[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 3rd 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) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
132/22:41:26
692 -1
1 1
1 1
1
N/A -0
1 -0
1 222
0
000/00:02:49
384 -0
0 -0
0 213
9
134/06:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
9
Coasting Arc #1 (Orbit 3140)
---------------------------------------
Vector Time (GMT): 2018/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4422324
43 A = 6777892
10 meter
Y = -214547
33 meter E =
0007413
Z = 5128165
55 I = 51
27620
XDOT = 2036
764769 Wp = 48
67787
YDOT = 7253
759472 meter/sec RA = 245
45874 deg
ZDOT = -1446
770461 TA = 55
34489
MA = 55
27504
Ha = 221
586 n
mi
Hp = 213
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14508938
43 X = 4399484
51
Y = -703895
45 feet Y = -165221
72 meter
Z = 16824690
12 Z = 5149592
57
XDOT = 6682
299112 XDOT = 1962
527649
YDOT = 23798
423466 feet/sec YDOT = 7276
120938 meter/sec
ZDOT = -4746
622246 ZDOT = -1437
056468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10665933
08 X = 3250976
40
Y = -9696226
22 feet Y = -2955409
75 meter
Z = 16920284
55 Z = 5157302
73
XDOT = 19605
714579 XDOT = 5975
821804
YDOT = 13322
224614 feet/sec YDOT = 4060
614062 meter/sec
ZDOT = -4704
230580 ZDOT = -1433
849481
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18122
54579039
00016717 00000-0 10270-3 0 9003
2 25544 51
6406 246
2395 0002936 38
5583 321
5779 15
54175366 31413
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
54579039 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 246
2395 deg
Eccentricity:
0002936
Arg of perigee: 38
5583 deg
Mean anomaly: 321
5779 deg
Mean motion: 15
54175366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3141
Checksum: 320
Coasting Arc #2 (Orbit 3155)
---------------------------------------
Vector Time (GMT): 2018/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4915550
68 A = 6780591
16 meter
Y = -1430667
20 meter E =
0010897
Z = -4456062
94 I = 51
30053
XDOT = -924
025287 Wp = 96
01766
YDOT = -6881
561766 meter/sec RA = 240
43951 deg
ZDOT = 3234
425912 TA = 206
71023
MA = 206
76639
Ha = 221
692 n
mi
Hp = 213
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16127134
79 X = -4877541
70
Y = -4693790
03 feet Y = -1485423
55 meter
Z = -14619629
06 Z = -4479849
10
XDOT = -3031
579026 XDOT = -862
716489
YDOT = -22577
302382 feet/sec YDOT = -6891
552198 meter/sec
ZDOT = 10611
633569 ZDOT = 3230
085853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15242672
32 X = -4645966
52
Y = 6831466
77 feet Y = 2082231
07 meter
Z = -14725545
74 Z = -4488346
34
XDOT = -16513
450175 XDOT = -5033
299613
YDOT = -14051
670327 feet/sec YDOT = -4282
949116 meter/sec
ZDOT = 10593
151511 ZDOT = 3228
792581
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18123
51028194
00016717 00000-0 10270-3 0 9013
2 25544 51
6410 241
4322 0002956 41
2838 318
8538 15
54200628 31569
Satellite: ISS
Catalog Number: 25544
Epoch time: 18123
51028194 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 241
4322 deg
Eccentricity:
0002956
Arg of perigee: 41
2838 deg
Mean anomaly: 318
8538 deg
Mean motion: 15
54200628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3156
Checksum: 286
Coasting Arc #3 (Orbit 3171)
---------------------------------------
Vector Time (GMT): 2018/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5179956
48 A = 6784543
32 meter
Y = 2898617
50 meter E =
0014892
Z = 3274594
24 I = 51
32983
XDOT = -400
528152 Wp = 83
95770
YDOT = 6048
779762 meter/sec RA = 235
43010 deg
ZDOT = -4700
699480 TA = 57
