[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: June 28th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 ET - UTC (sec) : 68 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


179/14:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 216 1

180/09:42:42 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 216 0

183/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 216 2

187/05:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 8
000/00:00:00 000 0 0 0 0 216 1

Coasting Arc #1 (Orbit 4012)
---------------------------------------

Vector Time (GMT): 2018/178/13:51:28
206
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2592524
28                 A    =         6784505
84  meter
 Y    =        5149948
74  meter          E    =           
0009168
 Z    =        3566230
53                 I    =           51
43479
 XDOT =      -6257
961103                 Wp   =          101
81382
 YDOT =        -73
561479  meter/sec      RA   =          326
26878  deg
 ZDOT =      -4435
254143                 TA   =           35
90538
                                          MA   =           35
84380
                                          Ha   =            220
529  n
mi
                                          Hp   =            216
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8505657
08                 X    =        -2667242
54
 Y    =       16896157
28  feet           Y    =         5120538
97  meter
 Z    =       11700231
40                 Z    =         3553456
38
 XDOT =     -20531
368447                 XDOT =       -6235
129368
 YDOT =       -241
343434  feet/sec       YDOT =        -143
413908  meter/sec
 ZDOT =     -14551
358736                 ZDOT =       -4465
597606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18858685
06                 X    =         5748127
21
 Y    =       -1878778
71  feet           Y    =         -572651
75  meter
 Z    =       11642247
91                 Z    =         3548557
16
 XDOT =      10673
604447                 XDOT =        3253
314635
 YDOT =      15967
174515  feet/sec       YDOT =        4866
794792  meter/sec
 ZDOT =     -14687
079362                 ZDOT =       -4476
621790


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   18178
61706617  
00016717  00000-0  10270-3 0  9006
2 25544  51
6405 326
7213 0003991 232
0237 128
0555 15
53950097 40136


Satellite: ISS
Catalog Number: 25544
Epoch time:      18178
61706617   =   yrday
fracday
Element set:     900
Inclination:       51
6405  deg
RA of node:       326
7213  deg
Eccentricity:     
0003991     
Arg of perigee:   232
0237  deg
Mean anomaly:     128
0555  deg
Mean motion:   15
53950097  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4013
Checksum:              296


Coasting Arc #2 (Orbit 4027)
---------------------------------------

Vector Time (GMT): 2018/179/13:51:28
206
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3735480
17                 A    =         6787845
24  meter
 Y    =       -5228079
79  meter          E    =           
0002846
 Z    =       -2183762
26                 I    =           51
42033
 XDOT =       5185
585946                 Wp   =           17
99463
 YDOT =       1425
918162  meter/sec      RA   =          321
27624  deg
 ZDOT =       5461
125212                 TA   =          317
69843
                                          MA   =          317
72037
                                          Ha   =            220
316  n
mi
                                          Hp   =            216
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12255512
37                 X    =         3804271
86
 Y    =      -17152492
76  feet           Y    =        -5185922
08  meter
 Z    =       -7164574
34                 Z    =        -2165450
50
 XDOT =      17013
077250                 XDOT =        5142
728456
 YDOT =       4678
209194  feet/sec       YDOT =        1483
666418  meter/sec
 ZDOT =      17917
077468                 ZDOT =        5486
210967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21095420
78                 X    =        -6429884
25
 Y    =        -753547
57  feet           Y    =         -229681
30  meter
 Z    =       -7081815
08                 Z    =        -2158537
24
 XDOT =      -5507
158299                 XDOT =       -1678
581850
 YDOT =     -15122
386349  feet/sec       YDOT =       -4609
303359  meter/sec
 ZDOT =      18029
059179                 ZDOT =        5495
257238


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   18179
58169074  
00016717  00000-0  10270-3 0  9014
2 25544  51
6416 321
9140 0003830 239
4439 120
6336 15
53958448 40280


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
58169074   =   yrday
fracday
Element set:     901
Inclination:       51
6416  deg
RA of node:       321
9140  deg
Eccentricity:     
0003830     
Arg of perigee:   239
4439  deg
Mean anomaly:     120
6336  deg
Mean motion:   15
53958448  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4028
Checksum:              318


