[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 14th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 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
050/05:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 214
5
054/08:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
2
000/00:00:00
000 0
0 0
0 214
1
057/02:24:53
072 -3
0 3
0 3
0
N/A -0
0 -0
3 224
4
000/00:07:46
144 -0
3 -0
2 215
7
057/14:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
7
Coasting Arc #1 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2019/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4127272
78 A = 6785782
70 meter
Y = -3863081
47 meter E =
0008598
Z = -3756805
05 I = 51
26700
XDOT = 1893
840522 Wp = 62
88375
YDOT = -6111
742936 meter/sec RA = 255
31715 deg
ZDOT = 4215
359859 TA = 251
91974
MA = 252
01342
Ha = 223
637 n
mi
Hp = 215
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13540921
20 X = -4065519
71
Y = -12674151
80 feet Y = -3908890
30 meter
Z = -12325475
88 Z = -3776703
50
XDOT = 6213
387541 XDOT = 1941
567365
YDOT = -20051
650054 feet/sec YDOT = -6090
297757 meter/sec
ZDOT = 13829
920796 ZDOT = 4224
675346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2913432
76 X = -888014
31
Y = -18256264
73 feet Y = -5564509
49 meter
Z = -12414859
41 Z = -3784049
15
XDOT = 15762
476552 XDOT = 4804
402853
YDOT = -11924
180120 feet/sec YDOT = -3634
490101 meter/sec
ZDOT = 13872
550396 ZDOT = 4228
353361
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 19044
50810224
00016717 00000-0 10270-3 0 9007
2 25544 51
6390 256
2621 0005598 18
8550 341
2809 15
53262466 36033
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
50810224 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 256
2621 deg
Eccentricity:
0005598
Arg of perigee: 18
8550 deg
Mean anomaly: 341
2809 deg
Mean motion: 15
53262466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 294
Coasting Arc #2 (Orbit 3618)
---------------------------------------
Vector Time (GMT): 2019/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3954906
79 A = 6788818
52 meter
Y = 4859602
85 meter E =
0015596
Z = 2603763
38 I = 51
28641
XDOT = -2654
574651 Wp = 81
43251
YDOT = 4964
519570 meter/sec RA = 250
31690 deg
ZDOT = -5204
484650 TA = 69
10782
MA = 68
94092
Ha = 223
742 n
mi
Hp = 214
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12975415
99 X = 3887623
95
Y = 15943578
89 feet Y = 4903453
18 meter
Z = 8542530
78 Z = 2622811
15
XDOT = -8709
234419 XDOT = -2684
611868
YDOT = 16287
793865 feet/sec YDOT = 4934
666305 meter/sec
ZDOT = -17075
080872 ZDOT = -5217
452365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 841628
66 X = 256528
42
Y = 20503251
84 feet Y = 6249391
16 meter
Z = 8627994
29 Z = 2629812
66
XDOT = -15124
315636 XDOT = -4609
891406
YDOT = 7870
804230 feet/sec YDOT = 2399
021129 meter/sec
ZDOT = -17134
068009 ZDOT = -5222
463929
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 19045
53751312
00016717 00000-0 10270-3 0 9014
2 25544 51
6384 251
1371 0005778 22
1209 338
0192 15
53298164 36191
Satellite: ISS
Catalog Number: 25544
Epoch time: 19045
53751312 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 251
1371 deg
Eccentricity:
0005778
Arg of perigee: 22
1209 deg
Mean anomaly: 338
0192 deg
Mean motion: 15
53298164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3619
Checksum: 299
Coasting Arc #3 (Orbit 3633)
---------------------------------------
Vector Time (GMT): 2019/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3695039
79 A = 6791121
27 meter
Y = -5538476
24 meter E =
0014269
Z = -1304907
18 I = 51
30436
XDOT = 3437
508203 Wp = 33
51031
YDOT = -3650
472339 meter/sec RA = 245
32298 deg
ZDOT = 5802
134908 TA = 312
22330
MA = 312
34429
Ha = 223
783 n
mi
Hp = 214
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12122833
97 X = -3626493
96
Y = -18170853
80 feet Y = -5579413
48 meter
Z = -4281191
52 Z = -1322689
55
XDOT = 11277
914053 XDOT = 3449
890275
YDOT = -11976
615287 feet/sec YDOT = -3611
962542 meter/sec
ZDOT = 19035
875684 ZDOT = 5818
862787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 774056
