[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 11th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
012/22:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
2
017/20:15:08
782 0
8 0
9 0
9
N/A 0
4 -0
1 221
6
000/00:00:17
563 -0
2 -0
0 214
2
018/18:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 1397)
---------------------------------------
Vector Time (GMT): 2018/010/11:02:00
930
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3861278
16 A = 6780369
56 meter
Y = 3317717
04 meter E =
0008513
Z = -4485814
89 I = 52
00944
XDOT = -1901
646008 Wp = 90
23094
YDOT = 6653
385995 meter/sec RA = 84
15775 deg
ZDOT = 3289
308092 TA = 212
74919
MA = 212
80200
Ha = 221
029 n
mi
Hp = 214
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12668235
43 X = 3845681
22
Y = 10884898
42 feet Y = 3360809
47 meter
Z = -14717240
45 Z = -4467095
95
XDOT = -6238
996089 XDOT = -1991
882297
YDOT = 21828
694210 feet/sec YDOT = 6631
615808 meter/sec
ZDOT = 10791
693216 ZDOT = 3279
851698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9835457
75 X = -2997847
52
Y = 13588986
40 feet Y = 4141923
06 meter
Z = -14634397
44 Z = -4460564
34
XDOT = -21270
869761 XDOT = -6483
361103
YDOT = -3839
021435 feet/sec YDOT = -1170
133733 meter/sec
ZDOT = 10748
527755 ZDOT = 3276
151260
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 18010
46991590
00016717 00000-0 10270-3 0 9000
2 25544 51
6415 84
9753 0003243 355
9001 4
2125 15
54310966 13980
Satellite: ISS
Catalog Number: 25544
Epoch time: 18010
46991590 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 84
9753 deg
Eccentricity:
0003243
Arg of perigee: 355
9001 deg
Mean anomaly: 4
2125 deg
Mean motion: 15
54310966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1398
Checksum: 294
Coasting Arc #2 (Orbit 1413)
---------------------------------------
Vector Time (GMT): 2018/011/11:02:00
930
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3513189
26 A = 6784363
43 meter
Y = -4789648
85 meter E =
0013062
Z = 3270003
25 I = 52
01875
XDOT = 2782
744336 Wp = 77
54085
YDOT = -5315
421493 meter/sec RA = 79
19587 deg
ZDOT = -4777
151521 TA = 64
73640
MA = 64
60109
Ha = 221
167 n
mi
Hp = 214
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11526211
50 X = -3475252
91
Y = -15714071
03 feet Y = -4828723
80 meter
Z = 10728357
11 Z = 3253029
33
XDOT = 9129
738634 XDOT = 2865
180791
YDOT = -17439
046892 feet/sec YDOT = -5283
841750 meter/sec
ZDOT = -15673
069293 ZDOT = -4763
434027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14520000
44 X = 4425696
13
Y = -13059677
41 feet Y = -3980589
67 meter
Z = 10653527
07 Z = 3247195
05
XDOT = 17298
043651 XDOT = 5272
443705
YDOT = 6446
807905 feet/sec YDOT = 1964
987050 meter/sec
ZDOT = -15611
123891 ZDOT = -4758
270562
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 18011
49864366
00016717 00000-0 10270-3 0 9015
2 25544 51
6420 79
8460 0003427
7087 359
4070 15
54299086 14149
Satellite: ISS
Catalog Number: 25544
Epoch time: 18011
49864366 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 79
8460 deg
Eccentricity:
0003427
Arg of perigee:
7087 deg
Mean anomaly: 359
4070 deg
Mean motion: 15
54299086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1414
Checksum: 308
Coasting Arc #3 (Orbit 1428)
---------------------------------------
Vector Time (GMT): 2018/012/11:02:00
930
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3038466
48 A = 6787715
34 meter
Y = 5813792
18 meter E =
0010749
Z = -1723752
27 I = 52
02178
XDOT = -3630
568274 Wp = 26
81266
YDOT = 3587
607469 meter/sec RA = 74
24463 deg
ZDOT = 5723
661774 TA = 314
37823
MA = 314
46621
Ha = 221
297 n
mi
Hp = 214
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9968722
05 X = 2981602
30
Y = 19074121
31 feet Y = 5847452
56 meter
Z = -5655355
22 Z = -1709130
25
XDOT = -11911
313234 XDOT = -3698
218429
YDOT = 11770
365712 feet/sec YDOT = 3546
629336 meter/sec
ZDOT = 18778
