[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 14th 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
012/22:30:00
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
013/10:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
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
023/19:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 213
7
Coasting Arc #1 (Orbit 1429)
---------------------------------------
Vector Time (GMT): 2018/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 150210
83 A = 6786377
55 meter
Y = -6342406
73 meter E =
0004423
Z = -2412890
67 I = 52
01672
XDOT = 4995
469686 Wp = 93
95506
YDOT = 2166
106487 meter/sec RA = 74
08110 deg
ZDOT = -5391
522655 TA = 112
85397
MA = 112
80726
Ha = 221
241 n
mi
Hp = 214
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 492817
69 X = 232842
66
Y = -20808421
03 feet Y = -6340264
79 meter
Z = -7916307
96 Z = -2411960
72
XDOT = 16389
336241 XDOT = 4997
065470
YDOT = 7106
648581 feet/sec YDOT = 2221
978530 meter/sec
ZDOT = -17688
722620 ZDOT = -5367
252494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19614666
86 X = 5978550
46
Y = -6969932
97 feet Y = -2124435
57 meter
Z = -7911135
50 Z = -2411314
10
XDOT = -1206
889484 XDOT = -367
859915
YDOT = 16525
922852 feet/sec YDOT = 5037
101285 meter/sec
ZDOT = -17580
978660 ZDOT = -5358
682296
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
52736990
00016717 00000-0 10270-3 0 9000
2 25544 51
6406 74
7176 0003490 5
9836 354
1358 15
54294786 14301
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
52736990 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 74
7176 deg
Eccentricity:
0003490
Arg of perigee: 5
9836 deg
Mean anomaly: 354
1358 deg
Mean motion: 15
54294786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1430
Checksum: 315
Coasting Arc #2 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2018/012/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4261486
12 A = 6783213
11 meter
Y = -3777235
83 meter E =
0013162
Z = 3679296
00 I = 52
00289
XDOT = 1603
894923 Wp = 69
23819
YDOT = -6090
080013 meter/sec RA = 71
86703 deg
ZDOT = -4377
362977 TA = 67
23805
MA = 67
09902
Ha = 221
410 n
mi
Hp = 214
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13981253
66 X = -4236803
30
Y = -12392505
99 feet Y = -3824752
93 meter
Z = 12071181
10 Z = 3658654
98
XDOT = 5262
122452 XDOT = 1693
139428
YDOT = -19980
577469 feet/sec YDOT = -6071
644855 meter/sec
ZDOT = -14361
427091 ZDOT = -4369
355530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12636532
36 X = -3851615
06
Y = 13840663
02 feet Y = 4218634
09 meter
Z = 11979865
14 Z = 3651462
90
XDOT = -18875
346668 XDOT = -5753
205664
YDOT = -4785
260651 feet/sec YDOT = -1458
547446 meter/sec
ZDOT = -14324
767177 ZDOT = -4366
189036
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
97743781
00016717 00000-0 10270-3 0 9016
2 25544 51
6416 72
4759 0003764 7
5592 352
5617 15
54287449 14370
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
97743781 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 72
4759 deg
Eccentricity:
0003764
Arg of perigee: 7
5592 deg
Mean anomaly: 352
5617 deg
Mean motion: 15
54287449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 330
Coasting Arc #3 (Orbit 1443)
---------------------------------------
Vector Time (GMT): 2018/013/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4576629
58 A = 6779657
09 meter
Y = 1824131
60 meter E =
0010227
Z = -4666218
66 I = 51
98652
XDOT = 183
416201 Wp = 90
97557
YDOT = 7068
296389 meter/sec RA = 69
49032 deg
ZDOT = 2948
449101 TA = 208
23893
MA = 208
29441
Ha = 221
243 n
mi
Hp = 214
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15015188
90 X = 4578557
