[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 14th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
348/03:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
6
354/01:40:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 214
1
358/04:25:00
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
6
361/02:52:50
495 -1
8 2
2 2
2
N/A 1
0 -0
0 221
4
000/00:05:40
991 0
7 -0
0 216
2
361/09:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 216
2
Coasting Arc #1 (Orbit 2625)
---------------------------------------
Vector Time (GMT): 2018/346/14:51:13
974
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3956599
57 A = 6778987
94 meter
Y = -2362622
92 meter E =
0008313
Z = 4964352
13 I = 51
43409
XDOT = 5539
948359 Wp = 93
83935
YDOT = 4882
321895 meter/sec RA = 208
35198 deg
ZDOT = -2089
289943 TA = 16
55101
MA = 16
52389
Ha = 222
525 n
mi
Hp = 213
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12980969
71 X = 3958610
87
Y = -7751387
53 feet Y = -2318366
71 meter
Z = 16287244
53 Z = 4983576
53
XDOT = 18175
683594 XDOT = 5495
089772
YDOT = 16018
116452 feet/sec YDOT = 4944
022829 meter/sec
ZDOT = -6854
625797 ZDOT = -2062
487342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13531326
90 X = 4124348
44
Y = 6531358
21 feet Y = 1990757
98 meter
Z = 16374018
13 Z = 4990800
73
XDOT = -2956
940289 XDOT = -901
275400
YDOT = 23029
550156 feet/sec YDOT = 7019
406888 meter/sec
ZDOT = -6734
480890 ZDOT = -2052
669775
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 18346
66360442
00016717 00000-0 10270-3 0 9000
2 25544 51
6355 209
2941 0005017 139
5923 220
5603 15
54043037 26265
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
66360442 = yrday
fracday
Element set: 900
Inclination: 51
6355 deg
RA of node: 209
2941 deg
Eccentricity:
0005017
Arg of perigee: 139
5923 deg
Mean anomaly: 220
5603 deg
Mean motion: 15
54043037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2626
Checksum: 289
Coasting Arc #2 (Orbit 2640)
---------------------------------------
Vector Time (GMT): 2018/347/14:51:13
974
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5207125
09 A = 6782112
97 meter
Y = 1347022
69 meter E =
0012439
Z = -4145169
65 I = 51
47424
XDOT = -4302
585707 Wp = 123
31917
YDOT = -5106
365688 meter/sec RA = 203
34637 deg
ZDOT = 3746
963558 TA = 185
39455
MA = 185
40797
Ha = 222
604 n
mi
Hp = 213
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17083743
75 X = -5201665
88
Y = 4419365
78 feet Y = 1288823
86 meter
Z = -13599637
94 Z = -4170450
62
XDOT = -14116
094840 XDOT = -4263
365845
YDOT = -16753
168268 feet/sec YDOT = -5154
261209 meter/sec
ZDOT = 12293
187525 ZDOT = 3726
157978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13199158
59 X = -4023103
54
Y = -11578217
12 feet Y = -3529040
58 meter
Z = -13713582
58 Z = -4179899
97
XDOT = 5042
670135 XDOT = 1537
005857
YDOT = -20193
066740 feet/sec YDOT = -6154
846742 meter/sec
ZDOT = 12200
038775 ZDOT = 3718
571819
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 18347
62817295
00016717 00000-0 10270-3 0 9011
2 25544 51
6351 204
4853 0005177 143
0885 217
0625 15
54069006 26410
Satellite: ISS
Catalog Number: 25544
Epoch time: 18347
62817295 = yrday
fracday
Element set: 901
Inclination: 51
6351 deg
RA of node: 204
4853 deg
Eccentricity:
0005177
Arg of perigee: 143
0885 deg
Mean anomaly: 217
0625 deg
Mean motion: 15
54069006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 305
Coasting Arc #3 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2018/348/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438073
59 A = 6780379
00 meter
Y = -2241507
11 meter E =
0010444
Z = 4600768
37 I = 51
48578
XDOT = 5400
530765 Wp = 92
87330
YDOT = 4566
736337 meter/sec RA = 200
63062 deg
ZDOT = -2979
293677 TA = 26
89899
MA = 26
84488
Ha = 222
390 n
mi
Hp = 213