417893 ZDOT = 5705
861744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17812732
07 X = -5429320
74
Y = 12108918
30 feet Y = 3690798
30 meter
Z = -5591175
15 Z = -1704190
19
XDOT = -12180
583212 XDOT = -3712
641763
YDOT = -9319
773214 feet/sec YDOT = -2840
666876 meter/sec
ZDOT = 18698
556399 ZDOT = 5699
319990
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 18012
46307280
00016717 00000-0 10270-3 0 9021
2 25544 51
6413 75
0379 0003558 2
3521 357
7648 15
54258837 14291
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
46307280 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 75
0379 deg
Eccentricity:
0003558
Arg of perigee: 2
3521 deg
Mean anomaly: 357
7648 deg
Mean motion: 15
54258837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1429
Checksum: 306
Coasting Arc #4 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2018/012/22:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3351142
80 A = 6787490
21 meter
Y = -5601690
70 meter E =
0013373
Z = 1844297
03 I = 52
01718
XDOT = 3381
062818 Wp = 98
63384
YDOT = -3900
542419 meter/sec RA = 71
85529 deg
ZDOT = -5670
614856 TA = 61
18682
MA = 61
05261
Ha = 221
358 n
mi
Hp = 214
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10994562
99 X = -3297212
69
Y = -18378250
34 feet Y = -5638864
07 meter
Z = 6050843
27 Z = 1828149
02
XDOT = 11092
725782 XDOT = 3451
973140
YDOT = -12797
055180 feet/sec YDOT = -3862
336175 meter/sec
ZDOT = -18604
379450 ZDOT = -5654
018969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18281195
12 X = -5572108
27
Y = 11193420
35 feet Y = 3411754
52 meter
Z = 5979837
02 Z = 1822654
32
XDOT = -12079
326437 XDOT = -3681
778698
YDOT = -9770
343502 feet/sec YDOT = -2978
000699 meter/sec
ZDOT = -18529
825150 ZDOT = -5647
890706
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 18012
97743593
00016717 00000-0 10270-3 0 9039
2 25544 51
6417 72
4758 0003682 7
5464 352
5744 15
54277308 14371
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
97743593 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 72
4758 deg
Eccentricity:
0003682
Arg of perigee: 7
5464 deg
Mean anomaly: 352
5744 deg
Mean motion: 15
54277308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 324
Coasting Arc #5 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2018/013/22:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2742235
87 A = 6788809
58 meter
Y = 6200235
48 meter E =
0015193
Z = -116238
14 I = 52
01176
XDOT = -4280
038565 Wp = 35
89345
YDOT = 1998
616238 meter/sec RA = 66
90838 deg
ZDOT = 6045
135245 TA = 322
86021
MA = 322
96523
Ha = 221
387 n
mi
Hp = 214
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8996836
86 X = 2673263
98
Y = 20341979
94 feet Y = 6230515
41 meter
Z = -381358
74 Z = -103084
46
XDOT = -14042
121275 XDOT = -4331
433357
YDOT = 6557
139890 feet/sec YDOT = 1950
466083 meter/sec
ZDOT = 19833
120884 ZDOT = 6024
219805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20102177
19 X = 6127143
61
Y = -9522724
57 feet Y = -2902526
45 meter
Z = -323797
50 Z = -98693
48
XDOT = 6229
077523 XDOT = 1898
622829
YDOT = 12532
062212 feet/sec YDOT = 3819
772562 meter/sec
ZDOT = 19739
631949 ZDOT = 6016
639818
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 18013
94185937
00016717 00000-0 10270-3 0 9040
2 25544 51
6427 67
6668 0003850 8
4104 351
7112 15
54306425 14526
Satellite: ISS
Catalog Number: 25544
Epoch time: 18013
94185937 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 67
6668 deg
Eccentricity:
0003850
Arg of perigee: 8
4104 deg
Mean anomaly: 351
7112 deg
Mean motion: 15
54306425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 300
Coasting Arc #6 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2018/014/22:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1884756
89 A = 6787694
10 meter
Y = -6304605
78 meter E =
0006092
Z = -1663483
51 I = 51
99400
XDOT = 5077
587223 Wp = 113
45528
YDOT = -8
407401 meter/sec RA = 61
