[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 4th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19965 9774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
249/18:14:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 219
3
250/16:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 219
0
253/21:33:20
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 218
7
254/16:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 218
5
257/11:11:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 218
1
Coasting Arc #1 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2019/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5652576
69 A = 6794250
81 meter
Y = 790372
63 meter E =
0012707
Z = 3670477
14 I = 51
49775
XDOT = -3550
545002 Wp = 58
96323
YDOT = 5234
987663 meter/sec RA = 337
19079 deg
ZDOT = 4335
887294 TA = 344
75932
MA = 344
79757
Ha = 228
037 n
mi
Hp = 220
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18545199
12 X = 5625489
34
Y = 2593086
06 feet Y = 853432
56 meter
Z = 12042247
83 Z = 3697869
27
XDOT = -11648
769693 XDOT = -3629
881513
YDOT = 17175
156374 feet/sec YDOT = 5194
839712 meter/sec
ZDOT = 14225
352016 ZDOT = 4318
447041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16532537
89 X = -5039117
55
Y = -8620289
55 feet Y = -2627464
26 meter
Z = 12166759
53 Z = 3708428
30
XDOT = 16184
440148 XDOT = 4933
017357
YDOT = -11052
760675 feet/sec YDOT = -3368
881454 meter/sec
ZDOT = 14145
507829 ZDOT = 4311
550786
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 19245
55656166
00016717 00000-0 10270-3 0 9008
2 25544 51
6446 337
4943 0007593 354
8102 5
2969 15
50442267 27251
Satellite: ISS
Catalog Number: 25544
Epoch time: 19245
55656166 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 337
4943 deg
Eccentricity:
0007593
Arg of perigee: 354
8102 deg
Mean anomaly: 5
2969 deg
Mean motion: 15
50442267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 323
Coasting Arc #2 (Orbit 2739)
---------------------------------------
Vector Time (GMT): 2019/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5440823
19 A = 6793251
58 meter
Y = -745657
52 meter E =
0011740
Z = -4011717
87 I = 51
46290
XDOT = 3648
237531 Wp = 32
89141
YDOT = -5458
634981 meter/sec RA = 332
22328 deg
ZDOT = -3929
046647 TA = 196
05744
MA = 196
09468
Ha = 228
307 n
mi
Hp = 219
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17850469
77 X = -5412593
97
Y = -2446382
95 feet Y = -806343
06 meter
Z = -13161804
02 Z = -4038078
71
XDOT = 11969
283237 XDOT = 3728
091534
YDOT = -17908
907418 feet/sec YDOT = -5417
391577 meter/sec
ZDOT = -12890
572989 ZDOT = -3911
130592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16059285
59 X = 4894870
25
Y = 7972142
72 feet Y = 2429909
10 meter
Z = -13281620
09 Z = -4048237
80
XDOT = -16547
151595 XDOT = -5043
571806
YDOT = 11971
061370 feet/sec YDOT = 3648
779506 meter/sec
ZDOT = -12808
553084 ZDOT = -3904
046980
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 19246
52340297
00016717 00000-0 10270-3 0 9012
2 25544 51
6436 332
7025 0007609 357
8595 2
2522 15
50413462 27400
Satellite: ISS
Catalog Number: 25544
Epoch time: 19246
52340297 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 332
7025 deg
Eccentricity:
0007609
Arg of perigee: 357
8595 deg
Mean anomaly: 2
2522 deg
Mean motion: 15
50413462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2740
Checksum: 296
Coasting Arc #3 (Orbit 2755)
---------------------------------------
Vector Time (GMT): 2019/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5193089
99 A = 6792076
28 meter
Y = 740118
69 meter E =
0010475
Z = 4303585
63 I = 51
43102
XDOT = -3720
953554 Wp = 62
91911
YDOT = 5716
383940 meter/sec RA = 327
25150 deg
ZDOT = 3505
032236 TA = 351
29824
MA = 351
31639
Ha = 228
251 n
mi
Hp = 219
