[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 22nd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
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
033/17:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 216
5
Coasting Arc #1 (Orbit 3245)
---------------------------------------
Vector Time (GMT): 2019/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5776207
29 A = 6787824
50 meter
Y = 1536952
93 meter E =
0008526
Z = 3210827
32 I = 51
71479
XDOT = -3883
546342 Wp = 82
10909
YDOT = -4546
037243 meter/sec RA = 10
18807 deg
ZDOT = -4798
271818 TA = 60
81428
MA = 60
72901
Ha = 221
293 n
mi
Hp = 217
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18950811
32 X = -5808560
63
Y = 5042496
50 feet Y = 1472178
22 meter
Z = 10534210
37 Z = 3182690
95
XDOT = -12741
293773 XDOT = -3809
115927
YDOT = -14914
820352 feet/sec YDOT = -4589
049234 meter/sec
ZDOT = -15742
361609 ZDOT = -4816
955703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13800187
30 X = -4206297
09
Y = -14027788
91 feet Y = -4275670
06 meter
Z = 10406996
56 Z = 3172052
55
XDOT = 5678
974544 XDOT = 1730
951441
YDOT = -17357
631686 feet/sec YDOT = -5290
606138 meter/sec
ZDOT = -15826
055497 ZDOT = -4823
781716
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
53873460
00016717 00000-0 10270-3 0 9006
2 25544 51
6382 10
6069 0004825 294
9592 65
1058 15
53181150 32468
Satellite: ISS
Catalog Number: 25544
Epoch time: 19021
53873460 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 10
6069 deg
Eccentricity:
0004825
Arg of perigee: 294
9592 deg
Mean anomaly: 65
1058 deg
Mean motion: 15
53181150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3246
Checksum: 298
Coasting Arc #2 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2019/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6405229
77 A = 6790496
83 meter
Y = -1003881
92 meter E =
0007459
Z = -2003281
55 I = 51
69050
XDOT = 2469
557420 Wp = 1
62535
YDOT = 4648
106155 meter/sec RA = 5
22153 deg
ZDOT = 5574
621579 TA = 336
27458
MA = 336
30896
Ha = 221
465 n
mi
Hp = 217
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21014533
38 X = 6425709
97
Y = -3293575
84 feet Y = -932139
57 meter
Z = -6572446
02 Z = -1972118
54
XDOT = 8102
222508 XDOT = 2390
319816
YDOT = 15249
692108 feet/sec YDOT = 4675
279173 meter/sec
ZDOT = 18289
440877 ZDOT = 5586
425177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13573940
96 X = 4137337
20
Y = 16432811
01 feet Y = 5008720
80 meter
Z = -6431652
24 Z = -1960367
60
XDOT = -7849
692572 XDOT = -2392
586296
YDOT = 13652
752947 feet/sec YDOT = 4161
359098 meter/sec
ZDOT = 18342
067676 ZDOT = 5590
662228
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
50386641
00016717 00000-0 10270-3 0 9015
2 25544 51
6380 5
8033 0004651 297
9214 62
1467 15
53166513 32618
Satellite: ISS
Catalog Number: 25544
Epoch time: 19022
50386641 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 5
8033 deg
Eccentricity:
0004651
Arg of perigee: 297
9214 deg
Mean anomaly: 62
1467 deg
Mean motion: 15
53166513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 287
Coasting Arc #3 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2019/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6740883
18 A = 6791940
58 meter
Y = 475018
73 meter E =
0008282
Z = 638837
78 I = 51
66344
XDOT = -902
814049 Wp = 131
56019
YDOT = -4724
186316 meter/sec RA =
25645 deg
ZDOT = -5968
845685 TA = 41
54838
MA = 41
48547
Ha = 221
519 n
mi
Hp = 217
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22115758
47 X = -6748797
02