96230 deg
ZDOT = -5740
099699 TA = 84
66698
MA = 84
59748
Ha = 221
442 n
mi
Hp = 214
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6183585
58 X = -1806036
78
Y = -20684402
18 feet Y = -6325242
14 meter
Z = -5457623
06 Z = -1672448
20
XDOT = 16658
750733 XDOT = 5105
185913
YDOT = -27
583337 feet/sec YDOT = 48
528422 meter/sec
ZDOT = -18832
348095 ZDOT = -5715
367796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20400839
03 X = -6218175
74
Y = 7032861
19 feet Y = 2143616
09 meter
Z = -5496499
24 Z = -1675332
97
XDOT = -239
252549 XDOT = -72
924177
YDOT = -15277
970891 feet/sec YDOT = -4656
725528 meter/sec
ZDOT = -18722
187062 ZDOT = -5706
522616
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 18014
97057554
00016717 00000-0 10270-3 0 9058
2 25544 51
6427 62
5379 0003750 12
6007 347
5239 15
54279884 14685
Satellite: ISS
Catalog Number: 25544
Epoch time: 18014
97057554 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 62
5379 deg
Eccentricity:
0003750
Arg of perigee: 12
6007 deg
Mean anomaly: 347
5239 deg
Mean motion: 15
54279884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 327
Coasting Arc #7 (Orbit 1483)
---------------------------------------
Vector Time (GMT): 2018/015/22:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 825430
20 A = 6784419
99 meter
Y = 5902760
54 meter E =
0014615
Z = 3223916
73 I = 51
96594
XDOT = -5685
556462 Wp = 71
71846
YDOT = -1841
634373 meter/sec RA = 57
00767 deg
ZDOT = 4814
235891 TA = 325
44117
MA = 325
53609
Ha = 221
580 n
mi
Hp = 213
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2708104
32 X = 743702
74
Y = 19366012
26 feet Y = 5911533
85 meter
Z = 10577154
63 Z = 3227728
27
XDOT = -18653
400465 XDOT = -5687
924920
YDOT = -6042
107522 feet/sec YDOT = -1905
227760 meter/sec
ZDOT = 15794
737176 ZDOT = 4786
611948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19172731
28 X = 5843848
49
Y = -3800563
45 feet Y = -1158411
74 meter
Z = 10593137
05 Z = 3228788
17
XDOT = -5176
700156 XDOT = -1577
858207
YDOT = 17688
880669 feet/sec YDOT = 5391
570828 meter/sec
ZDOT = 15672
004283 ZDOT = 4776
826906
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 18015
99928915
00016717 00000-0 10270-3 0 9060
2 25544 51
6417 57
4082 0004000 16
8901 343
2384 15
54295317 14847
Satellite: ISS
Catalog Number: 25544
Epoch time: 18015
99928915 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 57
4082 deg
Eccentricity:
0004000
Arg of perigee: 16
8901 deg
Mean anomaly: 343
2384 deg
Mean motion: 15
54295317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1484
Checksum: 311
Coasting Arc #8 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2018/016/22:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 443562
34 A = 6780391
15 meter
Y = -5103254
98 meter E =
0012076
Z = -4454747
78 I = 51
93408
XDOT = 5983
036145 Wp = 54
36427
YDOT = 3428
241701 meter/sec RA = 52
04153 deg
ZDOT = -3331
062647 TA = 182
09523
MA = 182
10029
Ha = 221
508 n
mi
Hp = 213
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1455257
01 X = 522233
77
Y = -16742962
52 feet Y = -5097854
59 meter
Z = -14615314
22 Z = -4452402
40
XDOT = 19629
383678 XDOT = 5960
436212
YDOT = 11247
512144 feet/sec YDOT = 3495
021962 meter/sec
ZDOT = -10928
683224 ZDOT = -3302
054312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16814051
84 X = -5124923
00
Y = -250556
43 feet Y = -76369
60 meter
Z = -14604001
47 Z = -4451299
65
XDOT = 9669
357835 XDOT = 2947
220268
YDOT = -19286
433455 feet/sec YDOT = -5878
504917 meter/sec
ZDOT = -10800
054195 ZDOT = -3291
856519
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 18016
96370404
00016717 00000-0 10270-3 0 9073
2 25544 51
6418 52
5995 0003911 17
4609 342
6677 15
54319699 14993
Satellite: ISS
Catalog Number: 25544
Epoch time: 18016
96370404 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 52
5995 deg
Eccentricity:
0003911
Arg of perigee: 17
4609 deg
Mean anomaly: 342