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17037696
83 X = 5163523
37
Y = 2428210
93 feet Y = 798026
36 meter
Z = 14119375
42 Z = 4328739
88
XDOT = -12207
852866 XDOT = -3801
624771
YDOT = 18754
540484 feet/sec YDOT = 5674
322715 meter/sec
ZDOT = 11499
449592 ZDOT = 3486
761032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15418518
29 X = -4699564
37
Y = -7430156
86 feet Y = -2264711
81 meter
Z = 14233697
58 Z = 4338431
02
XDOT = 16831
828363 XDOT = 5130
341285
YDOT = -13047
390711 feet/sec YDOT = -3976
844689 meter/sec
ZDOT = 11415
798524 ZDOT = 3479
535390
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 19247
55469457
00016717 00000-0 10270-3 0 9027
2 25544 51
6443 327
5897 0007718 1
6660 358
4515 15
50451331 27567
Satellite: ISS
Catalog Number: 25544
Epoch time: 19247
55469457 = yrday
fracday
Element set: 902
Inclination: 51
6443 deg
RA of node: 327
5897 deg
Eccentricity:
0007718
Arg of perigee: 1
6660 deg
Mean anomaly: 358
4515 deg
Mean motion: 15
50451331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2756
Checksum: 328
Coasting Arc #4 (Orbit 2770)
---------------------------------------
Vector Time (GMT): 2019/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4970264
92 A = 6791197
73 meter
Y = -775020
87 meter E =
0015242
Z = -4577159
42 I = 51
39932
XDOT = 3729
101459 Wp = 42
01445
YDOT = -5949
360475 meter/sec RA = 322
27811 deg
ZDOT = -3036
807528 TA = 197
43231
MA = 197
48469
Ha = 228
581 n
mi
Hp = 219
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16306643
43 X = -4938995
71
Y = -2542719
39 feet Y = -830427
17 meter
Z = -15016927
24 Z = -4601227
13
XDOT = 12234
584840 XDOT = 3810
102895
YDOT = -19518
899197 feet/sec YDOT = -5907
206220 meter/sec
ZDOT = -9963
279292 ZDOT = -3018
496036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14804921
02 X = 4512539
93
Y = 7063249
65 feet Y = 2152878
49 meter
Z = -15126300
39 Z = -4610496
36
XDOT = -16846
087788 XDOT = -5134
687558
YDOT = 14116
683906 feet/sec YDOT = 4302
765255 meter/sec
ZDOT = -9879
431433 ZDOT = -3011
250701
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 19248
52153043
00016717 00000-0 10270-3 0 9037
2 25544 51
6434 322
7977 0007823 5
6155 354
5082 15
50417114 27717
Satellite: ISS
Catalog Number: 25544
Epoch time: 19248
52153043 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 322
7977 deg
Eccentricity:
0007823
Arg of perigee: 5
6155 deg
Mean anomaly: 354
5082 deg
Mean motion: 15
50417114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2771
Checksum: 298
Coasting Arc #5 (Orbit 2786)
---------------------------------------
Vector Time (GMT): 2019/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931697
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4722843
84 A = 6790183
23 meter
Y = 855718
58 meter E =
0008628
Z = 4794764
81 I = 51
37051
XDOT = -3714
977004 Wp = 60
52560
YDOT = 6203
698154 meter/sec RA = 317
30137 deg
ZDOT = 2552
776813 TA = 4
25542
MA = 4
24809
Ha = 228
504 n
mi
Hp = 219
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15494894
49 X = 4689633
69
Y = 2807475
66 feet Y = 908347
16 meter
Z = 15730855
67 Z = 4817625
88
XDOT = -12188
244763 XDOT = -3796
472388
YDOT = 20353
340400 feet/sec YDOT = 6161
699047 meter/sec
ZDOT = 8375
252012 ZDOT = 2534
532827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14066552
30 X = -4287485
14
Y = -6843016
31 feet Y = -2085751
37 meter
Z = 15834731
74 Z = 4826426
24
XDOT = 16767
604670 XDOT = 5110
765903
YDOT = -15285
864169 feet/sec YDOT = -4659
131399 meter/sec
ZDOT = 8291
696640 ZDOT = 2527
309136
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 19249
55281853
00016717 00000-0 10270-3 0 9043
2 25544 51
6433 317
6854 0007855 9
4530 350
6768 15
50450640 27873
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
55281853 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 317
