[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 19th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 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
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
029/16:58:30
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
3
030/15:25:14
630 1
4 1
5 1
5
N/A -0
6 -0
1 222
1
000/00:00:29
261 0
0 -0
0 214
1
Coasting Arc #1 (Orbit 1538)
---------------------------------------
Vector Time (GMT): 2018/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5834064
51 A = 6787861
92 meter
Y = -2962241
48 meter E =
0014498
Z = 1787916
04 I = 51
89753
XDOT = 827
301792 Wp = 100
58855
YDOT = -5081
653085 meter/sec RA = 39
29235 deg
ZDOT = -5683
373073 TA = 59
84068
MA = 59
69711
Ha = 221
777 n
mi
Hp = 213
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19140631
58 X = -5809190
90
Y = -9718640
03 feet Y = -3027342
96 meter
Z = 5865866
28 Z = 1759637
11
XDOT = 2714
244723 XDOT = 911
670974
YDOT = -16672
090173 feet/sec YDOT = -5071
929747 meter/sec
ZDOT = -18646
237116 ZDOT = -5679
149628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -408947
93 X = -124647
33
Y = -21496615
96 feet Y = -6552168
54 meter
Z = 5740417
47 Z = 1749679
25
XDOT = 14489
866933 XDOT = 4416
511441
YDOT = -5282
280477 feet/sec YDOT = -1610
039090 meter/sec
ZDOT = -18626
555157 ZDOT = -5677
374012
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
53562654
00016717 00000-0 10270-3 0 9002
2 25544 51
6396 39
7742 0003526 27
0102 333
1234 15
54187636 15395
Satellite: ISS
Catalog Number: 25544
Epoch time: 18019
53562654 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 39
7742 deg
Eccentricity:
0003526
Arg of perigee: 27
0102 deg
Mean anomaly: 333
1234 deg
Mean motion: 15
54187636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1539
Checksum: 301
Coasting Arc #2 (Orbit 1553)
---------------------------------------
Vector Time (GMT): 2018/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5642674
94 A = 6789083
40 meter
Y = 3759920
70 meter E =
0015329
Z = -99707
42 I = 51
87693
XDOT = -2559
034217 Wp = 41
00314
YDOT = 3986
265017 meter/sec RA = 34
33816 deg
ZDOT = 6033
814550 TA = 317
92594
MA = 318
04355
Ha = 221
744 n
mi
Hp = 213
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18512713
05 X = 5600695
44
Y = 12335697
83 feet Y = 3822786
24 meter
Z = -327124
08 Z = -72399
73
XDOT = -8395
781551 XDOT = -2632
728020
YDOT = 13078
297300 feet/sec YDOT = 3957
236039 meter/sec
ZDOT = 19795
979496 ZDOT = 6021
204949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1833416
86 X = -558825
46
Y = 22171898
49 feet Y = 6757994
66 meter
Z = -206144
60 Z = -62832
88
XDOT = -13955
653218 XDOT = -4253
683101
YDOT = -996
393092 feet/sec YDOT = -303
700614 meter/sec
ZDOT = 19739
133791 ZDOT = 6016
487980
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
50012375
00016717 00000-0 10270-3 0 9012
2 25544 51
6406 34
9661 0003447 28
7192 331
4150 15
54212866 15542
Satellite: ISS
Catalog Number: 25544
Epoch time: 18020
50012375 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 34
9661 deg
Eccentricity:
0003447
Arg of perigee: 28
7192 deg
Mean anomaly: 331
4150 deg
Mean motion: 15
54212866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1554
Checksum: 278
Coasting Arc #3 (Orbit 1569)
---------------------------------------
Vector Time (GMT): 2018/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4994953