82240
MA = 57
67805
Ha = 221
751 n
mi
Hp = 213
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16994607
87 X = 5131251
91
Y = 9509899
93 feet Y = 2956270
85 meter
Z = 10743419
44 Z = 3299638
85
XDOT = -1314
068741 XDOT = -445
303681
YDOT = 19845
077960 feet/sec YDOT = 6044
050660 meter/sec
ZDOT = -15422
242387 ZDOT = -4702
753582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18980248
93 X = 5785179
87
Y = -4074296
12 feet Y = -1241845
46 meter
Z = 10854778
51 Z = 3308536
49
XDOT = 11930
636814 XDOT = 3636
458101
YDOT = 14291
717311 feet/sec YDOT = 4356
115436 meter/sec
ZDOT = -15432
167898 ZDOT = -4703
724775
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18124
53907165
00016717 00000-0 10270-3 0 9021
2 25544 51
6402 236
3033 0002980 47
3100 312
8303 15
54178171 31727
Satellite: ISS
Catalog Number: 25544
Epoch time: 18124
53907165 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 236
3033 deg
Eccentricity:
0002980
Arg of perigee: 47
3100 deg
Mean anomaly: 312
8303 deg
Mean motion: 15
54178171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3172
Checksum: 272
Coasting Arc #4 (Orbit 3186)
---------------------------------------
Vector Time (GMT): 2018/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5166420
53 A = 6787798
08 meter
Y = -4022047
61 meter E =
0010373
Z = -1777194
72 I = 51
36101
XDOT = 1844
153221 Wp = 40
98579
YDOT = -4850
906772 meter/sec RA = 230
43273 deg
ZDOT = 5643
658624 TA = 299
41921
MA = 299
52270
Ha = 221
790 n
mi
Hp = 213
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16950198
58 X = -5112428
15
Y = -13195694
26 feet Y = -4079520
10 meter
Z = -5830691
35 Z = -1802160
72
XDOT = 6050
371460 XDOT = 1870
846131
YDOT = -15915
048466 feet/sec YDOT = -4830
135212 meter/sec
ZDOT = 18515
940366 ZDOT = 5652
681564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21385366
90 X = -6518259
83
Y = 1672209
30 feet Y = 509689
40 meter
Z = -5941577
14 Z = -1810992
71
XDOT = -6241
253676 XDOT = -1902
334121
YDOT = -14185
101322 feet/sec YDOT = -4323
618883 meter/sec
ZDOT = 18556
800007 ZDOT = 5656
112642
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18125
50355811
00016717 00000-0 10270-3 0 9035
2 25544 51
6410 231
4956 0003062 45
6720 314
4684 15
54175207 31870
Satellite: ISS
Catalog Number: 25544
Epoch time: 18125
50355811 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 231
4956 deg
Eccentricity:
0003062
Arg of perigee: 45
6720 deg
Mean anomaly: 314
4684 deg
Mean motion: 15
54175207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3187
Checksum: 289
Coasting Arc #5 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2018/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4784579
35 A = 6789114
30 meter
Y = 4809950
44 meter E =
0013027
Z = 43251
87 I = 51
38697
XDOT = -3359
545496 Wp = 120
77626
YDOT = 3407
734223 meter/sec RA = 225
44324 deg
ZDOT = -5990
999077 TA = 58
75628
MA = 58
62871
Ha = 221
848 n
mi
Hp = 213
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15697438
81 X = 4730227
47
Y = 15780677
29 feet Y = 4863151
00 meter
Z = 141902
47 Z = 66362
09
XDOT = -11022
130894 XDOT = -3368
300678
YDOT = 11180
230391 feet/sec YDOT = 3370
116787 meter/sec
ZDOT = -19655
508782 ZDOT = -6007
339827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22247412
91 X = 6781011
45
Y = 672584
55 feet Y = 205003
77 meter
Z = 244430
61 Z = 74502
45
XDOT = -177
981312 XDOT = -54
248704
YDOT = 13983
629976 feet/sec YDOT = 4262
210417 meter/sec
ZDOT = -19728
840246 ZDOT = -6013
350507
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18126