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14560608
89 X = 4440460
84
Y = -7354025
94 feet Y = -2191864
48 meter
Z = 15094384
41 Z = 4622332
58
XDOT = 17718
276787 XDOT = 5363
534669
YDOT = 14982
730763 feet/sec YDOT = 4626
922190 meter/sec
ZDOT = -9774
585555 ZDOT = -2953
149340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15858450
95 X = -4833655
85
Y = -3414014
70 feet Y = -1040591
68 meter
Z = 15191692
01 Z = 4630427
73
XDOT = -4599
406397 XDOT = -1401
899070
YDOT = -21685
901237 feet/sec YDOT = -6609
862697 meter/sec
ZDOT = -9657
337072 ZDOT = -2943
556340
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 18348
20691317
00016717 00000-0 10270-3 0 9022
2 25544 51
6357 201
6036 0004920 143
6572 216
4916 15
54072253 26506
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
20691317 = yrday
fracday
Element set: 902
Inclination: 51
6357 deg
RA of node: 201
6036 deg
Eccentricity:
0004920
Arg of perigee: 143
6572 deg
Mean anomaly: 216
4916 deg
Mean motion: 15
54072253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 292
Coasting Arc #4 (Orbit 2664)
---------------------------------------
Vector Time (GMT): 2018/349/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5625484
36 A = 6784094
70 meter
Y = 1356719
34 meter E =
0009291
Z = -3552297
87 I = 51
53042
XDOT = -3971
004577 Wp = 120
67203
YDOT = -4792
914255 meter/sec RA = 195
63404 deg
ZDOT = 4462
082455 TA = 197
39986
MA = 197
43172
Ha = 222
489 n
mi
Hp = 213
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18456313
53 X = -5622982
30
Y = 4451178
95 feet Y = 1293825
48 meter
Z = -11654520
57 Z = -3579618
35
XDOT = -13028
230241 XDOT = -3938
788170
YDOT = -15724
784301 feet/sec YDOT = -4837
140935 meter/sec
ZDOT = 14639
378133 ZDOT = 4442
870645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17206038
93 X = 5244400
67
Y = 7843155
87 feet Y = 2390593
91 meter
Z = -11777668
83 Z = -3589833
46
XDOT = 1192
560007 XDOT = 363
492290
YDOT = 19217
978939 feet/sec YDOT = 5857
639981 meter/sec
ZDOT = 14553
346785 ZDOT = 4435
860100
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 18349
17147849
00016717 00000-0 10270-3 0 9036
2 25544 51
6367 196
7957 0004871 145
5805 214
5664 15
54052381 26653
Satellite: ISS
Catalog Number: 25544
Epoch time: 18349
17147849 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 196
7957 deg
Eccentricity:
0004871
Arg of perigee: 145
5805 deg
Mean anomaly: 214
5664 deg
Mean motion: 15
54052381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2665
Checksum: 343
Coasting Arc #5 (Orbit 2680)
---------------------------------------
Vector Time (GMT): 2018/350/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6423096
30 A = 6787525
41 meter
Y = -493015
89 meter E =
0017841
Z = 2106981
53 I = 51
57410
XDOT = 2191
428701 Wp = 119
97103
YDOT = 4864
737157 meter/sec RA = 190
64958 deg
ZDOT = -5515
971154 TA = 36
65014
MA = 36
52823
Ha = 222
307 n
mi
Hp = 213
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21073150
59 X = 6417897
34
Y = -1617506
21 feet Y = -421217
55 meter
Z = 6912669
06 Z = 2138170
12
XDOT = 7189
726710 XDOT = 2163
660714
YDOT = 15960
423743 feet/sec YDOT = 4889
088284 meter/sec
ZDOT = -18097
018222 ZDOT = -5505
393101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17739498
40 X = -5406999
11
Y = -11403598
08 feet Y = -3475816
69 meter
Z = 7053165
46 Z = 2149804
83
XDOT = 2974
078476 XDOT = 906
499119
YDOT = -15842
606274 feet/sec YDOT = -4828
826392 meter/sec
ZDOT = -18049
859127 ZDOT = -5501
597062
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 18350
20034679
00016717 00000-0 10270-3 0 9049
2 25544 51
6365 191
6668 0004780 149
4773 210
6659 15
54076199 26812
Satellite: ISS
Catalog Number: 25544
Epoch time: 18350
20034679 = yrday
fracday
Element set: 904
Inclination: 51
6365 deg
