[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: June 20th 2014

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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


176/10:51:32 563 1 4 3 3 3 3
N/A 3 0 -0 0 227 2
000/00:01:05 126 0 5 -0 0 220 8

Coasting Arc #1 (Orbit 1152)
---------------------------------------

Vector Time (GMT): 2014/169/11:48:51
734
Vector Time (MET): N/A
Weight (LBS)     : 888319
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4093710
37                 A    =         6787463
93  meter
 Y    =        1205250
81  meter          E    =           
0018240
 Z    =       -5294032
30                 I    =           51
98714
 XDOT =      -1019
948161                 Wp   =           99
48402
 YDOT =       7524
483303  meter/sec      RA   =           92
26063  deg
 ZDOT =        924
138431                 TA   =          179
33778
                                          MA   =          179
33536
                                          Ha   =            227
686  n
mi
                                          Hp   =            218
728

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13430808
29                 X    =         4105645
30
 Y    =        3954234
95  feet           Y    =         1251096
49  meter
 Z    =      -17368872
37                 Z    =        -5274116
63
 XDOT =      -3346
286619                 XDOT =       -1108
501988
 YDOT =      24686
625010  feet/sec       YDOT =        7512
582376  meter/sec
 ZDOT =       3031
950234                 ZDOT =         918
969237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5566076
58                 X    =         1696540
14
 Y    =      -12960033
40  feet           Y    =        -3950218
18  meter
 Z    =      -17284578
05                 Z    =        -5268339
39
 XDOT =      23151
233854                 XDOT =        7056
496079
 YDOT =       5929
420177  feet/sec       YDOT =        1807
287270  meter/sec
 ZDOT =       3008
707079                 ZDOT =         917
053918


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   14169
50682858  
00016717  00000-0  10270-3 0  9000
2 25544  51
6469  93
0372 0003888 108
3879 251
7695 15
50759850 11530


Satellite: ISS
Catalog Number: 25544
Epoch time:      14169
50682858   =   yrday
fracday
Element set:     900
Inclination:       51
6469  deg
RA of node:        93
0372  deg
Eccentricity:     
0003888     
Arg of perigee:   108
3879  deg
Mean anomaly:     251
7695  deg
Mean motion:   15
50759850  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1153
Checksum:              344


Coasting Arc #2 (Orbit 1168)
---------------------------------------

Vector Time (GMT): 2014/170/11:48:51
734
Vector Time (MET): N/A
Weight (LBS)     : 888319
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4108580
43                 A    =         6787890
87  meter
 Y    =       -1597897
29  meter          E    =           
0007683
 Z    =        5155385
84                 I    =           51
98923
 XDOT =        896
190151                 Wp   =           79
52944
 YDOT =      -7447
799289  meter/sec      RA   =           87
32054  deg
 ZDOT =      -1590
840428                 TA   =           25
75583
                                          MA   =           25
71760
                                          Ha   =            227
734  n
mi
                                          Hp   =            218
594

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13479594
58                 X    =        -4115450
18
 Y    =       -5242445
17  feet           Y    =        -1643880
89  meter
 Z    =       16913995
54                 Z    =         5135410
15
 XDOT =       2940
256402                 XDOT =         987
134312
 YDOT =     -24435
037039  feet/sec       YDOT =       -7437
268893  meter/sec
 ZDOT =      -5219
292742                 ZDOT =       -1586
266552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6628345
47                 X    =        -2020319
70
 Y    =       12965276
69  feet           Y    =         3951816
34  meter
 Z    =       16829515
23                 Z    =         5129636
24
 XDOT =     -23047
122473                 XDOT =       -7024
762930
 YDOT =      -5020
175823  feet/sec       YDOT =       -1530
149591  meter/sec
 ZDOT =      -5198
577424                 ZDOT =       -1584
526399


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   14170
53788968  
00016717  00000-0  10270-3 0  9015
2 25544  51
6468  87
9238 0003821 111
9305 248
2253 15
50797113 11695