53234098
00016717 00000-0 10270-3 0 9043
2 25544 51
6406 226
3664 0003029 51
9213 308
2212 15
54201269 32039
Satellite: ISS
Catalog Number: 25544
Epoch time: 18126
53234098 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 226
3664 deg
Eccentricity:
0003029
Arg of perigee: 51
9213 deg
Mean anomaly: 308
2212 deg
Mean motion: 15
54201269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 276
Coasting Arc #6 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2018/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4044858
16 A = 6787968
96 meter
Y = -5183450
45 meter E =
0017058
Z = 1653438
81 I = 51
40724
XDOT = 4777
402364 Wp = 61
92314
YDOT = -1899
511175 meter/sec RA = 220
45571 deg
ZDOT = 5695
173212 TA = 316
25864
MA = 316
39367
Ha = 221
890 n
mi
Hp = 213
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13270532
03 X = -3994626
37
Y = -17006071
03 feet Y = -5228402
03 meter
Z = 5424668
01 Z = 1633911
98
XDOT = 15673
892271 XDOT = 4770
623820
YDOT = -6231
992043 feet/sec YDOT = -1846
125079 meter/sec
ZDOT = 18684
951484 ZDOT = 5718
363798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21405468
65 X = -6524386
84
Y = -2837339
68 feet Y = -864821
13 meter
Z = 5338156
09 Z = 1627069
98
XDOT = 6541
798608 XDOT = 1993
940216
YDOT = -13771
307090 feet/sec YDOT = -4197
494401 meter/sec
ZDOT = 18788
670796 ZDOT = 5726
786859
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18127
56112021
00016717 00000-0 10270-3 0 9059
2 25544 51
6408 221
2378 0003169 53
6338 306
5107 15
54212189 32193
Satellite: ISS
Catalog Number: 25544
Epoch time: 18127
56112021 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 221
2378 deg
Eccentricity:
0003169
Arg of perigee: 53
6338 deg
Mean anomaly: 306
5107 deg
Mean motion: 15
54212189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 286
Coasting Arc #7 (Orbit 3233)
---------------------------------------
Vector Time (GMT): 2018/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2910835
38 A = 6784779
25 meter
Y = 5222046
42 meter E =
0007107
Z = -3214858
72 I = 51
42132
XDOT = -5983
735852 Wp = 84
03569
YDOT = 405
987520 meter/sec RA = 215
46381 deg
ZDOT = -4766
777150 TA = 133
25238
MA = 133
19304
Ha = 221
897 n
mi
Hp = 213
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9549984
84 X = 2867840
88
Y = 17132698
22 feet Y = 5254357
07 meter
Z = -10547436
75 Z = -3200823
10
XDOT = -19631
679304 XDOT = -5964
676356
YDOT = 1331
980052 feet/sec YDOT = 339
179952 meter/sec
ZDOT = -15639
032643 ZDOT = -4795
797945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18952117
86 X = 5776605
52
Y = 5182007
68 feet Y = 1579475
94 meter
Z = -10485418
72 Z = -3195955
63
XDOT = -12387
834400 XDOT = -3775
811925
YDOT = 13455
243590 feet/sec YDOT = 4101
158246 meter/sec
ZDOT = -15768
602703 ZDOT = -4806
270104
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18128
52559947
00016717 00000-0 10270-3 0 9069
2 25544 51
6399 216
4298 0003050 57
9396 302
2053 15
54204334 32342
Satellite: ISS
Catalog Number: 25544
Epoch time: 18128
52559947 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 216
4298 deg
Eccentricity:
0003050
Arg of perigee: 57
9396 deg
Mean anomaly: 302
2053 deg
Mean motion: 15
54204334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3234
Checksum: 315
Coasting Arc #8 (Orbit 3249)
---------------------------------------
Vector Time (GMT): 2018/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1484328
70 A = 6780826
67 meter
Y = -4937850
79 meter E =
0011655
Z = 4394823
58 I = 51
43687
XDOT = 6842
746018 Wp = 98
16994
YDOT = 929
