[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 14th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 30138 95 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 2254)
---------------------------------------
Vector Time (GMT): 2013/347/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4722351
53 A = 6799057
13 meter
Y = -3999335
82 meter E =
0008561
Z = 2806150
36 I = 51
34732
XDOT = 1635
380699 Wp = 75
44877
YDOT = 5500
502228 meter/sec RA = 298
47435 deg
ZDOT = 5076
292688 TA = 316
47723
MA = 316
54475
Ha = 226
251 n
mi
Hp = 223
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15493279
29 X = 4753090
35
Y = -13121180
52 feet Y = -3946355
80 meter
Z = 9206530
06 Z = 2829165
75
XDOT = 5365
422241 XDOT = 1549
091808
YDOT = 18046
267152 feet/sec YDOT = 5518
307276 meter/sec
ZDOT = 16654
503570 ZDOT = 5084
028090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20192518
20 X = 6154679
55
Y = 1632555
94 feet Y = 497603
05 meter
Z = 9303990
93 Z = 2835856
44
XDOT = -8918
394970 XDOT = -2718
326787
YDOT = 15011
675980 feet/sec YDOT = 4575
558839 meter/sec
ZDOT = 16686
097084 ZDOT = 5085
922391
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 13347
70693309
00016717 00000-0 10270-3 0 9002
2 25544 51
6506 298
8414 0004856 268
9629 91
0965 15
49626820 22553
Satellite: ISS
Catalog Number: 25544
Epoch time: 13347
70693309 = yrday
fracday
Element set: 900
Inclination: 51
6506 deg
RA of node: 298
8414 deg
Eccentricity:
0004856
Arg of perigee: 268
9629 deg
Mean anomaly: 91
0965 deg
Mean motion: 15
49626820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2255
Checksum: 339
Coasting Arc #2 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2013/348/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4439126
81 A = 6798479
12 meter
Y = 4180396
65 meter E =
0001547
Z = -3003916
02 I = 51
33246
XDOT = -1888
993272 Wp = 209
29333
YDOT = -5547
977020 meter/sec RA = 293
50224 deg
ZDOT = -4929
562157 TA = 5
17801
MA = 5
17641
Ha = 226
174 n
mi
Hp = 223
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14564064
33 X = -4470950
66
Y = 13715212
10 feet Y = 4130577
82 meter
Z = -9855367
51 Z = -3025558
04
XDOT = -6197
484487 XDOT = -1802
867474
YDOT = -18202
024343 feet/sec YDOT = -5568
618972 meter/sec
ZDOT = -16173
104188 ZDOT = -4938
530071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19958931
79 X = -6083482
41
Y = -209414
05 feet Y = -63829
40 meter
Z = -9947083
45 Z = -3031871
03
XDOT = 8244
798740 XDOT = 2513
014656
YDOT = -15873
822931 feet/sec YDOT = -4838
341229 meter/sec
ZDOT = -16209
876866 ZDOT = -4940
770469
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 13348
67425053
00016717 00000-0 10270-3 0 9019
2 25544 51
6512 294
0522 0005032 271
6196 88
4378 15
49658118 22705
Satellite: ISS
Catalog Number: 25544
Epoch time: 13348
67425053 = yrday
fracday
Element set: 901
Inclination: 51
6512 deg
RA of node: 294
0522 deg
Eccentricity:
0005032
Arg of perigee: 271
6196 deg
Mean anomaly: 88
4378 deg
Mean motion: 15
49658118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 308
Coasting Arc #3 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2013/349/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147333
75 A = 6797887
19 meter
Y = -4332001
53 meter E =
0007990
Z = 3192330
34 I = 51
31937
XDOT = 2157
634943 Wp = 80
39141
YDOT = 5590
555365 meter/sec RA = 288
52834 deg
ZDOT = 4774
352066 TA = 316
61570
MA = 316
67857
Ha = 226
154 n
mi
Hp = 223
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13606738
04 X = 4179959
34
Y = -14212603
43 feet Y = -4285441
29 meter
Z = 10473524
73 Z = 3212556
67
XDOT = 7078
854799 XDOT = 2071