07 X = 235932
29
Y = -21814101
43 feet Y = -6648938
12 meter
Z = -4360899
92 Z = -1329202
29
XDOT = 14451
170353 XDOT = 4404
716724
YDOT = -3280
768130 feet/sec YDOT = -999
978126 meter/sec
ZDOT = 19111
699482 ZDOT = 5825
246002
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 19046
50258738
00016717 00000-0 10270-3 0 9027
2 25544 51
6369 246
3322 0005539 26
3211 333
8221 15
53254151 36341
Satellite: ISS
Catalog Number: 25544
Epoch time: 19046
50258738 = yrday
fracday
Element set: 902
Inclination: 51
6369 deg
RA of node: 246
3322 deg
Eccentricity:
0005539
Arg of perigee: 26
3211 deg
Mean anomaly: 333
8221 deg
Mean motion: 15
53254151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3634
Checksum: 292
Coasting Arc #4 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2019/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3264356
96 A = 6791780
82 meter
Y = 5951758
75 meter E =
0011687
Z = -136598
87 I = 51
32186
XDOT = -4253
651715 Wp = 107
66386
YDOT = 2205
542280 meter/sec RA = 240
33357 deg
ZDOT = -5980
728311 TA = 73
81290
MA = 73
68432
Ha = 223
910 n
mi
Hp = 214
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10709832
54 X = 3198223
61
Y = 19526767
56 feet Y = 5987893
30 meter
Z = -448159
03 Z = -120902
77
XDOT = -13955
550246 XDOT = -4248
948162
YDOT = 7236
031101 feet/sec YDOT = 2158
001331 meter/sec
ZDOT = -19621
812045 ZDOT = -6001
379056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2306037
88 X = -702880
34
Y = 22152548
53 feet Y = 6752096
79 meter
Z = -377880
83 Z = -115178
08
XDOT = -13868
734957 XDOT = -4227
190415
YDOT = -1751
646882 feet/sec YDOT = -533
901969 meter/sec
ZDOT = -19715
204205 ZDOT = -6009
194242
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 19047
53199663
00016717 00000-0 10270-3 0 9033
2 25544 51
6370 241
2065 0005703 29
6993 330
4482 15
53282107 36509
Satellite: ISS
Catalog Number: 25544
Epoch time: 19047
53199663 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 241
2065 deg
Eccentricity:
0005703
Arg of perigee: 29
6993 deg
Mean anomaly: 330
4482 deg
Mean motion: 15
53282107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 306
Coasting Arc #5 (Orbit 3665)
---------------------------------------
Vector Time (GMT): 2019/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2690428
72 A = 6790909
77 meter
Y = -6034868
77 meter E =
0019051
Z = 1522961
41 I = 51
33456
XDOT = 5035
268937 Wp = 54
44512
YDOT = -787
261094 meter/sec RA = 235
34405 deg
ZDOT = 5735
835226 TA = 322
27252
MA = 322
40595
Ha = 223
984 n
mi
Hp = 214
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8826865
87 X = -2630142
66
Y = -19799438
23 feet Y = -6064617
94 meter
Z = 4996592
56 Z = 1510039
12
XDOT = 16519
911211 XDOT = 5015
837337
YDOT = -2582
877606 feet/sec YDOT = -731
061828 meter/sec
ZDOT = 18818
357040 ZDOT = 5760
246822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3616858
56 X = 1102418
49
Y = -21387465
65 feet Y = -6518899
53 meter
Z = 4938815
65 Z = 1505351
01
XDOT = 13510
710780 XDOT = 4118
064646
YDOT = 6686
301729 feet/sec YDOT = 2037
984767 meter/sec
ZDOT = 18928
600133 ZDOT = 5769
437321
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 19048
56140485
00016717 00000-0 10270-3 0 9046
2 25544 51
6355 236
0803 0005613 35
0450 325
1070 15
53257373 36661
Satellite: ISS
Catalog Number: 25544
Epoch time: 19048
56140485 = yrday
fracday
Element set: 904
Inclination: 51
6355 deg
RA of node: 236
0803 deg
Eccentricity:
0005613
Arg of perigee: 35
0450 deg
Mean anomaly: 325
1070 deg
Mean motion: 15
53257373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3666
Checksum: 291
Coasting Arc #6 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2019/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1907684
53 A = 6788400
20 meter
Y = 5866337
21 meter E =
0008023
Z = -2843263
97 I = 51
34562
XDOT = -5727
424556 Wp = 74
40902
YDOT = -580
571989 meter/sec RA = 230
35283 deg
ZDOT = -5050
495125 TA = 138
00400
MA = 137
94246
Ha = 224
069 n
mi
Hp = 214
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6258807
53 X = 1855754
29
Y = 19246513
