[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 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) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
122/14:29:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 213
9
128/00:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
5
Coasting Arc #1 (Orbit 3062)
---------------------------------------
Vector Time (GMT): 2018/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -805552
29 A = 6788764
33 meter
Y = 6674237
23 meter E =
0008851
Z = -926995
49 I = 51
27693
XDOT = -4709
056321 Wp = 124
39687
YDOT = -1379
985047 meter/sec RA = 270
53432 deg
ZDOT = -5888
808921 TA = 65
68680
MA = 65
59440
Ha = 221
494 n
mi
Hp = 214
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2642888
09 X = -875622
65
Y = 21897103
76 feet Y = 6664837
15 meter
Z = -3041323
80 Z = -931079
20
XDOT = -15449
659846 XDOT = -4664
669903
YDOT = -4527
509996 feet/sec YDOT = -1432
397112 meter/sec
ZDOT = -19320
239241 ZDOT = -5911
576260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10258690
90 X = 3126848
99
Y = 19522055
34 feet Y = 5950322
47 meter
Z = -3060437
46 Z = -932821
34
XDOT = -13764
183652 XDOT = -4195
323177
YDOT = 4211
414176 feet/sec YDOT = 1283
639041 meter/sec
ZDOT = -19421
574554 ZDOT = -5919
695924
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 18117
53038744
00016717 00000-0 10270-3 0 9009
2 25544 51
6369 271
2428 0002922 21
4284 338
6990 15
54194433 30633
Satellite: ISS
Catalog Number: 25544
Epoch time: 18117
53038744 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 271
2428 deg
Eccentricity:
0002922
Arg of perigee: 21
4284 deg
Mean anomaly: 338
6990 deg
Mean motion: 15
54194433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3063
Checksum: 306
Coasting Arc #2 (Orbit 3078)
---------------------------------------
Vector Time (GMT): 2018/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1564298
96 A = 6786391
61 meter
Y = -6088471
08 meter E =
0015475
Z = 2535551
82 I = 51
27076
XDOT = 4484
535075 Wp = 68
42901
YDOT = 3346
994299 meter/sec RA = 265
53552 deg
ZDOT = 5249
938518 TA = 320
22415
MA = 320
33751
Ha = 221
430 n
mi
Hp = 214
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5132214
43 X = 1619949
08
Y = -19975298
82 feet Y = -6070666
73 meter
Z = 8318739
58 Z = 2543286
22
XDOT = 14713
041585 XDOT = 4421
272946
YDOT = 10980
952423 feet/sec YDOT = 3396
789990 meter/sec
ZDOT = 17224
207737 ZDOT = 5271
569351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7478491
22 X = -2279444
13
Y = -19205097
09 feet Y = -5853713
59 meter
Z = 8354042
79 Z = 2546312
24
XDOT = 16862
473503 XDOT = 5139
681924
YDOT = 996
692881 feet/sec YDOT = 303
791990 meter/sec
ZDOT = 17320
215419 ZDOT = 5279
201660
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 18118
55919332
00016717 00000-0 10270-3 0 9014
2 25544 51
6379 266
1139 0002657 25
2984 334
8298 15
54194099 30794
Satellite: ISS
Catalog Number: 25544
Epoch time: 18118
55919332 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 266
1139 deg
Eccentricity:
0002657
Arg of perigee: 25
2984 deg
Mean anomaly: 334
8298 deg
Mean motion: 15
54194099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3079
Checksum: 342
Coasting Arc #3 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2018/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2339453
04 A = 6782659
36 meter
Y = 5032905
32 meter E =
0008766
Z = -3908955
52 I = 51
26281
XDOT = -4120
111030 Wp = 60
49519
YDOT = -5044
015105 meter/sec RA = 260
52761 deg
ZDOT = -4031
112743 TA = 167
08422
MA = 167
06175
Ha = 221
569 n
