[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 13th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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
166/13:46:01
000 0
0 0
0 0
0
N/A 0
0 0
0 230
2
000/00:00:00
000 0
0 0
0 216
1
170/12:58:27
645 -0
1 3
2 3
2
N/A 3
1 0
0 230
0
000/00:06:55
289 -0
4 -0
1 217
9
Coasting Arc #1 (Orbit 3397)
---------------------------------------
Vector Time (GMT): 2013/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 881745
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3926095
44 A = 6798869
96 meter
Y = -5494374
62 meter E =
0019993
Z = 757164
21 I = 51
92989
XDOT = 4265
300430 Wp = 97
11611
YDOT = 2207
039443 meter/sec RA = 130
58662 deg
ZDOT = -5968
736539 TA = 74
74715
MA = 74
52620
Ha = 230
069 n
mi
Hp = 216
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12880890
55 X = 3983564
84
Y = -18026163
44 feet Y = -5450149
30 meter
Z = 2484134
56 Z = 776375
71
XDOT = 13993
767816 XDOT = 4269
298270
YDOT = 7240
943055 feet/sec YDOT = 2254
759811 meter/sec
ZDOT = -19582
468959 ZDOT = -5948
006154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15562649
53 X = -4743495
58
Y = -15756096
13 feet Y = -4802458
10 meter
Z = 2565191
72 Z = 781870
44
XDOT = 8395
712225 XDOT = 2559
013086
YDOT = -11535
280663 feet/sec YDOT = -3515
953546 meter/sec
ZDOT = -19496
080085 ZDOT = -5942
405210
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 13163
53380867
00016717 00000-0 10270-3 0 9001
2 25544 51
6448 131
4237 0010723 58
9557 301
2645 15
50763621 33983
Satellite: ISS
Catalog Number: 25544
Epoch time: 13163
53380867 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 131
4237 deg
Eccentricity:
0010723
Arg of perigee: 58
9557 deg
Mean anomaly: 301
2645 deg
Mean motion: 15
50763621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3398
Checksum: 308
Coasting Arc #2 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2013/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 881745
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3827551
36 A = 6799060
21 meter
Y = 5605460
87 meter E =
0022007
Z = -200605
58 I = 51
94985
XDOT = -3996
640422 Wp = 53
29455
YDOT = -2529
906693 meter/sec RA = 125
65176 deg
ZDOT = 6033
175586 TA = 304
55551
MA = 304
76300
Ha = 230
065 n
mi
Hp = 216
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12557583
20 X = -3888973
88
Y = 18390619
66 feet Y = 5562315
37 meter
Z = -658154
78 Z = -219348
01
XDOT = -13112
337343 XDOT = -3997
360868
YDOT = -8300
218809 feet/sec YDOT = -2574
604333 meter/sec
ZDOT = 19793
883157 ZDOT = 6013
758294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16239643
68 X = 4949843
39
Y = 15233888
23 feet Y = 4643289
13 meter
Z = -737277
15 Z = -224722
08
XDOT = -9125
639374 XDOT = -2781
494881
YDOT = 10615
592752 feet/sec YDOT = 3235
632671 meter/sec
ZDOT = 19713
021749 ZDOT = 6008
529029
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 13164
50043553
00016717 00000-0 10270-3 0 9018
2 25544 51
6448 126
6304 0010694 63
1750 297
0493 15
50780051 34131
Satellite: ISS
Catalog Number: 25544
Epoch time: 13164
50043553 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 126
6304 deg
Eccentricity:
0010694
Arg of perigee: 63
1750 deg
Mean anomaly: 297
0493 deg
Mean motion: 15
50780051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 283
Coasting Arc #3 (Orbit 3428)
---------------------------------------
Vector Time (GMT): 2013/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 881745
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3756574
69 A = 6798987
86 meter
Y = -5647673
55 meter E =
0017711
Z = -440619
86 I = 51
96776
XDOT = 3728
257985 Wp = 103
05673
YDOT = 2932
835725 meter/sec RA = 120
71751 deg
ZDOT = -6012
945187 TA = 81
66397
MA = 81
46319
Ha = 230
094 n
mi
Hp = 216
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12324720
12 X = 3821589
41
Y = -18529112
68 feet Y = -5605301
60 meter
Z = -1445603
21 Z = -422213
41
XDOT = 12231
817537 XDOT = 3724
394486