RA of node: 191
6668 deg
Eccentricity:
0004780
Arg of perigee: 149
4773 deg
Mean anomaly: 210
6659 deg
Mean motion: 15
54076199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2681
Checksum: 335
Coasting Arc #6 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2018/351/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6764029
14 A = 6789323
66 meter
Y = -287785
74 meter E =
0010149
Z = -482859
02 I = 51
61289
XDOT = -216
069756 Wp = 68
16842
YDOT = -4785
016224 meter/sec RA = 185
67536 deg
ZDOT = 5983
399368 TA = 286
62422
MA = 286
73564
Ha = 222
299 n
mi
Hp = 213
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22191696
67 X = -6757962
84
Y = -944178
94 feet Y = -363391
87 meter
Z = -1584183
12 Z = -515701
78
XDOT = -708
890274 XDOT = -191
610653
YDOT = -15698
872127 feet/sec YDOT = -4787
296052 meter/sec
ZDOT = 19630
575354 ZDOT = 5982
408902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17354173
31 X = 5289552
03
Y = 13845761
54 feet Y = 4220188
12 meter
Z = -1732070
20 Z = -527935
00
XDOT = -7571
307211 XDOT = -2307
734438
YDOT = 11905
736588 feet/sec YDOT = 3628
868512 meter/sec
ZDOT = 19626
580968 ZDOT = 5982
181879
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 18351
16490984
00016717 00000-0 10270-3 0 9051
2 25544 51
6363 186
8593 0004877 153
9098 206
2301 15
54087695 26964
Satellite: ISS
Catalog Number: 25544
Epoch time: 18351
16490984 = yrday
fracday
Element set: 905
Inclination: 51
6363 deg
RA of node: 186
8593 deg
Eccentricity:
0004877
Arg of perigee: 153
9098 deg
Mean anomaly: 206
2301 deg
Mean motion: 15
54087695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 349
Coasting Arc #7 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2018/352/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6584248
93 A = 6788857
27 meter
Y = 1058733
96 meter E =
0013762
Z = -1235551
21 I = 51
64575
XDOT = -1831
241535 Wp = 147
79834
YDOT = 4608
041119 meter/sec RA = 180
70465 deg
ZDOT = -5851
468373 TA = 45
63457
MA = 45
52191
Ha = 222
241 n
mi
Hp = 213
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21601866
57 X = 6577922
22
Y = 3473536
60 feet Y = 1132328
32 meter
Z = -4053645
71 Z = -1203582
26
XDOT = -6008
010287 XDOT = -1854
210273
YDOT = 15118
245142 feet/sec YDOT = 4587
434881 meter/sec
ZDOT = -19197
730881 ZDOT = -5860
419449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15681968
53 X = -4779864
01
Y = -15294700
00 feet Y = -4661824
56 meter
Z = -3909751
19 Z = -1191692
16
XDOT = 12397
039547 XDOT = 3778
617654
YDOT = -7829
024503 feet/sec YDOT = -2386
286669 meter/sec
ZDOT = -19238
498873 ZDOT = -5863
894456
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 18352
19377451
00016717 00000-0 10270-3 0 9069
2 25544 51
6377 181
7301 0004676 157
8540 202
2816 15
54083425 27125
Satellite: ISS
Catalog Number: 25544
Epoch time: 18352
19377451 = yrday
fracday
Element set: 906
Inclination: 51
6377 deg
RA of node: 181
7301 deg
Eccentricity:
0004676
Arg of perigee: 157
8540 deg
Mean anomaly: 202
2816 deg
Mean motion: 15
54083425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 308
Coasting Arc #8 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2018/353/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5925402
58 A = 6786214
45 meter
Y = -1767035
57 meter E =
0014875
Z = 2786527
54 I = 51
66947
XDOT = 3712
992128 Wp = 97
91375
YDOT = -4336
434988 meter/sec RA = 175
73235 deg
ZDOT = 5120
181140 TA = 293
67110
MA = 293
82714
Ha = 222
166 n
mi
Hp = 214
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19440297
16 X = -5918738
31
Y = -5797360
78 feet Y = -1833260
52 meter
Z = 9142150
72 Z = 2757759
74
XDOT = 12181
732703 XDOT = 3736
336028
YDOT = -14227
148910 feet/sec YDOT = -4294
783658 meter/sec
ZDOT = 16798
494554 ZDOT = 5138
274056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12877402
