[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 4th 2013
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) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
191/05:40:05
424 4
2 4
6 4
6
N/A 0
2 -0
7 228
9
000/00:10:10
849 1
9 -0
1 221
0
Coasting Arc #1 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2013/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3824481
97 A = 6789243
43 meter
Y = 2487335
38 meter E =
0011867
Z = 5017470
30 I = 51
79770
XDOT = -5718
796366 Wp = 94
10026
YDOT = -4692
752639 meter/sec RA = 26
90395 deg
ZDOT = -2029
391492 TA = 15
59103
MA = 15
55451
Ha = 229
551 n
mi
Hp = 217
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12547513
04 X = -3876385
15
Y = 8160549
16 feet Y = 2444276
77 meter
Z = 16461516
72 Z = 4998765
56
XDOT = -18762
455270 XDOT = -5656
037726
YDOT = -15396
170075 feet/sec YDOT = -4756
352672 meter/sec
ZDOT = -6658
108568 ZDOT = -2057
021035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10398852
07 X = 3169570
11
Y = 10884961
55 feet Y = 3317736
28 meter
Z = 16382846
72 Z = 4993491
68
XDOT = -10800
123021 XDOT = -3291
877497
YDOT = 20528
116079 feet/sec YDOT = 6256
969781 meter/sec
ZDOT = -6772
967519 ZDOT = -2064
400500
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 13184
54477987
00016717 00000-0 10270-3 0 9005
2 25544 51
6490 27
2633 0007995 122
2796 237
9130 15
50531216 37249
Satellite: ISS
Catalog Number: 25544
Epoch time: 13184
54477987 = yrday
fracday
Element set: 900
Inclination: 51
6490 deg
RA of node: 27
2633 deg
Eccentricity:
0007995
Arg of perigee: 122
2796 deg
Mean anomaly: 237
9130 deg
Mean motion: 15
50531216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 318
Coasting Arc #2 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2013/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4114579
65 A = 6790051
08 meter
Y = -2446952
40 meter E =
0019198
Z = -4833698
71 I = 51
77124
XDOT = 5660
769094 Wp = 115
10012
YDOT = 4457
571577 meter/sec RA = 21
95164 deg
ZDOT = 2562
111379 TA = 180
14577
MA = 180
14633
Ha = 229
401 n
mi
Hp = 217
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13499277
08 X = 4165116
94
Y = -8028059
05 feet Y = -2400657
34 meter
Z = -15858591
55 Z = -4813588
07
XDOT = 18572
077081 XDOT = 5598
056829
YDOT = 14624
578666 feet/sec YDOT = 4520
522877 meter/sec
ZDOT = 8405
877227 ZDOT = 2589
459110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10649435
42 X = -3245947
92
Y = -11659512
34 feet Y = -3553819
36 meter
Z = -15774043
14 Z = -4807928
35
XDOT = 9662
048033 XDOT = 2944
992240
YDOT = -20350
849887 feet/sec YDOT = -6202
939045 meter/sec
ZDOT = 8519
589296 ZDOT = 2596
770817
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 13185
51154902
00016717 00000-0 10270-3 0 9013
2 25544 51
6476 22
4689 0008072 125
6757 234
5147 15
50544406 37394
Satellite: ISS
Catalog Number: 25544
Epoch time: 13185
51154902 = yrday
fracday
Element set: 901
Inclination: 51
6476 deg
RA of node: 22
4689 deg
Eccentricity:
0008072
Arg of perigee: 125
6757 deg
Mean anomaly: 234
5147 deg
Mean motion: 15
50544406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 311
Coasting Arc #3 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2013/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4389711
14 A = 6791008
96 meter
Y = 2423240
79 meter E =
0014294
Z = 4566874
52 I = 51
74593
XDOT = -5579