6854 deg
Eccentricity:
0007855
Arg of perigee: 9
4530 deg
Mean anomaly: 350
6768 deg
Mean motion: 15
50450640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2787
Checksum: 330
Coasting Arc #6 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2019/249/18:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4075937
14 A = 6788852
35 meter
Y = 1764364
37 meter E =
0007616
Z = 5128568
73 I = 51
35647
XDOT = -4500
043569 Wp = 44
24900
YDOT = 6021
960901 meter/sec RA = 316
00318 deg
ZDOT = 1508
697842 TA = 31
18211
MA = 31
13694
Ha = 228
721 n
mi
Hp = 219
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13372497
17 X = 4030992
91
Y = 5788597
02 feet Y = 1809693
17 meter
Z = 16826012
90 Z = 5148258
85
XDOT = -14763
922472 XDOT = -4574
376818
YDOT = 19757
089571 feet/sec YDOT = 5971
222649 meter/sec
ZDOT = 4949
796069 ZDOT = 1486
657730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8387499
28 X = -2556509
78
Y = 11788381
05 feet Y = 3593098
54 meter
Z = 16915382
77 Z = 5155808
67
XDOT = -15440
422529 XDOT = -4706
240787
YDOT = -17925
154277 feet/sec YDOT = -5463
587024 meter/sec
ZDOT = 4848
998576 ZDOT = 1477
974766
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 19249
81064219
00016717 00000-0 10270-3 0 9058
2 25544 51
6403 316
4086 0008233 11
0288 349
1041 15
50430192 27916
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
81064219 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 316
4086 deg
Eccentricity:
0008233
Arg of perigee: 11
0288 deg
Mean anomaly: 349
1041 deg
Mean motion: 15
50430192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2791
Checksum: 288
Coasting Arc #7 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2019/250/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5433052
93 A = 6794048
65 meter
Y = 1616488
43 meter E =
0012259
Z = -3760436
80 I = 51
35263
XDOT = 1049
205085 Wp = 40
52716
YDOT = -6294
069958 meter/sec RA = 311
39260 deg
ZDOT = -4220
156589 TA = 184
53105
MA = 184
54215
Ha = 228
948 n
mi
Hp = 218
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17824976
81 X = -5432459
17
Y = 5303439
74 feet Y = 1555735
47 meter
Z = -12337391
07 Z = -3786826
96
XDOT = 3442
273901 XDOT = 1140
008270
YDOT = -20649
835819 feet/sec YDOT = -6281
829364 meter/sec
ZDOT = -13845
658101 ZDOT = -4214
839329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6268275
61 X = 1910570
41
Y = -17423712
67 feet Y = -5310747
62 meter
Z = -12457545
80 Z = -3797059
96
XDOT = 13245
852735 XDOT = 4037
335914
YDOT = 14649
996834 feet/sec YDOT = 4465
319035 meter/sec
ZDOT = -13820
889668 ZDOT = -4212
607171
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 19250
71301754
00016717 00000-0 10270-3 0 9068
2 25544 51
6407 311
9353 0008188 15
4789 344
6611 15
50424555 28055
Satellite: ISS
Catalog Number: 25544
Epoch time: 19250
71301754 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 311
9353 deg
Eccentricity:
0008188
Arg of perigee: 15
4789 deg
Mean anomaly: 344
6611 deg
Mean motion: 15
50424555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 307
Coasting Arc #8 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2019/251/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5196466
20 A = 6792860
32 meter
Y = -1547687
21 meter E =
0013813
Z = 4077023
19 I = 51
32798
XDOT = -1045
315704 Wp = 66
70218
YDOT = 6568
395222 meter/sec RA = 306
41498 deg
ZDOT = 3820
812362 TA = 343
63130
MA = 343
67586
Ha = 228
810 n
mi
Hp = 218
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17048773
62 X = 5193582
94
Y = -5077713
93 feet Y = -1489592
70 meter
Z = 13376060
33 Z = 4102258
47
XDOT = -3429
513464 XDOT = -1137
246924
YDOT = 21549
853090 feet/sec YDOT = 6556
191823 meter/sec
ZDOT = 12535
473630 ZDOT = 3815
511241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5697438
21 X = -1736579
17
