[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 27th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21667 75 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
477 4
1 4
6 4
7
N/A 0
4 -0
7 228
6
000/00:10:10
954 2
1 -0
1 220
9
Coasting Arc #1 (Orbit 3614)
---------------------------------------
Vector Time (GMT): 2013/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2507082
59 A = 6789209
93 meter
Y = -3744755
87 meter E =
0021192
Z = -5096675
49 I = 51
94766
XDOT = 4746
598851 Wp = 83
89056
YDOT = 5699
784456 meter/sec RA = 61
51770 deg
ZDOT = -1857
454026 TA = 168
16629
MA = 168
11641
Ha = 229
872 n
mi
Hp = 217
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8225336
59 X = 2573528
87
Y = -12285944
45 feet Y = -3716347
97 meter
Z = -16721376
27 Z = -5084335
52
XDOT = 15572
830876 XDOT = 4691
532738
YDOT = 18700
080236 feet/sec YDOT = 5752
556248 meter/sec
ZDOT = -6094
009271 ZDOT = -1834
528858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12833157
23 X = -3911546
33
Y = -7460174
02 feet Y = -2273861
04 meter
Z = -16669160
04 Z = -5080759
98
XDOT = 17032
786181 XDOT = 5191
593228
YDOT = -15928
715214 feet/sec YDOT = -4855
072397 meter/sec
ZDOT = -5998
939728 ZDOT = -1828
476829
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 13177
51933753
00016717 00000-0 10270-3 0 9002
2 25544 51
6500 62
0901 0008392 96
4064 263
8043 15
50445356 36157
Satellite: ISS
Catalog Number: 25544
Epoch time: 13177
51933753 = yrday
fracday
Element set: 900
Inclination: 51
6500 deg
RA of node: 62
0901 deg
Eccentricity:
0008392
Arg of perigee: 96
4064 deg
Mean anomaly: 263
8043 deg
Mean motion: 15
50445356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3615
Checksum: 293
Coasting Arc #2 (Orbit 3630)
---------------------------------------
Vector Time (GMT): 2013/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2573247
94 A = 6788624
43 meter
Y = 3502814
07 meter E =
0012400
Z = 5205394
23 I = 51
93038
XDOT = -4994
571540 Wp = 108
13678
YDOT = -5666
239956 meter/sec RA = 56
57747 deg
ZDOT = 1337
527524 TA = 329
03046
MA = 329
10352
Ha = 229
943 n
mi
Hp = 217
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8442414
51 X = -2637512
02
Y = 11492172
15 feet Y = 3473678
56 meter
Z = 17078065
05 Z = 5192738
02
XDOT = -16386
389568 XDOT = -4937
336482
YDOT = -18590
026101 feet/sec YDOT = -5721
772520 meter/sec
ZDOT = 4388
213660 ZDOT = 1313
403088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12187698
57 X = 3714810
53
Y = 7525227
93 feet Y = 2293689
47 meter
Z = 17024559
83 Z = 5189085
84
XDOT = -16556
608714 XDOT = -5046
454336
YDOT = 17066
147144 feet/sec YDOT = 5201
761649 meter/sec
ZDOT = 4288
123809 ZDOT = 1307
020137
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 13178
55062094
00016717 00000-0 10270-3 0 9019
2 25544 51
6500 56
9778 0008395 100
4126 259
7971 15
50454457 36313
Satellite: ISS
Catalog Number: 25544
Epoch time: 13178
55062094 = yrday
fracday
Element set: 901
Inclination: 51
6500 deg
RA of node: 56
9778 deg
Eccentricity:
0008395
Arg of perigee: 100
4126 deg
Mean anomaly: 259
7971 deg
Mean motion: 15
50454457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3631
Checksum: 316
Coasting Arc #3 (Orbit 3645)
---------------------------------------
Vector Time (GMT): 2013/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2719486