Y = 1558460
40 feet Y = 399593
22 meter
Z = 2095924
48 Z = 606074
80
XDOT = -2961
988350 XDOT = -820
927244
YDOT = -15499
298938 feet/sec YDOT = -4733
824273 meter/sec
ZDOT = -19582
827049 ZDOT = -5973
032277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12939494
41 X = -3943957
90
Y = -18019525
00 feet Y = -5492351
22 meter
Z = 1947992
30 Z = 593748
05
XDOT = 10395
235767 XDOT = 3168
467862
YDOT = -9600
656741 feet/sec YDOT = -2926
280175 meter/sec
ZDOT = -19601
068427 ZDOT = -5974
405657
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
53333781
00016717 00000-0 10270-3 0 9027
2 25544 51
6391
6780 0004834 302
8928 57
1759 15
53178894 32773
Satellite: ISS
Catalog Number: 25544
Epoch time: 19023
53333781 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node:
6780 deg
Eccentricity:
0004834
Arg of perigee: 302
8928 deg
Mean anomaly: 57
1759 deg
Mean motion: 15
53178894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 324
Coasting Arc #4 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2019/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6742089
69 A = 6791763
92 meter
Y = 41384
64 meter E =
0012644
Z = 751064
32 I = 51
63001
XDOT = -696
458487 Wp = 32
18478
YDOT = 4786
140576 meter/sec RA = 355
29178 deg
ZDOT = 5952
506173 TA = 335
93318
MA = 335
99221
Ha = 221
544 n
mi
Hp = 217
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22119716
83 X = 6737477
67
Y = 135776
38 feet Y = 116753
61 meter
Z = 2464121
77 Z = 783802
85
XDOT = -2284
968791 XDOT = -778
839951
YDOT = 15702
560945 feet/sec YDOT = 4777
891719 meter/sec
ZDOT = 19529
219729 ZDOT = 5948
922998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11806262
34 X = 3598548
76
Y = 18685891
88 feet Y = 5695459
85 meter
Z = 2611860
99 Z = 796095
23
XDOT = -13164
296634 XDOT = -4012
477614
YDOT = 5574
742324 feet/sec YDOT = 1699
181460 meter/sec
ZDOT = 19512
392587 ZDOT = 5947
377260
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
56280591
00016717 00000-0 10270-3 0 9032
2 25544 51
6393 355
5540 0004754 305
1801 54
8906 15
53200446 32933
Satellite: ISS
Catalog Number: 25544
Epoch time: 19024
56280591 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 355
5540 deg
Eccentricity:
0004754
Arg of perigee: 305
1801 deg
Mean anomaly: 54
8906 deg
Mean motion: 15
53200446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 299
Coasting Arc #5 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2019/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6426529
19 A = 6790145
48 meter
Y = -598293
68 meter E =
0001528
Z = -2106509
77 I = 51
59150
XDOT = 2255
230244 Wp = 161
25523
YDOT = -4819
352418 meter/sec RA = 350
32237 deg
ZDOT = -5513
974168 TA = 42
06990
MA = 42
05817
Ha = 221
814 n
mi
Hp = 217
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21084413
35 X = -6409129
23
Y = -1962905
77 feet Y = -670062
36 meter
Z = -6911121
30 Z = -2137684
53
XDOT = 7399
049356 XDOT = 2335
737262
YDOT = -15811
523681 feet/sec YDOT = -4793
682818 meter/sec
ZDOT = -18090
466430 ZDOT = -5502
823710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10014511
70 X = -3052423
17
Y = -18605159
08 feet Y = -5670852
49 meter
Z = -7051715
69 Z = -2149362
94
XDOT = 15974
453001 XDOT = 4869
013275
YDOT = -1764
257501 feet/sec YDOT = -537
745686 meter/sec
ZDOT = -18039
493456 ZDOT = -5498
437605
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
52793381
00016717 00000-0 10270-3 0 9046
2 25544 51
6393 350
7498 0004927 311
0289 49
0437 15
53174380 33089
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