YDOT = 9622
164451 feet/sec YDOT = 2974
506428 meter/sec
ZDOT = -19727
510457 ZDOT = -5994
842787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16666726
80 X = -5080018
33
Y = -14753496
65 feet Y = -4496865
78 meter
Z = -1367869
14 Z = -416926
51
XDOT = 10145
121735 XDOT = 3092
233105
YDOT = -9705
227964 feet/sec YDOT = -2958
153483 meter/sec
ZDOT = -19652
197778 ZDOT = -5989
989883
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 13165
53149480
00016717 00000-0 10270-3 0 9029
2 25544 51
6457 121
5160 0010676 65
9498 294
2769 15
50784563 34298
Satellite: ISS
Catalog Number: 25544
Epoch time: 13165
53149480 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 121
5160 deg
Eccentricity:
0010676
Arg of perigee: 65
9498 deg
Mean anomaly: 294
2769 deg
Mean motion: 15
50784563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3429
Checksum: 331
Coasting Arc #4 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2013/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 881745
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3606953
04 A = 6798611
33 meter
Y = 5662575
78 meter E =
0023960
Z = 1003658
51 I = 51
98130
XDOT = -3543
734941 Wp = 62
04911
YDOT = -3325
830196 meter/sec RA = 115
78459 deg
ZDOT = 5931
872543 TA = 308
76781
MA = 308
98165
Ha = 230
079 n
mi
Hp = 216
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11833835
42 X = -3674880
60
Y = 18578004
53 feet Y = 5621860
67 meter
Z = 3292842
89 Z = 985971
74
XDOT = -11626
426973 XDOT = -3535
096836
YDOT = -10911
516391 feet/sec YDOT = -3365
410680 meter/sec
ZDOT = 19461
524090 ZDOT = 5914
678098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17024167
12 X = 5188966
14
Y = 13994508
10 feet Y = 4265526
07 meter
Z = 3218105
72 Z = 980878
62
XDOT = -11218
315830 XDOT = -3419
342665
YDOT = 9113
430971 feet/sec YDOT = 2777
773760 meter/sec
ZDOT = 19390
060092 ZDOT = 5910
090316
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 13166
56254420
00016717 00000-0 10270-3 0 9035
2 25544 51
6455 116
4027 0010632 69
9726 290
2569 15
50804284 34456
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
56254420 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 116
4027 deg
Eccentricity:
0010632
Arg of perigee: 69
9726 deg
Mean anomaly: 290
2569 deg
Mean motion: 15
50804284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 305
Coasting Arc #5 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2013/166/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 924038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4694900
50 A = 6789632
40 meter
Y = 1263192
17 meter E =
0017079
Z = 4724619
48 I = 51
95387
XDOT = 931
702733 Wp = 89
97817
YDOT = -7079
636163 meter/sec RA = 115
43330 deg
ZDOT = 2809
942290 TA = 332
26731
MA = 332
35828
Ha = 230
182 n
mi
Hp = 216
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15403216
86 X = -4731627
77
Y = 4144331
28 feet Y = 1210485
08 meter
Z = 15500720
08 Z = 4701722
97
XDOT = 3056
767498 XDOT = 997
149569
YDOT = -23227
152766 feet/sec YDOT = -7068
851577 meter/sec
ZDOT = 9218
970768 ZDOT = 2814
626792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9126428
38 X = 2781735
37
Y = 13194988
23 feet Y = 4021832
41 meter
Z = 15404787
74 Z = 4695379
30
XDOT = -21916
380014 XDOT = -6680
112628
YDOT = 4338
089892 feet/sec YDOT = 1322
249799 meter/sec
ZDOT = 9239
520001 ZDOT = 2816
205696
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 13166
62698415
00016717 00000-0 10270-3 0 9049
2 25544 51
6469 116
0837 0010599 70
2466 289
9827 15
50815239 34469
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
62698415 = yrday
fracday
Element set: 904
Inclination: 51
6469 deg
RA of node: 116
0837 deg
Eccentricity:
0010599
Arg of perigee: 70
2466 deg
Mean anomaly: 289
9827 deg
Mean motion: 15
50815239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 342
Coasting Arc #6 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2013/167/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 924038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4521212