106079 Wp = 96
33407
YDOT = -4258
480558 meter/sec RA = 16
99960 deg
ZDOT = -3096
294216 TA = 24
63004
MA = 24
56184
Ha = 229
408 n
mi
Hp = 217
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14401939
44 X = -4438666
62
Y = 7950265
05 feet Y = 2373877
89 meter
Z = 14983184
13 Z = 4545431
24
XDOT = -18304
153803 XDOT = -5516
031293
YDOT = -13971
392908 feet/sec YDOT = -4320
516532 meter/sec
ZDOT = -10158
445592 ZDOT = -3123
244285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10971752
97 X = 3344190
31
Y = 12366718
93 feet Y = 3769375
93 meter
Z = 14893061
48 Z = 4539405
14
XDOT = -8670
672354 XDOT = -2642
820933
YDOT = 20088
204091 feet/sec YDOT = 6122
884607 meter/sec
ZDOT = -10270
522406 ZDOT = -3130
455229
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 13186
54275899
00016717 00000-0 10270-3 0 9027
2 25544 51
6477 17
3564 0007953 129
8256 230
3596 15
50555685 37558
Satellite: ISS
Catalog Number: 25544
Epoch time: 13186
54275899 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 17
3564 deg
Eccentricity:
0007953
Arg of perigee: 129
8256 deg
Mean anomaly: 230
3596 deg
Mean motion: 15
50555685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 349
Coasting Arc #4 (Orbit 3769)
---------------------------------------
Vector Time (GMT): 2013/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4671195
12 A = 6792061
38 meter
Y = -2463761
85 meter E =
0015935
Z = -4288166
13 I = 51
71896
XDOT = 5416
582083 Wp = 121
06959
YDOT = 4043
840546 meter/sec RA = 12
04475 deg
ZDOT = 3578
879066 TA = 185
51166
MA = 185
52922
Ha = 229
284 n
mi
Hp = 217
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15325443
30 X = 4719228
84
Y = -8083208
17 feet Y = -2411256
41 meter
Z = -14068786
52 Z = -4265357
75
XDOT = 17770
938594 XDOT = 5353
575325
YDOT = 13267
193393 feet/sec YDOT = 4104
059382 meter/sec
ZDOT = 11741
729220 ZDOT = 3605
039671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11531070
01 X = -3514670
14
Y = -13035700
22 feet Y = -3973281
43 meter
Z = -13972944
03 Z = -4258953
34
XDOT = 7707
144947 XDOT = 2349
137780
YDOT = -19513
539025 feet/sec YDOT = -5947
726695 meter/sec
ZDOT = 11850
535761 ZDOT = 3612
043300
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 13187
50951019
00016717 00000-0 10270-3 0 9030
2 25544 51
6468 12
5619 0008110 133
0294 227
1538 15
50570183 37708
Satellite: ISS
Catalog Number: 25544
Epoch time: 13187
50951019 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 12
5619 deg
Eccentricity:
0008110
Arg of perigee: 133
0294 deg
Mean anomaly: 227
1538 deg
Mean motion: 15
50570183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3770
Checksum: 292
Coasting Arc #5 (Orbit 3785)
---------------------------------------
Vector Time (GMT): 2013/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4926697
24 A = 6793241
29 meter
Y = 2513330
01 meter E =
0016988
Z = 3927058
10 I = 51
69284
XDOT = -5225
011076 Wp = 103
50954
YDOT = -3881
701809 meter/sec RA = 7
08994 deg
ZDOT = -4059
865391 TA = 28
94684
MA = 28
85272
Ha = 229
268 n
mi
Hp = 217
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16163704
85 X = -4973512
05
Y = 8245833
36 feet Y = 2457974
26 meter
Z = 12884048
88 Z = 3903011
55
XDOT = -17142
424790 XDOT = -5161
495202
YDOT = -12735
242154 feet/sec YDOT = -3939
775478 meter/sec
ZDOT = -13319
768344 ZDOT = -4085
094017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12123015