52793381 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 350
7498 deg
Eccentricity:
0004927
Arg of perigee: 311
0289 deg
Mean anomaly: 49
0437 deg
Mean motion: 15
53174380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 319
Coasting Arc #6 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2019/025/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4245062
01 A = 6783501
75 meter
Y = 2849427
97 meter E =
0004560
Z = 4454406
01 I = 51
56893
XDOT = -5891
891861 Wp = 92
00464
YDOT = 3659
005043 meter/sec RA = 350
13715 deg
ZDOT = 3271
316950 TA = 324
98465
MA = 325
01462
Ha = 221
601 n
mi
Hp = 217
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13927368
82 X = 4191246
82
Y = 9348516
98 feet Y = 2896598
40 meter
Z = 14614192
93 Z = 4474895
75
XDOT = -19330
353874 XDOT = -5948
259909
YDOT = 12004
609722 feet/sec YDOT = 3592
802687 meter/sec
ZDOT = 10732
667159 ZDOT = 3242
559961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3854556
29 X = 1174868
76
Y = 16242203
96 feet Y = 4950623
77 meter
Z = 14706264
42 Z = 4482469
40
XDOT = -21224
097644 XDOT = -6469
104962
YDOT = -4571
957829 feet/sec YDOT = -1393
532746 meter/sec
ZDOT = 10602
403486 ZDOT = 3231
612583
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
59227437
00016717 00000-0 10270-3 0 9058
2 25544 51
6399 350
4300 0004949 309
2210 50
8502 15
53203285 33092
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
59227437 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 350
4300 deg
Eccentricity:
0004949
Arg of perigee: 309
2210 deg
Mean anomaly: 50
8502 deg
Mean motion: 15
53203285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 294
Coasting Arc #7 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2019/026/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4758958
72 A = 6784358
67 meter
Y = 2291978
16 meter E =
0005923
Z = 4252122
05 I = 51
54318
XDOT = -5267
260160 Wp = 85
41513
YDOT = 4259
150833 meter/sec RA = 345
97365 deg
ZDOT = 3595
471471 TA = 327
78897
MA = 327
82514
Ha = 221
790 n
mi
Hp = 217
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15613381
62 X = 4712321
38
Y = 7519613
40 feet Y = 2344935
46 meter
Z = 13950531
67 Z = 4275125
59
XDOT = -17281
037270 XDOT = -5331
960219
YDOT = 13973
591973 feet/sec YDOT = 4199
886956 meter/sec
ZDOT = 11796
166244 ZDOT = 3569
728321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10317181
95 X = -3144677
06
Y = 13819550
51 feet Y = 4212199
00 meter
Z = 14054016
70 Z = 4283664
29
XDOT = -9435
500839 XDOT = -2875
940656
YDOT = -18934
576424 feet/sec YDOT = -5771
258894 meter/sec
ZDOT = 11679
431611 ZDOT = 3559
890755
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
42871717
00016717 00000-0 10270-3 0 9068
2 25544 51
6389 346
2662 0004845 313
4971 46
5778 15
53162712 33222
Satellite: ISS
Catalog Number: 25544
Epoch time: 19026
42871717 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 346
2662 deg
Eccentricity:
0004845
Arg of perigee: 313
4971 deg
Mean anomaly: 46
5778 deg
Mean motion: 15
53162712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3322
Checksum: 324
Coasting Arc #8 (Orbit 3336)
---------------------------------------
Vector Time (GMT): 2019/027/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3647988
43 A = 6781696
05 meter
Y = -2897202
70 meter E =
0011197
Z = -4938442
49 I = 51
50276
XDOT = 6157
743716 Wp = 51
12291
YDOT = -3981
287913 meter/sec RA = 340
98174 deg
ZDOT = -2209
506474 TA = 197
22649
MA = 197
26452
Ha = 222
030 n
mi
Hp = 217
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11968465
97 X = -3591332