Satellite: ISS
Catalog Number: 25544
Epoch time:      14170
53788968   =   yrday
fracday
Element set:     901
Inclination:       51
6468  deg
RA of node:        87
9238  deg
Eccentricity:     
0003821     
Arg of perigee:   111
9305  deg
Mean anomaly:     248
2253  deg
Mean motion:   15
50797113  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1169
Checksum:              324


Coasting Arc #3 (Orbit 1183)
---------------------------------------

Vector Time (GMT): 2014/171/11:48:51
734
Vector Time (MET): N/A
Weight (LBS)     : 888319
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4189224
04                 A    =         6788726
44  meter
 Y    =        1978363
76  meter          E    =           
0016075
 Z    =       -4977078
46                 I    =           51
99026
 XDOT =       -786
061353                 Wp   =          108
30282
 YDOT =       7275
331385  meter/sec      RA   =           82
37974  deg
 ZDOT =       2231
280489                 TA   =          183
41781
                                          MA   =          183
42881
                                          Ha   =            227
581  n
mi
                                          Hp   =            218
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13744173
35                 X    =         4190967
26
 Y    =        6490694
74  feet           Y    =         2025220
50  meter
 Z    =      -16328997
56                 Z    =        -4956723
36
 XDOT =      -2578
941448                 XDOT =        -878
196208
 YDOT =      23869
197458  feet/sec       YDOT =        7266
025805  meter/sec
 ZDOT =       7320
474045                 ZDOT =        2227
238707

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7670626
02                 X    =         2338006
81
 Y    =      -13228559
90  feet           Y    =        -4032065
06  meter
 Z    =      -16242976
34                 Z    =        -4950859
19
 XDOT =      22585
859122                 XDOT =        6884
169860
 YDOT =       4134
589721  feet/sec       YDOT =        1260
222947  meter/sec
 ZDOT =       7302
033521                 ZDOT =        2225
659817


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   14171
50450084  
00016717  00000-0  10270-3 0  9029
2 25544  51
6475  83
1288 0003835 115
1285 245
0265 15
50793240 11846


Satellite: ISS
Catalog Number: 25544
Epoch time:      14171
50450084   =   yrday
fracday
Element set:     902
Inclination:       51
6475  deg
RA of node:        83
1288  deg
Eccentricity:     
0003835     
Arg of perigee:   115
1285  deg
Mean anomaly:     245
0265  deg
Mean motion:   15
50793240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1184
Checksum:              289


Coasting Arc #4 (Orbit 1199)
---------------------------------------

Vector Time (GMT): 2014/172/11:48:51
734
Vector Time (MET): N/A
Weight (LBS)     : 888319
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4289189
21                 A    =         6789702
66  meter
 Y    =       -2344279
73  meter          E    =           
0010728
 Z    =        4704153
60                 I    =           51
98874
 XDOT =        717
650774                 Wp   =           80
58763
 YDOT =      -7076
896298  meter/sec      RA   =           77
44044  deg
 ZDOT =      -2865
114570                 TA   =           37
75745
                                          MA   =           37
68222
                                          Ha   =            227
637  n
mi
                                          Hp   =            218
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14072143
08                 X    =        -4285507
53
 Y    =       -7691206
47  feet           Y    =        -2392224
05  meter
 Z    =       15433574
79                 Z    =         4683325
95
 XDOT =       2354
497291                 XDOT =         810
650772
 YDOT =     -23218
163707  feet/sec       YDOT =       -7068
350808  meter/sec
 ZDOT =      -9399
982185                 ZDOT =       -2861
403070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8662139
02                 X    =        -2640219
97
 Y    =       13596120
43  feet           Y    =         4144097
51  meter
 Z    =       15345616
81                 Z    =         4677344
00
 XDOT =     -22001
846045                 XDOT =       -6706
162675
 YDOT =      -3400
098068  feet/sec       YDOT =       -1036
349891  meter/sec
 ZDOT =      -9382
963748                 ZDOT =       -2859
927350


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   14172
53554214  
00016717  00000-0  10270-3 0  9034
2 25544  51
6474  78
0152 0003790 118
5291 241
6242 15
50820743 12007