40 X = 3695095
10
Y = 13597235
25 feet Y = 4144437
30 meter
Z = 12783017
21 Z = 3896263
64
XDOT = -6963
685489 XDOT = -2122
531337
YDOT = 18863
313788 feet/sec YDOT = 5749
538043 meter/sec
ZDOT = -13424
701085 ZDOT = -4091
848891
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 13188
54070064
00016717 00000-0 10270-3 0 9048
2 25544 51
6469 7
4489 0007990 137
1953 222
9821 15
50579529 37867
Satellite: ISS
Catalog Number: 25544
Epoch time: 13188
54070064 = yrday
fracday
Element set: 904
Inclination: 51
6469 deg
RA of node: 7
4489 deg
Eccentricity:
0007990
Arg of perigee: 137
1953 deg
Mean anomaly: 222
9821 deg
Mean motion: 15
50579529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3786
Checksum: 339
Coasting Arc #6 (Orbit 3800)
---------------------------------------
Vector Time (GMT): 2013/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5167544
22 A = 6794363
89 meter
Y = -2624982
19 meter E =
0012309
Z = -3560725
43 I = 51
66621
XDOT = 4968
173494 Wp = 122
38768
YDOT = 3722
549598 meter/sec RA = 2
13308 deg
ZDOT = 4470
729428 TA = 195
75202
MA = 195
79035
Ha = 229
156 n
mi
Hp = 218
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16953885
25 X = 5213810
09
Y = -8612146
30 feet Y = -2566936
30 meter
Z = -11682170
06 Z = -3535510
27
XDOT = 16299
781805 XDOT = 4904
460595
YDOT = 12213
089232 feet/sec YDOT = 3777
750029 meter/sec
ZDOT = 14667
747467 ZDOT = 4494
709778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12920473
27 X = -3938160
25
Y = -14040250
05 feet Y = -4279468
21 meter
Z = -11576231
48 Z = -3528435
35
XDOT = 6319
699636 XDOT = 1926
244449
YDOT = -17978
163668 feet/sec YDOT = -5479
744286 meter/sec
ZDOT = 14767
483230 ZDOT = 4501
128888
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 13189
50743362
00016717 00000-0 10270-3 0 9054
2 25544 51
6469 2
6546 0008168 140
1583 220
0169 15
50598743 38010
Satellite: ISS
Catalog Number: 25544
Epoch time: 13189
50743362 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 2
6546 deg
Eccentricity:
0008168
Arg of perigee: 140
1583 deg
Mean anomaly: 220
0169 deg
Mean motion: 15
50598743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3801
Checksum: 308
Coasting Arc #7 (Orbit 3816)
---------------------------------------
Vector Time (GMT): 2013/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5372237
28 A = 6795576
20 meter
Y = 2732762
05 meter E =
0019293
Z = 3114138
94 I = 51
63945
XDOT = -4681
533688 Wp = 113
40254
YDOT = -3630
927166 meter/sec RA = 357
17583 deg
ZDOT = -4873
440520 TA = 30
76650
MA = 30
65355
Ha = 229
105 n
mi
Hp = 218
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17625450
39 X = -5417523
75
Y = 8965754
76 feet Y = 2672432
72 meter
Z = 10216991
26 Z = 3087931
81
XDOT = -15359
362494 XDOT = -4616
910440
YDOT = -11912
490701 feet/sec YDOT = -3682
917133 meter/sec
ZDOT = -15988
978084 ZDOT = -4896
026107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13689706
69 X = 4172622
60
Y = 14348203
04 feet Y = 4373332
29 meter
Z = 10106887
28 Z = 3080579
24
XDOT = -5956
741548 XDOT = -1815
614824
YDOT = 17050
636607 feet/sec YDOT = 5197
034038 meter/sec
ZDOT = -16082
893257 ZDOT = -4902
065865
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 13190
53860448
00016717 00000-0 10270-3 0 9065
2 25544 51
6467 357
5413 0008050 144
3244 215
8446 15
50606517 38179
Satellite: ISS