767089
YDOT = 18341
717076 feet/sec YDOT = 5614
202833 meter/sec
ZDOT = 15663
884730 ZDOT = 4784
625707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19596096
39 X = 5972890
18
Y = -1153279
96 feet Y = -351519
73 meter
Z = 10559312
87 Z = 3218478
56
XDOT = -7493
401160 XDOT = -2283
988674
YDOT = 16745
331441 feet/sec YDOT = 5103
977023 meter/sec
ZDOT = 15706
147199 ZDOT = 4787
233666
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 13349
70603439
00016717 00000-0 10270-3 0 9021
2 25544 51
6512 288
9430 0004897 276
7227 83
3367 15
49692519 22866
Satellite: ISS
Catalog Number: 25544
Epoch time: 13349
70603439 = yrday
fracday
Element set: 902
Inclination: 51
6512 deg
RA of node: 288
9430 deg
Eccentricity:
0004897
Arg of perigee: 276
7227 deg
Mean anomaly: 83
3367 deg
Mean motion: 15
49692519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2286
Checksum: 341
Coasting Arc #4 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2013/350/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3867738
17 A = 6797233
69 meter
Y = 4440645
86 meter E =
0000810
Z = -3395300
80 I = 51
30877
XDOT = -2427
153844 Wp = 345
92418
YDOT = -5626
183890 meter/sec RA = 283
55407 deg
ZDOT = -4592
490810 TA = 233
86302
MA = 233
87052
Ha = 226
157 n
mi
Hp = 223
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12689429
69 X = -3900613
49
Y = 14569048
11 feet Y = 4397210
89 meter
Z = -11139438
31 Z = -3414169
37
XDOT = -7963
103163 XDOT = -2341
751063
YDOT = -18458
608563 feet/sec YDOT = -5652
847870 meter/sec
ZDOT = -15067
227068 ZDOT = -4604
074902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19127527
40 X = -5830070
35
Y = 2371838
63 feet Y = 722936
41 meter
Z = -11219534
37 Z = -3419714
08
XDOT = 6687
214560 XDOT = 2038
262998
YDOT = -17585
549450 feet/sec YDOT = -5360
075472 meter/sec
ZDOT = -15115
002786 ZDOT = -4607
052849
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
67330907
00016717 00000-0 10270-3 0 9037
2 25544 51
6514 284
1538 0005126 278
8519 81
2051 15
49723844 23019
Satellite: ISS
Catalog Number: 25544
Epoch time: 13350
67330907 = yrday
fracday
Element set: 903
Inclination: 51
6514 deg
RA of node: 284
1538 deg
Eccentricity:
0005126
Arg of perigee: 278
8519 deg
Mean anomaly: 81
2051 deg
Mean motion: 15
49723844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 300
Coasting Arc #5 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2013/351/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3587936
15 A = 6796574
02 meter
Y = -4516878
44 meter E =
0007126
Z = 3587480
40 I = 51
30041
XDOT = 2712
411536 Wp = 85
88196
YDOT = 5655
463746 meter/sec RA = 278
57813 deg
ZDOT = 4400
765483 TA = 316
70338
MA = 316
75936
Ha = 226
186 n
mi
Hp = 223
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11771444
06 X = 3620751
22
Y = -14819154
99 feet Y = -4476572
76 meter
Z = 11769948
83 Z = 3604989
49
XDOT = 8898
987980 XDOT = 2627
591568
YDOT = 18554
671084 feet/sec YDOT = 5685
320928 meter/sec
ZDOT = 14438
206966 ZDOT = 4413
736723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18552798
33 X = 5654892
93
Y = -3494460
92 feet Y = -1065111
69 meter
Z = 11844338
84 Z = 3610154
48
XDOT = -5795
890981 XDOT = -1766
587571
YDOT = 18426
220041 feet/sec YDOT = 5616
311868 meter/sec
ZDOT = 14491
822179 ZDOT = 4417
107400
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
70504802
00016717 00000-0 10270-3 0 9040
2 25544 51
6513 279
0445 0004981 284
4794 75
5804 15
49755318 23174
Satellite: ISS
Catalog Number: 25544
Epoch time: 13351
70504802 = yrday
fracday
Element set: 904
Inclination: 51
6513 deg
RA of node: 279
0445 deg
Eccentricity:
0004981
Arg of perigee: 284