36 X = 3925032
24
Y = 15749816
28 feet Y = 4800544
00 meter
Z = 9012727
74 Z = 2747079
42
XDOT = -16827
858277 XDOT = -5129
131203
YDOT = 4050
725980 feet/sec YDOT = 1234
661279 meter/sec
ZDOT = 16880
426967 ZDOT = 5145
154139
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 18353
22263660
00016717 00000-0 10270-3 0 9071
2 25544 51
6370 176
6019 0004727 161
4172 198
7154 15
54100796 27288
Satellite: ISS
Catalog Number: 25544
Epoch time: 18353
22263660 = yrday
fracday
Element set: 907
Inclination: 51
6370 deg
RA of node: 176
6019 deg
Eccentricity:
0004727
Arg of perigee: 161
4172 deg
Mean anomaly: 198
7154 deg
Mean motion: 15
54100796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 313
Coasting Arc #9 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2018/354/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3589711
22 A = 6779934
24 meter
Y = -3242259
78 meter E =
0011467
Z = 4747330
40 I = 51
67675
XDOT = 6445
256166 Wp = 135
57033
YDOT = -3158
699612 meter/sec RA = 171
21735 deg
ZDOT = 2704
362220 TA = 287
66075
MA = 287
78593
Ha = 222
113 n
mi
Hp = 214
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11777267
78 X = -3576248
81
Y = -10637335
24 feet Y = -3282327
68 meter
Z = 15575230
97 Z = 4729925
00
XDOT = 21145
853564 XDOT = 6466
962115
YDOT = -10363
187703 feet/sec YDOT = -3086
503209 meter/sec
ZDOT = 8872
579461 ZDOT = 2735
723715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5189801
32 X = -1581851
44
Y = 15078117
93 feet Y = 4595810
34 meter
Z = 15497131
32 Z = 4723525
63
XDOT = -16636
061714 XDOT = -5070
671610
YDOT = -15031
263785 feet/sec YDOT = -4581
529202 meter/sec
ZDOT = 9014
191481 ZDOT = 2747
525563
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 18354
12289046
00016717 00000-0 10270-3 0 9088
2 25544 51
6353 172
1145 0004697 165
9155 194
2129 15
54102937 27424
Satellite: ISS
Catalog Number: 25544
Epoch time: 18354
12289046 = yrday
fracday
Element set: 908
Inclination: 51
6353 deg
RA of node: 172
1145 deg
Eccentricity:
0004697
Arg of perigee: 165
9155 deg
Mean anomaly: 194
2129 deg
Mean motion: 15
54102937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 316
Coasting Arc #10 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2018/355/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1929409
89 A = 6777775
65 meter
Y = 3814144
61 meter E =
0015579
Z = -5272883
97 I = 51
70258
XDOT = -7199
663363 Wp = 100
85930
YDOT = 2462
889703 meter/sec RA = 166
22305 deg
ZDOT = -857
924604 TA = 160
96236
MA = 160
90407
Ha = 222
013 n
mi
Hp = 214
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6330084
93 X = 1912228
73
Y = 12513597
80 feet Y = 3835625
25 meter
Z = -17299488
08 Z = -5263552
71
XDOT = -23620
942792 XDOT = -7222
501615
YDOT = 8080
346795 feet/sec YDOT = 2382
250480 meter/sec
ZDOT = -2814
713269 ZDOT = -892
953483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8841835
76 X = 2694991
54
Y = -10950889
29 feet Y = -3337831
05 meter
Z = -17257820
18 Z = -5260183
59
XDOT = 16127
865399 XDOT = 4915
773374
YDOT = 17680
700247 feet/sec YDOT = 5389
077435 meter/sec
ZDOT = -2972
808151 ZDOT = -906
111924
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 18355
08744753
00016717 00000-0 10270-3 0 9096
2 25544 51
6358 167
3053 0004668 167
9105 192
2161 15
54078082 27571
Satellite: ISS
Catalog Number: 25544
Epoch time: 18355
08744753 = yrday
fracday
Element set: 909
Inclination: 51
6358 deg
RA of node: 167
3053 deg
Eccentricity:
0004668
Arg of perigee: 167
9105 deg
Mean anomaly: 192
2161 deg
Mean motion: 15
54078082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 331
Coasting Arc #11 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2018/356/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -197986
55 A = 6777818
49 meter
Y = -4294725
38 meter E =
0004530
Z = 5236138
