[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 18th 2019
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) : 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
018/18:05:09
698 3
1 3
2 3
2
N/A 0
6 -0
3 221
0
000/00:08:19
397 -0
5 -0
1 217
9
020/01:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 217
9
025/12:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 217
5
026/08:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 3167)
---------------------------------------
Vector Time (GMT): 2019/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -415942
98 A = 6780879
85 meter
Y = -4840895
92 meter E =
0009374
Z = -4739115
20 I = 51
85213
XDOT = 6816
569021 Wp = 60
15521
YDOT = 2127
757980 meter/sec RA = 35
08293 deg
ZDOT = -2771
292022 TA = 182
45189
MA = 182
45648
Ha = 220
800 n
mi
Hp = 216
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1364642
32 X = -338759
92
Y = -15882204
46 feet Y = -4845115
42 meter
Z = -15548278
22 Z = -4740948
54
XDOT = 22364
071590 XDOT = 6805
730548
YDOT = 6980
833268 feet/sec YDOT = 2203
925181 meter/sec
ZDOT = -9092
165428 ZDOT = -2738
206021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13896053
09 X = 4235516
98
Y = -7795491
42 feet Y = -2376065
78 meter
Z = -15555887
79 Z = -4741434
60
XDOT = 2482
061724 XDOT = 756
532414
YDOT = 22273
297421 feet/sec YDOT = 6788
901054 meter/sec
ZDOT = -8943
107409 ZDOT = -2725
859138
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 19016
52092079
00016717 00000-0 10270-3 0 9008
2 25544 51
6412 35
5970 0002480 294
6806 65
4088 15
53763179 31685
Satellite: ISS
Catalog Number: 25544
Epoch time: 19016
52092079 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 35
5970 deg
Eccentricity:
0002480
Arg of perigee: 294
6806 deg
Mean anomaly: 65
4088 deg
Mean motion: 15
53763179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3168
Checksum: 317
Coasting Arc #2 (Orbit 3183)
---------------------------------------
Vector Time (GMT): 2019/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1033713
39 A = 6778736
89 meter
Y = 4168073
78 meter E =
0001171
Z = 5244229
14 I = 51
81633
XDOT = -6949
970482 Wp = 122
34572
YDOT = -3062
512630 meter/sec RA = 30
10248 deg
ZDOT = 1063
338148 TA = 317
48961
MA = 317
49868
Ha = 220
941 n
mi
Hp = 215
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3391448
11 X = -1105718
52
Y = 13674782
73 feet Y = 4156111
02 meter
Z = 17205476
18 Z = 5239033
25
XDOT = -22801
740427 XDOT = -6920
373145
YDOT = -10047
613615 feet/sec YDOT = -3140
066640 meter/sec
ZDOT = 3488
642219 ZDOT = 1029
649626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13841807
78 X = -4218983
01
Y = 2780719
43 feet Y = 847563
28 meter
Z = 17181442
62 Z = 5236903
71
XDOT = -658
797745 XDOT = -200
801553
YDOT = -23913
854416 feet/sec YDOT = -7288
942826 meter/sec
ZDOT = 3337
001793 ZDOT = 1017
118147
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 19017
54999475
00016717 00000-0 10270-3 0 9018
2 25544 51
6404 30
4692 0002473 302
3646 57
7267 15
53768810 31840
Satellite: ISS
Catalog Number: 25544
Epoch time: 19017
54999475 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 30
4692 deg
Eccentricity:
0002473
Arg of perigee: 302
3646 deg
Mean anomaly: 57
7267 deg
Mean motion: 15
53768810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3184
Checksum: 322
Coasting Arc #3 (Orbit 3198)
---------------------------------------
Vector Time (GMT): 2019/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2524280
56 A = 6778669
09 meter
Y = -3418345
52 meter E =
0012389
Z = -5292095
62 I = 51
78565
XDOT = 6634
207695 Wp = 89
75994
YDOT = 3754
504075 meter/sec RA = 25
11846 deg
ZDOT = 740
841760 TA = 187
30283
MA = 187
32090
Ha = 220
950 n
mi
Hp = 216
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8281760