6677 deg
Mean motion: 15
54319699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 340
Coasting Arc #9 (Orbit 1512)
---------------------------------------
Vector Time (GMT): 2018/017/20:15:17
563
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1200711
80 A = 6778760
99 meter
Y = -4462690
79 meter E =
0014635
Z = -4972722
21 I = 51
90864
XDOT = 6084
338491 Wp = 61
87844
YDOT = 4093
722710 meter/sec RA = 47
55327 deg
ZDOT = -2202
944807 TA = 186
67016
MA = 186
68966
Ha = 221
610 n
mi
Hp = 214
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3939343
16 X = 1274679
95
Y = -14641373
99 feet Y = -4448849
77 meter
Z = -16314705
43 Z = -4966710
27
XDOT = 19961
740455 XDOT = 6048
809717
YDOT = 13430
848787 feet/sec YDOT = 4161
563413 meter/sec
ZDOT = -7227
509210 ZDOT = -2173
475854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10686416
54 X = -3257219
76
Y = -10797526
75 feet Y = -3291086
15 meter
Z = -16287166
35 Z = -4964328
30
XDOT = 20819
679051 XDOT = 6345
838175
YDOT = -9891
467862 feet/sec YDOT = -3014
919404 meter/sec
ZDOT = -7096
944959 ZDOT = -2163
148824
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 18017
86382426
00016717 00000-0 10270-3 0 9081
2 25544 51
6421 48
1102 0003559 16
0943 344
0323 15
54179564 15138
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
86382426 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 48
1102 deg
Eccentricity:
0003559
Arg of perigee: 16
0943 deg
Mean anomaly: 344
0323 deg
Mean motion: 15
54179564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1513
Checksum: 293
Coasting Arc #10 (Orbit 1527)
---------------------------------------
Vector Time (GMT): 2018/018/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5113833
37 A = 6780987
32 meter
Y = 16587
37 meter E =
0011936
Z = 4448306
54 I = 51
89223
XDOT = -2922
795035 Wp = 56
36675
YDOT = -6264
657575 meter/sec RA = 42
83327 deg
ZDOT = -3323
878885 TA = 67
11238
MA = 66
98642
Ha = 221
835 n
mi
Hp = 214
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16777668
54 X = -5135245
87
Y = 54420
52 feet Y = -40718
91 meter
Z = 14594181
57 Z = 4423413
82
XDOT = -9589
222555 XDOT = -2836
379403
YDOT = -20553
338501 feet/sec YDOT = -6296
858966 meter/sec
ZDOT = -10905
114452 ZDOT = -3337
866869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12840888
96 X = -3913902
95
Y = 10946633
17 feet Y = 3336533
79 meter
Z = 14483302
51 Z = 4414510
61
XDOT = -19747
507262 XDOT = -6019
040214
YDOT = -8599
133182 feet/sec YDOT = -2621
015794 meter/sec
ZDOT = -10966
348139 ZDOT = -3342
542913
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 18018
82833669
00016717 00000-0 10270-3 0 9099
2 25544 51
6402 43
3019 0003571 20
0504 340
0788 15
54153060 15283
Satellite: ISS
Catalog Number: 25544
Epoch time: 18018
82833669 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 43
3019 deg
Eccentricity:
0003571
Arg of perigee: 20
0504 deg
Mean anomaly: 340
0788 deg
Mean motion: 15
54153060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1528
Checksum: 286
Coasting Arc #11 (Orbit 1542)
---------------------------------------
Vector Time (GMT): 2018/019/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5802596
80 A = 6784718
45 meter
Y = 1240876
83 meter E =
0007062
Z = -3290507
89 I = 51
88075
XDOT = 1438
732799 Wp = 56
34439
YDOT = 5840
011312 meter/sec RA = 37
86333 deg
ZDOT = 4750
555419 TA = 265
59975
MA = 265
68044
Ha = 221
780 n
mi
Hp = 214
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19037391
09 X = 5804272
95
Y = 4071118
22 feet Y = 1305774
89 meter
Z = -10795629
56 Z = -3262317
37
XDOT = 4720
251965 XDOT = 1350
246074
YDOT = 19160
142100 feet/sec YDOT = 5855
605350 meter/sec
ZDOT = 15585
811742 ZDOT = 4757
329346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17050978
06 X = 5197138
11
Y = -9536829
92 feet Y = -2906825
76 meter
Z = -10670281
30 Z = -3252301
74
XDOT = 15408
912419 XDOT = 4696
636505
YDOT = 10120