04 A = 6788146
70 meter
Y = -3270028
37 meter E =
0022483
Z = -5309944
77 I = 51
91097
XDOT = 5183
275945 Wp = 90
85748
YDOT = 5566
834204 meter/sec RA = 51
63450 deg
ZDOT = -776
785689 TA = 171
74443
MA = 171
70738
Ha = 229
707 n
mi
Hp = 217
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8922198
28 X = 2781644
13
Y = -10728439
54 feet Y = -3239269
36 meter
Z = -17421078
64 Z = -5296583
17
XDOT = 17005
498508 XDOT = 5124
414549
YDOT = 18263
891746 feet/sec YDOT = 5624
467824 meter/sec
ZDOT = -2548
509477 ZDOT = -751
748510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11605521
66 X = -3537363
00
Y = -7872714
65 feet Y = -2399603
43 meter
Z = -17364655
16 Z = -5292746
89
XDOT = 15832
845125 XDOT = 4825
851194
YDOT = -17970
942425 feet/sec YDOT = -5477
543251 meter/sec
ZDOT = -2444
591041 ZDOT = -745
111349
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 13179
51743289
00016717 00000-0 10270-3 0 9029
2 25544 51
6496 52
1841 0008217 103
4784 256
7283 15
50494203 36464
Satellite: ISS
Catalog Number: 25544
Epoch time: 13179
51743289 = yrday
fracday
Element set: 902
Inclination: 51
6496 deg
RA of node: 52
1841 deg
Eccentricity:
0008217
Arg of perigee: 103
4784 deg
Mean anomaly: 256
7283 deg
Mean motion: 15
50494203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3646
Checksum: 317
Coasting Arc #4 (Orbit 3661)
---------------------------------------
Vector Time (GMT): 2013/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2876253
10 A = 6787916
91 meter
Y = 3045969
60 meter E =
0010633
Z = 5332113
29 I = 51
89090
XDOT = -5380
971985 Wp = 105
03366
YDOT = -5462
650460 meter/sec RA = 46
69109 deg
ZDOT = 214
884876 TA = 342
90816
MA = 342
94394
Ha = 229
769 n
mi
Hp = 217
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9436525
92 X = -2936001
84
Y = 9993338
57 feet Y = 3013471
00 meter
Z = 17493810
02 Z = 5317995
91
XDOT = -17654
107562 XDOT = -5320
531365
YDOT = -17922
081561 feet/sec YDOT = -5522
485962 meter/sec
ZDOT = 705
002875 ZDOT = 188
891092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11071477
84 X = 3374586
44
Y = 8271475
37 feet Y = 2521145
69 meter
Z = 17434256
50 Z = 5313961
38
XDOT = -15061
740184 XDOT = -4590
818408
YDOT = 18880
717025 feet/sec YDOT = 5754
842549 meter/sec
ZDOT = 597
073806 ZDOT = 181
988096
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 13180
54868353
00016717 00000-0 10270-3 0 9035
2 25544 51
6499 47
0719 0008201 107
5247 252
6800 15
50505638 36629
Satellite: ISS
Catalog Number: 25544
Epoch time: 13180
54868353 = yrday
fracday
Element set: 903
Inclination: 51
6499 deg
RA of node: 47
0719 deg
Eccentricity:
0008201
Arg of perigee: 107
5247 deg
Mean anomaly: 252
6800 deg
Mean motion: 15
50505638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3662
Checksum: 308
Coasting Arc #5 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2013/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3102029
32 A = 6787886
72 meter
Y = -2851426
46 meter E =
0022584
Z = -5341308
81 I = 51
86845
XDOT = 5502
606485 Wp = 98
99062
YDOT = 5295
843596 meter/sec RA = 41
74448 deg
ZDOT = 366
442760 TA = 174
51496
MA = 174
49018
Ha = 229
541 n
mi
Hp = 217
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10177261
56 X = 3159630
61
Y = -9355073