38 X = 2588023
66
Y = -11215044
34 feet Y = -3389760
31 meter
Z = -17362518
43 Z = -5279679
26
XDOT = 21765
773279 XDOT = 6588
132148
YDOT = 12317
926756 feet/sec YDOT = 3828
434705 meter/sec
ZDOT = 2430
583202 ZDOT = 772
956413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13794563
14 X = 4204582
85
Y = 2456508
58 feet Y = 748743
82 meter
Z = -17305993
59 Z = -5274866
85
XDOT = -1042
538873 XDOT = -317
765848
YDOT = 23959
355516 feet/sec YDOT = 7302
811561 meter/sec
ZDOT = 2575
016318 ZDOT = 784
864974
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 19018
51475110
00016717 00000-0 10270-3 0 9022
2 25544 51
6396 25
6635 0002563 305
6792 54
4122 15
53747440 31997
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
51475110 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 25
6635 deg
Eccentricity:
0002563
Arg of perigee: 305
6792 deg
Mean anomaly: 54
4122 deg
Mean motion: 15
53747440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3199
Checksum: 303
Coasting Arc #4 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/018/18:09:19
397
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1978558
02 A = 6780171
19 meter
Y = -3711730
04 meter E =
0010235
Z = -5326608
92 I = 51
77910
XDOT = 6910
970304 Wp = 86
86763
YDOT = 3291
298565 meter/sec RA = 23
84693 deg
ZDOT = 274
597325 TA = 185
74194
MA = 185
75368
Ha = 220
953 n
mi
Hp = 217
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6491332
10 X = 2045790
00
Y = -12177592
01 feet Y = -3689227
96 meter
Z = -17475751
06 Z = -5316835
03
XDOT = 22673
787086 XDOT = 6872
318617
YDOT = 10798
223637 feet/sec YDOT = 3368
365702 meter/sec
ZDOT = 900
909858 ZDOT = 308
074324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -199542
08 X = -60820
43
Y = -13854585
28 feet Y = -4222877
59 meter
Z = -17431111
96 Z = -5313002
93
XDOT = 24041
390062 XDOT = 7327
815691
YDOT = -1665
131537 feet/sec YDOT = -507
532093 meter/sec
ZDOT = 1051
556221 ZDOT = 320
514336
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 19018
77202277
00016717 00000-0 10270-3 0 9033
2 25544 51
6413 24
3813 0004715 283
8226 76
2402 15
53173002 32037
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
77202277 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 24
3813 deg
Eccentricity:
0004715
Arg of perigee: 283
8226 deg
Mean anomaly: 76
2402 deg
Mean motion: 15
53173002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 274
Coasting Arc #5 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2019/019/18:09:19
397
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3248389
28 A = 6781230
78 meter
Y = 3116075
65 meter E =
0004617
Z = 5073166
47 I = 51
75182
XDOT = -6443
067076 Wp = 358
62420
YDOT = -3727
559557 meter/sec RA = 18
86718 deg
ZDOT = -1831
508506 TA = 109
11272
MA = 109
06272
Ha = 221
063 n
mi
Hp = 217
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10657445
15 X = -3307634
90
Y = 10223345
31 feet Y = 3079418
10 meter
Z = 16644246
93 Z = 5057243
71
XDOT = -21138
671510 XDOT = -6392
009300
YDOT = -12229
526105 feet/sec YDOT = -3799
324743 meter/sec
ZDOT = -6008
886175 ZDOT = -1862
682372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4140353
73 X = -1261979
82
Y = 14260340
16 feet Y = 4346551
68 meter
Z = 16571935
67 Z = 5051125
99
XDOT = -23346
458776 XDOT = -7116
000635
YDOT = 384
535787 feet/sec YDOT = 117
206508 meter/sec
ZDOT = -6149
072281 ZDOT = -1874
237231
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 19019
80149532
00016717 00000-0 10270-3 0 9043
2 25544 51
6411 19
2573 0004922 287
4621 72
5993 15
53196396 32192
Satellite: ISS
Catalog Number: 25544
Epoch time: 19019
80149532 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 19
2573 deg
Eccentricity:
0004922
Arg of perigee: 287
4621 deg
Mean anomaly: 72
5993 deg
Mean motion: 15