Coasting Arc #3 (Orbit 4028)
---------------------------------------

Vector Time (GMT): 2018/179/14:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2051344
30                 A    =         6777862
88  meter
 Y    =        3745355
74  meter          E    =           
0000849
 Z    =        5263894
09                 I    =           51
38718
 XDOT =      -6269
892306                 Wp   =          224
86702
 YDOT =       4364
851452  meter/sec      RA   =          321
18181  deg
 ZDOT =       -662
944056                 TA   =          231
48141
                                          MA   =          231
48903
                                          Ha   =            220
138  n
mi
                                          Hp   =            216
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6730132
23                 X    =         1983741
21
 Y    =       12287912
54  feet           Y    =         3767916
42  meter
 Z    =       17269993
72                 Z    =         5273695
17
 XDOT =     -20570
512815                 XDOT =       -6315
015074
 YDOT =      14320
378781  feet/sec       YDOT =        4294
485008  meter/sec
 ZDOT =      -2175
013308                 ZDOT =        -693
509682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4847475
83                 X    =         1477510
63
 Y    =      -13087942
91  feet           Y    =        -3989205
00  meter
 Z    =       17313228
65                 Z    =         5277072
09
 XDOT =      23379
193684                 XDOT =        7125
978235
 YDOT =       5602
969322  feet/sec       YDOT =        1707
785049  meter/sec
 ZDOT =      -2312
446159                 ZDOT =        -704
833589


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   18179
64599803  
00016717  00000-0  10270-3 0  9029
2 25544  51
6418 321
5934 0003879 239
4057 120
6713 15
54007726 40293


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
64599803   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:       321
5934  deg
Eccentricity:     
0003879     
Arg of perigee:   239
4057  deg
Mean anomaly:     120
6713  deg
Mean motion:   15
54007726  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4029
Checksum:              326


Coasting Arc #4 (Orbit 4040)
---------------------------------------

Vector Time (GMT): 2018/180/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1329912
01                 A    =         6778795
92  meter
 Y    =       -4301699
94  meter          E    =           
0010801
 Z    =       -5077095
18                 I    =           51
36558
 XDOT =       6313
163118                 Wp   =          115
65356
 YDOT =      -3982
953394  meter/sec      RA   =          317
14428  deg
 ZDOT =       1719
246633                 TA   =          171
05409
                                          MA   =          171
03483
                                          Ha   =            220
242  n
mi
                                          Hp   =            215
991

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4363228
38                 X    =        -1257048
77
 Y    =      -14113188
77  feet           Y    =        -4316163
71  meter
 Z    =      -16657136
43                 Z    =        -5083379
10
 XDOT =      20712
477422                 XDOT =        6348
881278
 YDOT =     -13067
432394  feet/sec       YDOT =       -3912
155816  meter/sec
 ZDOT =       5640
572943                 ZDOT =        1749
999618

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14470157
87                 X    =        -4410504
12
 Y    =       -2814291
45  feet           Y    =         -857796
03  meter
 Z    =      -16684554
18                 Z    =        -5085452
11
 XDOT =      -2132
842036                 XDOT =        -650
090253
 YDOT =     -23326
587247  feet/sec       YDOT =       -7109
943793  meter/sec
 ZDOT =       5778
775820                 ZDOT =        1761
370870


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   18180
41769633  
00016717  00000-0  10270-3 0  9037
2 25544  51
6377 317
7474 0003624 242
0246 118
0540 15
53987226 40415


Satellite: ISS
Catalog Number: 25544
Epoch time:      18180
41769633   =   yrday
fracday
Element set:     903
Inclination:       51
6377  deg
RA of node:       317
7474  deg
Eccentricity:     
0003624     
Arg of perigee:   242
0246  deg
Mean anomaly:     118
0540  deg
Mean motion:   15
53987226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4041
Checksum:              306


Coasting Arc #5 (Orbit 4056)
---------------------------------------

Vector Time (GMT): 2018/181/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -20404
32                 A    =         6781791
39  meter
 Y    =        5203006
78  meter          E    =           
0005894
 Z    =        4345835
60                 I    =           51
35134
 XDOT =      -6252
048969                 Wp   =           74
62886
 YDOT =       2835
770025  meter/sec      RA   =          312
13236  deg
 ZDOT =      -3419
035140                 TA   =           50
20432
                                          MA   =           50
15244
                                          Ha   =            220
132  n
mi
                                          Hp   =            216
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -66943
32                 X    =          -99693
78
 Y    =       17070232
23  feet           Y    =         5202334
62  meter
 Z    =       14257990
82                 Z    =         4345544
69
 XDOT =     -20511
971683                 XDOT =       -6266
686995
 YDOT =       9303
707430  feet/sec       YDOT =        2765
773970  meter/sec
 ZDOT =     -11217
306889                 ZDOT =       -3449
440198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15166510
21                 X    =         4622752
31
 Y    =        7838043
01  feet           Y    =         2389035
51  meter
 Z    =       14255864
11                 Z    =         4345187
38
 XDOT =       -334
882007                 XDOT =        -102
072036
 YDOT =      21330
581509  feet/sec       YDOT =        6501
561244  meter/sec
 ZDOT =     -11353
762600                 ZDOT =       -3460
626840