67 feet Y = -2816415
07 meter
Z = -17523979
03 Z = -5326099
80
XDOT = 18053
170883 XDOT = 5441
198173
YDOT = 17374
814947 feet/sec YDOT = 5357
033832 meter/sec
ZDOT = 1202
240027 ZDOT = 393
025171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10681791
43 X = -3255810
03
Y = -8901439
16 feet Y = -2713158
66 meter
Z = -17459885
74 Z = -5321773
17
XDOT = 14079
659354 XDOT = 4291
480171
YDOT = -19484
019492 feet/sec YDOT = -5938
729141 meter/sec
ZDOT = 1312
648357 ZDOT = 400
095219
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 13181
51546539
00016717 00000-0 10270-3 0 9043
2 25544 51
6491 42
2779 0008068 110
7999 249
4017 15
50539013 36779
Satellite: ISS
Catalog Number: 25544
Epoch time: 13181
51546539 = yrday
fracday
Element set: 904
Inclination: 51
6491 deg
RA of node: 42
2779 deg
Eccentricity:
0008068
Arg of perigee: 110
7999 deg
Mean anomaly: 249
4017 deg
Mean motion: 15
50539013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3677
Checksum: 326
Coasting Arc #6 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2013/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3334341
43 A = 6788082
42 meter
Y = 2671800
13 meter E =
0010407
Z = 5265537
61 I = 51
84616
XDOT = -5617
972700 Wp = 97
68833
YDOT = -5135
793273 meter/sec RA = 36
79797 deg
ZDOT = -951
302118 TA = 1
38697
MA = 1
38409
Ha = 229
579 n
mi
Hp = 217
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10939440
38 X = -3389548
80
Y = 8765748
44 feet Y = 2634204
21 meter
Z = 17275385
86 Z = 5249205
85
XDOT = -18431
668964 XDOT = -5555
504440
YDOT = -16849
715461 feet/sec YDOT = -5198
267618 meter/sec
ZDOT = -3121
069940 ZDOT = -978
442489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10368588
25 X = 3160345
70
Y = 9558935
44 feet Y = 2913563
52 meter
Z = 17206620
50 Z = 5244577
93
XDOT = -13105
695644 XDOT = -3994
616032
YDOT = 20038
309294 feet/sec YDOT = 6107
676673 meter/sec
ZDOT = -3233
828163 ZDOT = -985
670824
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 13182
54668359
00016717 00000-0 10270-3 0 9053
2 25544 51
6494 37
1658 0008005 114
8891 245
3093 15
50555138 36931
Satellite: ISS
Catalog Number: 25544
Epoch time: 13182
54668359 = yrday
fracday
Element set: 905
Inclination: 51
6494 deg
RA of node: 37
1658 deg
Eccentricity:
0008005
Arg of perigee: 114
8891 deg
Mean anomaly: 245
3093 deg
Mean motion: 15
50555138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 328
Coasting Arc #7 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2013/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3618433
59 A = 6788522
81 meter
Y = -2539081
06 meter E =
0021327
Z = -5171130
24 I = 51
82138
XDOT = 5645
508038 Wp = 107
54166
YDOT = 4924
468056 meter/sec RA = 31
84801 deg
ZDOT = 1531
365164 TA = 177
22434
MA = 177
21248
Ha = 229
378 n
mi
Hp = 217
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11871501
28 X = 3671677
17
Y = -8330318
43 feet Y = -2498319
17 meter
Z = -16965650
40 Z = -5153423
17
XDOT = 18522
007998 XDOT = 5582
583023
YDOT = 16156
391259 feet/sec YDOT = 4987
247686 meter/sec
ZDOT = 5024
163924 ZDOT = 1558
638257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10261980
83 X = -3127851
76
Y = -10370191
76 feet Y = -3160834
45 meter
Z = -16891148
97 Z = -5148422
21
XDOT = 11990
428440 XDOT = 3654
682589
YDOT = -20238