53196396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 319
Coasting Arc #6 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2019/020/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2285744
68 A = 6783215
62 meter
Y = 4475627
68 meter E =
0004069
Z = 4554297
71 I = 51
74656
XDOT = -6992
641574 Wp = 125
98679
YDOT = 392
714656 meter/sec RA = 17
34351 deg
ZDOT = 3119
305226 TA = 292
78681
MA = 292
82980
Ha = 220
846 n
mi
Hp = 217
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7499162
35 X = 2213405
25
Y = 14683817
84 feet Y = 4500783
52 meter
Z = 14941921
63 Z = 4565225
56
XDOT = -22941
737447 XDOT = -7011
664881
YDOT = 1288
433910 feet/sec YDOT = 314
411380 meter/sec
ZDOT = 10233
941031 ZDOT = 3085
292070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2851658
15 X = 869185
40
Y = -16194518
89 feet Y = -4936089
36 meter
Z = 14990616
00 Z = 4569139
76
XDOT = 18031
710932 XDOT = 5496
065492
YDOT = 12519
111854 feet/sec YDOT = 3815
825293 meter/sec
ZDOT = 10080
358139 ZDOT = 3072
493161
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 19020
12320502
00016717 00000-0 10270-3 0 9059
2 25544 51
6390 17
6499 0004748 282
6444 77
4177 15
53188799 32245
Satellite: ISS
Catalog Number: 25544
Epoch time: 19020
12320502 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 17
6499 deg
Eccentricity:
0004748
Arg of perigee: 282
6444 deg
Mean anomaly: 77
4177 deg
Mean motion: 15
53188799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3224
Checksum: 318
Coasting Arc #7 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2019/021/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -974766
93 A = 6780980
25 meter
Y = -4350475
27 meter E =
0009853
Z = -5118019
02 I = 51
70775
XDOT = 7470
212749 Wp = 63
73077
YDOT = 289
855178 meter/sec RA = 12
36439 deg
ZDOT = -1667
379965 TA = 190
15669
MA = 190
17661
Ha = 221
082 n
mi
Hp = 217
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3198054
23 X = -901186
37
Y = -14273212
82 feet Y = -4360963
93 meter
Z = -16791400
98 Z = -5122575
62
XDOT = 24508
572011 XDOT = 7474
515316
YDOT = 950
968431 feet/sec YDOT = 373
416501 meter/sec
ZDOT = -5470
406708 ZDOT = -1631
082888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5833824
47 X = -1778149
70
Y = 13388357
39 feet Y = 4080771
33 meter
Z = -16811355
70 Z = -5124101
22
XDOT = -18389
930186 XDOT = -5605
250721
YDOT = -14683
826134 feet/sec YDOT = -4475
630206 meter/sec
ZDOT = -5306
613238 ZDOT = -1617
455715
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 19021
08833466
00016717 00000-0 10270-3 0 9064
2 25544 51
6398 12
8465 0004558 288
3080 71
7576 15
53181749 32395
Satellite: ISS
Catalog Number: 25544
Epoch time: 19021
08833466 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 12
8465 deg
Eccentricity:
0004558
Arg of perigee: 288
3080 deg
Mean anomaly: 71
7576 deg
Mean motion: 15
53181749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 333
Coasting Arc #8 (Orbit 3254)
---------------------------------------
Vector Time (GMT): 2019/022/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -424945
77 A = 6780180
84 meter
Y = 4185071
52 meter E =
0002454
Z = 5319052
14 I = 51
67177
XDOT = -7611
937905 Wp = 310
62996
YDOT = -902
852786 meter/sec RA = 7
37786 deg
ZDOT = 103
837031 TA = 138
39002
MA = 138
37135
Ha = 221
261 n
mi
Hp = 217
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1394179
02 X = -497549
10
Y = 13730549
62 feet Y = 4179913
22 meter
Z = 17450958
46 Z = 5316811
88
XDOT = -24973
549556 XDOT = -7601
780591
YDOT = -2962
115438 feet/sec YDOT = -987
917991 meter/sec
ZDOT = 340
672675 ZDOT = 66
886750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9069716
06 X = 2764449
46
Y = -10420423
24 feet Y = -3176145
00 meter
Z = 17440261
15 Z = 5315791
60
XDOT = 18070
466854 XDOT = 5507