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   18181
44662223  
00016717  00000-0  10270-3 0  9049
2 25544  51
6372 312
6195 0003754 246
3473 113
7285 15
53965766 40577


Satellite: ISS
Catalog Number: 25544
Epoch time:      18181
44662223   =   yrday
fracday
Element set:     904
Inclination:       51
6372  deg
RA of node:       312
6195  deg
Eccentricity:     
0003754     
Arg of perigee:   246
3473  deg
Mean anomaly:     113
7285  deg
Mean motion:   15
53965766  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4057
Checksum:              320


Coasting Arc #6 (Orbit 4071)
---------------------------------------

Vector Time (GMT): 2018/182/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1228754
35                 A    =         6785378
48  meter
 Y    =       -5858713
58  meter          E    =           
0001120
 Z    =       -3196195
64                 I    =           51
34432
 XDOT =       5834
231145                 Wp   =          110
09065
 YDOT =      -1380
202627  meter/sec      RA   =          307
12742  deg
 ZDOT =       4773
864712                 TA   =          212
81452
                                          MA   =          212
82147
                                          Ha   =            220
055  n
mi
                                          Hp   =            216
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4031346
30                 X    =         1309702
00
 Y    =      -19221501
25  feet           Y    =        -5844519
76  meter
 Z    =      -10486206
18                 Z    =        -3190031
05
 XDOT =      19141
178297                 XDOT =        5826
042733
 YDOT =      -4528
223842  feet/sec       YDOT =       -1315
006666  meter/sec
 ZDOT =      15662
285801                 ZDOT =        4802
184937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15520936
94                 X    =        -4730781
58
 Y    =      -12058817
88  feet           Y    =        -3675527
69  meter
 Z    =      -10457715
39                 Z    =        -3187511
65
 XDOT =       3331
234590                 XDOT =        1015
360303
 YDOT =     -17977
604677  feet/sec       YDOT =       -5479
573906  meter/sec
 ZDOT =      15789
180756                 ZDOT =        4812
542294


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   18182
41123457  
00016717  00000-0  10270-3 0  9059
2 25544  51
6391 307
8116 0003644 249
8447 110
2313 15
54005877 40724


Satellite: ISS
Catalog Number: 25544
Epoch time:      18182
41123457   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:       307
8116  deg
Eccentricity:     
0003644     
Arg of perigee:   249
8447  deg
Mean anomaly:     110
2313  deg
Mean motion:   15
54005877  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4072
Checksum:              297


Coasting Arc #7 (Orbit 4087)
---------------------------------------

Vector Time (GMT): 2018/183/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922867
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2255101
54                 A    =         6788453
50  meter
 Y    =        6163274
17  meter          E    =           
0011412
 Z    =        1709987
40                 I    =           51
33416
 XDOT =      -5159
580114                 Wp   =          127
57078
 YDOT =       -310
314356  meter/sec      RA   =          302
13103  deg
 ZDOT =      -5666
716378                 TA   =           33
58967
                                          MA   =           33
51737
                                          Ha   =            219
944  n
mi
                                          Hp   =            216
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7398627
10                 X    =        -2332159
47
 Y    =       20220715
80  feet           Y    =         6137625
01  meter
 Z    =        5610194
88                 Z    =         1698846
63
 XDOT =     -16927
756281                 XDOT =       -5128
201080
 YDOT =      -1018
091719  feet/sec       YDOT =        -367
836206  meter/sec
 ZDOT =     -18591
589168                 ZDOT =       -5691
703320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15232937
52                 X    =         4642999
36
 Y    =       15236202
13  feet           Y    =         4643994
41  meter
 Z    =        5559413
30                 Z    =         1694509
17
 XDOT =      -6867
404466                 XDOT =       -2093
184881
 YDOT =      13713
610707  feet/sec       YDOT =        4179
908543  meter/sec
 ZDOT =     -18703
309355                 ZDOT =       -5700
768691