mi
Hp = 213
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7675370
87 X = -2376570
50
Y = 16512156
56 feet Y = 5006536
28 meter
Z = -12824657
21 Z = -3920410
29
XDOT = -13517
424639 XDOT = -4043
819884
YDOT = -16548
605988 feet/sec YDOT = -5089
662582 meter/sec
ZDOT = -13225
435510 ZDOT = -4050
941715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3726705
72 X = 1135899
90
Y = 17786072
42 feet Y = 5421194
87 meter
Z = -12876403
11 Z = -3924727
67
XDOT = -19344
826068 XDOT = -5896
302986
YDOT = -5578
735067 feet/sec YDOT = -1700
398449 meter/sec
ZDOT = -13313
190790 ZDOT = -4057
860553
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 18119
52369618
00016717 00000-0 10270-3 0 9029
2 25544 51
6390 261
3053 0002809 27
9013 332
2290 15
54179753 30941
Satellite: ISS
Catalog Number: 25544
Epoch time: 18119
52369618 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 261
3053 deg
Eccentricity:
0002809
Arg of perigee: 27
9013 deg
Mean anomaly: 332
2290 deg
Mean motion: 15
54179753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 304
Coasting Arc #4 (Orbit 3109)
---------------------------------------
Vector Time (GMT): 2018/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3078003
17 A = 6779045
70 meter
Y = -3606623
39 meter E =
0007506
Z = 4838946
14 I = 51
25818
XDOT = 3624
476044 Wp = 98
74883
YDOT = 6321
909448 meter/sec RA = 255
50966 deg
ZDOT = 2402
110277 TA = 327
56380
MA = 327
60991
Ha = 221
429 n
mi
Hp = 213
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10098435
60 X = 3094599
14
Y = -11832753
90 feet Y = -3572110
19 meter
Z = 15875807
54 Z = 4853938
65
XDOT = 11891
325605 XDOT = 3541
844934
YDOT = 20741
172729 feet/sec YDOT = 6361
978840 meter/sec
ZDOT = 7880
939230 ZDOT = 2419
516304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 723329
68 X = 220470
89
Y = -15470192
24 feet Y = -4715314
59 meter
Z = 15943138
89 Z = 4859468
73
XDOT = 20892
576716 XDOT = 6368
057383
YDOT = 9192
424889 feet/sec YDOT = 2801
851106 meter/sec
ZDOT = 7957
732038 ZDOT = 2425
516725
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 18120
55249342
00016717 00000-0 10270-3 0 9036
2 25544 51
6396 256
1762 0002797 30
6568 329
4747 15
54213960 31101
Satellite: ISS
Catalog Number: 25544
Epoch time: 18120
55249342 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 256
1762 deg
Eccentricity:
0002797
Arg of perigee: 30
6568 deg
Mean anomaly: 329
4747 deg
Mean motion: 15
54213960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3110
Checksum: 311
Coasting Arc #5 (Orbit 3124)
---------------------------------------
Vector Time (GMT): 2018/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3797812
88 A = 6777239
16 meter
Y = 1955353
38 meter E =
0016746
Z = -5276085
85 I = 51
26108
XDOT = -2929
630317 Wp = 78
44569
YDOT = -7055
664242 meter/sec RA = 250
48576 deg
ZDOT = -504
153500 TA = 186
70043
MA = 186
72284
Ha = 221
654 n
mi
Hp = 213
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12460016
01 X = -3793766
97
Y = 6415201
37 feet Y = 1912906
31 meter
Z = -17309992
94 Z = -5294524
82
XDOT = -9611
648022 XDOT = -2848
065257
YDOT = -23148
504732 feet/sec YDOT = -7087
969321 meter/sec
ZDOT = -1654
046915 ZDOT = -518
186882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5670141
87 X = -1728259
24
Y = 12704085
61 feet Y = 3872205
29 meter
Z = -17392480
08 Z = -5301227
93
XDOT = -20996
171146 XDOT = -6399
632965
YDOT = -11728
613290 feet/sec YDOT = -3574
881331 meter/sec
ZDOT = -1715
715504 ZDOT = -522
950086
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 18121
51699032