878297
YDOT = 16010
653977 feet/sec YDOT = 4880
047332 meter/sec
ZDOT = 174
021353 ZDOT = 53
041708
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 19022
11780521
00016717 00000-0 10270-3 0 9073
2 25544 51
6395 7
7210 0004594 292
1610 67
9054 15
53156728 32550
Satellite: ISS
Catalog Number: 25544
Epoch time: 19022
11780521 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 7
7210 deg
Eccentricity:
0004594
Arg of perigee: 292
1610 deg
Mean anomaly: 67
9054 deg
Mean motion: 15
53156728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3255
Checksum: 297
Coasting Arc #9 (Orbit 3269)
---------------------------------------
Vector Time (GMT): 2019/023/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1821100
78 A = 6780859
80 meter
Y = -4012699
15 meter E =
0009261
Z = -5161964
38 I = 51
64196
XDOT = 7374
554658 Wp = 94
38664
YDOT = 1466
758728 meter/sec RA = 2
39070 deg
ZDOT = 1463
060633 TA = 189
70209
MA = 189
71999
Ha = 221
272 n
mi
Hp = 217
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5974740
11 X = 1890909
80
Y = -13165023
47 feet Y = -3991943
87 meter
Z = -16935578
66 Z = -5152948
96
XDOT = 24194
733129 XDOT = 7350
498332
YDOT = 4812
200550 feet/sec YDOT = 1549
091591 meter/sec
ZDOT = 4800
067695 ZDOT = 1498
824040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12379426
70 X = -3773249
26
Y = 7560458
42 feet Y = 2304427
73 meter
Z = -16894331
90 Z = -5149392
36
XDOT = -16858
437023 XDOT = -5138
451605
YDOT = -16529
123046 feet/sec YDOT = -5038
076704 meter/sec
ZDOT = 4961
276550 ZDOT = 1512
197092
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 19023
08293147
00016717 00000-0 10270-3 0 9084
2 25544 51
6404 2
9178 0004607 294
8562 65
2111 15
53184421 32704
Satellite: ISS
Catalog Number: 25544
Epoch time: 19023
08293147 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 2
9178 deg
Eccentricity:
0004607
Arg of perigee: 294
8562 deg
Mean anomaly: 65
2111 deg
Mean motion: 15
53184421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3270
Checksum: 292
Coasting Arc #10 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2019/024/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3150442
00 A = 6783160
48 meter
Y = 3819207
29 meter E =
0006795
Z = 4636405
98 I = 51
61699
XDOT = -6785
887148 Wp = 32
36460
YDOT = -2021
787287 meter/sec RA = 357
40294 deg
ZDOT = -2937
973284 TA = 86
94338
MA = 86
86562
Ha = 221
540 n
mi
Hp = 217
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10336095
79 X = -3215435
79
Y = 12530207
65 feet Y = 3783613
45 meter
Z = 15211305
70 Z = 4620944
86
XDOT = -22263
409277 XDOT = -6748
503951
YDOT = -6633
160391 feet/sec YDOT = -2097
462786 meter/sec
ZDOT = -9639
019959 ZDOT = -2970
844916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15560537
55 X = 4742851
85
Y = -4883081
57 feet Y = -1488363
26 meter
Z = 15141003
48 Z = 4614977
86
XDOT = 14713
898261 XDOT = 4484
796190
YDOT = 16462
963740 feet/sec YDOT = 5017
911348 meter/sec
ZDOT = -9787
092206 ZDOT = -2983
105704
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 19024
11239907
00016717 00000-0 10270-3 0 9094
2 25544 51
6414 357
7926 0004532 299
4380 60
6320 15
53147594 32861
Satellite: ISS
Catalog Number: 25544
Epoch time: 19024
11239907 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 357
7926 deg
Eccentricity:
0004532
Arg of perigee: 299
4380 deg
Mean anomaly: 60
6320 deg
Mean motion: 15
53147594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3286
Checksum: 319
Coasting Arc #11 (Orbit 3300)
---------------------------------------
Vector Time (GMT): 2019/025/01:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4304438
54 A = 6786108
65 meter
Y = -3614334
00 meter E =
0002287
Z = -3803120
75 I = 51
59378
XDOT = 5870
603806 Wp = 55
46796
YDOT = 2576
745583 meter/sec RA = 352