09
Y = -9505258
20 feet Y = -2937680
30 meter
Z = -16202239
12 Z = -4956025
17
XDOT = 20202
571246 XDOT = 6212
538350
YDOT = -13061
968220 feet/sec YDOT = -3912
121368 meter/sec
ZDOT = -7249
036989 ZDOT = -2179
461776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11404649
95 X = 3476137
31
Y = -10048077
41 feet Y = -3062653
99 meter
Z = -16281178
20 Z = -4962503
12
XDOT = 8651
992388 XDOT = 2637
127280
YDOT = 21363
870393 feet/sec YDOT = 6511
707696 meter/sec
ZDOT = -7112
943687 ZDOT = -2168
025236
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
39384042
00016717 00000-0 10270-3 0 9076
2 25544 51
6393 341
4622 0004761 318
3350 41
7439 15
53174230 33377
Satellite: ISS
Catalog Number: 25544
Epoch time: 19027
39384042 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 341
4622 deg
Eccentricity:
0004761
Arg of perigee: 318
3350 deg
Mean anomaly: 41
7439 deg
Mean motion: 15
53174230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3337
Checksum: 297
Coasting Arc #9 (Orbit 3352)
---------------------------------------
Vector Time (GMT): 2019/028/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2401356
55 A = 6780276
43 meter
Y = 3525364
28 meter E =
0002650
Z = 5270532
25 I = 51
46564
XDOT = -6741
242637 Wp = 351
04834
YDOT = 3590
290743 meter/sec RA = 335
98242 deg
ZDOT = 672
571132 TA = 92
52813
MA = 92
49780
Ha = 222
125 n
mi
Hp = 217
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7878466
38 X = 2336155
47
Y = 11566155
79 feet Y = 3551853
33 meter
Z = 17291772
48 Z = 5282038
66
XDOT = -22116
937784 XDOT = -6784
156194
YDOT = 11779
169104 feet/sec YDOT = 3514
665519 meter/sec
ZDOT = 2206
598201 ZDOT = 639
720918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12630993
02 X = -3849926
67
Y = 5875597
39 feet Y = 1790882
08 meter
Z = 17343210
72 Z = 5286210
63
XDOT = -7777
459912 XDOT = -2370
569781
YDOT = -22768
694805 feet/sec YDOT = -6939
898177 meter/sec
ZDOT = 2057
911346 ZDOT = 627
251378
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
42330330
00016717 00000-0 10270-3 0 9083
2 25544 51
6382 336
3374 0004923 321
8048 38
2754 15
53167714 33533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19028
42330330 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 336
3374 deg
Eccentricity:
0004923
Arg of perigee: 321
8048 deg
Mean anomaly: 38
2754 deg
Mean motion: 15
53167714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3353
Checksum: 300
Coasting Arc #10 (Orbit 3367)
---------------------------------------
Vector Time (GMT): 2019/029/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1135032
56 A = 6780476
27 meter
Y = -4154128
93 meter E =
0011690
Z = -5246974
49 I = 51
43604
XDOT = 6970
298335 Wp = 78
53821
YDOT = -3042
073669 meter/sec RA = 330
98019 deg
ZDOT = 904
633084 TA = 200
12713
MA = 200
17326
Ha = 222
288 n
mi
Hp = 217
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3723860
10 X = -1063009
01
Y = -13629031
92 feet Y = -4166418
83 meter
Z = -17214483
22 Z = -5252313
14
XDOT = 22868
432856 XDOT = 6999
403468
YDOT = -9980
556656 feet/sec YDOT = -2963
964216 meter/sec
ZDOT = 2967
956313 ZDOT = 938
562361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13997877
81 X = 4266553
16
Y = -1693045
25 feet Y = -516040
19 meter
Z = -17238013
00 Z = -5254146
36
XDOT = 6608
030285 XDOT = 2014
127631
YDOT = 22986
116782 feet/sec YDOT = 7006
168395 meter/sec
ZDOT = 3121
428112 ZDOT = 951
411289
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
38842373
00016717 00000-0 10270-3 0 9095
2 25544 51
6380 331
5336 0004945 325