Y = 16759959
71 feet Y = 5108435
72 meter
Z = 13490952
49 Z = 4112042
32
XDOT = -14297
669501 XDOT = -4357
929664
YDOT = -14943
949296 feet/sec YDOT = -4554
915745 meter/sec
ZDOT = 12510
766992 ZDOT = 3813
281779
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 19251
74430028
00016717 00000-0 10270-3 0 9070
2 25544 51
6409 306
8235 0008215 17
9810 342
1630 15
50459456 28212
Satellite: ISS
Catalog Number: 25544
Epoch time: 19251
74430028 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 306
8235 deg
Eccentricity:
0008215
Arg of perigee: 17
9810 deg
Mean anomaly: 342
1630 deg
Mean motion: 15
50459456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 296
Coasting Arc #9 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2019/252/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4997300
02 A = 6791892
21 meter
Y = 1441823
23 meter E =
0015917
Z = -4384407
38 I = 51
30485
XDOT = 994
506861 Wp = 46
52462
YDOT = -6796
187704 meter/sec RA = 301
43410 deg
ZDOT = -3365
464473 TA = 189
14500
MA = 189
17402
Ha = 229
151 n
mi
Hp = 218
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16395341
29 X = -4991754
73
Y = 4730391
16 feet Y = 1385970
77 meter
Z = -14384538
63 Z = -4408668
69
XDOT = 3262
817787 XDOT = 1086
777254
YDOT = -22297
203752 feet/sec YDOT = -6784
550615 meter/sec
ZDOT = -11041
550108 ZDOT = -3360
409272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5321206
01 X = 1621903
59
Y = -16114554
61 feet Y = -4911716
25 meter
Z = -14494987
56 Z = -4418072
21
XDOT = 15322
802968 XDOT = 4670
390345
YDOT = 14979
182564 feet/sec YDOT = 4565
654845 meter/sec
ZDOT = -11017
957823 ZDOT = -3358
273544
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 19252
71112831
00016717 00000-0 10270-3 0 9088
2 25544 51
6402 302
0304 0008358 22
2894 337
8618 15
50430238 28369
Satellite: ISS
Catalog Number: 25544
Epoch time: 19252
71112831 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 302
0304 deg
Eccentricity:
0008358
Arg of perigee: 22
2894 deg
Mean anomaly: 337
8618 deg
Mean motion: 15
50430238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 291
Coasting Arc #10 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2019/253/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4786904
47 A = 6790799
62 meter
Y = -1290896
78 meter E =
0011486
Z = 4629186
46 I = 51
28475
XDOT = -907
321989 Wp = 69
45851
YDOT = 7042
462113 meter/sec RA = 296
45243 deg
ZDOT = 2900
202830 TA = 351
54545
MA = 351
56478
Ha = 228
959 n
mi
Hp = 218
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15705067
15 X = 4778498
14
Y = -4235225
65 feet Y = -1237413
03 meter
Z = 15187619
61 Z = 4652418
80
XDOT = -2976
778178 XDOT = -1000
092801
YDOT = 23105
190661 feet/sec YDOT = 7031
797220 meter/sec
ZDOT = 9515
101148 ZDOT = 2895
569809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5072649
66 X = -1546143
62
Y = 15350279
34 feet Y = 4678765
14 meter
Z = 15293371
43 Z = 4661419
61
XDOT = -16477
771806 XDOT = -5022
424846
YDOT = -14909
625481 feet/sec YDOT = -4544
453847 meter/sec
ZDOT = 9493
426137 ZDOT = 2893
596287
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 19253
74240848
00016717 00000-0 10270-3 0 9093
2 25544 51
6398 296
9189 0008259 24
7048 335
4496 15
50465186 28529
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
74240848 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 296
9189 deg
Eccentricity:
0008259
Arg of perigee: 24
7048 deg
Mean anomaly: 335
4496 deg
Mean motion: 15
50465186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 356
Coasting Arc #11 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2019/253/21:33:20
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -598403
35 A = 6797140
92 meter
Y = 6225320
12 meter E =
0017471
Z = 2654654
51 I = 51
30540
XDOT = -5390
694296 Wp = 74
66514
YDOT = 1701
100504 meter/sec RA = 295
