00000-0 10270-3 0 9049
2 25544 51
6498 264
9953 0004958 293
1788 66
8840 15
49914332 23612
Satellite: ISS
Catalog Number: 25544
Epoch time: 13354
54208319 = yrday
fracday
Element set: 904
Inclination: 51
6498 deg
RA of node: 264
9953 deg
Eccentricity:
0004958
Arg of perigee: 293
1788 deg
Mean anomaly: 66
8840 deg
Mean motion: 15
49914332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 345
Coasting Arc #6 (Orbit 2375)
---------------------------------------
Vector Time (GMT): 2013/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4047089
71 A = 6794139
37 meter
Y = -3553193
02 meter E =
0002814
Z = -4144664
03 I = 51
29371
XDOT = 1831
312047 Wp = 96
58424
YDOT = -6433
018333 meter/sec RA = 259
35724 deg
ZDOT = 3728
658204 TA = 212
01328
MA = 212
03038
Ha = 226
296 n
mi
Hp = 222
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13277853
38 X = -3986922
85
Y = -11657457
41 feet Y = -3598113
45 meter
Z = -13597979
10 Z = -4164178
36
XDOT = 6008
241623 XDOT = 1884
998727
YDOT = -21105
703191 feet/sec YDOT = -6412
239516 meter/sec
ZDOT = 12233
130590 ZDOT = 3737
684426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11796255
44 X = 3595498
66
Y = -13069895
36 feet Y = -3983704
11 meter
Z = -13679507
74 Z = -4169513
96
XDOT = 20088
260883 XDOT = 6122
901917
YDOT = 5292
557605 feet/sec YDOT = 1613
171558 meter/sec
ZDOT = 12272
126682 ZDOT = 3740
544213
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 13355
50922457
00016717 00000-0 10270-3 0 9053
2 25544 51
6502 260
2044 0005008 296
7397 63
3241 15
49961270 23766
Satellite: ISS
Catalog Number: 25544
Epoch time: 13355
50922457 = yrday
fracday
Element set: 905
Inclination: 51
6502 deg
RA of node: 260
2044 deg
Eccentricity:
0005008
Arg of perigee: 296
7397 deg
Mean anomaly: 63
3241 deg
Mean motion: 15
49961270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2376
Checksum: 303
Coasting Arc #7 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2013/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4255672
47 A = 6794815
58 meter
Y = 3561024
58 meter E =
0007928
Z = 3919225
97 I = 51
30229
XDOT = -1578
115083 Wp = 56
15840
YDOT = 6325
163768 meter/sec RA = 254
37946 deg
ZDOT = -4023
259592 TA = 76
17900
MA = 76
09079
Ha = 226
421 n
mi
Hp = 222
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13962180
03 X = 4196497
64
Y = 11683151
52 feet Y = 3608283
14 meter
Z = 12858352
92 Z = 3939755
93
XDOT = -5177
542923 XDOT = -1629
183441
YDOT = 20751
849634 feet/sec YDOT = 6307
230965 meter/sec
ZDOT = -13199
670579 ZDOT = -4031
049557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11590691
12 X = -3532842
65
Y = 13959950
32 feet Y = 4254992
86 meter
Z = 12944164
97 Z = 3945381
48
XDOT = -19766
531661 XDOT = -6024
838850
YDOT = -4110
384047 feet/sec YDOT = -1252
845058 meter/sec
ZDOT = -13233
438518 ZDOT = -4033
552060
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 13356
54081759
00016717 00000-0 10270-3 0 9060
2 25544 51
6496 255
0947 0005002 300
6233 59
4424 15
49991998 23927
Satellite: ISS
Catalog Number: 25544
Epoch time: 13356
54081759 = yrday
fracday
Element set: 906
Inclination: 51
6496 deg
RA of node: 255
0947 deg
Eccentricity:
0005002
Arg of perigee: 300
6233 deg
Mean anomaly: 59
4424 deg
Mean motion: 15
49991998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 331
Coasting Arc #8 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2013/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4481599
83 A = 6795438
25 meter
Y = -3537191
45 meter E =
0002219
Z = -3684912
69 I = 51
31453
XDOT = 1352
451640 Wp = 37
76322
YDOT = -6191
198220 meter/sec RA = 249
40146 deg
ZDOT = 4301
251420 TA = 278
23297
MA = 278
25814
Ha = 226
423 n
mi
Hp = 222
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14703411