4594 34
6236 15
53159496 33685
Satellite: ISS
Catalog Number: 25544
Epoch time: 19029
38842373 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 331
5336 deg
Eccentricity:
0004945
Arg of perigee: 325
4594 deg
Mean anomaly: 34
6236 deg
Mean motion: 15
53159496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 334
Coasting Arc #11 (Orbit 3383)
---------------------------------------
Vector Time (GMT): 2019/030/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -123421
31 A = 6782136
84 meter
Y = 4745998
73 meter E =
0008601
Z = 4843316
09 I = 51
41355
XDOT = -6892
891290 Wp = 23
89502
YDOT = 2312
033674 meter/sec RA = 325
97710 deg
ZDOT = -2431
994182 TA = 90
09804
MA = 89
99947
Ha = 222
398 n
mi
Hp = 216
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -404925
57 X = -200009
02
Y = 15570861
96 feet Y = 4744190
15 meter
Z = 15890144
64 Z = 4842530
70
XDOT = -22614
472735 XDOT = -6906
419713
YDOT = 7585
412315 feet/sec YDOT = 2234
876997 meter/sec
ZDOT = -7978
983538 ZDOT = -2465
509540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15395841
26 X = -4692652
42
Y = -2390887
48 feet Y = -728742
50 meter
Z = 15885972
82 Z = 4842044
51
XDOT = -4974
643897 XDOT = -1516
271460
YDOT = -22189
748143 feet/sec YDOT = -6763
435234 meter/sec
ZDOT = -8130
483185 ZDOT = -2478
171275
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
41788304
00016717 00000-0 10270-3 0 9106
2 25544 51
6383 326
4086 0005028 328
7275 31
3577 15
53186202 33843
Satellite: ISS
Catalog Number: 25544
Epoch time: 19030
41788304 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 326
4086 deg
Eccentricity:
0005028
Arg of perigee: 328
7275 deg
Mean anomaly: 31
3577 deg
Mean motion: 15
53186202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3384
Checksum: 303
Coasting Arc #12 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2019/031/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1250993
27 A = 6784972
66 meter
Y = -5246630
40 meter E =
0005241
Z = -4118865
27 I = 51
39638
XDOT = 6519
222554 Wp = 65
28008
YDOT = -1404
228509 meter/sec RA = 320
97790 deg
ZDOT = 3774
686746 TA = 243
76746
MA = 243
82134
Ha = 222
586 n
mi
Hp = 216
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4104308
63 X = 1329576
39
Y = -17213354
32 feet Y = -5232201
37 meter
Z = -13513337
52 Z = -4112597
88
XDOT = 21388
525440 XDOT = 6516
105516
YDOT = -4607
048913 feet/sec YDOT = -1331
343597 meter/sec
ZDOT = 12384
142868 ZDOT = 3806
346487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16685556
82 X = 5085757
72
Y = 5959780
75 feet Y = 1816541
17 meter
Z = -13484376
66 Z = -4110038
01
XDOT = 2803
005475 XDOT = 854
356069
YDOT = 20451
729705 feet/sec YDOT = 6233
687214 meter/sec
ZDOT = 12527
146342 ZDOT = 3818
274205
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
38299899
00016717 00000-0 10270-3 0 9110
2 25544 51
6388 321
6045 0005112 333
6906 26
3986 15
53166832 33991
Satellite: ISS
Catalog Number: 25544
Epoch time: 19031
38299899 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 321
6045 deg
Eccentricity:
0005112
Arg of perigee: 333
6906 deg
Mean anomaly: 26
3986 deg
Mean motion: 15
53166832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 335
Coasting Arc #13 (Orbit 3414)
---------------------------------------
Vector Time (GMT): 2019/032/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2258948
48 A = 6788062
37 meter
Y = 5607059
60 meter E =
0011461
Z = 3082791
77 I = 51
38141
XDOT = -5912
912106 Wp = 72
14836
YDOT = 304
916526 meter/sec RA = 315
98355 deg
ZDOT = -4868
922481 TA = 72