00016717 00000-0 10270-3 0 9049
2 25544 51
6394 251
3691 0002905 35
9202 324
2146 15
54201109 31255
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
51699032 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 251
3691 deg
Eccentricity:
0002905
Arg of perigee: 35
9202 deg
Mean anomaly: 324
2146 deg
Mean motion: 15
54201109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3125
Checksum: 278
Coasting Arc #6 (Orbit 3140)
---------------------------------------
Vector Time (GMT): 2018/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4423686
88 A = 6777876
50 meter
Y = -209673
28 meter E =
0007439
Z = 5127143
65 I = 51
27596
XDOT = 2032
955637 Wp = 48
87407
YDOT = 7253
979581 meter/sec RA = 245
45876 deg
ZDOT = -1451
190235 TA = 55
19234
MA = 55
12237
Ha = 221
584 n
mi
Hp = 213
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14513408
41 X = 4400797
32
Y = -687904
47 feet Y = -160332
72 meter
Z = 16821337
43 Z = 5148577
17
XDOT = 6669
801959 XDOT = 1958
737808
YDOT = 23799
145608 feet/sec YDOT = 7276
298559 meter/sec
ZDOT = -4761
122818 ZDOT = -1441
494699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10679567
25 X = 3255132
10
Y = -9686739
88 feet Y = -2952518
32 meter
Z = 16916960
22 Z = 5156289
47
XDOT = 19597
293023 XDOT = 5973
254913
YDOT = 13329
671537 feet/sec YDOT = 4062
883885 meter/sec
ZDOT = -4718
813500 ZDOT = -1438
294355
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 18122
54578245
00016717 00000-0 10270-3 0 9056
2 25544 51
6403 246
2394 0002947 39
0861 321
0504 15
54182210 31413
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
54578245 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 246
2394 deg
Eccentricity:
0002947
Arg of perigee: 39
0861 deg
Mean anomaly: 321
0504 deg
Mean motion: 15
54182210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3141
Checksum: 283
Coasting Arc #7 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2018/122/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4603294
81 A = 6784809
57 meter
Y = -3848122
49 meter E =
0006902
Z = -3169473
32 I = 51
30132
XDOT = 1537
134034 Wp = 62
59503
YDOT = -5778
290905 meter/sec RA = 244
93033 deg
ZDOT = 4794
207217 TA = 260
64297
MA = 260
72102
Ha = 221
600 n
mi
Hp = 213
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15102673
26 X = -4544526
02
Y = -12625073
79 feet Y = -3899271
00 meter
Z = -10398534
51 Z = -3191692
31
XDOT = 5043
090663 XDOT = 1578
346072
YDOT = -18957
647325 feet/sec YDOT = -5760
871343 meter/sec
ZDOT = 15729
026301 ZDOT = 4801
774120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15718730
88 X = -4791069
17
Y = 11761985
67 feet Y = 3585053
23 meter
Z = -10497139
61 Z = -3199528
15
XDOT = -16475
091238 XDOT = -5021
607809
YDOT = -7981
385736 feet/sec YDOT = -2432
726372 meter/sec
ZDOT = 15763
518815 ZDOT = 4804
720535
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 18122
61008008
00016717 00000-0 10270-3 0 9060
2 25544 51
6410 245
9214 0002882 34
3855 325
7484 15
54189282 31422
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
61008008 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 245
9214 deg
Eccentricity:
0002882
Arg of perigee: 34
3855 deg
Mean anomaly: 325
7484 deg
Mean motion: 15
54189282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 296
Coasting Arc #8 (Orbit 3157)
---------------------------------------
Vector Time (GMT): 2018/123/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4350867
87 A = 6787981
09 meter
Y = 4948841
60 meter E =
0014937
Z = 1606481
09 I = 51
32663
XDOT = -2780
009008 Wp = 105
20812