74 I = 51
73530
XDOT = 7419
665430 Wp = 124
85698
YDOT = -1635
941181 meter/sec RA = 161
22948 deg
ZDOT = -1063
142291 TA = 335
29782
MA = 335
31951
Ha = 221
928 n
mi
Hp = 214
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -649562
16 X = -175381
48
Y = -14090306
38 feet Y = -4296813
80 meter
Z = 17178932
87 Z = 5235231
25
XDOT = 24342
734352 XDOT = 7442
571738
YDOT = -5367
261094 feet/sec YDOT = -1552
841090 meter/sec
ZDOT = -3487
999644 ZDOT = -1027
044621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12467552
13 X = -3800109
89
Y = 6606393
38 feet Y = 2013628
70 meter
Z = 17175276
11 Z = 5235024
16
XDOT = -14615
773397 XDOT = -4454
887731
YDOT = -18954
152126 feet/sec YDOT = -5777
225568 meter/sec
ZDOT = -3325
140678 ZDOT = -1013
502879
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 18356
11630530
00016717 00000-0 10270-3 0 9100
2 25544 51
6362 162
1766 0004550 171
7375 188
3854 15
54082365 27734
Satellite: ISS
Catalog Number: 25544
Epoch time: 18356
11630530 = yrday
fracday
Element set: 910
Inclination: 51
6362 deg
RA of node: 162
1766 deg
Eccentricity:
0004550
Arg of perigee: 171
7375 deg
Mean anomaly: 188
3854 deg
Mean motion: 15
54082365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 308
Coasting Arc #12 (Orbit 2787)
---------------------------------------
Vector Time (GMT): 2018/357/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1490702
58 A = 6780178
15 meter
Y = 4685136
53 meter E =
0013137
Z = -4681596
42 I = 51
77409
XDOT = -7066
904960 Wp = 128
03686
YDOT = 632
021328 meter/sec RA = 156
24118 deg
ZDOT = 2880
336215 TA = 170
58358
MA = 170
55892
Ha = 221
792 n
mi
Hp = 214
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4890756
49 X = -1520241
64
Y = 15371182
83 feet Y = 4668302
02 meter
Z = -15359568
32 Z = -4688908
74
XDOT = -23185
383728 XDOT = -7087
438284
YDOT = 2073
560787 feet/sec YDOT = 552
879030 meter/sec
ZDOT = 9449
921965 ZDOT = 2845
957965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15921903
41 X = 4852996
16
Y = -2378528
38 feet Y = -724975
45 meter
Z = -15393007
97 Z = -4691788
83
XDOT = 11812
144012 XDOT = 3600
341495
YDOT = 18866
773967 feet/sec YDOT = 5750
592705 meter/sec
ZDOT = 9294
884602 ZDOT = 2833
080827
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 18357
08085791
00016717 00000-0 10270-3 0 9111
2 25544 51
6360 157
3685 0004471 175
9601 184
1588 15
54074441 27888
Satellite: ISS
Catalog Number: 25544
Epoch time: 18357
08085791 = yrday
fracday
Element set: 911
Inclination: 51
6360 deg
RA of node: 157
3685 deg
Eccentricity:
0004471
Arg of perigee: 175
9601 deg
Mean anomaly: 184
1588 deg
Mean motion: 15
54074441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2788
Checksum: 333
Coasting Arc #13 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2018/358/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2981232
56 A = 6783760
01 meter
Y = -4887016
08 meter E =
0012353
Z = 3626332
18 I = 51
81766
XDOT = 6253
284746 Wp = 107
09235
YDOT = 531
584339 meter/sec RA = 151
26378 deg
ZDOT = -4415
632422 TA = 30
00222
MA = 29
93150
Ha = 221
615 n
mi
Hp = 214
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9780946
70 X = 3018044
33
Y = -16033517
33 feet Y = -4853472
57 meter
Z = 11897415
30 Z = 3640902
54
XDOT = 20516
026071 XDOT = 6268
324277
YDOT = 1744
043108 feet/sec YDOT = 601
597658 meter/sec
ZDOT = -14486
983012 ZDOT = -4385
219804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18684243
13 X = -5694957
31
Y = -1435344
96 feet Y = -437493
14 meter
Z = 11963608
61 Z = 3646507
90
XDOT = -7837
576726 XDOT = -2388
893386
YDOT = -17823
552551 feet/sec YDOT = -5432
618818 meter/sec
ZDOT = -14349
915837 ZDOT = -4373
854347
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 18358
10971308
00016717 00000-0 10270-3 0 9124
2 25544 51
6373 152