15 feet Y = 5887379
82 meter
Z = -9328293
86 Z = -2834123
74
XDOT = -18790
762979 XDOT = -5695
975012
YDOT = -1904
763744 feet/sec YDOT = -644
444355 meter/sec
ZDOT = -16569
865895 ZDOT = -5078
239559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5085489
00 X = -1550057
05
Y = 19608601
38 feet Y = 5976701
70 meter
Z = -9287548
65 Z = -2830844
83
XDOT = -13255
109196 XDOT = -4040
157283
YDOT = -11329
925564 feet/sec YDOT = -3453
361312 meter/sec
ZDOT = -16695
043745 ZDOT = -5088
649333
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 19049
52647352
00016717 00000-0 10270-3 0 9059
2 25544 51
6349 231
2753 0005728 39
1994 320
9572 15
53280838 36819
Satellite: ISS
Catalog Number: 25544
Epoch time: 19049
52647352 = yrday
fracday
Element set: 905
Inclination: 51
6349 deg
RA of node: 231
2753 deg
Eccentricity:
0005728
Arg of perigee: 39
1994 deg
Mean anomaly: 320
9572 deg
Mean motion: 15
53280838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 332
Coasting Arc #7 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2019/050/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2497785
08 A = 6779949
98 meter
Y = -3475039
72 meter E =
0007034
Z = 5252714
55 I = 51
33770
XDOT = 5650
652130 Wp = 66
31627
YDOT = 5140
796365 meter/sec RA = 226
59554 deg
ZDOT = 715
998949 TA = 16
83162
MA = 16
80829
Ha = 223
929 n
mi
Hp = 214
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8194832
94 X = 2510944
34
Y = -11401048
94 feet Y = -3447033
88 meter
Z = 17233315
46 Z = 5264879
63
XDOT = 18538
884942 XDOT = 5589
268513
YDOT = 16866
129805 feet/sec YDOT = 5203
642724 meter/sec
ZDOT = 2349
077917 ZDOT = 743
297483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5305496
35 X = 1617115
29
Y = 12926137
64 feet Y = 3939886
75 meter
Z = 17288523
36 Z = 5269541
92
XDOT = -23218
270357 XDOT = -7076
928805
YDOT = 6232
596689 feet/sec YDOT = 1899
695471 meter/sec
ZDOT = 2471
867583 ZDOT = 753
425239
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 19050
29852790
00016717 00000-0 10270-3 0 9060
2 25544 51
6387 227
4348 0005670 40
2648 319
8923 15
53297592 36938
Satellite: ISS
Catalog Number: 25544
Epoch time: 19050
29852790 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 227
4348 deg
Eccentricity:
0005670
Arg of perigee: 40
2648 deg
Mean anomaly: 319
8923 deg
Mean motion: 15
53297592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 342
Coasting Arc #8 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2019/051/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3539746
24 A = 6780066
94 meter
Y = 2465646
05 meter E =
0018563
Z = -5246351
74 I = 51
36299
XDOT = -5186
843882 Wp = 82
48012
YDOT = -5556
961114 meter/sec RA = 221
58429 deg
ZDOT = 893
076107 TA = 196
08141
MA = 196
14041
Ha = 224
138 n
mi
Hp = 214
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11613340
69 X = -3541571
59
Y = 8089389
94 feet Y = 2426051
49 meter
Z = -17212440
08 Z = -5263550
64
XDOT = -17017
204338 XDOT = -5128
656823
YDOT = -18231
499717 feet/sec YDOT = -5614
638605 meter/sec
ZDOT = 2930
039720 ZDOT = 868
022889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -919857
20 X = -280372
47
Y = -14027683
12 feet Y = -4275637
81 meter
Z = -17290285
54 Z = -5270079
03
XDOT = 23412
160021 XDOT = 7136
026375
YDOT = -4987
363020 feet/sec YDOT = -1520
148248 meter/sec
ZDOT = 2817
394541 ZDOT = 858
741856
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 19051
26359443
00016717 00000-0 10270-3 0 9076
2 25544 51
6400 222
6298 0005810 43
5462 316
6148 15
53282460 37080
Satellite: ISS
Catalog Number: 25544
Epoch time: 19051
26359443 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 222
6298 deg
Eccentricity:
0005810
Arg of perigee: 43
5462 deg
Mean anomaly: 316
6148 deg
Mean motion: 15
53282460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 300
Coasting Arc #9 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2019/052/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4532917
88 A = 6781681
06 meter
Y = -1437663
74 meter E =
0012746
Z = 4828983
36 I = 51
39432
XDOT = 4451
228998 Wp = 53
78630
YDOT = 5744