68 A = 6788562
28 meter
Y = -923787
76 meter E =
0023092
Z = -5000212
38 I = 51
96327
XDOT = -908
440785 Wp = 73
83739
YDOT = 7274
859550 meter/sec RA = 110
49105 deg
ZDOT = -2167
510982 TA = 175
07566
MA = 175
05291
Ha = 230
076 n
mi
Hp = 216
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14833374
93 X = 4555496
40
Y = -3030799
72 feet Y = -873036
61 meter
Z = -16404896
26 Z = -4978165
47
XDOT = -2980
448769 XDOT = -979
193105
YDOT = 23867
649443 feet/sec YDOT = 7264
305365 meter/sec
ZDOT = -7111
256501 ZDOT = -2172
095398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8111071
42 X = -2472254
57
Y = -12901410
13 feet Y = -3932349
81 meter
Z = -16312557
04 Z = -4972067
39
XDOT = 22425
364972 XDOT = 6835
251244
YDOT = -5090
390541 feet/sec YDOT = -1551
551037 meter/sec
ZDOT = -7131
424357 ZDOT = -2173
658144
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 13167
59358467
00016717 00000-0 10270-3 0 9057
2 25544 51
6475 111
2889 0010703 73
3187 286
9138 15
50825330 34613
Satellite: ISS
Catalog Number: 25544
Epoch time: 13167
59358467 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 111
2889 deg
Eccentricity:
0010703
Arg of perigee: 73
3187 deg
Mean anomaly: 286
9138 deg
Mean motion: 15
50825330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 324
Coasting Arc #7 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2013/168/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 924038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4350668
82 A = 6787666
12 meter
Y = 557441
60 meter E =
0014171
Z = 5167978
45 I = 51
97014
XDOT = 848
505231 Wp = 91
60249
YDOT = -7474
252006 meter/sec RA = 105
54919 deg
ZDOT = 1516
558588 TA = 343
84406
MA = 343
88919
Ha = 230
156 n
mi
Hp = 216
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14273847
83 X = -4381683
70
Y = 1828876
63 feet Y = 508615
84 meter
Z = 16955309
88 Z = 5146767
87
XDOT = 2783
809814 XDOT = 924
653791
YDOT = -24521
824166 feet/sec YDOT = -7464
337838 meter/sec
ZDOT = 4975
585920 ZDOT = 1520
864929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7009511
49 X = 2136499
10
Y = 12686903
37 feet Y = 3866968
15 meter
Z = 16866513
76 Z = 5140913
39
XDOT = -22880
204683 XDOT = -6973
886387
YDOT = 5983
853739 feet/sec YDOT = 1823
878620 meter/sec
ZDOT = 4994
631185 ZDOT = 1522
363585
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 13168
62461455
00016717 00000-0 10270-3 0 9065
2 25544 51
6472 106
1750 0010552 77
2442 282
9888 15
50850358 34772
Satellite: ISS
Catalog Number: 25544
Epoch time: 13168
62461455 = yrday
fracday
Element set: 906
Inclination: 51
6472 deg
RA of node: 106
1750 deg
Eccentricity:
0010552
Arg of perigee: 77
2442 deg
Mean anomaly: 282
9888 deg
Mean motion: 15
50850358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 321
Coasting Arc #8 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2013/169/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 924038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4252237
00 A = 6787148
17 meter
Y = -150412
41 meter E =
0025118
Z = -5309702
11 I = 51
97652
XDOT = -760
825162 Wp = 82
27475
YDOT = 7561
570129 meter/sec RA = 100
60652 deg
ZDOT = -823
562491 TA = 179
86500
MA = 179
86432
Ha = 230
040 n
mi
Hp = 216
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13950908
81 X = 4279396
24
Y = -493479
04 feet Y = -102708
86 meter
Z = -17420282
50 Z = -5288978
97
XDOT = -2496
145544 XDOT = -841
323046
YDOT = 24808
300948 feet/sec YDOT = 7552
612089 meter/sec
ZDOT = -2701
976677 ZDOT = -827
453371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5871093
97 X = -1789509
44
Y = -12783386
55 feet Y = -3896376
22 meter
Z = -17333577
37 Z = -5283274
38
XDOT = 22917
095971 XDOT = 6985
130852
YDOT = -6838
277234 feet/sec YDOT = -2084
306901 meter/sec
ZDOT = -2719
311965 ZDOT = -828
846287
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 13169
59119837
00016717 00000-0 10270-3 0 9077
2 25544 51
6480 101