951139 feet/sec YDOT = -6168
832307 meter/sec
ZDOT = 5137
501813 ZDOT = 1565
910553
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 13183
51343568
00016717 00000-0 10270-3 0 9064
2 25544 51
6481 32
3713 0007963 118
3205 241
8749 15
50581276 37084
Satellite: ISS
Catalog Number: 25544
Epoch time: 13183
51343568 = yrday
fracday
Element set: 906
Inclination: 51
6481 deg
RA of node: 32
3713 deg
Eccentricity:
0007963
Arg of perigee: 118
3205 deg
Mean anomaly: 241
8749 deg
Mean motion: 15
50581276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 312
Coasting Arc #8 (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 = -3900948
25 A = 6789156
48 meter
Y = 2424061
16 meter E =
0011935
Z = 4989393
24 I = 51
79743
XDOT = -5652
718695 Wp = 93
49583
YDOT = -4734
583265 meter/sec RA = 26
89835 deg
ZDOT = -2115
655747 TA = 17
07039
MA = 17
03027
Ha = 229
386 n
mi
Hp = 217
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12798386
65 X = -3952001
81
Y = 7952956
57 feet Y = 2380152
21 meter
Z = 16369400
38 Z = 4970319
09
XDOT = -18545
665010 XDOT = -5589
078159
YDOT = -15533
409662 feet/sec YDOT = -4797
439434 meter/sec
ZDOT = -6941
127779 ZDOT = -2142
962154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10242127
37 X = 3121800
42
Y = 11169890
24 feet Y = 3404582
54 meter
Z = 16289194
79 Z = 4964946
57
XDOT = -10955
323171 XDOT = -3339
182503
YDOT = 20350
780241 feet/sec YDOT = 6202
917818 meter/sec
ZDOT = -7054
627828 ZDOT = -2150
250562
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
54462150
00016717 00000-0 10270-3 0 9078
2 25544 51
6484 27
2589 0007851 122
4586 237
7325 15
50602142 37243
Satellite: ISS
Catalog Number: 25544
Epoch time: 13184
54462150 = yrday
fracday
Element set: 907
Inclination: 51
6484 deg
RA of node: 27
2589 deg
Eccentricity:
0007851
Arg of perigee: 122
4586 deg
Mean anomaly: 237
7325 deg
Mean motion: 15
50602142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 305
Coasting Arc #9 (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 = 4213370
00 A = 6790006
21 meter
Y = -2368012
00 meter E =
0018761
Z = -4787207
23 I = 51
77120
XDOT = 5568
384842 Wp = 115
50631
YDOT = 4511
019367 meter/sec RA = 21
94539 deg
ZDOT = 2669
827269 TA = 180
87819
MA = 180
88149
Ha = 229
217 n
mi
Hp = 217
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13823392
38 X = 4262791
37
Y = -7769068
23 feet Y = -2320618
45 meter
Z = -15706060
48 Z = -4766619
39
XDOT = 18268
979142 XDOT = 5504
558525
YDOT = 14799
932307 feet/sec YDOT = 4572
931324 meter/sec
ZDOT = 8759
275816 ZDOT = 2696
723508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10462283
87 X = -3188904
12
Y = -12028960
68 feet Y = -3666427
21 meter
Z = -15619528
01 Z = -4760832
14
XDOT = 9869
419311 XDOT = 3008
199006
YDOT = -20101
717731 feet/sec YDOT = -6127
003564 meter/sec
ZDOT = 8871
089966 ZDOT = 2703
908222
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
51134375
00016717 00000-0 10270-3 0 9082
2 25544 51
6470 22
4642 0007916 125
8668 234
3219 15
50624005 37398
Satellite: ISS
Catalog Number: 25544
Epoch time: 13185
51134375 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 22
4642 deg
Eccentricity:
0007916
Arg of perigee: 125
8668 deg
Mean anomaly: 234
3219 deg
Mean motion: 15
50624005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 304