51 X = -4423812
91
Y = -11604958
82 feet Y = -3586984
29 meter
Z = -12089608
55 Z = -3706543
53
XDOT = 4437
177298 XDOT = 1400
688313
YDOT = -20312
330118 feet/sec YDOT = -6175
804727 meter/sec
ZDOT = 14111
717257 ZDOT = 4307
938352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11252766
39 X = 3429843
20
Y = -14901181
80 feet Y = -4541880
21 meter
Z = -12180067
47 Z = -3712484
57
XDOT = 19322
749450 XDOT = 5889
574032
YDOT = 3041
459671 feet/sec YDOT = 927
036908 meter/sec
ZDOT = 14140
814027 ZDOT = 4310
120115
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 13357
50791171
00016717 00000-0 10270-3 0 9074
2 25544 51
6501 250
3033 0005118 303
8717 56
1947 15
50035498 24075
Satellite: ISS
Catalog Number: 25544
Epoch time: 13357
50791171 = yrday
fracday
Element set: 907
Inclination: 51
6501 deg
RA of node: 250
3033 deg
Eccentricity:
0005118
Arg of perigee: 303
8717 deg
Mean anomaly: 56
1947 deg
Mean motion: 15
50035498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 293
Coasting Arc #9 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2013/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4707934
16 A = 6796176
27 meter
Y = 3518485
83 meter E =
0008929
Z = 3408298
11 I = 51
32870
XDOT = -1179
201251 Wp = 69
17565
YDOT = 6026
647567 meter/sec RA = 244
42508 deg
ZDOT = -4579
758670 TA = 70
84375
MA = 70
74711
Ha = 226
581 n
mi
Hp = 222
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15445978
22 X = 4651683
26
Y = 11543588
67 feet Y = 3570818
31 meter
Z = 11182080
42 Z = 3431032
22
XDOT = -3868
770510 XDOT = -1224
257807
YDOT = 19772
465771 feet/sec YDOT = 6013
209228 meter/sec
ZDOT = -15025
454954 ZDOT = -4585
596315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10902625
83 X = -3323120
35
Y = 15837589
02 feet Y = 4827297
13 meter
Z = 11277195
08 Z = 3437289
06
XDOT = -18754
791458 XDOT = -5716
460436
YDOT = -2163
941288 feet/sec YDOT = -659
569305 meter/sec
ZDOT = -15050
944738 ZDOT = -4587
527956
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 13358
53945533
00016717 00000-0 10270-3 0 9082
2 25544 51
6498 245
1931 0005088 308
0463 52
0228 15
50068040 24234
Satellite: ISS
Catalog Number: 25544
Epoch time: 13358
53945533 = yrday
fracday
Element set: 908
Inclination: 51
6498 deg
RA of node: 245
1931 deg
Eccentricity:
0005088
Arg of perigee: 308
0463 deg
Mean anomaly: 52
0228 deg
Mean motion: 15
50068040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 300
Coasting Arc #10 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2013/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4943603
54 A = 6796848
66 meter
Y = -3458985
32 meter E =
0004476
Z = -3124504
92 I = 51
34582
XDOT = 1039
223957 Wp = 5
74335
YDOT = -5849
351594 meter/sec RA = 239
44903 deg
ZDOT = 4836
235044 TA = 318
18105
MA = 318
21524
Ha = 226
574 n
mi
Hp = 222
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16219171
71 X = -4889379
01
Y = -11348377
05 feet Y = -3513964
56 meter
Z = -10251000
39 Z = -3148388
85
XDOT = 3409
527418 XDOT = 1081
062404
YDOT = -19190
786069 feet/sec YDOT = -5837
496563 meter/sec
ZDOT = 15866
912873 ZDOT = 4841
384911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10388218
39 X = 3166328
97
Y = -16789058
39 feet Y = -5117305
00 meter
Z = -10350972
83 Z = -3154976
52
XDOT = 18125
524219 XDOT = 5524
659782
YDOT = 1428
760491 feet/sec YDOT = 435
486198 meter/sec
ZDOT = 15889
475126 ZDOT = 4843
112018
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 13359
50650350
00016717 00000-0 10270-3 0 9091
2 25544 51
6502 240
4013 0005276 310
8832 49
1861 15
50104754 24388
Satellite: ISS
Catalog Number: 25544
Epoch time: 13359
50650350 = yrday
fracday
Element set: 909
Inclination: 51
6502 deg
RA of node: 240