608058 meter/sec RA = 210
46259 deg
ZDOT = 3346
334860 TA = 317
88825
MA = 317
97776
Ha = 221
868 n
mi
Hp = 213
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4869844
82 X = -1450349
88
Y = -16200297
87 feet Y = -4954259
65 meter
Z = 14418712
54 Z = 4387695
64
XDOT = 22449
954126 XDOT = 6815
587471
YDOT = 3049
895204 feet/sec YDOT = 1005
976460 meter/sec
ZDOT = 10978
788912 ZDOT = 3379
508838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15152223
19 X = -4618397
63
Y = -7581219
36 feet Y = -2310755
66 meter
Z = 14387479
15 Z = 4385303
65
XDOT = 17093
128569 XDOT = 5209
985588
YDOT = -12989
463654 feet/sec YDOT = -3959
188522 meter/sec
ZDOT = 11126
752777 ZDOT = 3391
434247
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18129
55437272
00016717 00000-0 10270-3 0 9070
2 25544 51
6408 211
3003 0003071 59
5486 300
5970 15
54242781 32507
Satellite: ISS
Catalog Number: 25544
Epoch time: 18129
55437272 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 211
3003 deg
Eccentricity:
0003071
Arg of perigee: 59
5486 deg
Mean anomaly: 300
5970 deg
Mean motion: 15
54242781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3250
Checksum: 291
Coasting Arc #9 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2018/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -177176
57 A = 6777990
93 meter
Y = 4442797
83 meter E =
0016591
Z = -5130680
81 I = 51
45522
XDOT = -7207
657521 Wp = 75
24501
YDOT = -2069
305848 meter/sec RA = 205
45424 deg
ZDOT = -1543
020880 TA = 179
82217
MA = 179
82158
Ha = 221
949 n
mi
Hp = 213
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -581287
95 X = -201921
60
Y = 14576108
36 feet Y = 4440678
18 meter
Z = -16832942
28 Z = -5131601
56
XDOT = -23647
170345 XDOT = -7176
487037
YDOT = -6789
061182 feet/sec YDOT = -2149
732547 meter/sec
ZDOT = -5062
404463 ZDOT = -1577
957813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10404045
07 X = 3171152
94
Y = 10217672
00 feet Y = 3114346
43 meter
Z = -16837571
12 Z = -5132091
68
XDOT = -20243
696321 XDOT = -6170
278639
YDOT = 12014
353092 feet/sec YDOT = 3661
974822 meter/sec
ZDOT = -5218
121717 ZDOT = -1590
483499
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18130
51884776
00016717 00000-0 10270-3 0 9084
2 25544 51
6401 206
4925 0003143 61
1927 298
9541 15
54199507 32654
Satellite: ISS
Catalog Number: 25544
Epoch time: 18130
51884776 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 206
4925 deg
Eccentricity:
0003143
Arg of perigee: 61
1927 deg
Mean anomaly: 298
9541 deg
Mean motion: 15
54199507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 322
Coasting Arc #10 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2018/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1913777
43 A = 6777033
77 meter
Y = -3777301
53 meter E =
0005737
Z = 5286763
86 I = 51
48304
XDOT = 7056
062667 Wp = 69
03505
YDOT = 2985
684353 meter/sec RA = 200
44243 deg
ZDOT = -418
652844 TA = 24
97747
MA = 24
94972
Ha = 221
819 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6278797
34 X = 1930193
38
Y = -12392721
55 feet Y = -3755808
58 meter
Z = 17345025
78 Z = 5296100
31
XDOT = 23149
811900 XDOT = 7024
185127
YDOT = 9795
552340 feet/sec YDOT = 3064
411869 meter/sec
ZDOT = -1373
532954 ZDOT = -384
453926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5162670
81 X = -1573582
06
Y = -12840824
02 feet Y = -3913883
16 meter
Z = 17387145
58 Z = 5299601
97
XDOT = 21773
488012 XDOT = 6636
559146
YDOT = -10418
176936 feet/sec YDOT = -3175
460330 meter/sec
ZDOT = -1221
199022 ZDOT = -372
221462
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18131