4794 deg
Mean anomaly: 75
5804 deg
Mean motion: 15
49755318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 318
Coasting Arc #6 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/352/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3329543
25 A = 6795841
77 meter
Y = 4556405
60 meter E =
0003012
Z = -3789629
68 I = 51
29413
XDOT = -2999
418836 Wp = 17
39500
YDOT = -5670
211650 meter/sec RA = 273
60206 deg
ZDOT = -4180
271394 TA = 208
19882
MA = 208
21513
Ha = 226
249 n
mi
Hp = 223
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10923698
31 X = -3361837
59
Y = 14948837
26 feet Y = 4518992
35 meter
Z = -12433168
24 Z = -3805882
21
XDOT = -9840
612979 XDOT = -2915
483792
YDOT = -18603
056594 feet/sec YDOT = -5703
283317 meter/sec
ZDOT = -13714
801162 ZDOT = -4194
638971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17921364
26 X = -5462431
83
Y = 4460533
17 feet Y = 1359570
51 meter
Z = -12502277
38 Z = -3810694
15
XDOT = 4832
257131 XDOT = 1472
871974
YDOT = -19210
533095 feet/sec YDOT = -5855
370487 meter/sec
ZDOT = -13774
299441 ZDOT = -4198
406469
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
67228046
00016717 00000-0 10270-3 0 9051
2 25544 51
6508 274
2551 0005202 286
1568 73
9010 15
49793098 23323
Satellite: ISS
Catalog Number: 25544
Epoch time: 13352
67228046 = yrday
fracday
Element set: 905
Inclination: 51
6508 deg
RA of node: 274
2551 deg
Eccentricity:
0005202
Arg of perigee: 286
1568 deg
Mean anomaly: 73
9010 deg
Mean motion: 15
49793098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 308
Coasting Arc #7 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2013/353/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3080070
57 A = 6795149
29 meter
Y = -4562457
82 meter E =
0005959
Z = 3978826
05 I = 51
29066
XDOT = 3301
388243 Wp = 91
82443
YDOT = 5676
537710 meter/sec RA = 268
62447 deg
ZDOT = 3948
210889 TA = 316
82676
MA = 316
87347
Ha = 226
308 n
mi
Hp = 223
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10105218
39 X = 3111532
13
Y = -14968693
64 feet Y = -4527838
98 meter
Z = 13053891
23 Z = 3993864
64
XDOT = 10831
326255 XDOT = 3218
487353
YDOT = 18623
811386 feet/sec YDOT = 5712
992035 meter/sec
ZDOT = 12953
447800 ZDOT = 3964
047817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17216055
85 X = 5247453
82
Y = -5301852
88 feet Y = -1616004
76 meter
Z = 13117891
65 Z = 3998333
37
XDOT = -3780
261192 XDOT = -1152
223611
YDOT = 19979
956102 feet/sec YDOT = 6089
890620 meter/sec
ZDOT = 13019
139753 ZDOT = 3968
233797
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
70397528
00016717 00000-0 10270-3 0 9069
2 25544 51
6504 269
1453 0005087 291
8471 68
2138 15
49815841 23486
Satellite: ISS
Catalog Number: 25544
Epoch time: 13353
70397528 = yrday
fracday
Element set: 906
Inclination: 51
6504 deg
RA of node: 269
1453 deg
Eccentricity:
0005087
Arg of perigee: 291
8471 deg
Mean anomaly: 68
2138 deg
Mean motion: 15
49815841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 329
Coasting Arc #8 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/354/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2859672
02 A = 6794355
29 meter
Y = 4540554
13 meter E =
0005344
Z = -4173032
54 I = 51
28893
XDOT = -3603
153326 Wp = 28
49237
YDOT = -5659
946551 meter/sec RA = 263
64682 deg
ZDOT = -3686
626368 TA = 203
38824
MA = 203
41256
Ha = 226
396 n
mi
Hp = 223
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9382126
05 X = -2889961
67
Y = 14896831
13 feet Y = 4508406
44 meter
Z = -13691051
64 Z = -4186997
65
XDOT = -11821
369180 XDOT = -3521
686266
YDOT = -18569
378448 feet/sec YDOT = -5699
783495 meter/sec