YDOT = 4308
581322 meter/sec RA = 239
93144 deg
ZDOT = -5703
041160 TA = 57
13093
MA = 56
98726
Ha = 221
726 n
mi
Hp = 213
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14274500
89 X = 4287401
65
Y = 16236356
97 feet Y = 4997141
07 meter
Z = 5270607
24 Z = 1627462
49
XDOT = -9120
764463 XDOT = -2800
279335
YDOT = 14135
765491 feet/sec YDOT = 4277
380268 meter/sec
ZDOT = -18710
764959 ZDOT = -5716
594725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18876033
00 X = 5753414
86
Y = -10492258
88 feet Y = -3198040
51 meter
Z = 5363566
54 Z = 1634815
08
XDOT = 11152
270786 XDOT = 3399
212136
YDOT = 10400
535644 feet/sec YDOT = 3170
083264 meter/sec
ZDOT = -18771
770115 ZDOT = -5721
635531
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 18123
63886641
00016717 00000-0 10270-3 0 9071
2 25544 51
6407 240
7927 0003068 39
9517 320
1861 15
54203419 31589
Satellite: ISS
Catalog Number: 25544
Epoch time: 18123
63886641 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 240
7927 deg
Eccentricity:
0003068
Arg of perigee: 39
9517 deg
Mean anomaly: 320
1861 deg
Mean motion: 15
54203419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3158
Checksum: 314
Coasting Arc #9 (Orbit 3173)
---------------------------------------
Vector Time (GMT): 2018/124/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3835981
62 A = 6789195
88 meter
Y = -5591835
09 meter E =
0015424
Z = 90312
70 I = 51
34713
XDOT = 4001
042934 Wp = 45
37354
YDOT = -2637
940419 meter/sec RA = 234
93967 deg
ZDOT = 5989
460724 TA = 315
60354
MA = 315
72710
Ha = 221
814 n
mi
Hp = 213
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12585241
55 X = -3773605
80
Y = -18345915
66 feet Y = -5634382
92 meter
Z = 296301
51 Z = 71829
82
XDOT = 13126
781280 XDOT = 4001
149735
YDOT = -8654
660167 feet/sec YDOT = -2593
197706 meter/sec
ZDOT = 19650
461693 ZDOT = 6008
896773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20440857
13 X = -6230373
25
Y = 8784876
09 feet Y = 2677630
23 meter
Z = 214551
96 Z = 65395
44
XDOT = -5324
065013 XDOT = -1622
775016
YDOT = -12938
914160 feet/sec YDOT = -3943
781036 meter/sec
ZDOT = 19737
499055 ZDOT = 6015
989712
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 18124
66764951
00016717 00000-0 10270-3 0 9085
2 25544 51
6401 235
6640 0003198 41
2705 318
8689 15
54174988 31745
Satellite: ISS
Catalog Number: 25544
Epoch time: 18124
66764951 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 235
6640 deg
Eccentricity:
0003198
Arg of perigee: 41
2705 deg
Mean anomaly: 318
8689 deg
Mean motion: 15
54174988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3174
Checksum: 334
Coasting Arc #10 (Orbit 3188)
---------------------------------------
Vector Time (GMT): 2018/125/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2985649
75 A = 6787694
49 meter
Y = 5816067
42 meter E =
0007728
Z = -1822658
87 I = 51
36140
XDOT = -5132
760848 Wp = 118
11187
YDOT = 879
574229 meter/sec RA = 229
94907 deg
ZDOT = -5622
973466 TA = 81
99754
MA = 81
90985
Ha = 221
813 n
mi
Hp = 213
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9795438
82 X = 2929244
60
Y = 19081586
01 feet Y = 5849139
72 meter
Z = -5979851
95 Z = -1808292
19
XDOT = -16839
766561 XDOT = -5114
901302
YDOT = 2885
742221 feet/sec YDOT = 822
276300 meter/sec
ZDOT = -18448
075676 ZDOT = -5647
863464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20522388
19 X = 6255223
92
Y = -6296273
59 feet Y = -1919104
19 meter
Z = -5916476
78 Z = -1803342
12
XDOT = -584
221380 XDOT = -178
070677
YDOT = 15467
444056 feet/sec YDOT = 4714
476948 meter/sec