36754 deg
ZDOT = -5171
213214 TA = 75
29380
MA = 75
10022
Ha = 229
222 n
mi
Hp = 218
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1963265
59 X = -680866
88
Y = 20424278
62 feet Y = 6218167
41 meter
Z = 8709496
41 Z = 2651547
13
XDOT = -17686
004908 XDOT = -5384
197279
YDOT = 5581
038400 feet/sec YDOT = 1640
854031 meter/sec
ZDOT = -16965
922619 ZDOT = -5197
383163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16516801
87 X = -5034321
21
Y = 12184253
39 feet Y = 3713760
43 meter
Z = 8694833
05 Z = 2650185
11
XDOT = -15026
990057 XDOT = -4580
226569
YDOT = -8100
591106 feet/sec YDOT = -2469
060169 meter/sec
ZDOT = -17085
066018 ZDOT = -5207
528122
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 19253
93577547
00016717 00000-0 10270-3 0 9105
2 25544 51
6429 295
9616 0008316 26
0754 334
0814 15
50430478 28559
Satellite: ISS
Catalog Number: 25544
Epoch time: 19253
93577547 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 295
9616 deg
Eccentricity:
0008316
Arg of perigee: 26
0754 deg
Mean anomaly: 334
0814 deg
Mean motion: 15
50430478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 328
Coasting Arc #12 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2019/254/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1575167
40 A = 6792756
17 meter
Y = -5136090
41 meter E =
0012277
Z = -4163520
54 I = 51
27724
XDOT = 4954
109449 Wp = 66
74934
YDOT = -4511
001726 meter/sec RA = 291
36890 deg
ZDOT = 3703
967001 TA = 241
51404
MA = 241
63774
Ha = 229
263 n
mi
Hp = 218
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5167872
05 X = -1497393
26
Y = -16850690
32 feet Y = -5153270
45 meter
Z = -13659844
30 Z = -4170982
80
XDOT = 16253
639923 XDOT = 4986
192978
YDOT = -14799
874429 feet/sec YDOT = -4455
421754 meter/sec
ZDOT = 12152
122708 ZDOT = 3728
110129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17232949
21 X = 5252602
92
Y = 3572354
31 feet Y = 1088853
59 meter
Z = -13693347
23 Z = -4173732
23
XDOT = 5559
657084 XDOT = 1694
583479
YDOT = 20014
146359 feet/sec YDOT = 6100
311810 meter/sec
ZDOT = 12262
279051 ZDOT = 3737
542655
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 19254
70923307
00016717 00000-0 10270-3 0 9111
2 25544 51
6402 292
1261 0008409 28
5159 331
6451 15
50429235 28676
Satellite: ISS
Catalog Number: 25544
Epoch time: 19254
70923307 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 292
1261 deg
Eccentricity:
0008409
Arg of perigee: 28
5159 deg
Mean anomaly: 331
6451 deg
Mean motion: 15
50429235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 301
Coasting Arc #13 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2019/255/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1605398
10 A = 6793839
03 meter
Y = 5383623
20 meter E =
0018015
Z = 3814048
53 I = 51
27015
XDOT = -4745
707999 Wp = 60
83510
YDOT = 4365
786896 meter/sec RA = 286
38531 deg
ZDOT = -4141
359735 TA = 73
10846
MA = 72
91101
Ha = 229
323 n
mi
Hp = 218
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5267054
15 X = 1526551
22
Y = 17662805
76 feet Y = 5401135
34 meter
Z = 12513282
57 Z = 3821654
93
XDOT = -15569
908132 XDOT = -4774
058561
YDOT = 14323
447821 feet/sec YDOT = 4312
558189 meter/sec
ZDOT = -13587
138239 ZDOT = -4164
481577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18061561
60 X = -5505163
98
Y = -3555370
73 feet Y = -1083677
00 meter
Z = 12547435
56 Z = 3824458
36
XDOT = -5820
850184 XDOT = -1774
195136
YDOT = -19024
373194 feet/sec YDOT = -5798
628950 meter/sec
ZDOT = -13692
623933 ZDOT = -4173
511775
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 19255
74050856
00016717 00000-0 10270-3 0 9127
2 25544 51
6403 287
0132 0008505 31
6936 328
4721 15
50461092 28831
Satellite: ISS
Catalog Number: 25544
Epoch time: 19255
74050856 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 287