37
Y = 5984683
73 feet Y = 1875321
73 meter
Z = -15309116
34 Z = -4643982
32
XDOT = 601
759189 XDOT = 90
041066
YDOT = 23189
948782 feet/sec YDOT = 7069
825162 meter/sec
ZDOT = 9673
389438 ZDOT = 2949
113803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8037278
36 X = -2449762
44
Y = 14131100
18 feet Y = 4307159
33 meter
Z = -15210376
21 Z = -4636122
67
XDOT = -22007
889137 XDOT = -6708
004609
YDOT = -2122
360769 feet/sec YDOT = -646
895562 meter/sec
ZDOT = 9675
187762 ZDOT = 2948
997230
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
42750174
00016717 00000-0 10270-3 0 9022
2 25544 51
6417 70
2289 0003346 7
9914 352
1291 15
54324452 14441
Satellite: ISS
Catalog Number: 25544
Epoch time: 18013
42750174 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 70
2289 deg
Eccentricity:
0003346
Arg of perigee: 7
9914 deg
Mean anomaly: 352
1291 deg
Mean motion: 15
54324452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1444
Checksum: 287
Coasting Arc #4 (Orbit 1459)
---------------------------------------
Vector Time (GMT): 2018/014/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4680580
72 A = 6783566
35 meter
Y = -3400384
36 meter E =
0013441
Z = 3534761
25 I = 51
98763
XDOT = 1007
368260 Wp = 73
25248
YDOT = -6109
794240 meter/sec RA = 64
52443 deg
ZDOT = -4525
654892 TA = 65
31478
MA = 65
17488
Ha = 221
369 n
mi
Hp = 214
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15356235
95 X = -4659378
67
Y = -11156116
67 feet Y = -3452607
55 meter
Z = 11596985
74 Z = 3512076
07
XDOT = 3305
013977 XDOT = 1097
597780
YDOT = -20045
256693 feet/sec YDOT = -6098
024298 meter/sec
ZDOT = -14847
949121 ZDOT = -4520
542827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12964525
90 X = 3951587
49
Y = -13946839
84 feet Y = -4250996
78 meter
Z = 11496509
32 Z = 3504136
04
XDOT = 18460
440827 XDOT = 5626
742364
YDOT = 4891
540848 feet/sec YDOT = 1490
941650 meter/sec
ZDOT = -14824
163406 ZDOT = -4518
405006
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
45622048
00016717 00000-0 10270-3 0 9035
2 25544 51
6423 65
0994 0003536 11
1063 349
0167 15
54319794 14604
Satellite: ISS
Catalog Number: 25544
Epoch time: 18014
45622048 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 65
0994 deg
Eccentricity:
0003536
Arg of perigee: 11
1063 deg
Mean anomaly: 349
0167 deg
Mean motion: 15
54319794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1460
Checksum: 293
Coasting Arc #5 (Orbit 1474)
---------------------------------------
Vector Time (GMT): 2018/015/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4551764
42 A = 6787166
97 meter
Y = 4595343
33 meter E =
0010060
Z = -2043064
11 I = 51
98330
XDOT = -2282
018061 Wp = 30
54988
YDOT = 4733
938057 meter/sec RA = 59
56906 deg
ZDOT = 5584
082965 TA = 306
97286
MA = 307
06492
Ha = 221
484 n
mi
Hp = 214
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14933610
31 X = 4509963
76
Y = 15076585
73 feet Y = 4646010
71 meter
Z = -6702966
24 Z = -2021054
68
XDOT = -7486
935896 XDOT = -2361
908799
YDOT = 15531
292838 feet/sec YDOT = 4707
971839 meter/sec
ZDOT = 18320
482168 ZDOT = 5572
804187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16573613
00 X = -5051637
24
Y = 13301351
19 feet Y = 4054251
84 meter
Z = -6605703
53 Z = -2013418
43
XDOT = -13672
504085 XDOT = -4167
379245
YDOT = -7996
925356 feet/sec YDOT = -2437
462849 meter/sec
ZDOT = 18269
449571 ZDOT = 5568
528229
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
42064153
00016717 00000-0 10270-3 0 9041
2 25544 51
6413 60
2913 0003622 13
1051 347
0195 15
54279458 14753
Satellite: ISS
Catalog Number: 25544
Epoch time: 18015
42064153 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 60
2913 deg
Eccentricity:
0003622
Arg of perigee: 13
1051 deg
Mean anomaly: 347
0195 deg
Mean motion: 15
54279458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1475
Checksum: 278
Coasting Arc #6 (Orbit 1490)
---------------------------------------
Vector Time (GMT): 2018/016/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4104763
02 A = 6788751
88 meter
Y = -5394941
86 meter E =
0011689
Z = 285279
88 I = 51
97087
XDOT = 3603
808383 Wp = 115
31861
YDOT = -3070
754127 meter/sec RA = 54
62030 deg
ZDOT = -6030
198674 TA = 61
62159
MA = 61
50380
Ha = 221
456 n
mi
Hp = 213
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13467070
27 X = -4045515
97
Y = -17699940
49 feet Y = -5440512
88 meter
Z = 935957
60 Z = 265484
20
XDOT = 11823
518316 XDOT = 3667
169588
YDOT = -10074
652649 feet/sec YDOT = -3030
099173 meter/sec
ZDOT = -19784
116383 ZDOT = -6012
539233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18822758
13 X = 5737176
68
Y = -11853665
43 feet Y = -3612997
22 meter
Z = 848695
24 Z = 258682
31
XDOT = 8114
511533 XDOT = 2473
303115
YDOT = 11425
874632 feet/sec YDOT = 3482
606588 meter/sec
ZDOT = -19704
937386 ZDOT = -6006
064915
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
44935509
00016717 00000-0 10270-3 0 9057
2 25544 51
6407 55
1621 0003577 19
6636 340
4654 15
54316773 14911
Satellite: ISS
Catalog Number: 25544
Epoch time: 18016
44935509 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 55
1621 deg
Eccentricity:
0003577
Arg of perigee: 19
6636 deg
Mean anomaly: 340
4654 deg
Mean motion: 15
54316773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1491
Checksum: 312
Coasting Arc #7 (Orbit 1506)
---------------------------------------
Vector Time (GMT): 2018/017/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906172
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3343611
84 A = 6787915
96 meter
Y = 5711611
72 meter E =
0016989
Z = 1466037
03 I = 51
94825
XDOT = -4834
741668 Wp = 53
39911
YDOT = 1330
017294 meter/sec RA = 49
67027 deg
ZDOT = 5808
368608 TA = 322
54167
MA = 322
65995
Ha = 221
605 n
mi
Hp = 213
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10969855
11 X = 3272373
45
Y = 18738883
58 feet Y = 5748603
87 meter
Z = 4809832
78 Z = 1482106
15
XDOT = -15862
013345 XDOT = -4877
468413
YDOT = 4363
573798 feet/sec YDOT = 1275
712658 meter/sec
ZDOT = 19056
327455 ZDOT = 5784
779856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19471971
06 X = -5935056
78
Y = 9572964
30 feet Y = 2917839
52 meter
Z = 4880437
28 Z = 1487557
28
XDOT = -2515
249553 XDOT = -766
648064
YDOT = -14838
029009 feet/sec YDOT = -4522
631242 meter/sec
ZDOT = 18951
030794 ZDOT = 5776
274186
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
47806474
00016717 00000-0 10270-3 0 9060
2 25544 51
6409 50
0321 0003766 23
2960 336
8363 15
54293885 15077
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
47806474 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 50
0321 deg
Eccentricity:
0003766
Arg of perigee: 23
2960 deg
Mean anomaly: 336
8363 deg
Mean motion: 15
54293885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1507
Checksum: 311
Coasting Arc #8 (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 = 1197512
49 A = 6778766
50 meter
Y = -4464824
40 meter E =
0014609
Z = -4971561
44 I = 51
90872
XDOT = 6085
150947 Wp = 61
81547
YDOT = 4090
756660 meter/sec RA = 47
55326 deg
ZDOT = -2206
267430 TA = 186
69923
MA = 186
71878
Ha = 221
603 n
mi
Hp = 214
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3928846
74 X = 1271499
10
Y = -14648374
02 feet Y = -4451019
05 meter
Z = -16310897
11 Z = -4965564
99
XDOT = 19964
405995 XDOT = 6049
671419
YDOT = 13421
117651 feet/sec YDOT = 4158
606724 meter/sec
ZDOT = -7238