ZDOT = -12095
230867 ZDOT = -3703
932611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16505707
38 X = -5030939
61
Y = 5989103
31 feet Y = 1825478
69 meter
Z = -13750528
25 Z = -4191161
01
XDOT = 2647
553238 XDOT = 806
974227
YDOT = -20658
100625 feet/sec YDOT = -6296
589070 meter/sec
ZDOT = -12167
121578 ZDOT = -3708
538657
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
67116634
00016717 00000-0 10270-3 0 9074
2 25544 51
6492 264
3553 0005240 293
3881 66
6718 15
49863571 23639
Satellite: ISS
Catalog Number: 25544
Epoch time: 13354
67116634 = yrday
fracday
Element set: 907
Inclination: 51
6492 deg
RA of node: 264
3553 deg
Eccentricity:
0005240
Arg of perigee: 293
3881 deg
Mean anomaly: 66
6718 deg
Mean motion: 15
49863571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 327
Coasting Arc #9 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2013/355/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2657478
79 A = 6793668
84 meter
Y = -4486329
25 meter E =
0004522
Z = 4351301
25 I = 51
29073
XDOT = 3917
233259 Wp = 97
70563
YDOT = 5632
777778 meter/sec RA = 258
66803 deg
ZDOT = 3411
539493 TA = 317
48670
MA = 317
52171
Ha = 226
465 n
mi
Hp = 223
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8718762
44 X = 2686311
15
Y = -14718928
00 feet Y = -4456450
72 meter
Z = 14275922
75 Z = 4364280
66
XDOT = 12851
815153 XDOT = 3837
382960
YDOT = 18480
242055 feet/sec YDOT = 5676
136077 meter/sec
ZDOT = 11192
714872 ZDOT = 3430
375325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15760924
14 X = 4803929
68
Y = -6532571
91 feet Y = -1991127
92 meter
Z = 14331238
77 Z = 4368161
58
XDOT = -1430
677373 XDOT = -436
070463
YDOT = 21301
037050 feet/sec YDOT = 6492
556093 meter/sec
ZDOT = 11271
060395 ZDOT = 3435
419208
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
70281791
00016717 00000-0 10270-3 0 9087
2 25544 51
6488 259
2449 0005180 298
6932 61
3697 15
49874971 23790
Satellite: ISS
Catalog Number: 25544
Epoch time: 13355
70281791 = yrday
fracday
Element set: 908
Inclination: 51
6488 deg
RA of node: 259
2449 deg
Eccentricity:
0005180
Arg of perigee: 298
6932 deg
Mean anomaly: 61
3697 deg
Mean motion: 15
49874971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 361
Coasting Arc #10 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2013/356/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2489773
84 A = 6792853
41 meter
Y = 4415160
90 meter E =
0007618
Z = -4529452
18 I = 51
29405
XDOT = -4226
115168 Wp = 37
75401
YDOT = -5574
683182 meter/sec RA = 253
68929 deg
ZDOT = -3107
862533 TA = 200
87996
MA = 200
91109
Ha = 226
556 n
mi
Hp = 222
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8168549
35 X = -2516957
44
Y = 14485436
02 feet Y = 4387166
91 meter
Z = -14860407
43 Z = -4541612
97
XDOT = -13865
207243 XDOT = -4148
366700
YDOT = -18289
642984 feet/sec YDOT = -5621
507411 meter/sec
ZDOT = -10196
399385 ZDOT = -3128
203903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15061157
44 X = -4590640
79
Y = 6940512
70 feet Y = 2115468
27 meter
Z = -14912262
88 Z = -4545257
73
XDOT = 138
076211 XDOT = 42
085629
YDOT = -21812
092621 feet/sec YDOT = -6648
325831 meter/sec
ZDOT = -10281
103551 ZDOT = -3133
680362
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
66996880
00016717 00000-0 10270-3 0 9096
2 25544 51
6474 254
4541 0005225 300
4994 59
5640 15
49932401 23942
Satellite: ISS
Catalog Number: 25544
Epoch time: 13356
66996880 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 254
4541 deg
Eccentricity:
0005225
Arg of perigee: 300
4994 deg
Mean anomaly: 59
5640 deg
Mean motion: 15
49932401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 332