54761755
00016717 00000-0 10270-3 0 9090
2 25544 51
6403 201
3639 0003149 64
8181 295
3298 15
54250602 32812
Satellite: ISS
Catalog Number: 25544
Epoch time: 18131
54761755 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 201
3639 deg
Eccentricity:
0003149
Arg of perigee: 64
8181 deg
Mean anomaly: 295
3298 deg
Mean motion: 15
54250602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 306
Coasting Arc #11 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2018/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3579012
93 A = 6778803
03 meter
Y = 3049614
88 meter E =
0014860
Z = -4896460
18 I = 51
51945
XDOT = -6306
506379 Wp = 98
93918
YDOT = -3663
785961 meter/sec RA = 195
43384 deg
ZDOT = 2331
593659 TA = 193
93122
MA = 193
97226
Ha = 221
988 n
mi
Hp = 213
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11742168
40 X = -3589063
75
Y = 10005298
16 feet Y = 3009535
74 meter
Z = -16064501
89 Z = -4913870
45
XDOT = -20690
637728 XDOT = -6276
394047
YDOT = -12020
295148 feet/sec YDOT = -3734
141311 meter/sec
ZDOT = 7649
585494 ZDOT = 2301
031445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6399
72 X = 1950
63
Y = 15345015
52 feet Y = 4677160
73 meter
Z = -16142589
28 Z = -4920261
21
XDOT = -21513
645938 XDOT = -6557
359282
YDOT = 7899
983850 feet/sec YDOT = 2407
915077 meter/sec
ZDOT = 7513
550419 ZDOT = 2290
130168
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18132
51208937
00016717 00000-0 10270-3 0 9108
2 25544 51
6397 196
5556 0003317 67
1504 292
9998 15
54227654 32966
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
51208937 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 196
5556 deg
Eccentricity:
0003317
Arg of perigee: 67
1504 deg
Mean anomaly: 292
9998 deg
Mean motion: 15
54227654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 338
Coasting Arc #12 (Orbit 3302)
---------------------------------------
Vector Time (GMT): 2018/132/22:42:51
384
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1245260
97 A = 6777629
71 meter
Y = 4042183
10 meter E =
0017156
Z = -5310687
23 I = 51
52945
XDOT = -7399
713192 Wp = 87
05358
YDOT = -1946
772898 meter/sec RA = 193
22291 deg
ZDOT = 254
906383 TA = 185
37458
MA = 185
39302
Ha = 222
022 n
mi
Hp = 213
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4085501
88 X = -1264572
24
Y = 13261755
56 feet Y = 4028149
83 meter
Z = -17423514
52 Z = -5316783
23
XDOT = -24277
274253 XDOT = -7378
632105
YDOT = -6387
050190 feet/sec YDOT = -2029
403719 meter/sec
ZDOT = 836
307032 ZDOT = 219
011672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3306969
85 X = -1007964
41
Y = -13441127
36 feet Y = -4096855
62 meter
Z = -17451200
25 Z = -5319125
84
XDOT = 23185
006110 XDOT = 7066
789862
YDOT = -6575
605913 feet/sec YDOT = -2004
244682 meter/sec
ZDOT = 676
257032 ZDOT = 206
123143
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18132
96217624
00016717 00000-0 10270-3 0 9111
2 25544 51
6414 194
3132 0002692 57
8350 302
3063 15
54040346 33031
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
96217624 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 194
3132 deg
Eccentricity:
0002692
Arg of perigee: 57
8350 deg
Mean anomaly: 302
3063 deg
Mean motion: 15
54040346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3303
Checksum: 276
Coasting Arc #13 (Orbit 3318)
---------------------------------------
Vector Time (GMT): 2018/133/22:42:51
384
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2936228
29 A = 6778950
11 meter
Y = -3555863
07 meter E =
0008779
Z = 4963849
14 I = 51
