[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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