29810
MA = 72
17302
Ha = 222
675 n
mi
Hp = 216
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7411248
30 X = -2336454
48
Y = 18395864
84 feet Y = 5581364
98 meter
Z = 10114146
23 Z = 3071630
86
XDOT = -19399
317933 XDOT = -5892
232299
YDOT = 1000
382303 feet/sec YDOT = 238
910044 meter/sec
ZDOT = -15974
155120 ZDOT = -4897
594338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17678548
70 X = -5388421
64
Y = -9046207
47 feet Y = -2757284
04 meter
Z = 10063073
34 Z = 3067224
75
XDOT = 18
258171 XDOT = 5
565091
YDOT = -18016
935638 feet/sec YDOT = -5491
561983 meter/sec
ZDOT = -16103
533726 ZDOT = -4908
357080
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 19032
41245467
00016717 00000-0 10270-3 0 9128
2 25544 51
6383 316
4798 0005195 337
0156 23
0763 15
53195200 34156
Satellite: ISS
Catalog Number: 25544
Epoch time: 19032
41245467 = yrday
fracday
Element set: 912
Inclination: 51
6383 deg
RA of node: 316
4798 deg
Eccentricity:
0005195
Arg of perigee: 337
0156 deg
Mean anomaly: 23
0763 deg
Mean motion: 15
53195200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3415
Checksum: 298
Coasting Arc #14 (Orbit 3429)
---------------------------------------
Vector Time (GMT): 2019/033/08:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3048182
44 A = 6790628
20 meter
Y = -5769806
75 meter E =
0010866
Z = -1857077
57 I = 51
36712
XDOT = 5144
865781 Wp = 14
76851
YDOT = 917
482641 meter/sec RA = 310
99450 deg
ZDOT = 5611
728556 TA = 324
71969
MA = 324
79156
Ha = 222
768 n
mi
Hp = 216
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10000598
57 X = 3121495
93
Y = -18929812
16 feet Y = -5735309
86 meter
Z = -6092774
17 Z = -1842093
13
XDOT = 16879
480910 XDOT = 5106
965869
YDOT = 3010
113650 feet/sec YDOT = 974
804019 meter/sec
ZDOT = 18411
182927 ZDOT = 5636
627753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18185586
08 X = 5542966
64
Y = 11334115
79 feet Y = 3454638
49 meter
Z = -6024444
82 Z = -1836250
78
XDOT = -3343
687382 XDOT = -1019
155914
YDOT = 15179
735300 feet/sec YDOT = 4626
783319 meter/sec
ZDOT = 18523
385863 ZDOT = 5645
928011
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 19033
37756805
00016717 00000-0 10270-3 0 9138
2 25544 51
6386 311
6760 0005135 340
5883 19
5073 15
53189892 34306
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
37756805 = yrday
fracday
Element set: 913
Inclination: 51
6386 deg
RA of node: 311
6760 deg
Eccentricity:
0005135
Arg of perigee: 340
5883 deg
Mean anomaly: 19
5073 deg
Mean motion: 15
53189892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3430
Checksum: 318
Coasting Arc #15 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2019/033/17:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5298582
45 A = 6789653
39 meter
Y = 3557477
64 meter E =
0002487
Z = -2320786
34 I = 51
35623
XDOT = -1214
141005 Wp = 67
04779
YDOT = -5316
074839 meter/sec RA = 309
21983 deg
ZDOT = -5380
546323 TA = 138
90008
MA = 138
88134
Ha = 222
747 n
mi
Hp = 216
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17383800
68 X = -5326696
57
Y = 11671514
58 feet Y = 3498068
07 meter
Z = -7614128
40 Z = -2346592
38
XDOT = -3983
402248 XDOT = -1128
469886
YDOT = -17441
190416 feet/sec YDOT = -5329
173037 meter/sec
ZDOT = -17652
711032 ZDOT = -5386
236094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6907645
08 X = -2105450
22
Y = 19720851
40 feet Y = 6010915
51 meter
Z = -7730988
91 Z = -2356405
42
XDOT = -12093
544098 XDOT = -3686
112241
YDOT = -11161
408552 feet/sec YDOT = -3401
997327 meter/sec
ZDOT = -17677