97 A = 6787979
97 meter
Y = -4292482
06 meter E =
0007430
Z = -1641458
17 I = 51
84427
XDOT = 4259
944912 Wp = 114
00653
YDOT = -2772
791282 meter/sec RA = 29
38208 deg
ZDOT = -5735
448363 TA = 83
90515
MA = 83
82049
Ha = 221
865 n
mi
Hp = 213
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16387644
26 X = -4938609
85
Y = -14082946
38 feet Y = -4348024
02 meter
Z = -5385361
45 Z = -1665584
63
XDOT = 13976
197217 XDOT = 4318
493691
YDOT = -9097
084259 feet/sec YDOT = -2724
826313 meter/sec
ZDOT = -18817
087806 ZDOT = -5714
613187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4045493
95 X = 1233066
56
Y = -21198053
98 feet Y = -6461166
85 meter
Z = -5492073
14 Z = -1673983
89
XDOT = 13374
839425 XDOT = 4076
651057
YDOT = 7384
017226 feet/sec YDOT = 2250
648450 meter/sec
ZDOT = -18723
819284 ZDOT = -5707
020118
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
52891847
00016717 00000-0 10270-3 0 9025
2 25544 51
6395 29
8366 0003636 33
3869 326
7513 15
54182156 15703
Satellite: ISS
Catalog Number: 25544
Epoch time: 18021
52891847 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 29
8366 deg
Eccentricity:
0003636
Arg of perigee: 33
3869 deg
Mean anomaly: 326
7513 deg
Mean motion: 15
54182156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1570
Checksum: 322
Coasting Arc #4 (Orbit 1585)
---------------------------------------
Vector Time (GMT): 2018/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3929429
46 A = 6784778
77 meter
Y = 4521705
16 meter E =
0015232
Z = 3168211
28 I = 51
80368
XDOT = -5737
781549 Wp = 75
22702
YDOT = 1581
018616 meter/sec RA = 24
41863 deg
ZDOT = 4844
315576 TA = 321
27710
MA = 321
38619
Ha = 221
770 n
mi
Hp = 213
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12891828
94 X = 3863185
22
Y = 14834990
67 feet Y = 4565276
37 meter
Z = 10394393
96 Z = 3187137
85
XDOT = -18824
742614 XDOT = -5778
565264
YDOT = 5187
068950 feet/sec YDOT = 1516
626829 meter/sec
ZDOT = 15893
423806 ZDOT = 4816
344768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6138931
89 X = -1871146
44
Y = 18623821
87 feet Y = 5676540
91 meter
Z = 10477900
62 Z = 3193664
11
XDOT = -12819
151470 XDOT = -3907
277368
YDOT = -13125
680640 feet/sec YDOT = -4000
707459 meter/sec
ZDOT = 15768
588836 ZDOT = 4806
265877
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
55771002
00016717 00000-0 10270-3 0 9030
2 25544 51
6385 24
7080 0003533 33
7761 326
3616 15
54205273 15863
Satellite: ISS
Catalog Number: 25544
Epoch time: 18022
55771002 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 24
7080 deg
Eccentricity:
0003533
Arg of perigee: 33
7761 deg
Mean anomaly: 326
3616 deg
Mean motion: 15
54205273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1586
Checksum: 287
Coasting Arc #5 (Orbit 1600)
---------------------------------------
Vector Time (GMT): 2018/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2482014
87 A = 6780949
45 meter
Y = -4545113
15 meter E =
0012317
Z = -4390417
85 I = 51
76064
XDOT = 6840
303117 Wp = 60
18510
YDOT = -438
645469 meter/sec RA = 19
44195 deg
ZDOT = -3414
109463 TA = 175
23447
MA = 175
22274
Ha = 221
949 n
mi
Hp = 213
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8143093
41 X = -2409679
64
Y = -14911788
55 feet Y = -4572464
34 meter
Z = -14404258
05 Z = -4402298
74
XDOT = 22441
939360 XDOT = 6861
283536
YDOT = -1439
125555 feet/sec YDOT = -362
035244 meter/sec
ZDOT = -11201