ZDOT = -18559
233493 ZDOT = -5656
854369
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 18125
63212790
00016717 00000-0 10270-3 0 9093
2 25544 51
6392 230
8558 0003112 46
5264 313
6147 15
54214855 31899
Satellite: ISS
Catalog Number: 25544
Epoch time: 18125
63212790 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 230
8558 deg
Eccentricity:
0003112
Arg of perigee: 46
5264 deg
Mean anomaly: 313
6147 deg
Mean motion: 15
54214855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3189
Checksum: 306
Coasting Arc #11 (Orbit 3204)
---------------------------------------
Vector Time (GMT): 2018/126/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1860068
82 A = 6784384
82 meter
Y = -5606703
87 meter E =
0015225
Z = 3320974
46 I = 51
37282
XDOT = 6044
494611 Wp = 80
95665
YDOT = 767
257296 meter/sec RA = 224
95215 deg
ZDOT = 4664
875545 TA = 317
89405
MA = 318
01094
Ha = 221
838 n
mi
Hp = 213
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6102588
00 X = -1813366
55
Y = -18394697
74 feet Y = -5627243
46 meter
Z = 10895585
49 Z = 3312052
00
XDOT = 19831
019066 XDOT = 6012
806011
YDOT = 2517
248347 feet/sec YDOT = 834
673609 meter/sec
ZDOT = 15304
709794 ZDOT = 4694
160901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19145824
41 X = -5835647
28
Y = 3145623
77 feet Y = 958786
12 meter
Z = 10856460
16 Z = 3309049
06
XDOT = 5878
398467 XDOT = 1791
735853
YDOT = -17674
272104 feet/sec YDOT = -5387
118137 meter/sec
ZDOT = 15435
289711 ZDOT = 4704
676304
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 18126
66089995
00016717 00000-0 10270-3 0 9108
2 25544 51
6396 225
7263 0003195 49
1245 311
0185 15
54231169 32058
Satellite: ISS
Catalog Number: 25544
Epoch time: 18126
66089995 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 225
7263 deg
Eccentricity:
0003195
Arg of perigee: 49
1245 deg
Mean anomaly: 311
0185 deg
Mean motion: 15
54231169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3205
Checksum: 310
Coasting Arc #12 (Orbit 3219)
---------------------------------------
Vector Time (GMT): 2018/127/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 457357
90 A = 6780532
17 meter
Y = 5066895
41 meter E =
0012715
Z = -4495435
22 I = 51
38321
XDOT = -6603
981701 Wp = 65
66768
YDOT = -2220
838650 meter/sec RA = 219
94703 deg
ZDOT = -3177
010195 TA = 172
26946
MA = 172
24984
Ha = 221
922 n
mi
Hp = 213
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1500518
04 X = 422501
10
Y = 16623672
61 feet Y = 5071815
16 meter
Z = -14748803
23 Z = -4493298
01
XDOT = -21666
606631 XDOT = -6563
224515
YDOT = -7286
216042 feet/sec YDOT = -2294
460921 meter/sec
ZDOT = -10423
261793 ZDOT = -3208
991343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16679922
70 X = 5084040
44
Y = 800877
39 feet Y = 244107
43 meter
Z = -14739878
44 Z = -4492714
95
XDOT = -10248
793226 XDOT = -3123
832175
YDOT = 19113
526837 feet/sec YDOT = 5825
802980 meter/sec
ZDOT = -10565
712663 ZDOT = -3220
429220
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 18127
62537203
00016717 00000-0 10270-3 0 9116
2 25544 51
6390 220
9182 0003308 53
1576 306
9880 15
54217735 32202
Satellite: ISS
Catalog Number: 25544
Epoch time: 18127
62537203 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 220
9182 deg
Eccentricity:
0003308
Arg of perigee: 53
1576 deg
Mean anomaly: 306
9880 deg
Mean motion: 15
54217735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3220
Checksum: 292
Coasting Arc #13 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2018/128/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3227107