410203 ZDOT = -2176
794411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10697724
12 X = -3260666
31
Y = -10791884
75 feet Y = -3289366
47 meter
Z = -16283426
69 Z = -4963188
45
XDOT = 20813
011667 XDOT = 6343
805956
YDOT = -9897
861067 feet/sec YDOT = -3016
868053 meter/sec
ZDOT = -7107
827336 ZDOT = -2166
465772
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
86383025
00016717 00000-0 10270-3 0 9076
2 25544 51
6421 48
1102 0003553 15
7555 344
3708 15
54179290 15133
Satellite: ISS
Catalog Number: 25544
Epoch time: 18017
86383025 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 48
1102 deg
Eccentricity:
0003553
Arg of perigee: 15
7555 deg
Mean anomaly: 344
3708 deg
Mean motion: 15
54179290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1513
Checksum: 293
Coasting Arc #9 (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 = -5112292
22 A = 6780980
32 meter
Y = 19903
57 meter E =
0011912
Z = 4450075
74 I = 51
89227
XDOT = -2926
249237 Wp = 56
26703
YDOT = -6264
628496 meter/sec RA = 42
83325 deg
ZDOT = -3320
863997 TA = 67
17778
MA = 67
05200
Ha = 221
828 n
mi
Hp = 214
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16772612
25 X = -5133750
50
Y = 65300
42 feet Y = -37385
73 meter
Z = 14599986
01 Z = 4425190
39
XDOT = -9600
555240 XDOT = -2839
848318
YDOT = -20553
243098 feet/sec YDOT = -6296
868597 meter/sec
ZDOT = -10895
223088 ZDOT = -3334
868796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12830028
32 X = -3910592
63
Y = 10951693
70 feet Y = 3338076
24 meter
Z = 14489139
24 Z = 4416289
64
XDOT = -19755
774050 XDOT = -6021
559930
YDOT = -8592
486214 feet/sec YDOT = -2618
989798 meter/sec
ZDOT = -10956
531675 ZDOT = -3339
550855
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
82834273
00016717 00000-0 10270-3 0 9080
2 25544 51
6402 43
3018 0003565 19
7210 340
4080 15
54153182 15288
Satellite: ISS
Catalog Number: 25544
Epoch time: 18018
82834273 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 43
3018 deg
Eccentricity:
0003565
Arg of perigee: 19
7210 deg
Mean anomaly: 340
4080 deg
Mean motion: 15
54153182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1528
Checksum: 282
Coasting Arc #10 (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 = 5801854
09 A = 6784710
41 meter
Y = 1237903
44 meter E =
0007044
Z = -3292919
17 I = 51
88078
XDOT = 1442
515989 Wp = 56
31766
YDOT = 5840
821084 meter/sec RA = 37
86329 deg
ZDOT = 4748
420212 TA = 265
59356
MA = 265
67404
Ha = 221
772 n
mi
Hp = 214
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19034954
35 X = 5803575
25
Y = 4061362
99 feet Y = 1302793
44 meter
Z = -10803540
57 Z = -3264732
15
XDOT = 4732
664005 XDOT = 1354
030299
YDOT = 19162
798833 feet/sec YDOT = 5856
457434 meter/sec
ZDOT = 15578
806469 ZDOT = 4755
212518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17042753
38 X = 5194631
23
Y = -9542593
44 feet Y = -2908582
48 meter
Z = -10678207
38 Z = -3254717
61
XDOT = 15419
610514 XDOT = 4699
897285
YDOT = 10114
616944 feet/sec YDOT = 3082
935244 meter/sec
ZDOT = 15608
058397 ZDOT = 4757
336200
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
79285206
00016717 00000-0 10270-3 0 9094
2 25544 51
6408 38
4931 0003516 21
8909 338
2394 15
54171316 15437
Satellite: ISS
Catalog Number: 25544
Epoch time: 18019
79285206 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 38
4931 deg
Eccentricity:
0003516
Arg of perigee: 21
8909 deg
Mean anomaly: 338
2394 deg
Mean motion: 15
54171316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1543
Checksum: 315
Coasting Arc #11 (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 = -6126347
73 A = 6788008
04 meter
Y = -2326307
50 meter E =
0014405
Z = 1751098
31 I = 51
86582