0132 deg
Eccentricity:
0008505
Arg of perigee: 31
6936 deg
Mean anomaly: 328
4721 deg
Mean motion: 15
50461092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 302
Coasting Arc #14 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2019/256/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 916589
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1722158
06 A = 6794941
55 meter
Y = -5577935
38 meter E =
0011970
Z = -3479255
66 I = 51
26457
XDOT = 4539
924866 Wp = 55
89569
YDOT = -4204
695167 meter/sec RA = 281
40271 deg
ZDOT = 4511
569208 TA = 263
08403
MA = 263
22021
Ha = 229
413 n
mi
Hp = 218
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5650124
88 X = -1642755
81
Y = -18300312
93 feet Y = -5596750
13 meter
Z = -11414880
78 Z = -3487427
82
XDOT = 14894
766621 XDOT = 4564
691028
YDOT = -13794
931651 feet/sec YDOT = -4153
787622 meter/sec
ZDOT = 14801
736246 ZDOT = 4533
682848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18864739
79 X = 5749972
69
Y = 3179179
23 feet Y = 969013
83 meter
Z = -11451605
99 Z = -3490449
50
XDOT = 5974
375656 XDOT = 1820
989700
YDOT = 18019
746573 feet/sec YDOT = 5492
418755 meter/sec
ZDOT = 14902
610727 ZDOT = 4542
315750
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 19256
70732853
00016717 00000-0 10270-3 0 9139
2 25544 51
6396 282
2208 0008517 35
1156 325
0555 15
50435187 28989
Satellite: ISS
Catalog Number: 25544
Epoch time: 19256
70732853 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 282
2208 deg
Eccentricity:
0008517
Arg of perigee: 35
1156 deg
Mean anomaly: 325
0555 deg
Mean motion: 15
50435187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 322
Coasting Arc #15 (Orbit 2909)
---------------------------------------
Vector Time (GMT): 2019/257/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4072127
64 A = 6788333
53 meter
Y = -1414454
51 meter E =
0020307
Z = -5260493
95 I = 51
24013
XDOT = 1609
641587 Wp = 75
77527
YDOT = -7438
177861 meter/sec RA = 277
60367 deg
ZDOT = 761
357124 TA = 201
51631
MA = 201
60178
Ha = 229
428 n
mi
Hp = 218
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13359998
81 X = -4030455
70
Y = -4640598
79 feet Y = -1459759
45 meter
Z = -17258838
43 Z = -5280173
38
XDOT = 5280
976336 XDOT = 1688
999577
YDOT = -24403
470673 feet/sec YDOT = -7419
733918 meter/sec
ZDOT = 2497
890827 ZDOT = 769
369629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10857543
09 X = 3309379
13
Y = 8890757
56 feet Y = 2709902
91 meter
Z = -17348210
79 Z = -5287734
65
XDOT = -12643
780253 XDOT = -3853
824221
YDOT = 20340
029450 feet/sec YDOT = 6199
640976 meter/sec
ZDOT = 2534
883727 ZDOT = 772
632560
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 19257
48078316
00016717 00000-0 10270-3 0 9143
2 25544 51
6417 278
3859 0008325 39
0100 321
1650 15
50434384 29106
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
48078316 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 278
3859 deg
Eccentricity:
0008325
Arg of perigee: 39
0100 deg
Mean anomaly: 321
1650 deg
Mean motion: 15
50434384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2910
Checksum: 303
Coasting Arc #16 (Orbit 2925)
---------------------------------------
Vector Time (GMT): 2019/258/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4066982
49 A = 6788587
06 meter
Y = 1699926
74 meter E =
0012729
Z = 5156415
89 I = 51
23758
XDOT = -1405
583976 Wp = 47
18447
YDOT = 7420
499426 meter/sec RA = 272
61475 deg
ZDOT = -1327
115805 TA = 55
69955
MA = 55
57912
Ha = 229
370 n
mi
Hp = 217
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13343118
41 X = 4022624
15
Y = 5577187
45 feet Y = 1745159
13 meter
Z = 16917374
97 Z = 5176063
84
XDOT = -4611
495985 XDOT = -1482
011289
YDOT = 24345
470558 feet/sec YDOT = 7404
353721 meter/sec
ZDOT = -4354
054478 ZDOT = -1334