42046 deg
ZDOT = 4198
684391 TA = 258
87733
MA = 258
90305
Ha = 221
641 n
mi
Hp = 217
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14122173
67 X = 4363008
16
Y = -11858051
18 feet Y = -3565871
34 meter
Z = -12477430
28 Z = -3782069
56
XDOT = 19260
511175 XDOT = 5820
959180
YDOT = 8453
889709 feet/sec YDOT = 2642
117253 meter/sec
ZDOT = 13775
211256 ZDOT = 4227
080330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18322080
29 X = -5584570
07
Y = 2593140
21 feet Y = 790389
14 meter
Z = -12381939
71 Z = -3774015
22
XDOT = -11646
184802 XDOT = -3549
757128
YDOT = -15950
480357 feet/sec YDOT = -4861
706413 meter/sec
ZDOT = 13903
000337 ZDOT = 4237
634503
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 19025
07752164
00016717 00000-0 10270-3 0 9107
2 25544 51
6413 352
9894 0004705 303
7276 56
3427 15
53161635 33016
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
07752164 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 352
9894 deg
Eccentricity:
0004705
Arg of perigee: 303
7276 deg
Mean anomaly: 56
3427 deg
Mean motion: 15
53161635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3301
Checksum: 297
Coasting Arc #12 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2019/025/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4234021
70 A = 6783463
40 meter
Y = 2856288
50 meter E =
0004538
Z = 4460476
23 I = 51
56885
XDOT = -5902
038149 Wp = 92
12918
YDOT = 3652
147403 meter/sec RA = 350
13778 deg
ZDOT = 3260
690920 TA = 324
98093
MA = 325
01077
Ha = 221
596 n
mi
Hp = 217
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13891147
31 X = 4180101
12
Y = 9371025
26 feet Y = 2903334
88 meter
Z = 14634108
37 Z = 4480912
09
XDOT = -19363
642221 XDOT = -5958
277145
YDOT = 11982
110902 feet/sec YDOT = 3585
832305 meter/sec
ZDOT = 10697
804856 ZDOT = 3231
884958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3812558
50 X = 1162067
83
Y = 16234174
73 feet Y = 4948176
46 meter
Z = 14725935
77 Z = 4488465
22
XDOT = -21233
791807 XDOT = -6472
059743
YDOT = -4607
830525 feet/sec YDOT = -1404
466744 meter/sec
ZDOT = 10567
321129 ZDOT = 3220
919480
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 19025
59225264
00016717 00000-0 10270-3 0 9111
2 25544 51
6399 350
4307 0004941 309
3121 50
7592 15
53208604 33091
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
59225264 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 350
4307 deg
Eccentricity:
0004941
Arg of perigee: 309
3121 deg
Mean anomaly: 50
7592 deg
Mean motion: 15
53208604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 296
Coasting Arc #13 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2019/026/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4747806
62 A = 6784316
52 meter
Y = 2300997
63 meter E =
0005898
Z = 4259667
79 I = 51
54308
XDOT = -5280
110983 Wp = 85
57063
YDOT = 4252
914730 meter/sec RA = 345
97425 deg
ZDOT = 3584
000312 TA = 327
77005
MA = 327
80607
Ha = 221
785 n
mi
Hp = 217
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15576793
38 X = 4701032
61
Y = 7549204
83 feet Y = 2353829
46 meter
Z = 13975288
03 Z = 4282616
82
XDOT = -17323
198764 XDOT = -5344
684634
YDOT = 13953
132316 feet/sec YDOT = 4193
507852 meter/sec
ZDOT = 11758
531206 ZDOT = 3558
195046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10339298
91 X = -3151418
31
Y = 13777868
76 feet Y = 4199494
40 meter
Z = 14078525
91 Z = 4291134
70
XDOT = -9410
528999 XDOT = -2868
329239
YDOT = -18970
252286 feet/sec YDOT = -5782
132897 meter/sec
ZDOT = 11641
517138 ZDOT = 3548
334424
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 19026
42869263
00016717 00000-0 10270-3 0 9128
2 25544 51
6389 346
2668 0004836 313
6018 46
4732 15
53167840 33228
Satellite: ISS
Catalog Number: 25544
Epoch time: 19026
42869263 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 346