56595
XDOT = 6863
023400 Wp = 57
88326
YDOT = 2693
428015 meter/sec RA = 188
21921 deg
ZDOT = -2122
867094 TA = 52
84208
MA = 52
76193
Ha = 221
891 n
mi
Hp = 213
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9633294
91 X = 2951660
42
Y = -11666217
41 feet Y = -3522942
01 meter
Z = 16285594
29 Z = 4978149
99
XDOT = 22516
480970 XDOT = 6842
706661
YDOT = 8836
706087 feet/sec YDOT = 2770
061540 meter/sec
ZDOT = -6964
787054 ZDOT = -2089
577464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2033173
43 X = -619711
26
Y = 14922118
26 feet Y = 4548261
65 meter
Z = 16349867
69 Z = 4983439
67
XDOT = -22767
858905 XDOT = -6939
643394
YDOT = 4392
683319 feet/sec YDOT = 1338
889876 meter/sec
ZDOT = -6816
438958 ZDOT = -2077
650594
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 18133
99107675
00016717 00000-0 10270-3 0 9120
2 25544 51
6408 189
1852 0002682 58
9203 301
2213 15
54069635 33197
Satellite: ISS
Catalog Number: 25544
Epoch time: 18133
99107675 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 189
1852 deg
Eccentricity:
0002682
Arg of perigee: 58
9203 deg
Mean anomaly: 301
2213 deg
Mean motion: 15
54069635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3319
Checksum: 311
Coasting Arc #14 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2018/134/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2471259
12 A = 6778748
95 meter
Y = -3759306
43 meter E =
0007853
Z = 5065689
62 I = 51
57249
XDOT = 7111
748733 Wp = 61
99384
YDOT = 2254
770801 meter/sec RA = 186
61547 deg
ZDOT = -1790
391100 TA = 45
36814
MA = 45
30413
Ha = 222
087 n
mi
Hp = 213
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8107805
50 X = 2488506
06
Y = -12333682
52 feet Y = -3731574
88 meter
Z = 16619716
60 Z = 5077736
14
XDOT = 23332
508968 XDOT = 7094
703673
YDOT = 7397
541998 feet/sec YDOT = 2334
204038 meter/sec
ZDOT = -5873
986550 ZDOT = -1755
885250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13389662
15 X = 4081169
02
Y = -6063627
47 feet Y = -1848193
65 meter
Z = 16673949
25 Z = 5082219
73
XDOT = 15237
604938 XDOT = 4644
421985
YDOT = 17866
592021 feet/sec YDOT = 5445
737248 meter/sec
ZDOT = -5720
150885 ZDOT = -1743
501990
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 18134
31261120
00016717 00000-0 10270-3 0 9134
2 25544 51
6382 187
5773 0002670 74
2178 285
9269 15
53993007 33244
Satellite: ISS
Catalog Number: 25544
Epoch time: 18134
31261120 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 187
5773 deg
Eccentricity:
0002670
Arg of perigee: 74
2178 deg
Mean anomaly: 285
9269 deg
Mean motion: 15
53993007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 312
Coasting Arc #15 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2018/135/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4033471
73 A = 6781591
32 meter
Y = 3320771
20 meter E =
0010902
Z = -4334353
89 I = 51
61532
XDOT = -6156
146871 Wp = 103
54317
YDOT = -2935
565324 meter/sec RA = 181
62012 deg
ZDOT = 3484
597479 TA = 201
91434
MA = 201
96100
Ha = 222
040 n
mi
Hp = 213
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13233174
95 X = -4049251
24
Y = 10894918
64 feet Y = 3275578
19 meter
Z = -14220321
17 Z = -4353985
66
XDOT = -20197
332254 XDOT = -6139
789756
YDOT = -9631
119830 feet/sec YDOT = -3004
316358 meter/sec
ZDOT = 11432
406427 ZDOT = 3454
731920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16902490
67 X = -5151879
16
Y = 2368427
97 feet Y = 721896
84 meter
Z = -14308391
38 Z = -4361197
69
XDOT = -12019
375168 XDOT = -3663
505551
YDOT = -17610
705792 feet/sec YDOT = -5367
743125 meter/sec