2398 0004432 180
2127 179
9024 15
54102147 28047
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
10971308 = yrday
fracday
Element set: 912
Inclination: 51
6373 deg
RA of node: 152
2398 deg
Eccentricity:
0004432
Arg of perigee: 180
2127 deg
Mean anomaly: 179
9024 deg
Mean motion: 15
54102147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 295
Coasting Arc #14 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2018/358/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4973630
07 A = 6781188
02 meter
Y = -1218922
43 meter E =
0011675
Z = 4442291
56 I = 51
81372
XDOT = 4305
111656 Wp = 131
54366
YDOT = -5407
278215 meter/sec RA = 150
74556 deg
ZDOT = 3323
138334 TA = 284
93654
MA = 285
06578
Ha = 221
787 n
mi
Hp = 214
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16317683
97 X = -4981208
18
Y = -3999089
35 feet Y = -1274584
04 meter
Z = 14574447
38 Z = 4418113
04
XDOT = 14124
382072 XDOT = 4349
115502
YDOT = -17740
414091 feet/sec YDOT = -5358
889907 meter/sec
ZDOT = 10902
684822 ZDOT = 3344
156958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13725566
04 X = 4183552
53
Y = 9850409
27 feet Y = 3002404
75 meter
Z = 14465556
20 Z = 4409101
53
XDOT = -18950
763428 XDOT = -5776
192693
YDOT = 10191
106940 feet/sec YDOT = 3106
249395 meter/sec
ZDOT = 10998
006769 ZDOT = 3352
192463
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 18358
23832037
00016717 00000-0 10270-3 0 9134
2 25544 51
6390 151
5996 0004497 180
2116 179
9035 15
54092545 28065
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
23832037 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 151
5996 deg
Eccentricity:
0004497
Arg of perigee: 180
2116 deg
Mean anomaly: 179
9035 deg
Mean motion: 15
54092545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 323
Coasting Arc #15 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2018/359/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3722328
78 A = 6778210
78 meter
Y = 2368958
19 meter E =
0013093
Z = -5156356
46 I = 51
83409
XDOT = -5432
691717 Wp = 97
14611
YDOT = 5171
491883 meter/sec RA = 145
76360 deg
ZDOT = -1550
860387 TA = 157
95804
MA = 157
90169
Ha = 221
557 n
mi
Hp = 214
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12212364
78 X = 3720608
27
Y = 7772172
54 feet Y = 2410574
89 meter
Z = -16917179
98 Z = -5138278
82
XDOT = -17823
791723 XDOT = -5482
583871
YDOT = 16966
836888 feet/sec YDOT = 5110
460977 meter/sec
ZDOT = -5088
124628 ZDOT = -1577
370670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8723229
88 X = -2658840
47
Y = -11670355
09 feet Y = -3557124
23 meter
Z = -16835901
24 Z = -5131582
70
XDOT = 21835
692893 XDOT = 6655
519194
YDOT = -8831
625140 feet/sec YDOT = -2691
879343 meter/sec
ZDOT = -5208
204988 ZDOT = -1587
460880
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 18359
20286868
00016717 00000-0 10270-3 0 9148
2 25544 51
6406 146
7915 0004367 183
6239 176
4883 15
54120201 28210
Satellite: ISS
Catalog Number: 25544
Epoch time: 18359
20286868 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 146
7915 deg
Eccentricity:
0004367
Arg of perigee: 183
6239 deg
Mean anomaly: 176
4883 deg
Mean motion: 15
54120201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 322
Coasting Arc #16 (Orbit 2836)
---------------------------------------
Vector Time (GMT): 2018/360/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2326146
65 A = 6777351
24 meter
Y = -3493593
84 meter E =
0004106
Z = 5319594
81 I = 51
85806
XDOT = 6112
590861 Wp = 154
53403
YDOT = -4619
567162 meter/sec RA = 140
77922 deg
ZDOT = -364
461397 TA = 298
90895
MA = 298
95013
Ha = 221
482 n
mi
Hp = 214
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7631714
74 X = -2312746
78
Y = -11461922
06 feet Y = -3519532
04 meter
Z = 17452738
87 Z = 5308327
58
XDOT = 20054
431959 XDOT = 6165