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   18183
44014853  
00016717  00000-0  10270-3 0  9063
2 25544  51
6377 302
6835 0003666 255
1678 104
9068 15
54011690 40883


Satellite: ISS
Catalog Number: 25544
Epoch time:      18183
44014853   =   yrday
fracday
Element set:     906
Inclination:       51
6377  deg
RA of node:       302
6835  deg
Eccentricity:     
0003666     
Arg of perigee:   255
1678  deg
Mean anomaly:     104
9068  deg
Mean motion:   15
54011690  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4088
Checksum:              320


Coasting Arc #8 (Orbit 4088)
---------------------------------------

Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1687811
08                 A    =         6787593
69  meter
 Y    =       -6174089
72  meter          E    =           
0003506
 Z    =       -2253110
41                 I    =           51
33253
 XDOT =       5400
175417                 Wp   =            8
66589
 YDOT =       -499
078316  meter/sec      RA   =          301
65038  deg
 ZDOT =       5417
390907                 TA   =          326
16656
                                          MA   =          326
18892
                                          Ha   =            219
965  n
mi
                                          Hp   =            216
198

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5537437
91                 X    =         1767670
28
 Y    =      -20256199
86  feet           Y    =        -6154768
66  meter
 Z    =       -7392094
52                 Z    =        -2244718
49
 XDOT =      17717
110948                 XDOT =        5379
040426
 YDOT =      -1637
396050  feet/sec       YDOT =        -438
808647  meter/sec
 ZDOT =      17773
592214                 ZDOT =        5443
571346

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20904814
33                 X    =        -6371787
41
 Y    =       -2129105
74  feet           Y    =         -648951
43  meter
 Z    =       -7353608
59                 Z    =        -2241379
90
 XDOT =      -4703
900440                 XDOT =       -1433
748854
 YDOT =     -15555
048505  feet/sec       YDOT =       -4741
178784  meter/sec
 ZDOT =      17890
775264                 ZDOT =        5453
108300


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   18183
50445569  
00016717  00000-0  10270-3 0  9073
2 25544  51
6409 302
3638 0003705 255
8234 104
2507 15
53991869 40892


Satellite: ISS
Catalog Number: 25544
Epoch time:      18183
50445569   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       302
3638  deg
Eccentricity:     
0003705     
Arg of perigee:   255
8234  deg
Mean anomaly:     104
2507  deg
Mean motion:   15
53991869  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4089
Checksum:              329


Coasting Arc #9 (Orbit 4104)
---------------------------------------

Vector Time (GMT): 2018/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2567810
80                 A    =         6789516
53  meter
 Y    =        6246010
66  meter          E    =           
0011156
 Z    =         633909
53                 I    =           51
32189
 XDOT =      -4666
297485                 Wp   =          143
50190
 YDOT =      -1310
530972  meter/sec      RA   =          296
65760  deg
 ZDOT =      -5943
941428                 TA   =           29
62254
                                          MA   =           29
55940
                                          Ha   =            219
874  n
mi
                                          Hp   =            216
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8424576
12                 X    =        -2640543
73
 Y    =       20492160
95  feet           Y    =         6216888
89  meter
 Z    =        2079755
66                 Z    =          621260
14
 XDOT =     -15309
374951                 XDOT =       -4622
423785
 YDOT =      -4299
642297  feet/sec       YDOT =       -1362
466801  meter/sec
 ZDOT =     -19501
120171                 ZDOT =       -5966
501983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21693874
40                 X    =         6612292
92
 Y    =        4529229
53  feet           Y    =         1380509
16  meter
 Z    =        2022231
49                 Z    =          616376
16
 XDOT =      -1108
547754                 XDOT =        -337
885356
 YDOT =      14129
690604  feet/sec       YDOT =        4306
729696  meter/sec
 ZDOT =     -19601
835348                 ZDOT =       -5974
639414


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   18184
53336540  
00016717  00000-0  10270-3 0  9086
2 25544  51
6400 297
2361 0003774 257
1403 102
9328 15
54009217 41050


Satellite: ISS
Catalog Number: 25544
Epoch time:      18184
53336540   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:       297
2361  deg
Eccentricity:     
0003774     
Arg of perigee:   257
1403  deg
Mean anomaly:     102
9328  deg
Mean motion:   15
54009217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4105
Checksum:              290