ZDOT = 11299
356521 ZDOT = 3444
043867
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 18135
27720372
00016717 00000-0 10270-3 0 9140
2 25544 51
6384 182
7703 0002486 75
9102 284
2327 15
54021510 33391
Satellite: ISS
Catalog Number: 25544
Epoch time: 18135
27720372 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 182
7703 deg
Eccentricity:
0002486
Arg of perigee: 75
9102 deg
Mean anomaly: 284
2327 deg
Mean motion: 15
54021510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3339
Checksum: 295
Coasting Arc #16 (Orbit 3354)
---------------------------------------
Vector Time (GMT): 2018/136/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5319937
74 A = 6785391
90 meter
Y = -2796665
11 meter E =
0015373
Z = 3135331
35 I = 51
66132
XDOT = 4748
888721 Wp = 92
34103
YDOT = 3567
506239 meter/sec RA = 176
63493 deg
ZDOT = -4855
671589 TA = 51
52523
MA = 51
38741
Ha = 222
034 n
mi
Hp = 213
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17453863
97 X = 5335585
32
Y = -9175410
45 feet Y = -2737086
68 meter
Z = 10286520
19 Z = 3161212
07
XDOT = 15580
343573 XDOT = 4732
229726
YDOT = 11704
416794 feet/sec YDOT = 3620
518859 meter/sec
ZDOT = -15930
681066 ZDOT = -4832
642801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19632921
07 X = 5984114
34
Y = 987555
04 feet Y = 301006
78 meter
Z = 10402459
69 Z = 3170669
71
XDOT = 7583
852779 XDOT = 2311
558327
YDOT = 16639
497046 feet/sec YDOT = 5071
718700 meter/sec
ZDOT = -15828
228156 ZDOT = -4824
443942
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 18136
30610185
00016717 00000-0 10270-3 0 9156
2 25544 51
6388 177
6411 0002562 80
6464 279
4978 15
54016732 33559
Satellite: ISS
Catalog Number: 25544
Epoch time: 18136
30610185 = yrday
fracday
Element set: 915
Inclination: 51
6388 deg
RA of node: 177
6411 deg
Eccentricity:
0002562
Arg of perigee: 80
6464 deg
Mean anomaly: 279
4978 deg
Mean motion: 15
54016732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3355
Checksum: 319
Coasting Arc #17 (Orbit 3369)
---------------------------------------
Vector Time (GMT): 2018/137/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905563
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6190718
40 A = 6788408
68 meter
Y = 2230258
02 meter E =
0009808
Z = -1657747
52 I = 51
70440
XDOT = -3009
239601 Wp = 48
91191
YDOT = -4123
121784 meter/sec RA = 171
66245 deg
ZDOT = 5719
021469 TA = 292
95199
MA = 293
05546
Ha = 222
085 n
mi
Hp = 213
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20310755
90 X = -6207145
05
Y = 7317119
48 feet Y = 2160937
47 meter
Z = -5438804
21 Z = -1687860
06
XDOT = -9872
833338 XDOT = -2990
690533
YDOT = -13527
302442 feet/sec YDOT = -4156
670071 meter/sec
ZDOT = 18763
193795 ZDOT = 5704
447988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21235052
48 X = -6472443
99
Y = -3695281
03 feet Y = -1126321
66 meter
Z = -5573605
51 Z = -1698834
96
XDOT = -2246
985342 XDOT = -684
881132
YDOT = -15153
943564 feet/sec YDOT = -4618
921998 meter/sec
ZDOT = 18698
569418 ZDOT = 5699
323959
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 18137
27069132
00016717 00000-0 10270-3 0 9164
2 25544 51
6390 172
8337 0002647 79
8967 280
2484 15
54022516 33704
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
27069132 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 172
8337 deg
Eccentricity:
0002647
Arg of perigee: 79
8967 deg
Mean anomaly: 280
2484 deg
Mean motion: 15
54022516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3370
Checksum: 322
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