146531 ZDOT = -3380
831070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8406764
30 X = 2562381
76
Y = -14713718
19 feet Y = -4484741
30 meter
Z = -14456378
14 Z = -4406304
06
XDOT = 12048
882306 XDOT = 3672
499327
YDOT = 17739
869032 feet/sec YDOT = 5407
112081 meter/sec
ZDOT = -11052
882748 ZDOT = -3368
918662
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
52220164
00016717 00000-0 10270-3 0 9047
2 25544 51
6387 19
8991 0003678 38
6972 321
4444 15
54186088 16014
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
52220164 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 19
8991 deg
Eccentricity:
0003678
Arg of perigee: 38
6972 deg
Mean anomaly: 321
4444 deg
Mean motion: 15
54186088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1601
Checksum: 315
Coasting Arc #6 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2018/023/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1748773
78 A = 6779441
46 meter
Y = -4508710
40 meter E =
0014286
Z = -4765030
33 I = 51
74939
XDOT = 7165
748557 Wp = 61
87146
YDOT = 71
581951 meter/sec RA = 17
83302 deg
ZDOT = -2697
170791 TA = 181
47544
MA = 181
47966
Ha = 221
839 n
mi
Hp = 213
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5737446
79 X = -1675080
44
Y = -14792356
96 feet Y = -4527854
40 meter
Z = -15633301
60 Z = -4773346
14
XDOT = 23509
673745 XDOT = 7177
516831
YDOT = 234
848922 feet/sec YDOT = 151
780035 meter/sec
ZDOT = -8848
985536 ZDOT = -2662
333864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15556163
16 X = -4741518
53
Y = -2933120
16 feet Y = -894015
02 meter
Z = -15669551
15 Z = -4776079
19
XDOT = 12309
320739 XDOT = 3751
880961
YDOT = -18831
855750 feet/sec YDOT = -5739
949633 meter/sec
ZDOT = -8693
873442 ZDOT = -2649
892625
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
84369728
00016717 00000-0 10270-3 0 9053
2 25544 51
6423 18
2979 0003658 33
4763 326
6620 15
54212051 16061
Satellite: ISS
Catalog Number: 25544
Epoch time: 18023
84369728 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 18
2979 deg
Eccentricity:
0003658
Arg of perigee: 33
4763 deg
Mean anomaly: 326
6620 deg
Mean motion: 15
54212051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 308
Coasting Arc #7 (Orbit 1621)
---------------------------------------
Vector Time (GMT): 2018/024/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -24958
88 A = 6777321
61 meter
Y = 4259161
34 meter E =
0005281
Z = 5267158
59 I = 51
71045
XDOT = -7555
344720 Wp = 74
38701
YDOT = -1057
930148 meter/sec RA = 12
84081 deg
ZDOT = 820
373906 TA = 7
78800
MA = 7
77981
Ha = 221
955 n
mi
Hp = 213
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -81886
10 X = -98168
98
Y = 13973626
44 feet Y = 4258472
90 meter
Z = 17280704
04 Z = 5266859
53
XDOT = -24787
876377 XDOT = -7546
938044
YDOT = -3470
899435 feet/sec YDOT = -1142
372185 meter/sec
ZDOT = 2691
515439 ZDOT = 783
693391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11936633
29 X = 3638285
83
Y = 7270301
63 feet Y = 2215987
94 meter
Z = 17278633
43 Z = 5266527
47
XDOT = -15064
168735 XDOT = -4591
558631
YDOT = 18729
426005 feet/sec YDOT = 5708
729046 meter/sec
ZDOT = 2528
376661 ZDOT = 770
649206
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
87248268
00016717 00000-0 10270-3 0 9063
2 25544 51
6422 13
1685 0003698 38
7959 321
3458 15
54203011 16222
Satellite: ISS
Catalog Number: 25544
Epoch time: 18024