Catalog Number: 25544
Epoch time: 13190
53860448 = yrday
fracday
Element set: 906
Inclination: 51
6467 deg
RA of node: 357
5413 deg
Eccentricity:
0008050
Arg of perigee: 144
3244 deg
Mean anomaly: 215
8446 deg
Mean motion: 15
50606517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3817
Checksum: 308
Coasting Arc #8 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2013/191/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4528896
52 A = 6796390
70 meter
Y = -3469008
81 meter E =
0008699
Z = -3704857
56 I = 51
61625
XDOT = 5668
294219 Wp = 130
04740
YDOT = 2794
248582 meter/sec RA = 353
50820 deg
ZDOT = 4313
940332 TA = 185
93954
MA = 185
94986
Ha = 228
901 n
mi
Hp = 221
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14858584
37 X = 4585348
04
Y = -11381262
48 feet Y = -3418047
80 meter
Z = -12155044
50 Z = -3682720
18
XDOT = 18596
765809 XDOT = 5615
671424
YDOT = 9167
482225 feet/sec YDOT = 2857
340347 meter/sec
ZDOT = 14153
347546 ZDOT = 4341
348439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11788098
80 X = 3593012
51
Y = -14615340
99 feet Y = -4454755
93 meter
Z = -12061853
36 Z = -3676452
90
XDOT = 19095
517466 XDOT = 5820
313724
YDOT = 3630
219434 feet/sec YDOT = 1106
490883 meter/sec
ZDOT = 14267
577589 ZDOT = 4348
757649
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 13191
24752905
00016717 00000-0 10270-3 0 9073
2 25544 51
6518 354
0289 0004833 166
5517 193
5763 15
49752054 38285
Satellite: ISS
Catalog Number: 25544
Epoch time: 13191
24752905 = yrday
fracday
Element set: 907
Inclination: 51
6518 deg
RA of node: 354
0289 deg
Eccentricity:
0004833
Arg of perigee: 166
5517 deg
Mean anomaly: 193
5763 deg
Mean motion: 15
49752054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 332
Coasting Arc #9 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2013/192/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4461885
42 A = 6796978
11 meter
Y = 3733754
74 meter E =
0013885
Z = 3498421
18 I = 51
58783
XDOT = -5657
771555 Wp = 108
45912
YDOT = -2513
534569 meter/sec RA = 348
55357 deg
ZDOT = -4522
856578 TA = 30
41897
MA = 30
33848
Ha = 228
886 n
mi
Hp = 221
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14638731
69 X = -4520299
58
Y = 12249851
51 feet Y = 3683532
20 meter
Z = 11477759
77 Z = 3476604
52
XDOT = -18562
242634 XDOT = -5607
273700
YDOT = -8246
504491 feet/sec YDOT = -2576
520603 meter/sec
ZDOT = -14838
768299 ZDOT = -4550
218659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11096707
64 X = -3382276
49
Y = 15598565
87 feet Y = 4754442
88 meter
Z = 11385873
67 Z = 3470414
29
XDOT = -18825
590964 XDOT = -5738
040126
YDOT = -2452
622991 feet/sec YDOT = -747
559488 meter/sec
ZDOT = -14952
850042 ZDOT = -4557
628693
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 13192
27926975
00016717 00000-0 10270-3 0 9088
2 25544 51
6517 348
9202 0004790 169
7020 190
4229 15
49758060 38441
Satellite: ISS
Catalog Number: 25544
Epoch time: 13192
27926975 = yrday
fracday
Element set: 908
Inclination: 51
6517 deg
RA of node: 348
9202 deg
Eccentricity:
0004790
Arg of perigee: 169
7020 deg
Mean anomaly: 190
4229 deg
Mean motion: 15
49758060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 333
Coasting Arc #10 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2013/193/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4375239
54 A = 6797479
48 meter