Coasting Arc #11 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2013/357/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2348993
16 A = 6792215
98 meter
Y = -4315098
12 meter E =
0002902
Z = 4687804
68 I = 51
30142
XDOT = 4542
624822 Wp = 101
08248
YDOT = 5504
513943 meter/sec RA = 248
70997 deg
ZDOT = 2788
606917 TA = 321
11146
MA = 321
13234
Ha = 226
627 n
mi
Hp = 222
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7706670
48 X = 2374299
04
Y = -14157146
06 feet Y = -4288688
89 meter
Z = 15379936
62 Z = 4699277
08
XDOT = 14903
624743 XDOT = 4467
188302
YDOT = 18059
428946 feet/sec YDOT = 5554
890561 meter/sec
ZDOT = 9148
972826 ZDOT = 2810
491432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14370218
34 X = 4380042
55
Y = -7197682
62 feet Y = -2193853
66 meter
Z = 15428875
35 Z = 4702721
21
XDOT = 1224
312412 XDOT = 373
170423
YDOT = 22265
705822 feet/sec YDOT = 6786
587134 meter/sec
ZDOT = 9240
195267 ZDOT = 2816
411517
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
70157819
00016717 00000-0 10270-3 0 9105
2 25544 51
6473 249
3432 0005220 305
2753 54
7909 15
49933164 24105
Satellite: ISS
Catalog Number: 25544
Epoch time: 13357
70157819 = yrday
fracday
Element set: 910
Inclination: 51
6473 deg
RA of node: 249
3432 deg
Eccentricity:
0005220
Arg of perigee: 305
2753 deg
Mean anomaly: 54
7909 deg
Mean motion: 15
49933164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 304
Coasting Arc #12 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2013/358/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2245158
35 A = 6791435
16 meter
Y = 4210902
33 meter E =
0009699
Z = -4841040
59 I = 51
31030
XDOT = -4846
111214 Wp = 46
63147
YDOT = -5397
060804 meter/sec RA = 243
73105 deg
ZDOT = -2443
605332 TA = 199
20699
MA = 199
24357
Ha = 226
710 n
mi
Hp = 222
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7366005
08 X = -2268562
37
Y = 13815296
36 feet Y = 4185664
85 meter
Z = -15882679
12 Z = -4852004
02
XDOT = -15899
315008 XDOT = -4773
529588
YDOT = -17706
892401 feet/sec YDOT = -5450
847195 meter/sec
ZDOT = -8017
077861 ZDOT = -2466
971092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13767849
60 X = -4196440
56
Y = 7353820
68 feet Y = 2241444
54 meter
Z = -15929456
34 Z = -4855298
29
XDOT = -2641
495362 XDOT = -805
127786
YDOT = -22547
074968 feet/sec YDOT = -6872
348450 meter/sec
ZDOT = -8114
563154 ZDOT = -2473
318849
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
66869020
00016717 00000-0 10270-3 0 9116
2 25544 51
6461 244
5519 0005153 307
6341 52
4341 15
49998475 24256
Satellite: ISS
Catalog Number: 25544
Epoch time: 13358
66869020 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 244
5519 deg
Eccentricity:
0005153
Arg of perigee: 307
6341 deg
Mean anomaly: 52
4341 deg
Mean motion: 15
49998475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 316
Coasting Arc #13 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2013/359/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2175650
48 A = 6790898
06 meter
Y = -4083278
08 meter E =
0001326
Z = 4969701
82 I = 51
32307
XDOT = 5150
625560 Wp = 85
85511
YDOT = 5277
502222 meter/sec RA = 238
75210 deg
ZDOT = 2080
934017 TA = 343
78537
MA = 343
78961
Ha = 226
785 n
mi
Hp = 222
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7137960
90 X = 2197007
49
Y = -13396581
62 feet Y = -4058829
32 meter
Z = 16304795
99 Z = 4980322
64
XDOT = 16898
377822 XDOT = 5081
119956
YDOT = 17314
639837 feet/sec YDOT = 5334
711101 meter/sec
ZDOT = 6827
211342 ZDOT = 2105
786601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13217162
07 X = 4028591