4013 deg
Eccentricity:
0005276
Arg of perigee: 310
8832 deg
Mean anomaly: 49
1861 deg
Mean motion: 15
50104754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 283
Coasting Arc #11 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2013/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5174774
38 A = 6797573
29 meter
Y = 3402788
12 meter E =
0009591
Z = 2795426
22 I = 51
36499
XDOT = -959
627943 Wp = 81
67175
YDOT = 5649
375504 meter/sec RA = 234
47522 deg
ZDOT = -5084
015074 TA = 66
54807
MA = 66
44727
Ha = 226
743 n
mi
Hp = 222
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16977606
23 X = 5122759
62
Y = 11164003
03 feet Y = 3460364
81 meter
Z = 9171345
88 Z = 2820438
61
XDOT = -3148
385639 XDOT = -998
032421
YDOT = 18534
696537 feet/sec YDOT = 5638
429801 meter/sec
ZDOT = -16679
839480 ZDOT = -5088
769921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9856213
72 X = -3004173
94
Y = 17714314
69 feet Y = 5399323
12 meter
Z = 9276085
84 Z = 2827350
96
XDOT = -17418
421796 XDOT = -5309
134963
YDOT = -918
451410 feet/sec YDOT = -279
943990 meter/sec
ZDOT = -16700
704757 ZDOT = -5090
374810
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 13360
53799901
00016717 00000-0 10270-3 0 9104
2 25544 51
6501 235
2908 0005209 315
2579 44
8151 15
50141582 24547
Satellite: ISS
Catalog Number: 25544
Epoch time: 13360
53799901 = yrday
fracday
Element set: 910
Inclination: 51
6501 deg
RA of node: 235
2908 deg
Eccentricity:
0005209
Arg of perigee: 315
2579 deg
Mean anomaly: 44
8151 deg
Mean motion: 15
50141582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 295
Coasting Arc #12 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2013/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5404177
14 A = 6798227
38 meter
Y = -3299849
77 meter E =
0007514
Z = -2462139
40 I = 51
38591
XDOT = 915
830108 Wp = 3
21098
YDOT = -5452
129446 meter/sec RA = 229
50194 deg
ZDOT = 5305
118725 TA = 329
15564
MA = 329
19977
Ha = 226
738 n
mi
Hp = 222
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17730239
96 X = -5354915
40
Y = -10826278
78 feet Y = -3360007
16 meter
Z = -8077885
19 Z = -2488272
98
XDOT = 3004
691955 XDOT = 950
958086
YDOT = -17887
563798 feet/sec YDOT = -5441
691914 meter/sec
ZDOT = 17405
245160 ZDOT = 5309
652794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9143360
15 X = 2786896
17
Y = -18606124
95 feet Y = -5671146
88 meter
Z = -8187370
14 Z = -2495510
42
XDOT = 16720
643095 XDOT = 5096
452015
YDOT = 560
699470 feet/sec YDOT = 170
901198 meter/sec
ZDOT = 17425
149221 ZDOT = 5311
185483
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 13361
50500247
00016717 00000-0 10270-3 0 9116
2 25544 51
6498 230
4988 0005436 317
7464 42
3267 15
50170771 24698
Satellite: ISS
Catalog Number: 25544
Epoch time: 13361
50500247 = yrday
fracday
Element set: 911
Inclination: 51
6498 deg
RA of node: 230
4988 deg
Eccentricity:
0005436
Arg of perigee: 317
7464 deg
Mean anomaly: 42
3267 deg
Mean motion: 15
50170771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 308
Coasting Arc #13 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2013/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5622087
43 A = 6798845
24 meter
Y = 3200218
04 meter E =
0009751
Z = 2081936
74 I = 51
40897
XDOT = -936
958844 Wp = 93
62923
YDOT = 5242
358840 meter/sec RA = 224
53151 deg
ZDOT = -5506
266748 TA = 63
29501
MA = 63
19522
Ha = 226
896 n
mi
Hp = 221
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18445168
75 X = 5575770
53
Y = 10499403
01 feet Y = 3262828
68 meter
Z = 6830501
10 Z = 2109136
12
XDOT = -3074
011954 XDOT = -968
762418
YDOT = 17199
340025 feet/sec YDOT = 5231
703737 meter/sec
ZDOT = -18065
179620 ZDOT = -5510