87248268 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 13
1685 deg
Eccentricity:
0003698
Arg of perigee: 38
7959 deg
Mean anomaly: 321
3458 deg
Mean motion: 15
54203011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1622
Checksum: 309
Coasting Arc #8 (Orbit 1636)
---------------------------------------
Vector Time (GMT): 2018/025/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1841741
47 A = 6777558
53 meter
Y = -3918001
74 meter E =
0016399
Z = -5228697
59 I = 51
67764
XDOT = 7322
954221 Wp = 87
66418
YDOT = 1921
208387 meter/sec RA = 7
84377 deg
ZDOT = 1143
557080 TA = 193
28877
MA = 193
33202
Ha = 221
932 n
mi
Hp = 213
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6042458
88 X = 1910814
80
Y = -12854336
42 feet Y = -3897019
84 meter
Z = -17154519
66 Z = -5219583
40
XDOT = 24025
440358 XDOT = 7295
371741
YDOT = 6303
177124 feet/sec YDOT = 2002
944443 meter/sec
ZDOT = 3751
827689 ZDOT = 1179
062217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8146523
66 X = -2483060
41
Y = -11695869
23 feet Y = -3564900
94 meter
Z = -17113258
43 Z = -5216121
17
XDOT = 16469
146999 XDOT = 5019
796005
YDOT = -17173
635606 feet/sec YDOT = -5234
524133 meter/sec
ZDOT = 3909
572596 ZDOT = 1191
637727
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
83696618
00016717 00000-0 10270-3 0 9077
2 25544 51
6408 8
3599 0003688 41
2522 318
8909 15
54220545 16379
Satellite: ISS
Catalog Number: 25544
Epoch time: 18025
83696618 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 8
3599 deg
Eccentricity:
0003688
Arg of perigee: 41
2522 deg
Mean anomaly: 318
8909 deg
Mean motion: 15
54220545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1637
Checksum: 330
Coasting Arc #9 (Orbit 1652)
---------------------------------------
Vector Time (GMT): 2018/026/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3561741
28 A = 6780060
86 meter
Y = 3469158
56 meter E =
0011951
Z = 4603883
53 I = 51
65430
XDOT = -6523
938794 Wp = 58
41348
YDOT = -2700
846543 meter/sec RA = 2
84885 deg
ZDOT = -3000
145767 TA = 61
55549
MA = 61
43513
Ha = 221
957 n
mi
Hp = 213
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11685502
90 X = -3622632
68
Y = 11381753
82 feet Y = 3428988
13 meter
Z = 15104604
77 Z = 4586434
19
XDOT = -21403
998667 XDOT = -6478
679326
YDOT = -8861
045089 feet/sec YDOT = -2773
548545 meter/sec
ZDOT = -9842
997922 ZDOT = -3031
726688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4360860
59 X = 1329190
31
Y = 15793580
87 feet Y = 4813883
45 meter
Z = 15026312
96 Z = 4580020
19
XDOT = -16836
118249 XDOT = -5131
648842
YDOT = 14184
067980 feet/sec YDOT = 4323
303920 meter/sec
ZDOT = -9983
127553 ZDOT = -3042
857278
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
86574457
00016717 00000-0 10270-3 0 9088
2 25544 51
6415 3
2311 0003628 41
7485 318
3944 15
54252492 16538
Satellite: ISS
Catalog Number: 25544
Epoch time: 18026
86574457 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 3
2311 deg
Eccentricity:
0003628
Arg of perigee: 41
7485 deg
Mean anomaly: 318
3944 deg
Mean motion: 15
54252492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1653
Checksum: 310
Coasting Arc #10 (Orbit 1667)
---------------------------------------
Vector Time (GMT): 2018/027/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4987174
12 A = 6783912
23 meter
Y = -2970891
54 meter E =
0007986
Z = -3514836
85 I = 51
63306
XDOT = 5187
729102 Wp = 73