233055 feet/sec YDOT = 3084
647035 meter/sec
ZDOT = 15614
981947 ZDOT = 4759
446497
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 18019
79284620
00016717 00000-0 10270-3 0 9105
2 25544 51
6408 38
4931 0003522 22
2208 337
9096 15
54170837 15433
Satellite: ISS
Catalog Number: 25544
Epoch time: 18019
79284620 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 38
4931 deg
Eccentricity:
0003522
Arg of perigee: 22
2208 deg
Mean anomaly: 337
9096 deg
Mean motion: 15
54170837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1543
Checksum: 302
Coasting Arc #12 (Orbit 1558)
---------------------------------------
Vector Time (GMT): 2018/020/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6126194
76 A = 6788014
44 meter
Y = -2328761
36 meter E =
0014423
Z = 1748371
51 I = 51
86578
XDOT = 311
767208 Wp = 101
05420
YDOT = -5124
611680 meter/sec RA = 32
90239 deg
ZDOT = -5696
297705 TA = 59
81680
MA = 59
67401
Ha = 221
816 n
mi
Hp = 214
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20099064
18 X = -6108191
12
Y = -7640293
19 feet Y = -2397168
02 meter
Z = 5736127
00 Z = 1718656
87
XDOT = 1022
858293 XDOT = 396
717898
YDOT = -16813
030445 feet/sec YDOT = -5120
650267 meter/sec
ZDOT = -18688
640766 ZDOT = -5694
576978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20044958
51 X = -6109703
35
Y = 7876698
20 feet Y = 2400817
61 meter
Z = 5604183
95 Z = 1708155
27
XDOT = -9878
135534 XDOT = -3010
855711
YDOT = -11759
057488 feet/sec YDOT = -3584
160722 meter/sec
ZDOT = -18680
096931 ZDOT = -5693
693544
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 18020
82165360
00016717 00000-0 10270-3 0 9111
2 25544 51
6415 33
3641 0003516 26
4278 333
7054 15
54156088 15596
Satellite: ISS
Catalog Number: 25544
Epoch time: 18020
82165360 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 33
3641 deg
Eccentricity:
0003516
Arg of perigee: 26
4278 deg
Mean anomaly: 333
7054 deg
Mean motion: 15
54156088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1559
Checksum: 291
Coasting Arc #13 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2018/021/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6012892
51 A = 6789216
49 meter
Y = 3134848
37 meter E =
0015615
Z = -61771
92 I = 51
84223
XDOT = -2149
496644 Wp = 41
04898
YDOT = 4224
539796 meter/sec RA = 27
94559 deg
ZDOT = 6031
660801 TA = 318
28726
MA = 318
40621
Ha = 221
877 n
mi
Hp = 213
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19727337
64 X = 5977690
96
Y = 10284935
61 feet Y = 3201891
83 meter
Z = -202663
77 Z = -32649
39
XDOT = -7052
154345 XDOT = -2225
874960
YDOT = 13860
038700 feet/sec YDOT = 4200
075633 meter/sec
ZDOT = 19788
913389 ZDOT = 6021
033937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21420222
46 X = 6528883
81
Y = -6013109
86 feet Y = -1832795
89 meter
Z = -73505
24 Z = -22404
40
XDOT = 3818
650917 XDOT = 1163
924799
YDOT = 13458
329767 feet/sec YDOT = 4102
098913 meter/sec
ZDOT = 19740
859508 ZDOT = 6017
013978
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 18021
78615712
00016717 00000-0 10270-3 0 9129
2 25544 51
6418 28
5557 0003667 28
5307 331
6046 15
54167676 15744
Satellite: ISS
Catalog Number: 25544
Epoch time: 18021
78615712 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 28
5557 deg
Eccentricity:
0003667
Arg of perigee: 28
5307 deg
Mean anomaly: 331
6046 deg
Mean motion: 15
54167676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 317
Coasting Arc #14 (Orbit 1589)
---------------------------------------
Vector Time (GMT): 2018/022/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5419220
17 A = 6788023
69 meter
Y = -3728632
21 meter E =
0007251
Z = -1672972
66 I = 51
80902
XDOT = 3965
251071 Wp = 114
92403
YDOT = -3206
364849 meter/sec RA = 22
98838 deg
ZDOT = -5720
759575 TA = 83
35267
MA = 83
27014
Ha = 221
841 n
mi
Hp = 213
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17779593
74 X = -5368996
53