Coasting Arc #10 (Orbit 4120)
---------------------------------------

Vector Time (GMT): 2018/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3223954
89                 A    =         6789161
99  meter
 Y    =       -5878554
32  meter          E    =           
0010447
 Z    =        1031203
32                 I    =           51
30817
 XDOT =       3816
370437                 Wp   =           47
08948
 YDOT =       3128
169588  meter/sec      RA   =          291
66553  deg
 ZDOT =       5870
326882                 TA   =          324
14155
                                          MA   =          324
21163
                                          Ha   =            219
825  n
mi
                                          Hp   =            216
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10577279
81                 X    =         3284441
89
 Y    =      -19286595
54  feet           Y    =        -5842163
72  meter
 Z    =        3383213
00                 Z    =         1047010
39
 XDOT =      12520
900383                 XDOT =        3752
592081
 YDOT =      10263
023583  feet/sec       YDOT =        3170
489728  meter/sec
 ZDOT =      19259
602632                 ZDOT =        5888
710686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21011698
09                 X    =        -6404365
58
 Y    =       -6470758
34  feet           Y    =        -1972287
14  meter
 Z    =        3454790
21                 Z    =         1053020
06
 XDOT =       7097
707524                 XDOT =        2163
381253
 YDOT =     -12668
088736  feet/sec       YDOT =       -3861
233447  meter/sec
 ZDOT =      19341
367396                 ZDOT =        5895
248782


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   18185
56226942  
00016717  00000-0  10270-3 0  9095
2 25544  51
6412 292
1079 0003681 263
5306  96
5427 15
54025107 41215


Satellite: ISS
Catalog Number: 25544
Epoch time:      18185
56226942   =   yrday
fracday
Element set:     909
Inclination:       51
6412  deg
RA of node:       292
1079  deg
Eccentricity:     
0003681     
Arg of perigee:   263
5306  deg
Mean anomaly:      96
5427  deg
Mean motion:   15
54025107  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4121
Checksum:              304


Coasting Arc #11 (Orbit 4135)
---------------------------------------

Vector Time (GMT): 2018/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3699633
43                 A    =         6786666
64  meter
 Y    =        5051102
31  meter          E    =           
0003162
 Z    =       -2614248
78                 I    =           51
28819
 XDOT =      -2908
739702                 Wp   =          173
78680
 YDOT =      -4820
928588  meter/sec      RA   =          286
66904  deg
 ZDOT =      -5202
011426                 TA   =           35
80297
                                          MA   =           35
78178
                                          Ha   =            219
771  n
mi
                                          Hp   =            216
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12137904
95                 X    =        -3743142
73
 Y    =       16571857
96  feet           Y    =         5009487
40  meter
 Z    =       -8576931
70                 Z    =        -2632325
43
 XDOT =      -9543
109258                 XDOT =       -2829
346121
 YDOT =     -15816
694842  feet/sec       YDOT =       -4853
011753  meter/sec
 ZDOT =     -17066
966622                 ZDOT =       -5215
948565

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18801565
99                 X    =         5730717
31
 Y    =        8188408
58  feet           Y    =         2495826
94  meter
 Z    =       -8658524
78                 Z    =        -2639118
35
 XDOT =     -12792
014026                 XDOT =       -3899
005875
 YDOT =      11272
644457  feet/sec       YDOT =        3435
902030  meter/sec
 ZDOT =     -17128
601106                 ZDOT =       -5220
797617


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   18186
52686194  
00016717  00000-0  10270-3 0  9103
2 25544  51
6407 287
3006 0003705 267
2026  92
8702 15
54028102 41361


Satellite: ISS
Catalog Number: 25544
Epoch time:      18186
52686194   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:       287
3006  deg
Eccentricity:     
0003705     
Arg of perigee:   267
2026  deg
Mean anomaly:      92
8702  deg
Mean motion:   15
54028102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4136
Checksum:              298


Coasting Arc #12 (Orbit 4146)
---------------------------------------

Vector Time (GMT): 2018/187/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2042863
74                 A    =         6783021
01  meter
 Y    =       -5145088
13  meter          E    =           
0003014
 Z    =       -3923156
75                 I    =           51
26606
 XDOT =       4413
093347                 Wp   =          118
96027
 YDOT =      -4811
474879  meter/sec      RA   =          282
98691  deg
 ZDOT =       4013
017057                 TA   =          193
20283
                                          MA   =          193
21073
                                          Ha   =            219
767  n
mi
                                          Hp   =            216
112