39263
YDOT = 3381
554412 meter/sec RA = 357
85924 deg
ZDOT = 4513
326063 TA = 245
26210
MA = 245
34523
Ha = 222
007 n
mi
Hp = 213
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16362119
81 X = 5037097
80
Y = -9747019
48 feet Y = -2914842
24 meter
Z = -11531616
95 Z = -3490490
04
XDOT = 17020
108604 XDOT = 5127
606982
YDOT = 11094
338623 feet/sec YDOT = 3439
230781 meter/sec
ZDOT = 14807
500206 ZDOT = 4538
380097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1028087
18 X = -313360
97
Y = -19083143
10 feet Y = -5816542
02 meter
Z = -11422706
73 Z = -3481641
01
XDOT = 16278
767863 XDOT = 4961
768445
YDOT = -9785
545089 feet/sec YDOT = -2982
634143 meter/sec
ZDOT = 14918
448625 ZDOT = 4547
143141
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 18027
83022243
00016717 00000-0 10270-3 0 9098
2 25544 51
6405 358
4211 0003630 46
9443 313
2013 15
54223685 16684
Satellite: ISS
Catalog Number: 25544
Epoch time: 18027
83022243 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 358
4211 deg
Eccentricity:
0003630
Arg of perigee: 46
9443 deg
Mean anomaly: 313
2013 deg
Mean motion: 15
54223685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1668
Checksum: 286
Coasting Arc #11 (Orbit 1683)
---------------------------------------
Vector Time (GMT): 2018/028/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6033751
83 A = 6787319
09 meter
Y = 2356557
19 meter E =
0016021
Z = 2007528
79 I = 51
61153
XDOT = -3430
287299 Wp = 99
64884
YDOT = -4013
475043 meter/sec RA = 352
87978 deg
ZDOT = -5563
449791 TA = 58
16154
MA = 58
00567
Ha = 222
010 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19795773
71 X = -6069406
41
Y = 7731486
85 feet Y = 2288884
18 meter
Z = 6586380
53 Z = 1978132
92
XDOT = -11254
223423 XDOT = -3358
128728
YDOT = -13167
569038 feet/sec YDOT = -4051
431101 meter/sec
ZDOT = -18252
788027 ZDOT = -5579
937628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1969177
94 X = -600205
44
Y = 21201012
83 feet Y = 6462068
71 meter
Z = 6455102
45 Z = 1967515
23
XDOT = -15214
351760 XDOT = -4637
334416
YDOT = 4202
370523 feet/sec YDOT = 1280
882535 meter/sec
ZDOT = -18325
489403 ZDOT = -5585
609170
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 18028
85899427
00016717 00000-0 10270-3 0 9109
2 25544 51
6401 353
2922 0003753 49
5891 310
5588 15
54256497 16846
Satellite: ISS
Catalog Number: 25544
Epoch time: 18028
85899427 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 353
2922 deg
Eccentricity:
0003753
Arg of perigee: 49
5891 deg
Mean anomaly: 310
5588 deg
Mean motion: 15
54256497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1684
Checksum: 339
Coasting Arc #12 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2018/029/16:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 905837
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3143463
18 A = 6778520
13 meter
Y = 3377853
72 meter E =
0008321
Z = 4958855
36 I = 51
55545
XDOT = -6692
570253 Wp = 98
24124
YDOT = 3089
714028 meter/sec RA = 348
50301 deg
ZDOT = 2133
608234 TA = 330
94266
MA = 330
98894
Ha = 222
001 n
mi
Hp = 213
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10313199
40 X = 3081370
49
Y = 11082197
25 feet Y = 3412658
65 meter
Z = 16269210
48 Z = 4973974
25
XDOT = -21957
251486 XDOT = -6736
986592
YDOT = 10136
857048 feet/sec YDOT = 3014
624666 meter/sec
ZDOT = 7000
027015 ZDOT = 2100
991016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13686570