Y = -12233045
31 feet Y = -3788952
85 meter
Z = -5488755
43 Z = -1699174
95
XDOT = 13009
353909 XDOT = 4028
598849
YDOT = -10519
569713 feet/sec YDOT = -3161
668564 meter/sec
ZDOT = -18768
896243 ZDOT = -5701
344133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21248910
64 X = -6476667
96
Y = 3599699
45 feet Y = 1097188
39 meter
Z = -5604796
85 Z = -1708342
08
XDOT = 2342
394585 XDOT = 713
961869
YDOT = -15148
929862 feet/sec YDOT = -4617
393822 meter/sec
ZDOT = -18681
882208 ZDOT = -5694
237697
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 18022
81496000
00016717 00000-0 10270-3 0 9132
2 25544 51
6421 23
4276 0003441 32
3203 327
8160 15
54150230 15908
Satellite: ISS
Catalog Number: 25544
Epoch time: 18022
81496000 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 23
4276 deg
Eccentricity:
0003441
Arg of perigee: 32
3203 deg
Mean anomaly: 327
8160 deg
Mean motion: 15
54150230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1590
Checksum: 254
Coasting Arc #15 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2018/023/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4379622
79 A = 6784807
83 meter
Y = 4068914
05 meter E =
0015314
Z = 3191573
71 I = 51
76844
XDOT = -5555
864401 Wp = 75
36456
YDOT = 2186
471580 meter/sec RA = 18
02135 deg
ZDOT = 4820
969837 TA = 321
47389
MA = 321
58309
Ha = 221
870 n
mi
Hp = 213
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14368841
16 X = 4318294
78
Y = 13349455
54 feet Y = 4117547
12 meter
Z = 10471042
35 Z = 3212699
17
XDOT = -18227
901579 XDOT = -5603
318670
YDOT = 7173
463188 feet/sec YDOT = 2124
076816 meter/sec
ZDOT = 15816
830173 ZDOT = 4793
866387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19549112
02 X = 5958569
34
Y = -734704
04 feet Y = -223937
79 meter
Z = 10564408
02 Z = 3220031
56
XDOT = -7884
109592 XDOT = -2403
076604
YDOT = 16635
819200 feet/sec YDOT = 5070
597692 meter/sec
ZDOT = 15695
763446 ZDOT = 4784
068698
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 18023
84375942
00016717 00000-0 10270-3 0 9148
2 25544 51
6426 18
2983 0003674 34
7604 325
3789 15
54170574 16060
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
84375942 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 18
2983 deg
Eccentricity:
0003674
Arg of perigee: 34
7604 deg
Mean anomaly: 325
3789 deg
Mean motion: 15
54170574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 322
Coasting Arc #16 (Orbit 1620)
---------------------------------------
Vector Time (GMT): 2018/024/18:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2940370
19 A = 6780859
03 meter
Y = -4248510
71 meter E =
0012341
Z = -4404283
04 I = 51
72380
XDOT = 6767
224509 Wp = 59
72311
YDOT = -1174
711198 meter/sec RA = 13
04285 deg
ZDOT = -3385
760956 TA = 176
00323
MA = 175
99337
Ha = 221
903 n
mi
Hp = 213
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9646883
84 X = -2871250
17
Y = -13938683
43 feet Y = -4281005
48 meter
Z = -14449747
50 Z = -4418398
33
XDOT = 22202
180148 XDOT = 6796
303597
YDOT = -3854
039363 feet/sec YDOT = -1098
872872 meter/sec
ZDOT = -11108
139621 ZDOT = -3352
817776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16670860
13 X = -5081278
17
Y = -2762754
83 feet Y = -842087
67 meter
Z = -14511859
80 Z = -4423214
87
XDOT = 12442
845335 XDOT = 3792
579258
YDOT = -17523
433564 feet/sec YDOT = -5341
142550 meter/sec
ZDOT = -10961
253767 ZDOT = -3340
990148
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 18024
80825447
00016717 00000-0 10270-3 0 9156
2 25544 51
6425 13
4904 0003655 36
6731 323
4671 15
54195478 16216
Satellite: ISS
Catalog Number: 25544
Epoch time: 18024
80825447 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 13
4904 deg
Eccentricity:
0003655
Arg of perigee: 36
6731 deg
Mean anomaly: 323
4671 deg
Mean motion: 15
54195478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1621
Checksum: 306
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