Y = -4023631
18 meter E =
0006461
Z = -3306308
69 I = 51
56037
XDOT = 5608
880033 Wp = 128
99416
YDOT = 2238
171169 meter/sec RA = 343
59634 deg
ZDOT = 4700
706311 TA = 192
64566
MA = 192
66188
Ha = 228
634 n
mi
Hp = 221
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14354460
45 X = 4435968
41
Y = -13200889
71 feet Y = -3974364
70 meter
Z = -10847469
44 Z = -3284907
25
XDOT = 18401
837380 XDOT = 5560
601022
YDOT = 7343
081262 feet/sec YDOT = 2300
622936 meter/sec
ZDOT = 15422
264800 ZDOT = 4727
836251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10290987
75 X = 3136693
07
Y = -16624021
49 feet Y = -5067001
75 meter
Z = -10757281
15 Z = -3278819
29
XDOT = 18400
618945 XDOT = 5608
508654
YDOT = 1342
695425 feet/sec YDOT = 409
253565 meter/sec
ZDOT = 15535
417299 ZDOT = 4735
195193
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 13193
24651654
00016717 00000-0 10270-3 0 9096
2 25544 51
6522 344
1302 0004659 175
2500 184
8696 15
49776715 38593
Satellite: ISS
Catalog Number: 25544
Epoch time: 13193
24651654 = yrday
fracday
Element set: 909
Inclination: 51
6522 deg
RA of node: 344
1302 deg
Eccentricity:
0004659
Arg of perigee: 175
2500 deg
Mean anomaly: 184
8696 deg
Mean motion: 15
49776715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 333
Coasting Arc #11 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2013/194/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4267088
75 A = 6798041
26 meter
Y = 4292965
80 meter E =
0014452
Z = 3075818
11 I = 51
53318
XDOT = -5551
693974 Wp = 114
17979
YDOT = -2003
243998 meter/sec RA = 338
63807 deg
ZDOT = -4893
532078 TA = 30
46848
MA = 30
38459
Ha = 228
588 n
mi
Hp = 221
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13999635
02 X = -4329717
81
Y = 14084533
46 feet Y = 4244898
16 meter
Z = 10091266
77 Z = 3054937
35
XDOT = -18214
219074 XDOT = -5505
109477
YDOT = -6572
322829 feet/sec YDOT = -2065
065794 meter/sec
ZDOT = -16054
895270 ZDOT = -4920
388360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9404556
58 X = -2866508
85
Y = 17541020
55 feet Y = 5346503
06 meter
Z = 10003221
59 Z = 3048981
94
XDOT = -17961
272857 XDOT = -5474
595967
YDOT = -386
879712 feet/sec YDOT = -117
920936 meter/sec
ZDOT = -16166
937136 ZDOT = -4927
682439
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 13194
27823851
00016717 00000-0 10270-3 0 9102
2 25544 51
6522 339
0215 0004616 178
0034 182
1136 15
49791999 38754
Satellite: ISS
Catalog Number: 25544
Epoch time: 13194
27823851 = yrday
fracday
Element set: 910
Inclination: 51
6522 deg
RA of node: 339
0215 deg
Eccentricity:
0004616
Arg of perigee: 178
0034 deg
Mean anomaly: 182
1136 deg
Mean motion: 15
49791999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 320
Coasting Arc #12 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2013/195/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4133419
09 A = 6798554
34 meter
Y = -4582004
53 meter E =
0004396
Z = -2859482
87 I = 51
50652
XDOT = 5466
167750 Wp = 120
54469
YDOT = 1779
510406 meter/sec RA = 333
67701 deg
ZDOT = 5053
577017 TA = 206
96366
MA = 206
98651
Ha = 228
359 n
mi
Hp = 221
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13561086
25 X = 4198239
33
Y = -15032823
26 feet Y = -4535419
44 meter
Z = -9381505
48 Z = -2839246
07
XDOT = 17933
621228 XDOT = 5421
313921
YDOT = 5838
288733 feet/sec YDOT = 1840
385486 meter/sec
ZDOT = 16579