67 X = 4171666
74
Y = 6299170
97 feet Y = 1919987
31 meter
Z = 16335930
21 Z = 4979191
53
XDOT = -15943
546524 XDOT = -4859
592981
YDOT = 16830
059719 feet/sec YDOT = 5129
802202 meter/sec
ZDOT = 6854
283805 ZDOT = 2089
185704
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 18029
75916998
00016717 00000-0 10270-3 0 9113
2 25544 51
6422 348
8055 0003737 56
2343 303
9165 15
54221021 16982
Satellite: ISS
Catalog Number: 25544
Epoch time: 18029
75916998 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 348
8055 deg
Eccentricity:
0003737
Arg of perigee: 56
2343 deg
Mean anomaly: 303
9165 deg
Mean motion: 15
54221021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 319
Coasting Arc #13 (Orbit 1711)
---------------------------------------
Vector Time (GMT): 2018/030/15:25:29
261
Vector Time (MET): N/A
Weight (LBS) : 905690
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1572859
39 A = 6777826
34 meter
Y = -3934156
47 meter E =
0017031
Z = -5305028
97 I = 51
52110
XDOT = 7258
081080 Wp = 80
97583
YDOT = -2407
851598 meter/sec RA = 343
81905 deg
ZDOT = -364
660899 TA = 185
52640
MA = 185
54522
Ha = 222
067 n
mi
Hp = 214
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5160299
83 X = -1502981
33
Y = -12907337
48 feet Y = -3951354
35 meter
Z = -17404950
69 Z = -5312499
60
XDOT = 23812
601968 XDOT = 7286
238181
YDOT = -7899
775583 feet/sec YDOT = -2326
529311 meter/sec
ZDOT = -1196
394025 ZDOT = -329
336271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5116562
74 X = -1559528
32
Y = -12880749
87 feet Y = -3926052
56 meter
Z = -17437529
42 Z = -5314958
97
XDOT = 22836
757215 XDOT = 6960
643599
YDOT = -7658
019977 feet/sec YDOT = -2334
164489 meter/sec
ZDOT = -1038
721900 ZDOT = -316
602435
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 18030
65934053
00016717 00000-0 10270-3 0 9127
2 25544 51
6426 344
3167 0002779 47
0274 313
1112 15
53979371 17126
Satellite: ISS
Catalog Number: 25544
Epoch time: 18030
65934053 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 344
3167 deg
Eccentricity:
0002779
Arg of perigee: 47
0274 deg
Mean anomaly: 313
1112 deg
Mean motion: 15
53979371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1712
Checksum: 297
Coasting Arc #14 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2018/031/15:25:29
261
Vector Time (MET): N/A
Weight (LBS) : 905690
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -114168
04 A = 6778490
09 meter
Y = 4422981
21 meter E =
0007578
Z = 5131244
80 I = 51
49214
XDOT = -7357
614097 Wp = 52
11872
YDOT = 1565
795967 meter/sec RA = 338
81215 deg
ZDOT = -1507
289882 TA = 52
45659
MA = 52
38776
Ha = 222
032 n
mi
Hp = 214
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -374567
07 X = -188542
69
Y = 14511093
22 feet Y = 4421288
60 meter
Z = 16834792
65 Z = 5130509
63
XDOT = -24139
153860 XDOT = -7367
255016
YDOT = 5137
125876 feet/sec YDOT = 1483
464191 meter/sec
ZDOT = -4945
176777 ZDOT = -1543
052983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -155765
53 X = -47477
33
Y = 14519761
13 feet Y = 4425623
19 meter
Z = 16830764
83 Z = 5130017
12
XDOT = -22924
320684 XDOT = -6987
332945
YDOT = 5694
331657 feet/sec YDOT = 1735
632289 meter/sec
ZDOT = -5104
648323 ZDOT = -1555
896809
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 18031
68828093
00016717 00000-0 10270-3 0 9138
2 25544 51
6424 339
1889 0002755 48
6794 311