Coasting Arc #10 (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 = -4512897
78 A = 6791016
68 meter
Y = 2327548
50 meter E =
0014543
Z = 4495971
81 I = 51
74617
XDOT = -5452
382430 Wp = 96
31639
YDOT = -4325
862441 meter/sec RA = 16
99269 deg
ZDOT = -3226
031589 TA = 26
09956
MA = 26
02632
Ha = 229
199 n
mi
Hp = 217
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14806095
09 X = -4560429
63
Y = 7636313
97 feet Y = 2276816
02 meter
Z = 14750563
68 Z = 4473933
55
XDOT = -17888
393799 XDOT = -5387
933357
YDOT = -14192
462076 feet/sec YDOT = -4386
473607 meter/sec
ZDOT = -10584
093139 ZDOT = -3252
362719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10755054
46 X = 3278140
60
Y = 12829095
04 feet Y = 3910308
17 meter
Z = 14657966
97 Z = 4467748
33
XDOT = -8945
450629 XDOT = -2726
573352
YDOT = 19745
166220 feet/sec YDOT = 6018
326664 meter/sec
ZDOT = -10693
569062 ZDOT = -3259
399850
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
54249710
00016717 00000-0 10270-3 0 9097
2 25544 51
6472 17
3512 0007777 130
0490 230
1344 15
50646686 37555
Satellite: ISS
Catalog Number: 25544
Epoch time: 13186
54249710 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 17
3512 deg
Eccentricity:
0007777
Arg of perigee: 130
0490 deg
Mean anomaly: 230
1344 deg
Mean motion: 15
50646686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 306
Coasting Arc #11 (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 = 4818227
65 A = 6792131
00 meter
Y = -2351097
39 meter E =
0015210
Z = -4186809
37 I = 51
71948
XDOT = 5251
218699 Wp = 121
06750
YDOT = 4127
742833 meter/sec RA = 12
03725 deg
ZDOT = 3727
637831 TA = 187
29690
MA = 187
31907
Ha = 229
058 n
mi
Hp = 217
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15807833
51 X = 4864498
25
Y = -7713574
11 feet Y = -2296957
61 meter
Z = -13736251
21 Z = -4163290
99
XDOT = 17228
407804 XDOT = 5186
563393
YDOT = 13542
463364 feet/sec YDOT = 4186
103232 meter/sec
ZDOT = 12229
782909 ZDOT = 3752
991129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11286812
84 X = -3440220
55
Y = -13590403
50 feet Y = -4142354
99 meter
Z = -13637456
20 Z = -4156696
65
XDOT = 8064
321185 XDOT = 2458
005097
YDOT = -19067
339553 feet/sec YDOT = -5811
725096 meter/sec
ZDOT = 12335
197616 ZDOT = 3759
768233
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
50918920
00016717 00000-0 10270-3 0 9102
2 25544 51
6462 12
5562 0007923 133
2521 226
9292 15
50669519 37701
Satellite: ISS
Catalog Number: 25544
Epoch time: 13187
50918920 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 12
5562 deg
Eccentricity:
0007923
Arg of perigee: 133
2521 deg
Mean anomaly: 226
9292 deg
Mean motion: 15
50669519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3770
Checksum: 307
Coasting Arc #12 (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 = -5097669
86 A = 6793368
72 meter
Y = 2382133
22 meter E =
0017358
Z = 3788228
23 I = 51
69369
XDOT = -5011
284739 Wp = 104
39532
YDOT = -3985
799971 meter/sec RA = 7
08188 deg
ZDOT = -4225
130574 TA = 30
23155
MA = 30
13151
Ha = 229
011 n
mi
Hp = 217
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16724638
66 X = -5142330
51
Y = 7815397
72 feet Y = 2324877
62 meter
Z = 12428570
32 Z = 3763356
33
XDOT = -16441
222897 XDOT = -4945
817897
YDOT = -13076
771560 feet/sec YDOT = -4041