895296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8417664
11 X = -2565704
02
Y = 19443104
64 feet Y = 5926258
29 meter
Z = 6944499
40 Z = 2116683
42
XDOT = -16001
073771 XDOT = -4877
127286
YDOT = -442
798106 feet/sec YDOT = -134
964863 meter/sec
ZDOT = -18085
449151 ZDOT = -5512
444901
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 13362
53645070
00016717 00000-0 10270-3 0 9125
2 25544 51
6497 225
3881 0005352 322
1112 37
9662 15
50213256 24852
Satellite: ISS
Catalog Number: 25544
Epoch time: 13362
53645070 = yrday
fracday
Element set: 912
Inclination: 51
6497 deg
RA of node: 225
3881 deg
Eccentricity:
0005352
Arg of perigee: 322
1112 deg
Mean anomaly: 37
9662 deg
Mean motion: 15
50213256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 291
Coasting Arc #14 (Orbit 2499)
---------------------------------------
Vector Time (GMT): 2013/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5825147
94 A = 6799390
15 meter
Y = -3052281
85 meter E =
0010541
Z = -1701783
15 I = 51
43256
XDOT = 992
666774 Wp = 8
25729
YDOT = -5051
565349 meter/sec RA = 219
56142 deg
ZDOT = 5677
112354 TA = 333
05502
MA = 333
10972
Ha = 226
900 n
mi
Hp = 221
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19111377
75 X = -5782316
90
Y = -10014048
06 feet Y = -3117182
73 meter
Z = -5583278
04 Z = -1729977
46
XDOT = 3256
780753 XDOT = 1021
502836
YDOT = -16573
377128 feet/sec YDOT = -5040
304012 meter/sec
ZDOT = 18625
696700 ZDOT = 5682
004215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7514975
71 X = 2290564
60
Y = -20192001
69 feet Y = -6154522
11 meter
Z = -5701501
54 Z = -1737817
67
XDOT = 15363
829432 XDOT = 4682
895211
YDOT = 466
028902 feet/sec YDOT = 142
045609 meter/sec
ZDOT = 18647
046463 ZDOT = 5683
619762
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 13363
50341025
00016717 00000-0 10270-3 0 9137
2 25544 51
6486 220
5956 0005554 324
4975 35
5805 15
50236474 25004
Satellite: ISS
Catalog Number: 25544
Epoch time: 13363
50341025 = yrday
fracday
Element set: 913
Inclination: 51
6486 deg
RA of node: 220
5956 deg
Eccentricity:
0005554
Arg of perigee: 324
4975 deg
Mean anomaly: 35
5805 deg
Mean motion: 15
50236474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2500
Checksum: 295
Coasting Arc #15 (Orbit 2515)
---------------------------------------
Vector Time (GMT): 2013/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6008393
53 A = 6799794
09 meter
Y = 2910344
14 meter E =
0009273
Z = 1274870
11 I = 51
45836
XDOT = -1113
049606 Wp = 104
65502
YDOT = 4859
749988 meter/sec RA = 214
59455 deg
ZDOT = -5815
109117 TA = 61
46957
MA = 61
37625
Ha = 227
035 n
mi
Hp = 221
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19712577
19 X = 5969209
90
Y = 9548373
15 feet Y = 2977314
59 meter
Z = 4182644
71 Z = 1303963
39
XDOT = -3651
737554 XDOT = -1139
061562
YDOT = 15944
061639 feet/sec YDOT = 4847
158360 meter/sec
ZDOT = -19078
441986 ZDOT = -5820
578837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6617856
60 X = -2017122
69
Y = 20854861
43 feet Y = 6356561
77 meter
Z = 4304692
16 Z = 1312070
17
XDOT = -14764
033153 XDOT = -4500
077305
YDOT = -720
255618 feet/sec YDOT = -219
533912 meter/sec
ZDOT = -19102
196602 ZDOT = -5822
349524
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 13364
53481143
00016717 00000-0 10270-3 0 9148
2 25544 51
6482 215
4845 0005499 328
7309 31
3514 15
50286241 25161
Satellite: ISS
Catalog Number: 25544
Epoch time: 13364
53481143 = yrday
fracday
Element set: 914
Inclination: 51
6482 deg
RA of node: 215
4845 deg
Eccentricity:
0005499
Arg of perigee: 328
7309 deg
Mean anomaly: 31
3514 deg
Mean motion: 15
50286241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2516
Checksum: 303
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