977090 ZDOT = 5080
022093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8390634
66 X = 2557465
45
Y = -18468377
26 feet Y = -5629161
39 meter
Z = -9296115
96 Z = -2833456
15
XDOT = 17415
254730 XDOT = 5308
169642
YDOT = -482
905556 feet/sec YDOT = -147
189613 meter/sec
ZDOT = 16690
330340 ZDOT = 5087
212688
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 13195
24546783
00016717 00000-0 10270-3 0 9117
2 25544 51
6519 334
2313 0004517 184
3036 175
8076 15
49800246 38903
Satellite: ISS
Catalog Number: 25544
Epoch time: 13195
24546783 = yrday
fracday
Element set: 911
Inclination: 51
6519 deg
RA of node: 334
2313 deg
Eccentricity:
0004517
Arg of perigee: 184
3036 deg
Mean anomaly: 175
8076 deg
Mean motion: 15
49800246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 314
Coasting Arc #13 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2013/196/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3980357
88 A = 6799055
21 meter
Y = 4845345
27 meter E =
0014799
Z = 2605419
95 I = 51
48128
XDOT = -5377
132024 Wp = 120
50623
YDOT = -1599
482680 meter/sec RA = 328
71509 deg
ZDOT = -5225
355049 TA = 30
12661
MA = 30
04158
Ha = 228
269 n
mi
Hp = 221
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13058916
95 X = -4046900
12
Y = 15896802
05 feet Y = 4800462
18 meter
Z = 8547965
73 Z = 2585922
48
XDOT = -17641
509265 XDOT = -5333
463391
YDOT = -5247
646588 feet/sec YDOT = -1659
368709 meter/sec
ZDOT = -17143
553312 ZDOT = -5251
370563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7313894
07 X = -2229274
91
Y = 19265288
44 feet Y = 5872059
92 meter
Z = 8465634
08 Z = 2580325
27
XDOT = -16887
026949 XDOT = -5147
165814
YDOT = 1191
574587 feet/sec YDOT = 363
191934 meter/sec
ZDOT = -17252
134213 ZDOT = -5258
450508
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 13196
27717092
00016717 00000-0 10270-3 0 9125
2 25544 51
6519 329
1224 0004460 186
9431 173
1659 15
49826768 39064
Satellite: ISS
Catalog Number: 25544
Epoch time: 13196
27717092 = yrday
fracday
Element set: 912
Inclination: 51
6519 deg
RA of node: 329
1224 deg
Eccentricity:
0004460
Arg of perigee: 186
9431 deg
Mean anomaly: 173
1659 deg
Mean motion: 15
49826768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 333
Coasting Arc #14 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2013/197/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3797585
46 A = 6799554
18 meter
Y = -5121574
03 meter E =
0003087
Z = -2365718
50 I = 51
45624
XDOT = 5270
904600 Wp = 94
98109
YDOT = 1433
613571 meter/sec RA = 323
75012 deg
ZDOT = 5363
306882 TA = 238
61048
MA = 238
64068
Ha = 228
088 n
mi
Hp = 221
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12459269
88 X = 3866065
76
Y = -16803064
42 feet Y = -5078723
98 meter
Z = -7761543
63 Z = -2347104
22
XDOT = 17292
994095 XDOT = 5228
428448
YDOT = 4703
456599 feet/sec YDOT = 1492
318300 meter/sec
ZDOT = 17596
151187 ZDOT = 5388
809325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6106692
57 X = 1861319
89
Y = -20037459
45 feet Y = -6107417
64 meter
Z = -7682868
19 Z = -2341738
22
XDOT = 16302
427120 XDOT = 4968
979786
YDOT = -1811
866521 feet/sec YDOT = -552
256916 meter/sec
ZDOT = 17702
608974 ZDOT = 5395
755215
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 13197
24438303
00016717 00000-0 10270-3 0 9139
2 25544 51
6509 324
3316 0004434 193
2124 166
8911 15