472686 meter/sec
ZDOT = -13861
976950 ZDOT = -4249
316224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11849414
28 X = 3611701
47
Y = 14246793
32 feet Y = 4342422
60 meter
Z = 12324106
50 Z = 3756387
66
XDOT = -7426
554808 XDOT = -2263
613906
YDOT = 18289
364637 feet/sec YDOT = 5574
598341 meter/sec
ZDOT = -13962
528410 ZDOT = -4255
778659
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
54030989
00016717 00000-0 10270-3 0 9118
2 25544 51
6463 7
4427 0007777 137
4618 222
7137 15
50691299 37864
Satellite: ISS
Catalog Number: 25544
Epoch time: 13188
54030989 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 7
4427 deg
Eccentricity:
0007777
Arg of perigee: 137
4618 deg
Mean anomaly: 222
7137 deg
Mean motion: 15
50691299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3786
Checksum: 336
Coasting Arc #13 (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 = 5359661
53 A = 6794543
89 meter
Y = -2474467
89 meter E =
0011396
Z = -3378690
40 I = 51
66730
XDOT = 4703
181982 Wp = 120
35244
YDOT = 3850
913707 meter/sec RA = 2
12457 deg
ZDOT = 4646
520438 TA = 200
35733
MA = 200
40280
Ha = 228
888 n
mi
Hp = 217
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17584191
38 X = 5403345
77
Y = -8118332
98 feet Y = -2414288
08 meter
Z = -11084942
26 Z = -3352548
21
XDOT = 15430
387079 XDOT = 4637
199448
YDOT = 12634
231323 feet/sec YDOT = 3903
138122 meter/sec
ZDOT = 15244
489625 ZDOT = 4669
208004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12615723
45 X = -3845272
51
Y = -14777573
66 feet Y = -4504204
45 meter
Z = -10975149
21 Z = -3345225
48
XDOT = 6908
739709 XDOT = 2105
783863
YDOT = -17274
960941 feet/sec YDOT = -5265
408095 meter/sec
ZDOT = 15338
794907 ZDOT = 4675
264688
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
50697145
00016717 00000-0 10270-3 0 9129
2 25544 51
6462 2
6479 0007948 140
4012 219
7721 15
50717867 38012
Satellite: ISS
Catalog Number: 25544
Epoch time: 13189
50697145 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 2
6479 deg
Eccentricity:
0007948
Arg of perigee: 140
4012 deg
Mean anomaly: 219
7721 deg
Mean motion: 15
50717867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3801
Checksum: 315
Coasting Arc #14 (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 = -5583150
88 A = 6795772
48 meter
Y = 2559806
56 meter E =
0019620
Z = 2881765
99 I = 51
64074
XDOT = -4354
783040 Wp = 115
26566
YDOT = -3788
516494 meter/sec RA = 357
16694 deg
ZDOT = -5053
018126 TA = 31
93538
MA = 31
81660
Ha = 228
794 n
mi
Hp = 218
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18317424
14 X = -5625358
86
Y = 8398315
49 feet Y = 2497135
91 meter
Z = 9454612
82 Z = 2854541
73
XDOT = -14287
345932 XDOT = -4287
549552
YDOT = -12429
516057 feet/sec YDOT = -3836
837914 meter/sec
ZDOT = -16578
143457 ZDOT = -5074
010090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13344679
86 X = 4067458
42
Y = 15169973
78 feet Y = 4623808
01 meter
Z = 9340280
98 Z = 2846917
64
XDOT = -6702
306576 XDOT = -2042
863044
YDOT = 16195
135118 feet/sec YDOT = 4936
277184 meter/sec
ZDOT = -16665
364726 ZDOT = -5079
603168
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
53805927
00016717 00000-0 10270-3 0 9134
2 25544 51
6461 357
5339 0007794 144
6108 215
5562 15
50740356 38172
Satellite: ISS