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6702308
85                 X    =        -1966121
58
 Y    =      -16880210
39  feet           Y    =        -5167503
40  meter
 Z    =      -12871249
19                 Z    =        -3932894
29
 XDOT =      14478
652713                 XDOT =        4447
075565
 YDOT =     -15785
678737  feet/sec       YDOT =       -4761
934970  meter/sec
 ZDOT =      13166
066459                 ZDOT =        4034
536349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7927818
32                 X    =        -2416399
02
 Y    =      -16306693
36  feet           Y    =        -4970280
14  meter
 Z    =      -12914060
21                 Z    =        -3936205
55
 XDOT =      11912
003329                 XDOT =        3630
778615
 YDOT =     -16292
513689  feet/sec       YDOT =       -4965
958173  meter/sec
 ZDOT =      13263
014880                 ZDOT =        4042
566936


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   18187
23422657  
00016717  00000-0  10270-3 0  9115
2 25544  51
6371 283
7759 0003752 276
4558  83
6167 15
54039906 41479


Satellite: ISS
Catalog Number: 25544
Epoch time:      18187
23422657   =   yrday
fracday
Element set:     911
Inclination:       51
6371  deg
RA of node:       283
7759  deg
Eccentricity:     
0003752     
Arg of perigee:   276
4558  deg
Mean anomaly:      83
6167  deg
Mean motion:   15
54039906  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4147
Checksum:              338


Coasting Arc #13 (Orbit 4162)
---------------------------------------

Vector Time (GMT): 2018/188/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1246016
11                 A    =         6786586
67  meter
 Y    =        6138251
59  meter          E    =           
0009588
 Z    =        2601358
24                 I    =           51
27279
 XDOT =      -4659
764331                 Wp   =          103
32236
 YDOT =       3158
795776  meter/sec      RA   =          277
98002  deg
 ZDOT =      -5207
571043                 TA   =           47
22803
                                          MA   =           47
14741
                                          Ha   =            219
681  n
mi
                                          Hp   =            216
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4087979
37                 X    =         1164647
89
 Y    =       20138620
70  feet           Y    =         6151730
19  meter
 Z    =        8534639
90                 Z    =         2607213
90
 XDOT =     -15287
940717                 XDOT =       -4669
444948
 YDOT =      10363
503202  feet/sec       YDOT =        3106
633448  meter/sec
 ZDOT =     -17085
206833                 ZDOT =       -5230
229730

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5946392
91                 X    =         1812460
56
 Y    =       19659177
22  feet           Y    =         5992117
22  meter
 Z    =        8559956
76                 Z    =         2609074
82
 XDOT =     -12675
717122                 XDOT =       -3863
558579
 YDOT =      11337
637032  feet/sec       YDOT =        3455
711767  meter/sec
 ZDOT =     -17187
006814                 ZDOT =       -5238
599677


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   18188
26311740  
00016717  00000-0  10270-3 0  9120
2 25544  51
6380 278
6472 0004020 282
2689  77
8014 15
54079503 41634


Satellite: ISS
Catalog Number: 25544
Epoch time:      18188
26311740   =   yrday
fracday
Element set:     912
Inclination:       51
6380  deg
RA of node:       278
6472  deg
Eccentricity:     
0004020     
Arg of perigee:   282
2689  deg
Mean anomaly:      77
8014  deg
Mean motion:   15
54079503  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4163
Checksum:              308


Coasting Arc #14 (Orbit 4177)
---------------------------------------

Vector Time (GMT): 2018/189/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -480721
71                 A    =         6789110
31  meter
 Y    =       -6687524
99  meter          E    =           
0008770
 Z    =       -1032374
14                 I    =           51
27664
 XDOT =       4776
502628                 Wp   =           15
56294
 YDOT =      -1246
169782  meter/sec      RA   =          272
98035  deg
 ZDOT =       5868
206280                 TA   =          333
18873
                                          MA   =          333
23403
                                          Ha   =            219
831  n
mi
                                          Hp   =            216
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1577170
98                 X    =         -400889
52
 Y    =      -21940698
79  feet           Y    =        -6692454
27  meter
 Z    =       -3387054
25                 Z    =        -1034516
16
 XDOT =      15670
940379                 XDOT =        4761
577997
 YDOT =      -4088
483537  feet/sec       YDOT =       -1192
839734  meter/sec
 ZDOT =      19252
645277                 ZDOT =        5891
372486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4026760
45                 X    =        -1227356
58
 Y    =      -21624253
23  feet           Y    =        -6591072
39  meter
 Z    =       -3395694
42                 Z    =        -1035007
66
 XDOT =      13403
981850                 XDOT =        4085
533668
 YDOT =      -5525
363886  feet/sec       YDOT =       -1684
130913  meter/sec
 ZDOT =      19356
442718                 ZDOT =        5899
843740