3802 0010638 80
3403 279
8950 15
50852200 34923
Satellite: ISS
Catalog Number: 25544
Epoch time: 13169
59119837 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 101
3802 deg
Eccentricity:
0010638
Arg of perigee: 80
3403 deg
Mean anomaly: 279
8950 deg
Mean motion: 15
50852200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 304
Coasting Arc #9 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2013/170/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4038983
06 A = 6788861
14 meter
Y = 1329406
10 meter E =
0022445
Z = -5311680
73 I = 51
98105
XDOT = -1396
893387 Wp = 91
82537
YDOT = 7472
904434 meter/sec RA = 95
80744 deg
ZDOT = 810
386048 TA = 185
89377
MA = 185
92023
Ha = 230
039 n
mi
Hp = 217
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13251256
76 X = 4049620
15
Y = 4361568
57 feet Y = 1374632
63 meter
Z = -17426774
05 Z = -5292033
51
XDOT = -4582
983553 XDOT = -1484
289877
YDOT = 24517
402998 feet/sec YDOT = 7456
794739 meter/sec
ZDOT = 2658
746878 ZDOT = 803
388541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1344988
52 X = 409952
50
Y = -13987898
30 feet Y = -4263511
40 meter
Z = -17344775
79 Z = -5286687
66
XDOT = 23910
689747 XDOT = 7287
978235
YDOT = -950
840879 feet/sec YDOT = -289
816300 meter/sec
ZDOT = 2628
411449 ZDOT = 801
139810
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 13170
55777497
00016717 00000-0 10270-3 0 9088
2 25544 51
6480 96
5856 0008055 83
8589 276
3479 15
50259945 35072
Satellite: ISS
Catalog Number: 25544
Epoch time: 13170
55777497 = yrday
fracday
Element set: 908
Inclination: 51
6480 deg
RA of node: 96
5856 deg
Eccentricity:
0008055
Arg of perigee: 83
8589 deg
Mean anomaly: 276
3479 deg
Mean motion: 15
50259945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3507
Checksum: 364
Coasting Arc #10 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2013/171/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4056707
79 A = 6789035
90 meter
Y = -1518439
85 meter E =
0011710
Z = 5218394
84 I = 51
98443
XDOT = 1126
074744 Wp = 76
19689
YDOT = -7476
050296 meter/sec RA = 90
87180 deg
ZDOT = -1294
824349 TA = 26
20507
MA = 26
14586
Ha = 230
059 n
mi
Hp = 217
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13309408
76 X = -4064776
58
Y = -4981758
03 feet Y = -1563850
34 meter
Z = 17120717
97 Z = 5198667
70
XDOT = 3694
470944 XDOT = 1215
879833
YDOT = -24527
724069 feet/sec YDOT = -7462
955513 meter/sec
ZDOT = -4248
111382 ZDOT = -1289
136802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1693875
30 X = -516293
19
Y = 14209173
03 feet Y = 4330955
94 meter
Z = 17038410
91 Z = 5193307
65
XDOT = -23680
197308 XDOT = -7217
724140
YDOT = 2261
579735 feet/sec YDOT = 689
329503 meter/sec
ZDOT = -4223
236197 ZDOT = -1287
242393
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 13171
58917395
00016717 00000-0 10270-3 0 9096
2 25544 51
6481 91
4742 0007909 87
2068 272
9987 15
50307829 35237
Satellite: ISS
Catalog Number: 25544
Epoch time: 13171
58917395 = yrday
fracday
Element set: 909
Inclination: 51
6481 deg
RA of node: 91
4742 deg
Eccentricity:
0007909
Arg of perigee: 87
2068 deg
Mean anomaly: 272
9987 deg
Mean motion: 15
50307829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 347
Coasting Arc #11 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2013/172/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4138511
28 A = 6789583
00 meter
Y = 1694670
91 meter E =
0021093
Z = -5127551
68 I = 51
98660
XDOT = -852
595979 Wp = 98
45727
YDOT = 7392
233840 meter/sec RA = 85
93632 deg
ZDOT = 1758
181722 TA = 188
49398
MA = 188
52974
Ha = 229
969 n
mi
Hp = 217
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13577792
90 X = 4144161
96
Y = 5559943
92 feet Y = 1740982
76 meter
Z = -16822676
11 Z = -5107433
01
XDOT = -2797
230903 XDOT = -943
735004
YDOT = 24252
735697 feet/sec YDOT = 7382
189707 meter/sec
ZDOT = 5768
312736 ZDOT = 1753
819657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1941872
08 X = 591882
61