564191
YDOT = -15156
060243 feet/sec YDOT = -4550
915692 meter/sec
ZDOT = -1195
739491 ZDOT = -334
640832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3359590
53 X = 1024003
20
Y = 13419783
33 feet Y = 4090349
96 meter
Z = 17402281
11 Z = 5304215
28
XDOT = -23057
959716 XDOT = -7028
066121
YDOT = 7133
052281 feet/sec YDOT = 2174
154335 meter/sec
ZDOT = -1060
766947 ZDOT = -323
321765
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 18360
23171854
00016717 00000-0 10270-3 0 9152
2 25544 51
6403 141
6635 0004394 189
1246 170
9828 15
54138221 28375
Satellite: ISS
Catalog Number: 25544
Epoch time: 18360
23171854 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 141
6635 deg
Eccentricity:
0004394
Arg of perigee: 189
1246 deg
Mean anomaly: 170
9828 deg
Mean motion: 15
54138221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2837
Checksum: 311
Coasting Arc #17 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2018/361/02:55:40
991
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -395458
29 A = 6782404
11 meter
Y = 5160984
56 meter E =
0008931
Z = -4391866
94 I = 51
89389
XDOT = -6403
424809 Wp = 139
03923
YDOT = 2429
837267 meter/sec RA = 136
09820 deg
ZDOT = 3429
321335 TA = 165
65325
MA = 165
62787
Ha = 221
376 n
mi
Hp = 216
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1297435
35 X = -431807
45
Y = 16932364
05 feet Y = 5156359
36 meter
Z = -14409012
27 Z = -4393875
81
XDOT = -21008
611578 XDOT = -6446
777586
YDOT = 7971
907045 feet/sec YDOT = 2357
987059 meter/sec
ZDOT = 11251
054249 ZDOT = 3398
111099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12100149
78 X = 3688125
65
Y = -11903699
55 feet Y = -3628247
62 meter
Z = -14418607
34 Z = -4394791
52
XDOT = 20217
710799 XDOT = 6162
358252
YDOT = 7083
706350 feet/sec YDOT = 2159
113696 meter/sec
ZDOT = 11110
022219 ZDOT = 3386
334772
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 18361
13196358
00016717 00000-0 10270-3 0 9169
2 25544 51
6398 137
1754 0004348 214
8936 145
1932 15
53700139 28519
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
13196358 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 137
1754 deg
Eccentricity:
0004348
Arg of perigee: 214
8936 deg
Mean anomaly: 145
1932 deg
Mean motion: 15
53700139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 322
Coasting Arc #18 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2018/361/09:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 545187
69 A = 6780907
34 meter
Y = 4779634
12 meter E =
0010950
Z = -4789081
53 I = 51
89164
XDOT = -6325
442284 Wp = 132
51207
YDOT = 3396
687452 meter/sec RA = 134
82868 deg
ZDOT = 2666
573848 TA = 163
76785
MA = 163
73275
Ha = 221
424 n
mi
Hp = 216
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1788673
51 X = 514962
43
Y = 15681214
31 feet Y = 4785562
12 meter
Z = -15712209
73 Z = -4786506
31
XDOT = -20752
763400 XDOT = -6375
907487
YDOT = 11143
987703 feet/sec YDOT = 3325
669602 meter/sec
ZDOT = 8748
601863 ZDOT = 2635
725182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13365654
11 X = -4073851
37
Y = -8414777
77 feet Y = -2564824
27 meter
Z = -15701088
34 Z = -4785691
73
XDOT = 3854
069564 XDOT = 1174
720403
YDOT = -22205
674668 feet/sec YDOT = -6768
289639 meter/sec
ZDOT = 8609
096395 ZDOT = 2624
052581
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 18361
38924299
00016717 00000-0 10270-3 0 9170
2 25544 51
6365 135
8901 0004578 214
4828 145
6028 15
53693734 28550
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
38924299 = yrday
fracday
Element set: 917
Inclination: 51
6365 deg
RA of node: 135
8901 deg
Eccentricity:
0004578
Arg of perigee: 214
4828 deg
Mean anomaly: 145
6028 deg
Mean motion: 15
53693734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 344
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