2668 deg
Eccentricity:
0004836
Arg of perigee: 313
6018 deg
Mean anomaly: 46
4732 deg
Mean motion: 15
53167840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3322
Checksum: 320
Coasting Arc #14 (Orbit 3336)
---------------------------------------
Vector Time (GMT): 2019/027/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3633148
95 A = 6781659
16 meter
Y = -2906795
17 meter E =
0011229
Z = -4943722
96 I = 51
50268
XDOT = 6168
901778 Wp = 51
32632
YDOT = -3972
355793 meter/sec RA = 340
98224 deg
ZDOT = -2194
389200 TA = 197
17842
MA = 197
21645
Ha = 222
024 n
mi
Hp = 217
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11919780
03 X = -3576360
81
Y = -9536729
55 feet Y = -2947106
08 meter
Z = -16219563
52 Z = -4961233
24
XDOT = 20239
179063 XDOT = 6223
522271
YDOT = -13032
663364 feet/sec YDOT = -3903
065445 meter/sec
ZDOT = -7199
439633 ZDOT = -2164
290724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11427259
77 X = 3483028
78
Y = -9994590
78 feet Y = -3046351
27 meter
Z = -16298174
63 Z = -4967683
63
XDOT = 8620
781678 XDOT = 2627
614255
YDOT = 21392
915571 feet/sec YDOT = 6520
560666 meter/sec
ZDOT = -7063
104898 ZDOT = -2152
834373
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 19027
39381261
00016717 00000-0 10270-3 0 9133
2 25544 51
6393 341
4628 0004752 318
4334 41
6456 15
53179431 33372
Satellite: ISS
Catalog Number: 25544
Epoch time: 19027
39381261 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 341
4628 deg
Eccentricity:
0004752
Arg of perigee: 318
4334 deg
Mean anomaly: 41
6456 deg
Mean motion: 15
53179431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3337
Checksum: 309
Coasting Arc #15 (Orbit 3352)
---------------------------------------
Vector Time (GMT): 2019/028/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2383124
70 A = 6780253
14 meter
Y = 3535042
89 meter E =
0002683
Z = 5272301
52 I = 51
46561
XDOT = -6749
524310 Wp = 351
08240
YDOT = 3578
082722 meter/sec RA = 335
98283 deg
ZDOT = 654
404272 TA = 92
66889
MA = 92
63817
Ha = 222
119 n
mi
Hp = 217
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7818650
58 X = 2317808
15
Y = 11597909
74 feet Y = 3561327
40 meter
Z = 17297577
16 Z = 5283719
08
XDOT = -22144
108627 XDOT = -6792
212495
YDOT = 11739
116543 feet/sec YDOT = 3502
366147 meter/sec
ZDOT = 2146
995642 ZDOT = 621
514376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12653084
43 X = -3856660
13
Y = 5811544
91 feet Y = 1771358
89 meter
Z = 17348613
29 Z = 5287857
33
XDOT = -7738
407726 XDOT = -2358
666675
YDOT = -22787
322147 feet/sec YDOT = -6945
575790 meter/sec
ZDOT = 1998
131401 ZDOT = 609
030451
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 19028
42327195
00016717 00000-0 10270-3 0 9145
2 25544 51
6381 336
3379 0004915 321
8957 38
1847 15
53173158 33538
Satellite: ISS
Catalog Number: 25544
Epoch time: 19028
42327195 = yrday
fracday
Element set: 914
Inclination: 51
6381 deg
RA of node: 336
3379 deg
Eccentricity:
0004915
Arg of perigee: 321
8957 deg
Mean anomaly: 38
1847 deg
Mean motion: 15
53173158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3353
Checksum: 327
Coasting Arc #16 (Orbit 3367)
---------------------------------------
Vector Time (GMT): 2019/029/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1114107
47 A = 6780473
37 meter
Y = -4163222
13 meter E =
0011671
Z = -5244229
64 I = 51
43607
XDOT = 6974
613726 Wp = 78
70392
YDOT = -3026
167249 meter/sec RA = 330
98054 deg
ZDOT = 924
647847 TA = 200
15516
MA = 200
20128
Ha = 222
282 n
mi
Hp = 217
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3655208
23 X = -1041997
13
Y = -13658865
27 feet Y = -4175277
55 meter
Z = -17205477
83 Z = -5249466
44
XDOT = 22882
590964 XDOT = 7003
443450
YDOT = -9928
370241 feet/sec YDOT = -2948