Y = -14639504
87 feet Y = -4462121
09 meter
Z = -16738754
38 Z = -5101972
33
XDOT = 23119
219819 XDOT = 7046
738201
YDOT = -3494
743179 feet/sec YDOT = -1065
197721 meter/sec
ZDOT = 5748
976499 ZDOT = 1752
288037
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 13172
55610475
00016717 00000-0 10270-3 0 9105
2 25544 51
6491 86
6822 0007962 90
7174 269
4889 15
50287309 35387
Satellite: ISS
Catalog Number: 25544
Epoch time: 13172
55610475 = yrday
fracday
Element set: 910
Inclination: 51
6491 deg
RA of node: 86
6822 deg
Eccentricity:
0007962
Arg of perigee: 90
7174 deg
Mean anomaly: 269
4889 deg
Mean motion: 15
50287309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 336
Coasting Arc #12 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2013/173/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224874
17 A = 6790058
12 meter
Y = -1876918
86 meter E =
0013623
Z = 4962723
68 I = 51
98574
XDOT = 611
963713 Wp = 77
54872
YDOT = -7311
670157 meter/sec RA = 81
00114 deg
ZDOT = -2236
299267 TA = 34
21383
MA = 34
12612
Ha = 229
983 n
mi
Hp = 217
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13861135
73 X = -4227679
68
Y = -6157870
28 feet Y = -1924180
62 meter
Z = 16281901
82 Z = 4942192
42
XDOT = 2007
754964 XDOT = 704
542268
YDOT = -23988
419149 feet/sec YDOT = -7304
308767 meter/sec
ZDOT = -7336
939852 ZDOT = -2233
102798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2190852
83 X = -667771
94
Y = 15100713
15 feet Y = 4602697
37 meter
Z = 16196277
46 Z = 4936625
37
XDOT = -22560
885553 XDOT = -6876
557917
YDOT = 4608
904990 feet/sec YDOT = 1404
794241 meter/sec
ZDOT = -7322
476262 ZDOT = -2231
890765
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 13173
58748703
00016717 00000-0 10270-3 0 9116
2 25544 51
6493 81
5708 0007838 93
9212 266
2835 15
50335775 35541
Satellite: ISS
Catalog Number: 25544
Epoch time: 13173
58748703 = yrday
fracday
Element set: 911
Inclination: 51
6493 deg
RA of node: 81
5708 deg
Eccentricity:
0007838
Arg of perigee: 93
9212 deg
Mean anomaly: 266
2835 deg
Mean motion: 15
50335775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 331
Coasting Arc #13 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2013/174/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4371393
66 A = 6790854
31 meter
Y = 2028325
46 meter E =
0018875
Z = -4802365
32 I = 51
98286
XDOT = -382
112352 Wp = 104
00583
YDOT = 7152
948309 meter/sec RA = 76
06603 deg
ZDOT = 2677
680853 TA = 192
35908
MA = 192
40544
Ha = 229
871 n
mi
Hp = 217
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14341842
71 X = 4371716
09
Y = 6654611
10 feet Y = 2077211
79 meter
Z = -15755791
74 Z = -4781128
43
XDOT = -1253
649450 XDOT = -475
077163
YDOT = 23467
678178 feet/sec YDOT = 7148
155022 meter/sec
ZDOT = 8785
042170 ZDOT = 2675
600041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2271222
21 X = 692268
53
Y = -15735203
30 feet Y = -4796089
97 meter
Z = -15667233
37 Z = -4775372
73
XDOT = 21723
512586 XDOT = 6621
326636
YDOT = -5587
371605 feet/sec YDOT = -1703
030865 meter/sec
ZDOT = 8775
258251 ZDOT = 2674
698715
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 13174
55440190
00016717 00000-0 10270-3 0 9124
2 25544 51
6497 76
7788 0007828 97
6030 262
6010 15
50314038 35697
Satellite: ISS
Catalog Number: 25544
Epoch time: 13174
55440190 = yrday
fracday
Element set: 912
Inclination: 51
6497 deg
RA of node: 76
7788 deg
Eccentricity:
0007828
Arg of perigee: 97
6030 deg
Mean anomaly: 262
6010 deg
Mean motion: 15
50314038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 315
Coasting Arc #14 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2013/175/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4517959
09 A = 6791583
23 meter
Y = -2180460
25 meter E =
0015816
Z = 4565659
94 I = 51
97745
XDOT = 198
392928 Wp = 82
67020
YDOT = -6997
942957 meter/sec RA = 71
13076 deg
ZDOT = -3134
506699 TA = 38
63411
MA = 38
52106
Ha = 229
880 n
mi
Hp = 217
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14822700