130024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10689984
45 X = -3258307
26
Y = -9583406
13 feet Y = -2921022
19 meter
Z = 17006585
90 Z = 5183607
38
XDOT = 11564
106303 XDOT = 3524
739601
YDOT = -20744
987228 feet/sec YDOT = -6323
072107 meter/sec
ZDOT = -4386
487556 ZDOT = -1337
001407
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 19258
51205319
00016717 00000-0 10270-3 0 9154
2 25544 51
6411 273
2731 0008460 43
2301 316
9513 15
50479197 29261
Satellite: ISS
Catalog Number: 25544
Epoch time: 19258
51205319 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 273
2731 deg
Eccentricity:
0008460
Arg of perigee: 43
2301 deg
Mean anomaly: 316
9513 deg
Mean motion: 15
50479197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2926
Checksum: 299
Coasting Arc #17 (Orbit 2940)
---------------------------------------
Vector Time (GMT): 2019/259/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4131547
66 A = 6789249
41 meter
Y = -1939763
07 meter E =
0018932
Z = -5041605
59 I = 51
24060
XDOT = 1186
736168 Wp = 81
55571
YDOT = -7325
550387 meter/sec RA = 267
62664 deg
ZDOT = 1854
729281 TA = 206
51203
MA = 206
60899
Ha = 229
560 n
mi
Hp = 217
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13554946
38 X = -4085060
17
Y = -6364052
06 feet Y = -1985705
55 meter
Z = -16540700
76 Z = -5061562
07
XDOT = 3893
491365 XDOT = 1259
555106
YDOT = -24033
957964 feet/sec YDOT = -7311
872115 meter/sec
ZDOT = 6085
069818 ZDOT = 1860
671658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10813597
76 X = 3295984
60
Y = 10212660
64 feet Y = 3112818
96 meter
Z = -16631301
14 Z = -5069220
59
XDOT = -10355
885773 XDOT = -3156
473984
YDOT = 20873
203090 feet/sec YDOT = 6362
152302 meter/sec
ZDOT = 6112
605472 ZDOT = 1863
122148
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 19259
47886730
00016717 00000-0 10270-3 0 9163
2 25544 51
6427 268
4802 0008474 45
7165 314
4679 15
50444669 29412
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
47886730 = yrday
fracday
Element set: 916
Inclination: 51
6427 deg
RA of node: 268
4802 deg
Eccentricity:
0008474
Arg of perigee: 45
7165 deg
Mean anomaly: 314
4679 deg
Mean motion: 15
50444669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2941
Checksum: 349
Coasting Arc #18 (Orbit 2955)
---------------------------------------
Vector Time (GMT): 2019/260/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 951418
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4205948
35 A = 6789891
55 meter
Y = 2209038
35 meter E =
0015451
Z = 4843579
08 I = 51
24382
XDOT = -1009
645859 Wp = 54
26013
YDOT = 7212
827682 meter/sec RA = 262
63857 deg
ZDOT = -2398
580696 TA = 59
46473
MA = 59
31232
Ha = 229
505 n
mi
Hp = 217
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13799043
14 X = 4157406
04
Y = 7247501
15 feet Y = 2255801
28 meter
Z = 15891007
47 Z = 4863892
04
XDOT = -3312
486415 XDOT = -1078
575678
YDOT = 23664
132816 feet/sec YDOT = 7201
151468 meter/sec
ZDOT = -7869
359240 ZDOT = -2403
653332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10966344
49 X = -3342541
80
Y = -10942582
18 feet Y = -3335299
05 meter
Z = 15983215
16 Z = 4871683
98
XDOT = 9253
014689 XDOT = 2820
318877
YDOT = -20869
899460 feet/sec YDOT = -6361
145355 meter/sec
ZDOT = -7892
917768 ZDOT = -2405
761336
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 19260
51013350
00016717 00000-0 10270-3 0 9171
2 25544 51
6408 263
3674 0008582 50
1272 310
0632 15
50488545 29569
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
51013350 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 263
3674 deg
Eccentricity:
0008582
Arg of perigee: 50
1272 deg
Mean anomaly: 310
0632 deg
Mean motion: 15
50488545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2956
Checksum: 294
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