XDOT = 308
026140 Wp = 101
02569
YDOT = -5126
021579 meter/sec RA = 32
90235 deg
ZDOT = -5695
228410 TA = 59
81433
MA = 59
67172
Ha = 221
808 n
mi
Hp = 214
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20099566
03 X = -6108384
76
Y = -7632242
44 feet Y = -2394716
09 meter
Z = 5745073
18 Z = 1721382
83
XDOT = 1010
584449 XDOT = 392
987680
YDOT = -16817
656098 feet/sec YDOT = -5122
101941 meter/sec
ZDOT = -18685
132580 ZDOT = -5693
525829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20039962
35 X = -6108180
53
Y = 7883036
92 feet Y = 2402749
65 meter
Z = 5613125
96 Z = 1710880
79
XDOT = -9889
887235 XDOT = -3014
437629
YDOT = -11754
582109 feet/sec YDOT = -3582
796627 meter/sec
ZDOT = -18676
669321 ZDOT = -5692
648809
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
82165902
00016717 00000-0 10270-3 0 9102
2 25544 51
6415 33
3641 0003509 26
1028 334
0301 15
54156931 15594
Satellite: ISS
Catalog Number: 25544
Epoch time: 18020
82165902 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 33
3641 deg
Eccentricity:
0003509
Arg of perigee: 26
1028 deg
Mean anomaly: 334
0301 deg
Mean motion: 15
54156931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1559
Checksum: 270
Coasting Arc #12 (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 = 6013781
39 A = 6789212
89 meter
Y = 3133086
02 meter E =
0015600
Z = -64276
45 I = 51
84229
XDOT = -2146
281812 Wp = 40
96532
YDOT = 4226
211916 meter/sec RA = 27
94554 deg
ZDOT = 6031
635936 TA = 318
34400
MA = 318
46271
Ha = 221
869 n
mi
Hp = 213
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19730253
91 X = 5978611
64
Y = 10279153
62 feet Y = 3200139
60 meter
Z = -210880
74 Z = -35149
53
XDOT = -7041
606994 XDOT = -2222
678944
YDOT = 13865
524658 feet/sec YDOT = 4201
783598 meter/sec
ZDOT = 19788
831810 ZDOT = 6021
024642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21418427
62 X = 6528336
74
Y = -6019358
13 feet Y = -1834700
36 meter
Z = -81702
34 Z = -24902
87
XDOT = 3829
638755 XDOT = 1167
273892
YDOT = 13455
236384 feet/sec YDOT = 4101
156050 meter/sec
ZDOT = 19740
846985 ZDOT = 6017
010161
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
78616191
00016717 00000-0 10270-3 0 9110
2 25544 51
6419 28
5557 0003661 28
2229 331
9121 15
54168895 15740
Satellite: ISS
Catalog Number: 25544
Epoch time: 18021
78616191 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 28
5557 deg
Eccentricity:
0003661
Arg of perigee: 28
2229 deg
Mean anomaly: 331
9121 deg
Mean motion: 15
54168895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 314
Coasting Arc #13 (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 = -5420589
80 A = 6788021
99 meter
Y = -3727514
41 meter E =
0007236
Z = -1670994
75 I = 51
80909
XDOT = 3962
869624 Wp = 114
98373
YDOT = -3208
000475 meter/sec RA = 22
98834 deg
ZDOT = -5721
502806 TA = 83
27060
MA = 83
18826
Ha = 221
832 n
mi
Hp = 213
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17784087
26 X = -5370388
16
Y = -12229378
00 feet Y = -3787850
49 meter
Z = -5482266
23 Z = -1697203
75
XDOT = 13001
540761 XDOT = 4026
239478
YDOT = -10524
935941 feet/sec YDOT = -3163
330698 meter/sec
ZDOT = -18771
334665 ZDOT = -5702
098878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21249605
53 X = -6476879
77
Y = 3605491
45 feet Y = 1098953
79 meter
Z = -5598337
71 Z = -1706373
33
XDOT = 2333
485982 XDOT = 711
246527
YDOT = -15147
290620 feet/sec YDOT = -4616
894181 meter/sec
ZDOT = -18684
371624 ZDOT = -5694
996471
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
81496388
00016717 00000-0 10270-3 0 9120
2 25544 51
6422 23
4276 0003434 32
0011 328
1350 15
54151795 15907
Satellite: ISS
Catalog Number: 25544
Epoch time: 18022