49824285 39212
Satellite: ISS
Catalog Number: 25544
Epoch time: 13197
24438303 = yrday
fracday
Element set: 913
Inclination: 51
6509 deg
RA of node: 324
3316 deg
Eccentricity:
0004434
Arg of perigee: 193
2124 deg
Mean anomaly: 166
8911 deg
Mean motion: 15
49824285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 305
Coasting Arc #15 (Orbit 3936)
---------------------------------------
Vector Time (GMT): 2013/198/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3598878
83 A = 6799960
38 meter
Y = 5366796
93 meter E =
0014885
Z = 2089299
83 I = 51
43381
XDOT = -5167
023324 Wp = 127
38634
YDOT = -1313
216508 meter/sec RA = 318
78471 deg
ZDOT = -5508
869644 TA = 29
44299
MA = 29
35923
Ha = 227
939 n
mi
Hp = 221
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11807345
25 X = -3668773
28
Y = 17607601
49 feet Y = 5326161
02 meter
Z = 6854658
25 Z = 2071647
51
XDOT = -16952
176259 XDOT = -5125
194066
YDOT = -4308
453109 feet/sec YDOT = -1370
763082 meter/sec
ZDOT = -18073
719306 ZDOT = -5533
869057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4861703
98 X = -1481847
37
Y = 20659699
66 feet Y = 6297076
46 meter
Z = 6779971
69 Z = 2066535
37
XDOT = -15769
738765 XDOT = -4806
616376
YDOT = 2274
410612 feet/sec YDOT = 693
240355 meter/sec
ZDOT = -18178
090405 ZDOT = -5540
681956
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 13198
27606726
00016717 00000-0 10270-3 0 9140
2 25544 51
6509 319
2223 0004346 196
3172 163
7839 15
49862281 39371
Satellite: ISS
Catalog Number: 25544
Epoch time: 13198
27606726 = yrday
fracday
Element set: 914
Inclination: 51
6509 deg
RA of node: 319
2223 deg
Eccentricity:
0004346
Arg of perigee: 196
3172 deg
Mean anomaly: 163
7839 deg
Mean motion: 15
49862281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3937
Checksum: 335
Coasting Arc #16 (Orbit 3951)
---------------------------------------
Vector Time (GMT): 2013/199/05:45:10
849
Vector Time (MET): N/A
Weight (LBS) : 921285
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3368391
06 A = 6800415
24 meter
Y = -5617256
42 meter E =
0003384
Z = -1827881
64 I = 51
41147
XDOT = 5057
320610 Wp = 60
95642
YDOT = 1206
864529 meter/sec RA = 313
81619 deg
ZDOT = 5620
259670 TA = 278
92922
MA = 278
96753
Ha = 227
831 n
mi
Hp = 221
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11051151
78 X = 3439833
43
Y = -18429318
97 feet Y = -5579189
30 meter
Z = -5996987
00 Z = -1811345
39
XDOT = 16592
259218 XDOT = 5016
147678
YDOT = 3959
529295 feet/sec YDOT = 1263
187887 meter/sec
ZDOT = 18439
172147 ZDOT = 5644
727747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3494426
95 X = 1065101
33
Y = -21222442
42 feet Y = -6468600
45 meter
Z = -5926932
13 Z = -1806528
91
XDOT = 15227
663929 XDOT = 4641
391966
YDOT = -2661
991637 feet/sec YDOT = -811
375051 meter/sec
ZDOT = 18541
338070 ZDOT = 5651
399844
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 13199
24326264
00016717 00000-0 10270-3 0 9155
2 25544 51
6496 314
4309 0004408 201
4990 158
5976 15
49849432 39527
Satellite: ISS
Catalog Number: 25544
Epoch time: 13199
24326264 = yrday
fracday
Element set: 915
Inclination: 51
6496 deg
RA of node: 314
4309 deg
Eccentricity:
0004408
Arg of perigee: 201
4990 deg
Mean anomaly: 158
5976 deg
Mean motion: 15
49849432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 336
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