966918 meter/sec RA = 216
57715 deg
ZDOT = -2456
024738 TA = 60
46242
MA = 60
33540
Ha = 224
026 n
mi
Hp = 214
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14871777
84 X = 4525201
41
Y = -4716744
57 feet Y = -1387016
13 meter
Z = 15843121
25 Z = 4850983
44
XDOT = 14603
769679 XDOT = 4398
586046
YDOT = 18848
316661 feet/sec YDOT = 5794
449066 meter/sec
ZDOT = -8057
823942 ZDOT = -2434
531332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3401078
34 X = -1036648
68
Y = 15122477
64 feet Y = 4609331
18 meter
Z = 15942561
99 Z = 4859292
89
XDOT = -22570
120293 XDOT = -6879
372665
YDOT = 3357
922222 feet/sec YDOT = 1023
494693 meter/sec
ZDOT = -7961
242981 ZDOT = -2426
586861
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 19052
29299540
00016717 00000-0 10270-3 0 9082
2 25544 51
6399 217
5047 0005858 46
1905 313
9731 15
53312609 37240
Satellite: ISS
Catalog Number: 25544
Epoch time: 19052
29299540 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 217
5047 deg
Eccentricity:
0005858
Arg of perigee: 46
1905 deg
Mean anomaly: 313
9731 deg
Mean motion: 15
53312609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 326
Coasting Arc #10 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2019/053/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5391879
19 A = 6784599
05 meter
Y = 518127
77 meter E =
0011585
Z = -4094470
44 I = 51
43146
XDOT = -3435
490049 Wp = 84
03407
YDOT = -5682
888066 meter/sec RA = 211
57774 deg
ZDOT = 3815
460670 TA = 225
50037
MA = 225
59512
Ha = 224
179 n
mi
Hp = 214
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17689892
35 X = -5377384
03
Y = 1699894
25 feet Y = 457912
60 meter
Z = -13433301
97 Z = -4120626
51
XDOT = -11271
292813 XDOT = -3390
220092
YDOT = -18644
645886 feet/sec YDOT = -5721
052570 meter/sec
ZDOT = 12517
915583 ZDOT = 3798
883255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7159955
46 X = 2182354
42
Y = -16166910
57 feet Y = -4927674
34 meter
Z = -13551441
78 Z = -4130479
45
XDOT = 20637
945840 XDOT = 6290
445892
YDOT = -1261
700133 feet/sec YDOT = -384
566201 meter/sec
ZDOT = 12443
508145 ZDOT = 3792
781283
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 19053
25806003
00016717 00000-0 10270-3 0 9098
2 25544 51
6403 212
7003 0005784 49
4435 310
7220 15
53273119 37393
Satellite: ISS
Catalog Number: 25544
Epoch time: 19053
25806003 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 212
7003 deg
Eccentricity:
0005784
Arg of perigee: 49
4435 deg
Mean anomaly: 310
7220 deg
Mean motion: 15
53273119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 285
Coasting Arc #11 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/054/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6063470
85 A = 6787837
60 meter
Y = 347151
32 meter E =
0017839
Z = 3018369
67 I = 51
47188
XDOT = 2154
120521 Wp = 83
57255
YDOT = 5466
882815 meter/sec RA = 206
58738 deg
ZDOT = -4929
021796 TA = 61
75406
MA = 61
57409
Ha = 224
230 n
mi
Hp = 214
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19893277
08 X = 6044476
92
Y = 1138947
90 feet Y = 414851
40 meter
Z = 9902787
64 Z = 3047777
13
XDOT = 7067
324544 XDOT = 2116
770292
YDOT = 17935
967242 feet/sec YDOT = 5490
762346 meter/sec
ZDOT = -16171
331351 ZDOT = -4918
649326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10437136
05 X = -3181239
07
Y = 16895524
43 feet Y = 5149755
84 meter
Z = 10035552
99 Z = 3058836
55
XDOT = -17956
496326 XDOT = -5473
140080
YDOT = -1462
686831 feet/sec YDOT = -445
826946 meter/sec
ZDOT = -16124
912775 ZDOT = -4914
873414
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 19054
28746006
00016717 00000-0 10270-3 0 9100
2 25544 51
6409 207
5755 0005879 53
7245 306
4450 15
53279545 37551
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
28746006 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 207
5755 deg
Eccentricity:
0005879
Arg of perigee: 53
7245 deg
Mean anomaly: 306
4450 deg
Mean motion: 15
53279545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 325
Coasting Arc #12 (Orbit 3755)
---------------------------------------