81496388 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 23
4276 deg
Eccentricity:
0003434
Arg of perigee: 32
0011 deg
Mean anomaly: 328
1350 deg
Mean motion: 15
54151795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1590
Checksum: 281
Coasting Arc #14 (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 = 4380968
19 A = 6784805
32 meter
Y = 4068378
62 meter E =
0015300
Z = 3190411
41 I = 51
76851
XDOT = -5554
495569 Wp = 75
31155
YDOT = 2187
737940 meter/sec RA = 18
02131 deg
ZDOT = 4821
968707 TA = 321
51122
MA = 321
62024
Ha = 221
861 n
mi
Hp = 213
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14373255
22 X = 4319651
72
Y = 13347698
88 feet Y = 4117026
80 meter
Z = 10467229
03 Z = 3211543
43
XDOT = -18223
410659 XDOT = -5601
968952
YDOT = 7177
617914 feet/sec YDOT = 2125
358376 meter/sec
ZDOT = 15820
107308 ZDOT = 4794
871861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19550994
32 X = 5959143
07
Y = -739091
47 feet Y = -225275
08 meter
Z = 10560624
02 Z = 3218878
20
XDOT = -7878
332035 XDOT = -2401
315604
YDOT = 16635
439937 feet/sec YDOT = 5070
482093 meter/sec
ZDOT = 15699
069763 ZDOT = 4785
076464
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
84376214
00016717 00000-0 10270-3 0 9130
2 25544 51
6427 18
2983 0003668 34
4632 325
6758 15
54172516 16069
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
84376214 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 18
2983 deg
Eccentricity:
0003668
Arg of perigee: 34
4632 deg
Mean anomaly: 325
6758 deg
Mean motion: 15
54172516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 313
Coasting Arc #15 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2018/023/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1787947
10 A = 6779542
21 meter
Y = -4509030
78 meter E =
0014120
Z = -4750150
23 I = 51
74967
XDOT = 7153
466101 Wp = 61
55621
YDOT = 40
299387 meter/sec RA = 17
83444 deg
ZDOT = -2730
416363 TA = 181
43615
MA = 181
44021
Ha = 221
832 n
mi
Hp = 213
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5865968
18 X = -1714319
54
Y = -14793408
08 feet Y = -4528613
21 meter
Z = -15584482
37 Z = -4758656
49
XDOT = 23469
376971 XDOT = 7165
746585
YDOT = 132
215836 feet/sec YDOT = 120
362983 meter/sec
ZDOT = -8958
058935 ZDOT = -2695
637855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15624427
46 X = -4762325
49
Y = -2823845
66 feet Y = -860708
16 meter
Z = -15621579
90 Z = -4761457
55
XDOT = 12209
102981 XDOT = 3721
334589
YDOT = -18846
815244 feet/sec YDOT = -5744
509286 meter/sec
ZDOT = -8803
201558 ZDOT = -2683
215835
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
84376070
00016717 00000-0 10270-3 0 9141
2 25544 51
6424 18
2987 0003604 32
4013 327
7360 15
54197626 16062
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
84376070 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 18
2987 deg
Eccentricity:
0003604
Arg of perigee: 32
4013 deg
Mean anomaly: 327
7360 deg
Mean motion: 15
54197626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 297
Coasting Arc #16 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2018/024/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 22137
05 A = 6777384
90 meter
Y = 4265713
66 meter E =
0005222
Z = 5261986
63 I = 51
71061
XDOT = -7555
252100 Wp = 75
11171
YDOT = -1024
017867 meter/sec RA = 12
84250 deg
ZDOT = 862
518966 TA = 6
65769
MA = 6
65075
Ha = 221
947 n
mi
Hp = 213
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 72628
11 X = -51124
70
Y = 13995123
54 feet Y = 4265551
59 meter
Z = 17263735
66 Z = 5261916
22
XDOT = -24787
572505 XDOT = -7547
429363
YDOT = -3359
638671 feet/sec YDOT = -1108
462133 meter/sec
ZDOT = 2829
786635 ZDOT = 825
837484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12033721