00
Y = -7365174
69 feet Y = -2244905
24 meter
Z = 16350109
65 Z = 4983513
42
XDOT = 4102
470618 XDOT = 1250
433044
YDOT = 22751
138141 feet/sec YDOT = 6934
546905 meter/sec
ZDOT = 6930
984106 ZDOT = 2112
563956
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
70025851
00016717 00000-0 10270-3 0 9129
2 25544 51
6462 239
4406 0005183 312
0391 48
0318 15
49990642 24414
Satellite: ISS
Catalog Number: 25544
Epoch time: 13359
70025851 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 239
4406 deg
Eccentricity:
0005183
Arg of perigee: 312
0391 deg
Mean anomaly: 48
0318 deg
Mean motion: 15
49990642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 297
Coasting Arc #14 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2013/360/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2141985
80 A = 6790214
19 meter
Y = 3965356
16 meter E =
0011436
Z = -5088721
33 I = 51
33777
XDOT = -5432
151457 Wp = 55
29208
YDOT = -5117
185784 meter/sec RA = 233
77421 deg
ZDOT = -1697
338594 TA = 198
18714
MA = 198
22808
Ha = 226
856 n
mi
Hp = 222
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7027512
46 X = -2161448
45
Y = 13009698
68 feet Y = 3941294
49 meter
Z = -16695279
96 Z = -5099174
02
XDOT = -17822
019217 XDOT = -5366
281002
YDOT = -16788
667269 feet/sec YDOT = -5177
563193 meter/sec
ZDOT = -5568
696175 ZDOT = -1723
567723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12786935
53 X = -3897457
95
Y = 7324048
16 feet Y = 2232369
88 meter
Z = -16739867
45 Z = -5102311
60
XDOT = -5581
271778 XDOT = -1701
171638
YDOT = -22749
908096 feet/sec YDOT = -6934
171988 meter/sec
ZDOT = -5678
298329 ZDOT = -1730
745331
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
66733270
00016717 00000-0 10270-3 0 9138
2 25544 51
6457 234
6493 0005043 314
9891 45
0851 15
50062512 24565
Satellite: ISS
Catalog Number: 25544
Epoch time: 13360
66733270 = yrday
fracday
Element set: 913
Inclination: 51
6457 deg
RA of node: 234
6493 deg
Eccentricity:
0005043
Arg of perigee: 314
9891 deg
Mean anomaly: 45
0851 deg
Mean motion: 15
50062512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 297
Coasting Arc #15 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2013/361/15:33:24
555
Vector Time (MET): N/A
Weight (LBS) : 901986
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2148053
35 A = 6789837
37 meter
Y = -3831004
55 meter E =
0001413
Z = 5177491
96 I = 51
35527
XDOT = 5706
558418 Wp = 8
84138
YDOT = 4946
904980 meter/sec RA = 228
79647 deg
ZDOT = 1294
153992 TA = 68
67732
MA = 68
66224
Ha = 226
938 n
mi
Hp = 222
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7047419
11 X = 2165581
94
Y = -12568912
58 feet Y = -3806885
93 meter
Z = 16986522
18 Z = 5187969
40
XDOT = 18722
304522 XDOT = 5644
530239
YDOT = 16230
003214 feet/sec YDOT = 5010
372464 meter/sec
ZDOT = 4245
912048 ZDOT = 1321
725603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12446254
80 X = 3793618
46
Y = -7156449
22 feet Y = -2181285
72 meter
Z = 17031194
65 Z = 5191108
13
XDOT = 7066
525847 XDOT = 2153
877078
YDOT = 22658
520841 feet/sec YDOT = 6906
317152 meter/sec
ZDOT = 4361
202404 ZDOT = 1329
294493
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
69886088
00016717 00000-0 10270-3 0 9149
2 25544 51
6456 229
5378 0005091 319
2853 40
7916 15
50047921 24727
Satellite: ISS
Catalog Number: 25544
Epoch time: 13361
69886088 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 229
5378 deg
Eccentricity:
0005091
Arg of perigee: 319
2853 deg
Mean anomaly: 40
7916 deg
Mean motion: 15
50047921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 330
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