4596 15
54011241 17283
Satellite: ISS
Catalog Number: 25544
Epoch time: 18031
68828093 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 339
1889 deg
Eccentricity:
0002755
Arg of perigee: 48
6794 deg
Mean anomaly: 311
4596 deg
Mean motion: 15
54011241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 325
Coasting Arc #15 (Orbit 1742)
---------------------------------------
Vector Time (GMT): 2018/032/15:25:29
261
Vector Time (MET): N/A
Weight (LBS) : 905690
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1695033
54 A = 6781324
75 meter
Y = -4809555
50 meter E =
0011034
Z = -4480371
93 I = 51
47082
XDOT = 6928
043687 Wp = 97
90880
YDOT = -551
666225 meter/sec RA = 333
80833 deg
ZDOT = 3218
572246 TA = 204
55670
MA = 204
60929
Ha = 222
099 n
mi
Hp = 214
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5561133
66 X = 1770451
96
Y = -15779381
56 feet Y = -4790178
87 meter
Z = -14699382
97 Z = -4471955
01
XDOT = 22729
802124 XDOT = 6918
063997
YDOT = -1809
928559 feet/sec YDOT = -474
247823 meter/sec
ZDOT = 10559
620230 ZDOT = 3252
201069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5023631
56 X = 1531202
90
Y = -15993814
32 feet Y = -4874914
60 meter
Z = -14661104
30 Z = -4468704
59
XDOT = 21403
143366 XDOT = 6523
678098
YDOT = -3078
276865 feet/sec YDOT = -938
258788 meter/sec
ZDOT = 10709
409929 ZDOT = 3264
228146
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 18032
65291172
00016717 00000-0 10270-3 0 9149
2 25544 51
6422 334
3822 0002722 51
8033 308
3365 15
53974990 17435
Satellite: ISS
Catalog Number: 25544
Epoch time: 18032
65291172 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 334
3822 deg
Eccentricity:
0002722
Arg of perigee: 51
8033 deg
Mean anomaly: 308
3365 deg
Mean motion: 15
53974990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1743
Checksum: 298
Coasting Arc #16 (Orbit 1758)
---------------------------------------
Vector Time (GMT): 2018/033/15:25:29
261
Vector Time (MET): N/A
Weight (LBS) : 905690
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3102649
33 A = 6785006
09 meter
Y = 5005676
63 meter E =
0014946
Z = 3358021
58 I = 51
45459
XDOT = -6076
133350 Wp = 84
55619
YDOT = -641
662174 meter/sec RA = 328
81112 deg
ZDOT = -4638
344254 TA = 56
14810
MA = 56
00595
Ha = 222
168 n
mi
Hp = 214
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10179295
71 X = -3174704
63
Y = 16422823
58 feet Y = 4970577
95 meter
Z = 11017131
16 Z = 3342775
15
XDOT = -19934
820701 XDOT = -6045
976498
YDOT = -2105
190860 feet/sec YDOT = -709
441265 meter/sec
ZDOT = -15217
664875 ZDOT = -4667
785934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9297347
81 X = -2833831
61
Y = 16982211
94 feet Y = 5176178
20 meter
Z = 10948432
58 Z = 3337082
25
XDOT = -18683
592270 XDOT = -5694
758924
YDOT = -292
683086 feet/sec YDOT = -89
209805 meter/sec
ZDOT = -15348
608260 ZDOT = -4678
255798
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 18033
68184592
00016717 00000-0 10270-3 0 9151
2 25544 51
6426 329
2546 0002817 55
8007 304
3412 15
53991485 17599
Satellite: ISS
Catalog Number: 25544
Epoch time: 18033
68184592 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 329
2546 deg
Eccentricity:
0002817
Arg of perigee: 55
8007 deg
Mean anomaly: 304
3412 deg
Mean motion: 15
53991485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1759
Checksum: 324
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