Catalog Number: 25544
Epoch time: 13190
53805927 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 357
5339 deg
Eccentricity:
0007794
Arg of perigee: 144
6108 deg
Mean anomaly: 215
5562 deg
Mean motion: 15
50740356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3817
Checksum: 320
Coasting Arc #15 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2013/191/05:45:10
954
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4816879
06 A = 6796701
84 meter
Y = -3317085
61 meter E =
0007412
Z = -3472234
89 I = 51
61797
XDOT = 5359
011717 Wp = 125
98736
YDOT = 3018
850579 meter/sec RA = 353
49789 deg
ZDOT = 4552
934274 TA = 193
37719
MA = 193
39685
Ha = 228
585 n
mi
Hp = 220
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15803408
97 X = 4870480
33
Y = -10882826
79 feet Y = -3262920
15 meter
Z = -11391846
75 Z = -3448705
45
XDOT = 17582
059438 XDOT = 5302
739411
YDOT = 9904
365418 feet/sec YDOT = 3078
463321 meter/sec
ZDOT = 14937
448405 ZDOT = 4578
831097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12819828
07 X = 3907483
59
Y = -14355530
30 feet Y = -4375565
63 meter
Z = -11292855
47 Z = -3442062
35
XDOT = 18300
136481 XDOT = 5577
881599
YDOT = 4513
670775 feet/sec YDOT = 1375
766852 meter/sec
ZDOT = 15045
318398 ZDOT = 4585
813048
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
24692290
00016717 00000-0 10270-3 0 9141
2 25544 51
6512 354
0212 0004445 166
3714 193
7558 15
49884924 38287
Satellite: ISS
Catalog Number: 25544
Epoch time: 13191
24692290 = yrday
fracday
Element set: 914
Inclination: 51
6512 deg
RA of node: 354
0212 deg
Eccentricity:
0004445
Arg of perigee: 166
3714 deg
Mean anomaly: 193
7558 deg
Mean motion: 15
49884924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 322
Coasting Arc #16 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2013/192/05:45:10
954
Vector Time (MET): N/A
Weight (LBS) : 921285
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4790383
06 A = 6797379
38 meter
Y = 3575059
31 meter E =
0014562
Z = 3218977
23 I = 51
58984
XDOT = -5304
457413 Wp = 110
46722
YDOT = -2792
178811 meter/sec RA = 348
54260 deg
ZDOT = -4780
315980 TA = 32
29682
MA = 32
20774
Ha = 228
569 n
mi
Hp = 220
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15716479
85 X = -4845640
79
Y = 11729197
22 feet Y = 3521180
98 meter
Z = 10560948
93 Z = 3195572
44
XDOT = -17403
075501 XDOT = -5249
619309
YDOT = -9160
691637 feet/sec YDOT = -2851
189573 meter/sec
ZDOT = -15683
451377 ZDOT = -4805
951202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12266020
24 X = -3738682
97
Y = 15368717
36 feet Y = 4684385
05 meter
Z = 10462443
43 Z = 3188952
76
XDOT = -17949
834504 XDOT = -5471
109557
YDOT = -3548
305542 feet/sec YDOT = -1081
523529 meter/sec
ZDOT = -15790
262740 ZDOT = -4812
872083
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
27857313
00016717 00000-0 10270-3 0 9155
2 25544 51
6511 348
9118 0004410 169
4942 190
6302 15
49892038 38448
Satellite: ISS
Catalog Number: 25544
Epoch time: 13192
27857313 = yrday
fracday
Element set: 915
Inclination: 51
6511 deg
RA of node: 348
9118 deg
Eccentricity:
0004410
Arg of perigee: 169
4942 deg
Mean anomaly: 190
6302 deg
Mean motion: 15
49892038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 317
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