Satellite: ISS
Catalog Number: 25544
Epoch time:      14172
53554214   =   yrday
fracday
Element set:     903
Inclination:       51
6474  deg
RA of node:        78
0152  deg
Eccentricity:     
0003790     
Arg of perigee:   118
5291  deg
Mean anomaly:     241
6242  deg
Mean motion:   15
50820743  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1200
Checksum:              275


Coasting Arc #5 (Orbit 1214)
---------------------------------------

Vector Time (GMT): 2014/173/11:48:51
734
Vector Time (MET): N/A
Weight (LBS)     : 888319
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4445657
95                 A    =         6790902
51  meter
 Y    =        2671011
84  meter          E    =           
0012448
 Z    =       -4396697
35                 I    =           51
98617
 XDOT =       -680
237138                 Wp   =          113
83850
 YDOT =       6798
602941  meter/sec      RA   =           72
50112  deg
 ZDOT =       3445
181524                 TA   =          191
00011
                                          MA   =          191
02735
                                          Ha   =            227
453  n
mi
                                          Hp   =            218
779

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14585491
95                 X    =         4436817
53
 Y    =        8763162
19  feet           Y    =         2720677
09  meter
 Z    =      -14424860
06                 Z    =        -4375122
02
 XDOT =      -2231
749139                 XDOT =        -772
945786
 YDOT =      22305
127759  feet/sec       YDOT =        6790
477356  meter/sec
 ZDOT =      11303
088988                 ZDOT =        3441
652558

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9524295
59                 X    =         2903005
30
 Y    =      -14192828
01  feet           Y    =        -4325973
98  meter
 Z    =      -14333792
28                 Z    =        -4368939
89
 XDOT =      21118
537856                 XDOT =        6436
930338
 YDOT =       2782
291600  feet/sec       YDOT =         848
042480  meter/sec
 ZDOT =      11286
880079                 ZDOT =        3440
241048


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   14173
50213413  
00016717  00000-0  10270-3 0  9046
2 25544  51
6485  73
2205 0003746 122
1678 237
9837 15
50827235 12153


Satellite: ISS
Catalog Number: 25544
Epoch time:      14173
50213413   =   yrday
fracday
Element set:     904
Inclination:       51
6485  deg
RA of node:        73
2205  deg
Eccentricity:     
0003746     
Arg of perigee:   122
1678  deg
Mean anomaly:     237
9837  deg
Mean motion:   15
50827235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1215
Checksum:              293


Coasting Arc #6 (Orbit 1230)
---------------------------------------

Vector Time (GMT): 2014/174/11:48:51
734
Vector Time (MET): N/A
Weight (LBS)     : 888319
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4607741
61                 A    =         6792236
83  meter
 Y    =       -2972896
98  meter          E    =           
0013840
 Z    =        3996095
57                 I    =           51
98053
 XDOT =        706
798362                 Wp   =           90
54905
 YDOT =      -6499
305746  meter/sec      RA   =           67
56304  deg
 ZDOT =      -4008
352657                 TA   =           41
06942
                                          MA   =           40
96531
                                          Ha   =            227
510  n
mi
                                          Hp   =            218
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15117262
51                 X    =        -4593567
39
 Y    =       -9753599
00  feet           Y    =        -3024344
95  meter
 Z    =       13110549
76                 Z    =         3973745
75
 XDOT =       2318
892263                 XDOT =         798
893935
 YDOT =     -21323
181582  feet/sec       YDOT =       -6490
886439  meter/sec
 ZDOT =     -13150
763311                 ZDOT =       -4004
696223

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10287309
85                 X    =        -3135572
04
 Y    =       14842479
80  feet           Y    =         4523987
84  meter
 Z    =       13016254
60                 Z    =         3967354
40
 XDOT =     -20143
019689                 XDOT =       -6139
592401
 YDOT =      -2408
800872  feet/sec       YDOT =        -734
202506  meter/sec
 ZDOT =     -13134
053465                 ZDOT =       -4003
259496


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   14174
53315604  
00016717  00000-0  10270-3 0  9056
2 25544  51
6484  68
1068 0003732 125
3804 234
7696 15
50843971 12314