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   18189
22770168  
00016717  00000-0  10270-3 0  9131
2 25544  51
6372 273
8382 0003754 283
8165  76
2570 15
54046871 41789


Satellite: ISS
Catalog Number: 25544
Epoch time:      18189
22770168   =   yrday
fracday
Element set:     913
Inclination:       51
6372  deg
RA of node:       273
8382  deg
Eccentricity:     
0003754     
Arg of perigee:   283
8165  deg
Mean anomaly:      76
2570  deg
Mean motion:   15
54046871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4178
Checksum:              334


Coasting Arc #15 (Orbit 4193)
---------------------------------------

Vector Time (GMT): 2018/190/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -295012
10                 A    =         6789238
54  meter
 Y    =        6746042
59  meter          E    =           
0007537
 Z    =        -663419
85                 I    =           51
27670
 XDOT =      -4789
370386                 Wp   =          153
06310
 YDOT =       -789
827436  meter/sec      RA   =          267
98573  deg
 ZDOT =      -5934
819356                 TA   =           34
13656
                                          MA   =           34
08812
                                          Ha   =            219
915  n
mi
                                          Hp   =            215
984

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -967887
47                 X    =         -367203
73
 Y    =       22132685
65  feet           Y    =         6742339
99  meter
 Z    =       -2176574
32                 Z    =         -665027
38
 XDOT =     -15713
157433                 XDOT =       -4751
354139
 YDOT =      -2591
297362  feet/sec       YDOT =        -843
172145  meter/sec
 ZDOT =     -19471
192112                 ZDOT =       -5957
992231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1936302
76                 X    =          590185
08
 Y    =       22068254
57  feet           Y    =         6726403
99  meter
 Z    =       -2184703
13                 Z    =         -665897
51
 XDOT =     -14179
408819                 XDOT =       -4321
883808
 YDOT =       -683
002337  feet/sec       YDOT =        -208
179112  meter/sec
 ZDOT =     -19574
738739                 ZDOT =       -5966
380368


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   18190
25658531  
00016717  00000-0  10270-3 0  9146
2 25544  51
6371 268
7098 0003733 291
6765  68
3990 15
54094353 41949


Satellite: ISS
Catalog Number: 25544
Epoch time:      18190
25658531   =   yrday
fracday
Element set:     914
Inclination:       51
6371  deg
RA of node:       268
7098  deg
Eccentricity:     
0003733     
Arg of perigee:   291
6765  deg
Mean anomaly:      68
3990  deg
Mean motion:   15
54094353  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4194
Checksum:              339


Coasting Arc #16 (Orbit 4209)
---------------------------------------

Vector Time (GMT): 2018/191/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1061295
87                 A    =         6787332
12  meter
 Y    =       -6300237
47  meter          E    =           
0011222
 Z    =        2272481
29                 I    =           51
27132
 XDOT =       4702
561990                 Wp   =           60
76233
 YDOT =       2745
964000  meter/sec      RA   =          262
98804  deg
 ZDOT =       5401
891688                 TA   =          324
67828
                                          MA   =          324
75258
                                          Ha   =            219
939  n
mi
                                          Hp   =            216
008

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3481941
82                 X    =         1120629
48
 Y    =      -20670070
45  feet           Y    =        -6288037
92  meter
 Z    =        7455647
29                 Z    =         2277779
86
 XDOT =      15428
352985                 XDOT =        4645
266867
 YDOT =       9009
068243  feet/sec       YDOT =        2798
230126  meter/sec
 ZDOT =      17722
741758                 ZDOT =        5424
596323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         351767
63                 X    =          107218
77
 Y    =      -20949583
24  feet           Y    =        -6385432
97  meter
 Z    =        7480215
87                 Z    =         2279969
80
 XDOT =      14942
627722                 XDOT =        4554
512930
 YDOT =       6632
405881  feet/sec       YDOT =        2021
557313  meter/sec
 ZDOT =      17823
933462                 ZDOT =        5432
734919


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   18191
28546808  
00016717  00000-0  10270-3 0  9154
2 25544  51
6362 263
5809 0003616 290
5069  69
5695 15
54058157 42103