42 X = -4515419
45
Y = -7153740
97 feet Y = -2230969
46 meter
Z = 14979199
27 Z = 4543718
12
XDOT = 650
895433 XDOT = 291
857131
YDOT = -22959
130435 feet/sec YDOT = -6995
201303 meter/sec
ZDOT = -10283
814628 ZDOT = -3133
317055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2333031
37 X = -711107
96
Y = 16376138
82 feet Y = 4991447
11 meter
Z = 14887710
05 Z = 4537774
02
XDOT = -20916
688806 XDOT = -6375
406748
YDOT = 6397
452851 feet/sec YDOT = 1949
943629 meter/sec
ZDOT = -10277
774826 ZDOT = -3132
665767
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 13175
58576753
00016717 00000-0 10270-3 0 9134
2 25544 51
6496 71
6672 0007736 100
6557 259
5466 15
50362720 35858
Satellite: ISS
Catalog Number: 25544
Epoch time: 13175
58576753 = yrday
fracday
Element set: 913
Inclination: 51
6496 deg
RA of node: 71
6672 deg
Eccentricity:
0007736
Arg of perigee: 100
6557 deg
Mean anomaly: 259
5466 deg
Mean motion: 15
50362720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 336
Coasting Arc #15 (Orbit 3599)
---------------------------------------
Vector Time (GMT): 2013/176/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4716230
68 A = 6792558
75 meter
Y = 2285906
04 meter E =
0016070
Z = -4337203
42 I = 51
96922
XDOT = -35
767124 Wp = 107
41917
YDOT = 6779
871206 meter/sec RA = 66
19504 deg
ZDOT = 3540
552334 TA = 198
54306
MA = 198
60169
Ha = 229
757 n
mi
Hp = 217
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15473197
76 X = 4711387
35
Y = 7499691
75 feet Y = 2338619
44 meter
Z = -14229670
02 Z = -4314304
13
XDOT = -117
346206 XDOT = -128
777273
YDOT = 22243
671936 feet/sec YDOT = 6778
950687 meter/sec
ZDOT = 11615
985348 ZDOT = 3540
153625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2174225
63 X = 662703
97
Y = -17136109
05 feet Y = -5223086
04 meter
Z = -14134187
06 Z = -4308100
22
XDOT = 19905
829044 XDOT = 6067
296693
YDOT = -7036
479139 feet/sec YDOT = -2144
718842 meter/sec
ZDOT = 11613
282992 ZDOT = 3539
728656
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 13176
55266656
00016717 00000-0 10270-3 0 9141
2 25544 51
6492 66
8746 0007680 104
6542 255
5461 15
50339003 36005
Satellite: ISS
Catalog Number: 25544
Epoch time: 13176
55266656 = yrday
fracday
Element set: 914
Inclination: 51
6492 deg
RA of node: 66
8746 deg
Eccentricity:
0007680
Arg of perigee: 104
6542 deg
Mean anomaly: 255
5461 deg
Mean motion: 15
50339003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3600
Checksum: 310
Coasting Arc #16 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2013/177/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4906619
96 A = 6793457
32 meter
Y = -2388206
71 meter E =
0017916
Z = 4030765
05 I = 51
95945
XDOT = -68
432185 Wp = 90
39706
YDOT = -6568
621708 meter/sec RA = 61
25915 deg
ZDOT = -3960
133696 TA = 40
63078
MA = 40
49723
Ha = 229
750 n
mi
Hp = 217
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16097834
50 X = -4899129
94
Y = -7835323
85 feet Y = -2443034
22 meter
Z = 13224294
77 Z = 4006947
35
XDOT = -224
515044 XDOT = 24
261649
YDOT = -21550
596155 feet/sec YDOT = -6568
868215 meter/sec
ZDOT = -12992
564619 ZDOT = -3960
241752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1989374
19 X = -606361
25
Y = 17865938
46 feet Y = 5445538
04 meter
Z = 13124983
09 Z = 4000494
84
XDOT = -18966
705187 XDOT = -5781
051741
YDOT = 7468
997620 feet/sec YDOT = 2276
550475 meter/sec
ZDOT = -12992
010957 ZDOT = -3959
964940
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
58401560
00016717 00000-0 10270-3 0 9151
2 25544 51
6492 61
7626 0007605 107
5652 252
6330 15
50387391 36160
Satellite: ISS
Catalog Number: 25544
Epoch time: 13177
58401560 = yrday
fracday
Element set: 915
Inclination: 51
6492 deg
RA of node: 61
7626 deg
Eccentricity:
0007605
Arg of perigee: 107
5652 deg
Mean anomaly: 252
6330 deg
Mean motion: 15
50387391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 305
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