Satellite: ISS
Catalog Number: 25544
Epoch time:      14174
53315604   =   yrday
fracday
Element set:     905
Inclination:       51
6484  deg
RA of node:        68
1068  deg
Eccentricity:     
0003732     
Arg of perigee:   125
3804  deg
Mean anomaly:     234
7696  deg
Mean motion:   15
50843971  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1231
Checksum:              304


Coasting Arc #7 (Orbit 1245)
---------------------------------------

Vector Time (GMT): 2014/175/11:48:51
734
Vector Time (MET): N/A
Weight (LBS)     : 888319
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4809600
09                 A    =         6793561
54  meter
 Y    =        3214627
83  meter          E    =           
0008384
 Z    =       -3571269
49                 I    =           51
97317
 XDOT =       -775
435957                 Wp   =          108
99324
 YDOT =       6146
879127  meter/sec      RA   =           62
62499  deg
 ZDOT =       4494
670270                 TA   =          209
18164
                                          MA   =          209
22850
                                          Ha   =            227
299  n
mi
                                          Hp   =            218
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15779527
85                 X    =         4790644
06
 Y    =       10546679
24  feet           Y    =         3268306
37  meter
 Z    =      -11716763
43                 Z    =        -3547950
66
 XDOT =      -2544
081224                 XDOT =        -865
947857
 YDOT =      20166
926269  feet/sec       YDOT =        6137
701006  meter/sec
 ZDOT =      14746
293537                 ZDOT =        4490
684295

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10835570
95                 X    =         3302682
03
 Y    =      -15656039
30  feet           Y    =        -4771960
78  meter
 Z    =      -11618404
51                 Z    =        -3541289
69
 XDOT =      18974
648186                 XDOT =        5783
472767
 YDOT =       2217
141919  feet/sec       YDOT =         675
784857  meter/sec
 ZDOT =      14728
237109                 ZDOT =        4489
166671


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   14175
49972914  
00016717  00000-0  10270-3 0  9066
2 25544  51
6492  63
3123 0003601 129
6298 230
5172 15
50858467 12466


Satellite: ISS
Catalog Number: 25544
Epoch time:      14175
49972914   =   yrday
fracday
Element set:     906
Inclination:       51
6492  deg
RA of node:        63
3123  deg
Eccentricity:     
0003601     
Arg of perigee:   129
6298  deg
Mean anomaly:     230
5172  deg
Mean motion:   15
50858467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1246
Checksum:              316


Coasting Arc #8 (Orbit 1260)
---------------------------------------

Vector Time (GMT): 2014/176/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4352386
79                 A    =         6789438
85  meter
 Y    =        -690921
37  meter          E    =           
0014149
 Z    =       -5177452
38                 I    =           51
93897
 XDOT =       2918
121845                 Wp   =          108
94950
 YDOT =       6905
471299  meter/sec      RA   =           57
89340  deg
 ZDOT =       1530
526090                 TA   =          175
77420
                                          MA   =          175
76224
                                          Ha   =            227
229  n
mi
                                          Hp   =            220
845

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14279484
22                 X    =         4384939
76
 Y    =       -2266802
40  feet           Y    =         -642067
42  meter
 Z    =      -16986392
32                 Z    =        -5156230
12
 XDOT =       9573
890568                 XDOT =        2833
251604
 YDOT =      22655
745730  feet/sec       YDOT =        6937
628853  meter/sec
 ZDOT =       5021
411057                 ZDOT =        1544
496783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1355727
02                 X    =          413225
60
 Y    =      -14500343
67  feet           Y    =        -4419704
75  meter
 Z    =      -16896201
48                 Z    =        -5149962
21
 XDOT =      23253
854412                 XDOT =        7087
774825
 YDOT =      -3748
547417  feet/sec       YDOT =       -1142
557253  meter/sec
 ZDOT =       5079
404536                 ZDOT =        1548
202503


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   14176
46629451  
00016717  00000-0  10270-3 0  9070
2 25544  51
6491  58
5178 0001885 178
6244 181
4912 15
50259504 12618