69 A = 6785917
33 meter
Y = -5288573
36 meter E =
0016713
Z = 2747944
59 I = 51
41248
XDOT = 5658
305236 Wp = 73
35039
YDOT = -778
933377 meter/sec RA = 217
88111 deg
ZDOT = 5124
669014 TA = 317
89524
MA = 318
02353
Ha = 222
008 n
mi
Hp = 213
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10587623
66 X = -3181077
72
Y = -17350962
45 feet Y = -5324403
81 meter
Z = 9015566
25 Z = 2732379
96
XDOT = 18563
993558 XDOT = 5641
701849
YDOT = -2555
555699 feet/sec YDOT = -715
751304 meter/sec
ZDOT = 16813
218549 ZDOT = 5152
114922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20180206
98 X = 6150927
09
Y = 2673798
34 feet Y = 814973
73 meter
Z = 8946739
99 Z = 2726966
35
XDOT = -9455
578949 XDOT = -2882
060464
YDOT = 14462
128523 feet/sec YDOT = 4408
056774 meter/sec
ZDOT = 16935
798328 ZDOT = 5162
031330
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 18128
07545861
00016717 00000-0 10270-3 0 9126
2 25544 51
6398 218
6756 0003566 50
6113 309
5355 15
54218056 32276
Satellite: ISS
Catalog Number: 25544
Epoch time: 18128
07545861 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 218
6756 deg
Eccentricity:
0003566
Arg of perigee: 50
6113 deg
Mean anomaly: 309
5355 deg
Mean motion: 15
54218056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 316
Coasting Arc #14 (Orbit 3241)
---------------------------------------
Vector Time (GMT): 2018/129/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1864881
29 A = 6781955
58 meter
Y = 5088557
29 meter E =
0010543
Z = -4088685
75 I = 51
42715
XDOT = -6607
017657 Wp = 65
59721
YDOT = -644
530183 meter/sec RA = 212
88298 deg
ZDOT = -3819
181039 TA = 164
78725
MA = 164
75553
Ha = 221
902 n
mi
Hp = 213
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6118376
93 X = 1827701
86
Y = 16694741
76 feet Y = 5109203
87 meter
Z = -13414323
31 Z = -4079716
95
XDOT = -21676
567115 XDOT = -6580
767606
YDOT = -2114
600338 feet/sec YDOT = -718
267560 meter/sec
ZDOT = -12530
121520 ZDOT = -3851
212109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16967003
87 X = -5171542
78
Y = -5415342
08 feet Y = -1650596
27 meter
Z = -13374896
58 Z = -4076668
48
XDOT = 14593
015774 XDOT = 4447
951208
YDOT = -14450
527050 feet/sec YDOT = -4404
520645 meter/sec
ZDOT = -12673
009732 ZDOT = -3862
733366
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 18129
03992396
00016717 00000-0 10270-3 0 9133
2 25544 51
6408 213
8675 0003399 51
8988 308
2471 15
54245395 32420
Satellite: ISS
Catalog Number: 25544
Epoch time: 18129
03992396 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 213
8675 deg
Eccentricity:
0003399
Arg of perigee: 51
8988 deg
Mean anomaly: 308
2471 deg
Mean motion: 15
54245395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3242
Checksum: 337
Coasting Arc #15 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2018/130/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -270835
23 A = 6778564
23 meter
Y = -4610747
96 meter E =
0008373
Z = 4954879
24 I = 51
44453
XDOT = 7136
035040 Wp = 100
57600
YDOT = 1863
386203 meter/sec RA = 207
87516 deg
ZDOT = 2119
468110 TA = 328
71665
MA = 328
76645
Ha = 221
967 n
mi
Hp = 213
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -888567
03 X = -243324
85
Y = -15127125
85 feet Y = -4613622
85 meter
Z = 16256165
49 Z = 4953630
39
XDOT = 23412
188451 XDOT = 7104
372438
YDOT = 6113
471796 feet/sec YDOT = 1943
009209 meter/sec
ZDOT = 6953
635533 ZDOT = 2154
055892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12663246
03 X = 3859757
39
Y = 8332186
03 feet Y = 2539650
30 meter
Z = 16251131