704838 ZDOT = -5388
164435
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 19033
76361131
00016717 00000-0 10270-3 0 9146
2 25544 51
6385 309
7527 0005247 340
2937 19
8012 15
53207790 34365
Satellite: ISS
Catalog Number: 25544
Epoch time: 19033
76361131 = yrday
fracday
Element set: 914
Inclination: 51
6385 deg
RA of node: 309
7527 deg
Eccentricity:
0005247
Arg of perigee: 340
2937 deg
Mean anomaly: 19
8012 deg
Mean motion: 15
53207790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 305
Coasting Arc #16 (Orbit 3451)
---------------------------------------
Vector Time (GMT): 2019/034/17:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5176291
21 A = 6786729
03 meter
Y = -2654965
09 meter E =
0011543
Z = 3481541
87 I = 51
32595
XDOT = 144
482577 Wp = 66
90479
YDOT = 6204
788244 meter/sec RA = 304
22520 deg
ZDOT = 4509
362147 TA = 334
22490
MA = 334
28237
Ha = 222
630 n
mi
Hp = 216
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16982582
70 X = 5188684
14
Y = -8710515
37 feet Y = -2597010
95 meter
Z = 11422381
47 Z = 3506715
72
XDOT = 474
024204 XDOT = 53
184781
YDOT = 20356
916811 feet/sec YDOT = 6205
893405 meter/sec
ZDOT = 14794
495234 ZDOT = 4509
842321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8041934
16 X = 2451181
53
Y = -17233507
93 feet Y = -5252773
22 meter
Z = 11536268
52 Z = 3516254
64
XDOT = 11497
069839 XDOT = 3504
306887
YDOT = 15285
847660 feet/sec YDOT = 4659
126367 meter/sec
ZDOT = 14795
892150 ZDOT = 4509
787927
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 19034
79306136
00016717 00000-0 10270-3 0 9155
2 25544 51
6381 304
6273 0005114 342
7465 17
3513 15
53219983 34523
Satellite: ISS
Catalog Number: 25544
Epoch time: 19034
79306136 = yrday
fracday
Element set: 915
Inclination: 51
6381 deg
RA of node: 304
6273 deg
Eccentricity:
0005114
Arg of perigee: 342
7465 deg
Mean anomaly: 17
3513 deg
Mean motion: 15
53219983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3452
Checksum: 302
Coasting Arc #17 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2019/035/17:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 914275
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4921310
53 A = 6783638
31 meter
Y = 1551399
01 meter E =
0011301
Z = -4415075
26 I = 51
29693
XDOT = 804
320428 Wp = 43
12966
YDOT = -6860
442663 meter/sec RA = 299
22326 deg
ZDOT = -3304
150834 TA = 193
28595
MA = 193
31573
Ha = 222
963 n
mi
Hp = 216
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16146031
94 X = -4916847
60
Y = 5089891
78 feet Y = 1496390
43 meter
Z = -14485155
07 Z = -4438969
62
XDOT = 2638
846547 XDOT = 897
025319
YDOT = -22508
013986 feet/sec YDOT = -6850
929854 meter/sec
ZDOT = -10840
389874 ZDOT = -3300
018685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9340115
70 X = -2846867
26
Y = 14007994
26 feet Y = 4269636
65 meter
Z = -14593128
47 Z = -4447985
56
XDOT = -10940
298069 XDOT = -3334
602851
YDOT = -18577
980083 feet/sec YDOT = -5662
568329 meter/sec
ZDOT = -10820
918991 ZDOT = -3298
216108
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 19035
75817208
00016717 00000-0 10270-3 0 9160
2 25544 51
6373 299
8233 0005054 349
9371 10
1679 15
53211004 34679
Satellite: ISS
Catalog Number: 25544
Epoch time: 19035
75817208 = yrday
fracday
Element set: 916
Inclination: 51
6373 deg
RA of node: 299
8233 deg
Eccentricity:
0005054
Arg of perigee: 349
9371 deg
Mean anomaly: 10
1679 deg
Mean motion: 15
53211004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3467
Checksum: 313
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