Satellite: ISS
Catalog Number: 25544
Epoch time:      14176
46629451   =   yrday
fracday
Element set:     907
Inclination:       51
6491  deg
RA of node:        58
5178  deg
Eccentricity:     
0001885     
Arg of perigee:   178
6244  deg
Mean anomaly:     181
4912  deg
Mean motion:   15
50259504  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1261
Checksum:              322


Coasting Arc #9 (Orbit 1276)
---------------------------------------

Vector Time (GMT): 2014/177/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4506140
58                 A    =         6789842
46  meter
 Y    =         586106
69  meter          E    =           
0004966
 Z    =        5041486
99                 I    =           51
92330
 XDOT =      -3109
816315                 Wp   =           72
27768
 YDOT =      -6715
496498  meter/sec      RA   =           52
95481  deg
 ZDOT =      -1995
782113                 TA   =           37
05491
                                          MA   =           37
02062
                                          Ha   =            227
202  n
mi
                                          Hp   =            220
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14783925
78                 X    =        -4536849
50
 Y    =        1922922
20  feet           Y    =          535543
67  meter
 Z    =       16540311
65                 Z    =         5019522
35
 XDOT =     -10202
809433                 XDOT =       -3024
796135
 YDOT =     -22032
468824  feet/sec       YDOT =       -6749
796791  meter/sec
 ZDOT =      -6547
841579                 ZDOT =       -2010
683611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1556313
68                 X    =         -474364
41
 Y    =       14930456
17  feet           Y    =         4550803
04  meter
 Z    =       16446986
56                 Z    =         5013041
50
 XDOT =     -22692
372200                 XDOT =       -6916
635046
 YDOT =       4927
013575  feet/sec       YDOT =        1501
753738  meter/sec
 ZDOT =      -6609
812402                 ZDOT =       -2014
670820


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   14177
49769634  
00016717  00000-0  10270-3 0  9083
2 25544  51
6489  53
4066 0001801 186
7580 173
3547 15
50305539 12777


Satellite: ISS
Catalog Number: 25544
Epoch time:      14177
49769634   =   yrday
fracday
Element set:     908
Inclination:       51
6489  deg
RA of node:        53
4066  deg
Eccentricity:     
0001801     
Arg of perigee:   186
7580  deg
Mean anomaly:     173
3547  deg
Mean motion:   15
50305539  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1277
Checksum:              334


Coasting Arc #10 (Orbit 1291)
---------------------------------------

Vector Time (GMT): 2014/178/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4695322
52                 A    =         6790569
53  meter
 Y    =        -513322
67  meter          E    =           
0012050
 Z    =       -4890134
36                 I    =           51
90625
 XDOT =       3254
329829                 Wp   =          115
86964
 YDOT =       6480
283873  meter/sec      RA   =           48
01473  deg
 ZDOT =       2444
011242                 TA   =          178
07526
                                          MA   =          178
07061
                                          Ha   =            227
038  n
mi
                                          Hp   =            220
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15404601
45                 X    =         4724468
20
 Y    =       -1684129
51  feet           Y    =         -460652
89  meter
 Z    =      -16043747
89                 Z    =        -4867254
56
 XDOT =      10676
935135                 XDOT =        3169
751801
 YDOT =      21260
773862  feet/sec       YDOT =        6516
202624  meter/sec
 ZDOT =       8018
409588                 ZDOT =        2459
615734

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1664467
23                 X    =          507329
61
 Y    =      -15507320
06  feet           Y    =        -4726631
16  meter
 Z    =      -15946550
02                 Z    =        -4860508
45
 XDOT =      21909
499910                 XDOT =        6678
015573
 YDOT =      -5962
179296  feet/sec       YDOT =       -1817
272249  meter/sec
 ZDOT =       8083
402064                 ZDOT =        2463
820949


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   14178
46462863  
00016717  00000-0  10270-3 0  9096
2 25544  51
6490  48
6143 0001804 190
5958 169
5155 15
50288485 12925