66 Z = 4953344
93
XDOT = -18366
286826 XDOT = -5598
044225
YDOT = 14020
780951 feet/sec YDOT = 4273
534034 meter/sec
ZDOT = 7107
809468 ZDOT = 2166
460326
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 18130
06868421
00016717 00000-0 10270-3 0 9140
2 25544 51
6412 208
7378 0003502 56
7822 303
3666 15
54243590 32589
Satellite: ISS
Catalog Number: 25544
Epoch time: 18130
06868421 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 208
7378 deg
Eccentricity:
0003502
Arg of perigee: 56
7822 deg
Mean anomaly: 303
3666 deg
Mean motion: 15
54243590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 303
Coasting Arc #16 (Orbit 3272)
---------------------------------------
Vector Time (GMT): 2018/131/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1458863
48 A = 6776985
55 meter
Y = 3972717
69 meter E =
0017976
Z = -5308610
33 I = 51
46856
XDOT = -7105
127702 Wp = 83
11326
YDOT = -2844
856875 meter/sec RA = 202
86301 deg
ZDOT = -174
793655 TA = 185
20482
MA = 185
22353
Ha = 221
959 n
mi
Hp = 213
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4786297
51 X = -1477392
36
Y = 13033850
70 feet Y = 3956300
09 meter
Z = -17416700
55 Z = -5315742
05
XDOT = -23310
786424 XDOT = -7071
938602
YDOT = -9333
519930 feet/sec YDOT = -2924
125734 meter/sec
ZDOT = -573
469997 ZDOT = -209
227676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7772740
07 X = -2369131
17
Y = -11456363
98 feet Y = -3491899
74 meter
Z = -17449000
03 Z = -5318455
21
XDOT = 20444
186243 XDOT = 6231
387967
YDOT = -12755
613622 feet/sec YDOT = -3887
911032 meter/sec
ZDOT = -726
861256 ZDOT = -221
547311
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 18131
03314395
00016717 00000-0 10270-3 0 9155
2 25544 51
6407 203
9297 0003509 58
3380 301
8114 15
54262753 32734
Satellite: ISS
Catalog Number: 25544
Epoch time: 18131
03314395 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 203
9297 deg
Eccentricity:
0003509
Arg of perigee: 58
3380 deg
Mean anomaly: 301
8114 deg
Mean motion: 15
54262753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3273
Checksum: 293
Coasting Arc #17 (Orbit 3288)
---------------------------------------
Vector Time (GMT): 2018/132/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3163021
97 A = 6777885
27 meter
Y = -3208265
64 meter E =
0008632
Z = 5058728
34 I = 51
50306
XDOT = 6533
019663 Wp = 57
71120
YDOT = 3602
554027 meter/sec RA = 197
85217 deg
ZDOT = -1793
323132 TA = 49
70174
MA = 49
62633
Ha = 221
769 n
mi
Hp = 213
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10377368
68 X = 3174089
60
Y = -10525805
90 feet Y = -3172832
69 meter
Z = 16596877
74 Z = 5074120
29
XDOT = 21433
791544 XDOT = 6500
960515
YDOT = 11819
402975 feet/sec YDOT = 3675
431507 meter/sec
ZDOT = -5883
606076 ZDOT = -1761
665379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2696593
93 X = 821921
83
Y = 14453808
62 feet Y = 4405520
87 meter
Z = 16665968
88 Z = 5079787
31
XDOT = -20969
927050 XDOT = -6391
633765
YDOT = 10559
350407 feet/sec YDOT = 3218
490004 meter/sec
ZDOT = -5742
680066 ZDOT = -1750
368884
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 18132
06189787
00016717 00000-0 10270-3 0 9165
2 25544 51
6410 198
8009 0003345 60
6429 299
5057 15
54292321 32899
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
06189787 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 198
8009 deg
Eccentricity:
0003345
Arg of perigee: 60
6429 deg
Mean anomaly: 299
5057 deg
Mean motion: 15
54292321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 328
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