Satellite: ISS
Catalog Number: 25544
Epoch time:      18191
28546808   =   yrday
fracday
Element set:     915
Inclination:       51
6362  deg
RA of node:       263
5809  deg
Eccentricity:     
0003616     
Arg of perigee:   290
5069  deg
Mean anomaly:      69
5695  deg
Mean motion:   15
54058157  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4210
Checksum:              331


Coasting Arc #17 (Orbit 4224)
---------------------------------------

Vector Time (GMT): 2018/192/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1860997
53                 A    =         6783718
57  meter
 Y    =        5396299
47  meter          E    =           
0003534
 Z    =       -3669876
29                 I    =           51
26609
 XDOT =      -4485
603086                 Wp   =           42
05576
 YDOT =      -4476
596468  meter/sec      RA   =          257
98350  deg
 ZDOT =      -4307
712138                 TA   =          181
83372
                                          MA   =          181
83501
                                          Ha   =            220
084  n
mi
                                          Hp   =            215
845

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6105634
95                 X    =        -1903375
90
 Y    =       17704394
60  feet           Y    =         5375252
17  meter
 Z    =      -12040276
55                 Z    =        -3679018
37
 XDOT =     -14716
545559                 XDOT =       -4414
286704
 YDOT =     -14686
996286  feet/sec       YDOT =       -4526
358114  meter/sec
 ZDOT =     -14132
913839                 ZDOT =       -4329
329044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3036479
08                 X    =         -925518
82
 Y    =       18452639
48  feet           Y    =         5624364
51  meter
 Z    =      -12081908
65                 Z    =        -3682565
76
 XDOT =     -15490
561786                 XDOT =       -4721
523232
 YDOT =     -11865
880126  feet/sec       YDOT =       -3616
720262  meter/sec
 ZDOT =     -14229
019164                 ZDOT =       -4337
005041


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   18192
25004162  
00016717  00000-0  10270-3 0  9165
2 25544  51
6378 258
7733 0003561 297
1892  62
8898 15
54082171 42258


Satellite: ISS
Catalog Number: 25544
Epoch time:      18192
25004162   =   yrday
fracday
Element set:     916
Inclination:       51
6378  deg
RA of node:       258
7733  deg
Eccentricity:     
0003561     
Arg of perigee:   297
1892  deg
Mean anomaly:      62
8898  deg
Mean motion:   15
54082171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4225
Checksum:              327


Coasting Arc #18 (Orbit 4240)
---------------------------------------

Vector Time (GMT): 2018/193/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2663992
20                 A    =         6780103
98  meter
 Y    =       -4118323
94  meter          E    =           
0004358
 Z    =        4678474
61                 I    =           51
26079
 XDOT =       4124
318857                 Wp   =          115
03055
 YDOT =       5835
751690  meter/sec      RA   =          252
96816  deg
 ZDOT =       2784
736994                 TA   =          307
20675
                                          MA   =          307
24652
                                          Ha   =            219
998  n
mi
                                          Hp   =            215
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8740131
90                 X    =         2687121
14
 Y    =      -13511561
48  feet           Y    =        -4088404
80  meter
 Z    =       15349326
14                 Z    =         4691470
70
 XDOT =      13531
229847                 XDOT =        4045
228725
 YDOT =      19146
166961  feet/sec       YDOT =        5881
429981  meter/sec
 ZDOT =       9136
276228                 ZDOT =        2804
580163

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6047538
95                 X    =         1843289
87
 Y    =      -14851735
60  feet           Y    =        -4526809
01  meter
 Z    =       15408025
01                 Z    =         4696366
02
 XDOT =      15633
269877                 XDOT =        4765
020658
 YDOT =      15948
641685  feet/sec       YDOT =        4861
145986  meter/sec
 ZDOT =       9224
284488                 ZDOT =        2811
561912


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   18193
27891613  
00016717  00000-0  10270-3 0  9174
2 25544  51
6366 253
6441 0003602 298
8206  61
2584 15
54081947 42411


Satellite: ISS
Catalog Number: 25544
Epoch time:      18193
27891613   =   yrday
fracday
Element set:     917
Inclination:       51
6366  deg
RA of node:       253
6441  deg
Eccentricity:     
0003602     
Arg of perigee:   298
8206  deg
Mean anomaly:      61
2584  deg
Mean motion:   15
54081947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4241
Checksum:              319
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