Satellite: ISS
Catalog Number: 25544
Epoch time:      14178
46462863   =   yrday
fracday
Element set:     909
Inclination:       51
6490  deg
RA of node:        48
6143  deg
Eccentricity:     
0001804     
Arg of perigee:   190
5958  deg
Mean anomaly:     169
5155  deg
Mean motion:   15
50288485  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1292
Checksum:              335


Coasting Arc #11 (Orbit 1307)
---------------------------------------

Vector Time (GMT): 2014/179/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4890205
53                 A    =         6791222
16  meter
 Y    =         459173
94  meter          E    =           
0007139
 Z    =        4684941
46                 I    =           51
88732
 XDOT =      -3363
415156                 Wp   =           74
30309
 YDOT =      -6250
909909  meter/sec      RA   =           43
07392  deg
 ZDOT =      -2892
579965                 TA   =           44
38666
                                          MA   =           44
32946
                                          Ha   =            227
018  n
mi
                                          Hp   =            220
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16043981
39                 X    =        -4917734
40
 Y    =        1506476
18  feet           Y    =          404333
96  meter
 Z    =       15370542
85                 Z    =         4661118
93
 XDOT =     -11034
826626                 XDOT =       -3279
214980
 YDOT =     -20508
234610  feet/sec       YDOT =       -6288
050594  meter/sec
 ZDOT =      -9490
091749                 ZDOT =       -2908
715162

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1696660
15                 X    =         -517142
01
 Y    =       16121433
22  feet           Y    =         4913812
85  meter
 Z    =       15269352
71                 Z    =         4654098
71
 XDOT =     -21091
715512                 XDOT =       -6428
754888
 YDOT =       6849
824559  feet/sec       YDOT =        2087
826525  meter/sec
 ZDOT =      -9557
375545                 ZDOT =       -2913
088066


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   14179
49601196  
00016717  00000-0  10270-3 0  9106
2 25544  51
6489  43
5027 0001710 198
1680 161
9410 15
50335947 13084


Satellite: ISS
Catalog Number: 25544
Epoch time:      14179
49601196   =   yrday
fracday
Element set:     910
Inclination:       51
6489  deg
RA of node:        43
5027  deg
Eccentricity:     
0001710     
Arg of perigee:   198
1680  deg
Mean anomaly:     161
9410  deg
Mean motion:   15
50335947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1308
Checksum:              304


Coasting Arc #12 (Orbit 1322)
---------------------------------------

Vector Time (GMT): 2014/180/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5106537
35                 A    =         6792155
93  meter
 Y    =        -448134
70  meter          E    =           
0009204
 Z    =       -4465505
01                 I    =           51
86651
 XDOT =       3421
763313                 Wp   =          121
17716
 YDOT =       5991
591574  meter/sec      RA   =           38
13141  deg
 ZDOT =       3312
091629                 TA   =          182
19949
                                          MA   =          182
20354
                                          Ha   =            226
851  n
mi
                                          Hp   =            221
028

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16753731
45                 X    =         5132860
72
 Y    =       -1470258
21  feet           Y    =         -390882
38  meter
 Z    =      -14650607
00                 Z    =        -4440634
55
 XDOT =      11226
257587                 XDOT =        3338
420752
 YDOT =      19657
452671  feet/sec       YDOT =        6029
389525  meter/sec
 ZDOT =      10866
442352                 ZDOT =        3328
512212

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1581605
59                 X    =          482073
38
 Y    =      -16835432
83  feet           Y    =        -5131439
93  meter
 Z    =      -14544971
21                 Z    =        -4433307
22
 XDOT =      20116
731021                 XDOT =        6131
579615
 YDOT =      -7556
234580  feet/sec       YDOT =       -2303
140300  meter/sec
 ZDOT =      10934
983261                 ZDOT =        3332
982898


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   14180
46292680  
00016717  00000-0  10270-3 0  9110
2 25544  51
6486  38
7099 0001759 203
2715 156
8356 15
50315954 13231


Satellite: ISS
Catalog Number: 25544
Epoch time:      14180
46292680   =   yrday
fracday
Element set:     911
Inclination:       51
6486  deg
RA of node:        38
7099  deg
Eccentricity:     
0001759     
Arg of perigee:   203
2715  deg
Mean anomaly:     156
8356  deg
Mean motion:   15
50315954  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1323
Checksum:              315