011080 meter/sec
ZDOT = 3033
621545 ZDOT = 958
597417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14017958
66 X = 4272673
80
Y = -1620994
17 feet Y = -494079
02 meter
Z = -17228546
89 Z = -5251261
09
XDOT = 6559
699280 XDOT = 1999
396340
YDOT = 22991
037079 feet/sec YDOT = 7007
668102 meter/sec
ZDOT = 3187
182773 ZDOT = 971
453309
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 19029
38838906
00016717 00000-0 10270-3 0 9159
2 25544 51
6379 331
5341 0004937 325
5591 34
5241 15
53164858 33681
Satellite: ISS
Catalog Number: 25544
Epoch time: 19029
38838906 = yrday
fracday
Element set: 915
Inclination: 51
6379 deg
RA of node: 331
5341 deg
Eccentricity:
0004937
Arg of perigee: 325
5591 deg
Mean anomaly: 34
5241 deg
Mean motion: 15
53164858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 334
Coasting Arc #17 (Orbit 3383)
---------------------------------------
Vector Time (GMT): 2019/030/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -146188
84 A = 6782154
52 meter
Y = 4753566
98 meter E =
0008632
Z = 4835250
74 I = 51
41365
XDOT = -6892
368501 Wp = 24
30152
YDOT = 2292
005195 meter/sec RA = 325
97745 deg
ZDOT = -2452
387153 TA = 89
90515
MA = 89
80624
Ha = 222
391 n
mi
Hp = 216
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -479622
18 X = -222820
31
Y = 15595692
20 feet Y = 4751503
56 meter
Z = 15863683
51 Z = 4834354
65
XDOT = -22612
757548 XDOT = -6905
573943
YDOT = 7519
702084 feet/sec YDOT = 2214
856171 meter/sec
ZDOT = -8045
889611 ZDOT = -2485
899188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15411473
87 X = -4697417
24
Y = -2467861
59 feet Y = -752204
21 meter
Z = 15859011
30 Z = 4833826
65
XDOT = -4915
285966 XDOT = -1498
179162
YDOT = -22178
513151 feet/sec YDOT = -6760
010808 meter/sec
ZDOT = -8197
371613 ZDOT = -2498
558868
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 19030
41784478
00016717 00000-0 10270-3 0 9160
2 25544 51
6382 326
4091 0005020 328
8231 31
2623 15
53191696 33847
Satellite: ISS
Catalog Number: 25544
Epoch time: 19030
41784478 = yrday
fracday
Element set: 916
Inclination: 51
6382 deg
RA of node: 326
4091 deg
Eccentricity:
0005020
Arg of perigee: 328
8231 deg
Mean anomaly: 31
2623 deg
Mean motion: 15
53191696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3384
Checksum: 301
Coasting Arc #18 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2019/031/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1274493
96 A = 6785004
56 meter
Y = -5251619
09 meter E =
0005214
Z = -4105245
15 I = 51
39652
XDOT = 6513
452257 Wp = 64
69830
YDOT = -1380
097777 meter/sec RA = 320
97830 deg
ZDOT = 3793
586232 TA = 244
58215
MA = 244
63613
Ha = 222
580 n
mi
Hp = 216
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4181410
64 X = 1353064
96
Y = -17229721
41 feet Y = -5236927
33 meter
Z = -13468652
08 Z = -4098863
63
XDOT = 21369
594020 XDOT = 6509
974010
YDOT = -4527
879845 feet/sec YDOT = -1307
279413 meter/sec
ZDOT = 12446
149054 ZDOT = 3825
217067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16693855
34 X = 5088287
11
Y = 6037866
61 feet Y = 1840341
74 meter
Z = -13439175
74 Z = -4096260
77
XDOT = 2731
963582 XDOT = 832
702500
YDOT = 20423
660573 feet/sec YDOT = 6225
131743 meter/sec
ZDOT = 12589
018968 ZDOT = 3837
132981
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 19031
38295734
00016717 00000-0 10270-3 0 9170
2 25544 51
6387 321
6050 0005104 333
7895 26
2998 15
53172272 33992
Satellite: ISS
Catalog Number: 25544
Epoch time: 19031
38295734 = yrday
fracday
Element set: 917
Inclination: 51
6387 deg
RA of node: 321
6050 deg
Eccentricity:
0005104
Arg of perigee: 333
7895 deg
Mean anomaly: 26
2998 deg
Mean motion: 15
53172272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 326
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