14 X = 3667878
20
Y = 7148055
19 feet Y = 2178727
22 meter
Z = 17262681
99 Z = 5261665
47
XDOT = -14977
557757 XDOT = -4565
159604
YDOT = 18779
414474 feet/sec YDOT = 5723
965532 meter/sec
ZDOT = 2666
637656 ZDOT = 812
791157
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
87255526
00016717 00000-0 10270-3 0 9158
2 25544 51
6423 13
1693 0003645 37
7971 322
3437 15
54188878 16228
Satellite: ISS
Catalog Number: 25544
Epoch time: 18024
87255526 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 13
1693 deg
Eccentricity:
0003645
Arg of perigee: 37
7971 deg
Mean anomaly: 322
3437 deg
Mean motion: 15
54188878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 320
Coasting Arc #17 (Orbit 1636)
---------------------------------------
Vector Time (GMT): 2018/025/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1790612
43 A = 6777560
30 meter
Y = -3931246
42 meter E =
0016387
Z = -5236512
22 I = 51
67760
XDOT = 7339
077126 Wp = 87
38869
YDOT = 1886
520907 meter/sec RA = 7
84559 deg
ZDOT = 1096
993122 TA = 193
11250
MA = 193
15515
Ha = 221
924 n
mi
Hp = 213
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5874712
69 X = 1859875
63
Y = -12897790
09 feet Y = -3910835
22 meter
Z = -17180158
19 Z = -5227645
93
XDOT = 24078
337026 XDOT = 7312
107513
YDOT = 6189
373056 feet/sec YDOT = 1968
440687 meter/sec
ZDOT = 3599
058800 ZDOT = 1132
578066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8266985
20 X = -2519777
09
Y = -11571537
69 feet Y = -3527004
69 meter
Z = -17139998
40 Z = -5224271
51
XDOT = 16405
796469 XDOT = 5000
486764
YDOT = -17267
882927 feet/sec YDOT = -5263
250716 meter/sec
ZDOT = 3757
165076 ZDOT = 1145
183915
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 18025
83704700
00016717 00000-0 10270-3 0 9169
2 25544 51
6409 8
3608 0003635 40
2333 319
9088 15
54207612 16372
Satellite: ISS
Catalog Number: 25544
Epoch time: 18025
83704700 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 8
3608 deg
Eccentricity:
0003635
Arg of perigee: 40
2333 deg
Mean anomaly: 319
9088 deg
Mean motion: 15
54207612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1637
Checksum: 295
Coasting Arc #18 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2018/026/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 906084
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3511440
77 A = 6780007
30 meter
Y = 3489812
90 meter E =
0011776
Z = 4626894
86 I = 51
65407
XDOT = -6558
656436 Wp = 57
72149
YDOT = -2666
667320 meter/sec RA = 2
85063 deg
ZDOT = -2954
523414 TA = 61
74711
MA = 61
62830
Ha = 221
949 n
mi
Hp = 213
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11520474
98 X = -3572678
65
Y = 11449517
40 feet Y = 3450203
02 meter
Z = 15180101
25 Z = 4609689
02
XDOT = -21517
901692 XDOT = -6513
998197
YDOT = -8748
908531 feet/sec YDOT = -2739
760921 meter/sec
ZDOT = -9693
318286 ZDOT = -2986
274439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4499061
76 X = 1371314
02
Y = 15681499
47 feet Y = 4779721
04 meter
Z = 15102889
93 Z = 4603360
85
XDOT = -16800
743077 XDOT = -5120
866490
YDOT = 14328
521645 feet/sec YDOT = 4367
333398 meter/sec
ZDOT = -9834
211209 ZDOT = -2997
467576
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 18026
86583389
00016717 00000-0 10270-3 0 9172
2 25544 51
6416 3
2320 0003577 40
6918 319
4501 15
54239614 16533
Satellite: ISS
Catalog Number: 25544
Epoch time: 18026
86583389 = yrday
fracday
Element set: 917
Inclination: 51
6416 deg
RA of node: 3
2320 deg
Eccentricity:
0003577
Arg of perigee: 40
6918 deg
Mean anomaly: 319
4501 deg
Mean motion: 15
54239614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 309
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