Coasting Arc #13 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2014/181/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5320327
93                 A    =         6792987
38  meter
 Y    =         455327
39  meter          E    =           
0009243
 Z    =        4191869
05                 I    =           51
84487
 XDOT =      -3436
306479                 Wp   =           82
64944
 YDOT =      -5748
230445  meter/sec      RA   =           33
18835  deg
 ZDOT =      -3728
791586                 TA   =           45
60522
                                          MA   =           45
52958
                                          Ha   =            226
826  n
mi
                                          Hp   =            220
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17455144
14                 X    =        -5345386
61
 Y    =        1493856
25  feet           Y    =          395691
49  meter
 Z    =       13752851
20                 Z    =         4165963
12
 XDOT =     -11273
971389                 XDOT =       -3353
659999
 YDOT =     -18859
023769  feet/sec       YDOT =       -5786
194922  meter/sec
 ZDOT =     -12233
568196                 ZDOT =       -3745
284382

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1381899
94                 X    =         -421203
10
 Y    =       17550452
26  feet           Y    =         5349377
85  meter
 Z    =       13642820
73                 Z    =         4158331
76
 XDOT =     -19152
162590                 XDOT =       -5837
579157
 YDOT =       8076
347518  feet/sec       YDOT =        2461
670724  meter/sec
 ZDOT =     -12302
458947                 ZDOT =       -3749
789487


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   14181
49429181  
00016717  00000-0  10270-3 0  9123
2 25544  51
6487  33
5980 0001660 210
8074 149
2980 15
50364533 13390


Satellite: ISS
Catalog Number: 25544
Epoch time:      14181
49429181   =   yrday
fracday
Element set:     912
Inclination:       51
6487  deg
RA of node:        33
5980  deg
Eccentricity:     
0001660     
Arg of perigee:   210
8074  deg
Mean anomaly:     149
2980  deg
Mean motion:   15
50364533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1339
Checksum:              307


Coasting Arc #14 (Orbit 1353)
---------------------------------------

Vector Time (GMT): 2014/182/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5539480
90                 A    =         6794039
64  meter
 Y    =        -511792
72  meter          E    =           
0005951
 Z    =       -3907031
49                 I    =           51
82082
 XDOT =       3402
194400                 Wp   =          120
77352
 YDOT =       5492
494508  meter/sec      RA   =           28
24325  deg
 ZDOT =       4105
916195                 TA   =          192
24469
                                          MA   =          192
25915
                                          Ha   =            226
684  n
mi
                                          Hp   =            221
095

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18174149
94                 X    =         5563771
07
 Y    =       -1679109
97  feet           Y    =         -449710
49  meter
 Z    =      -12818344
78                 Z    =        -3880062
82
 XDOT =      11162
055118                 XDOT =        3320
578216
 YDOT =      18019
995105  feet/sec       YDOT =        5530
083301  meter/sec
 ZDOT =      13470
853657                 ZDOT =        4122
245681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1000646
25                 X    =          304996
98
 Y    =      -18304135
35  feet           Y    =        -5579100
45  meter
 Z    =      -12703796
11                 Z    =        -3872117
05
 XDOT =      18109
583155                 XDOT =        5519
800946
 YDOT =      -8402
795436  feet/sec       YDOT =       -2561
172049  meter/sec
 ZDOT =      13539
097033                 ZDOT =        4126
716776


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   14182
46118955  
00016717  00000-0  10270-3 0  9136
2 25544  51
6479  28
8048 0001759 215
2168 144
8867 15
50341538 13547


Satellite: ISS
Catalog Number: 25544
Epoch time:      14182
46118955   =   yrday
fracday
Element set:     913
Inclination:       51
6479  deg
RA of node:        28
8048  deg
Eccentricity:     
0001759     
Arg of perigee:   215
2168  deg
Mean anomaly:     144
8867  deg
Mean motion:   15
50341538  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1354
Checksum:              327


Coasting Arc #15 (Orbit 1369)
---------------------------------------

Vector Time (GMT): 2014/183/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5746806
03                 A    =         6794945
85  meter
 Y    =         582925
60  meter          E    =           
0011009
 Z    =        3568347
50                 I    =           51
79688
 XDOT =      -3319
535378                 Wp   =           93
57807
 YDOT =      -5263
962451  meter/sec      RA   =           23
29794  deg
 ZDOT =      -4474
938957                 TA   =           44
44720
                                          MA   =           44
35891
                                          Ha   =            226
631  n
mi
                                          Hp   =            220
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18854350
48                 X    =        -5770231
03
 Y    =        1912485
58  feet           Y    =          518529
85  meter
 Z    =       11707176
82                 Z    =         3540373
74
 XDOT =     -10890
864102                 XDOT =       -3238
688230
 YDOT =     -17270
218015  feet/sec       YDOT =       -5300
631219  meter/sec
 ZDOT =     -14681
558258                 ZDOT =       -4490
868703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -541047
70                 X    =         -164911
34
 Y    =       19016294
41  feet           Y    =         5796166
54  meter
 Z    =       11588353
49                 Z    =         3532130
14
 XDOT =     -17132
147594                 XDOT =       -5221
878587
 YDOT =       8522
635157  feet/sec       YDOT =        2597
699196  meter/sec
 ZDOT =     -14748
145290                 ZDOT =       -4495
234684


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   14183
49253639  
00016717  00000-0  10270-3 0  9140
2 25544  51
6483  23
6929 0001667 223
6596 136
4423 15
50391459 13709


Satellite: ISS
Catalog Number: 25544
Epoch time:      14183
49253639   =   yrday
fracday
Element set:     914
Inclination:       51
6483  deg
RA of node:        23
6929  deg
Eccentricity:     
0001667     
Arg of perigee:   223
6596  deg
Mean anomaly:     136
4423  deg
Mean motion:   15
50391459  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1370
Checksum:              323


Coasting Arc #16 (Orbit 1384)
---------------------------------------

Vector Time (GMT): 2014/184/10:52:05
126
Vector Time (MET): N/A
Weight (LBS)     : 887995
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5943159
28                 A    =         6796006
96  meter
 Y    =        -703921
54  meter          E    =           
0003211
 Z    =       -3223252
43                 I    =           51
77008
 XDOT =       3196
118245                 Wp   =           96
05478
 YDOT =       5040
728818  meter/sec      RA   =           18
35019  deg
 ZDOT =       4796
071425                 TA   =          226
81396
                                          MA   =          226
84079
                                          Ha   =            226
543  n
mi
                                          Hp   =            221
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19498554
05                 X    =         5966246
39
 Y    =       -2309453
87  feet           Y    =         -637331
98  meter
 Z    =      -10574975
18                 Z    =        -3194325
59
 XDOT =      10485
952248                 XDOT =        3116
216524
 YDOT =      16537
824207  feet/sec       YDOT =        5076
022761  meter/sec
 ZDOT =      15735
142469                 ZDOT =        4811
403898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -109316
65                 X    =          -33319
72
 Y    =      -19700232
46  feet           Y    =        -6004630
85  meter
 Z    =      -10452089
66                 Z    =        -3185796
93
 XDOT =      16159
904964                 XDOT =        4925
539033
 YDOT =      -8465
401371  feet/sec       YDOT =       -2580
254338  meter/sec
 ZDOT =      15799
233452                 ZDOT =        4815
606356


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   14184
45941731  
00016717  00000-0  10270-3 0  9155
2 25544  51
6471  18
8993 0001785 225
4320 134
6685 15
50365597 13859


Satellite: ISS
Catalog Number: 25544
Epoch time:      14184
45941731   =   yrday
fracday
Element set:     915
Inclination:       51
6471  deg
RA of node:        18
8993  deg
Eccentricity:     
0001785     
Arg of perigee:   225
4320  deg
Mean anomaly:     134
6685  deg
Mean motion:   15
50365597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1385
Checksum:              328
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