Vector Time (GMT): 2019/054/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2162392
04 A = 6779825
60 meter
Y = 3649035
25 meter E =
0019614
Z = -5305823
62 I = 51
44560
XDOT = -6756
582593 Wp = 81
74332
YDOT = -3581
672768 meter/sec RA = 206
17182 deg
ZDOT = 294
075628 TA = 191
05164
MA = 191
09479
Ha = 224
217 n
mi
Hp = 214
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7094462
08 X = -2177263
50
Y = 11971900
42 feet Y = 3624770
17 meter
Z = -17407557
80 Z = -5316364
05
XDOT = -22167
265724 XDOT = -6717
457591
YDOT = -11750
894908 feet/sec YDOT = -3657
010804 meter/sec
ZDOT = 964
815052 ZDOT = 261
350558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12324494
29 X = -3756505
86
Y = -6332102
49 feet Y = -1930024
84 meter
Z = -17455434
08 Z = -5320416
31
XDOT = 10094
613070 XDOT = 3076
838064
YDOT = -21867
429290 feet/sec YDOT = -6665
192447 meter/sec
ZDOT = 817
315316 ZDOT = 249
117708
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 19054
35179574
00016717 00000-0 10270-3 0 9119
2 25544 51
6389 207
2529 0005728 52
8646 307
3029 15
53289613 37562
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
35179574 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 207
2529 deg
Eccentricity:
0005728
Arg of perigee: 52
8646 deg
Mean anomaly: 307
3029 deg
Mean motion: 15
53289613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3756
Checksum: 335
Coasting Arc #13 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2019/055/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3446213
77 A = 6780943
98 meter
Y = -2958183
80 meter E =
0011287
Z = 5028908
41 I = 51
47976
XDOT = 6243
665013 Wp = 56
51783
YDOT = 4035
893626 meter/sec RA = 201
16942 deg
ZDOT = -1895
424965 TA = 51
93979
MA = 51
83800
Ha = 224
160 n
mi
Hp = 214
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11306475
63 X = 3454609
54
Y = -9705327
44 feet Y = -2919598
46 meter
Z = 16499043
34 Z = 5045669
27
XDOT = 20484
465267 XDOT = 6207
277283
YDOT = 13241
120819 feet/sec YDOT = 4105
511030 meter/sec
ZDOT = -6218
585843 ZDOT = -1865
184673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10467172
24 X = 3190394
10
Y = 10486045
66 feet Y = 3196146
72 meter
Z = 16574961
68 Z = 5052048
32
XDOT = -11000
529923 XDOT = -3352
961521
YDOT = 20642
262527 feet/sec YDOT = 6291
761618 meter/sec
ZDOT = -6082
324110 ZDOT = -1853
892389
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 19055
38119267
00016717 00000-0 10270-3 0 9127
2 25544 51
6389 202
1278 0005739 56
6417 303
5283 15
53285362 37722
Satellite: ISS
Catalog Number: 25544
Epoch time: 19055
38119267 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 202
1278 deg
Eccentricity:
0005739
Arg of perigee: 56
6417 deg
Mean anomaly: 303
5283 deg
Mean motion: 15
53285362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3772
Checksum: 323
Coasting Arc #14 (Orbit 3786)
---------------------------------------
Vector Time (GMT): 2019/056/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4606143
53 A = 6783417
30 meter
Y = 2320893
72 meter E =
0013682
Z = -4418053
45 I = 51
51767
XDOT = -5369
320047 Wp = 92
44574
YDOT = -4319
407253 meter/sec RA = 196
17333 deg
ZDOT = 3337
222952 TA = 211
34800
MA = 211
42964
Ha = 224
276 n
mi
Hp = 213
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15112019
44 X = -4610293
87
Y = 7614480
72 feet Y = 2269361
10 meter
Z = -14494926
03 Z = -4440438
36
XDOT = -17615
879419 XDOT = -5336
830352
YDOT = -14171
283640 feet/sec YDOT = -4379
268851 meter/sec
ZDOT = 10948
894198 ZDOT = 3311
220310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8897212
07 X = -2711870
24
Y = -14291491
10 feet Y = -4356046
49 meter
Z = -14596205
96 Z = -4448923
58
XDOT = 11527
422287 XDOT = 3513
558313
YDOT = -18211
247715 feet/sec YDOT = -5550
788303 meter/sec
ZDOT = 10831
775715 ZDOT = 3301
525238
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 19056
34625226
00016717 00000-0 10270-3 0 9132
2 25544 51
6370 197
3227 0005732 61
1257 299
0470 15
53284569 37878
Satellite: ISS
Catalog Number: 25544
Epoch time: 19056
34625226 = yrday
fracday
Element set: 913
Inclination: 51
6370 deg
RA of node: 197
3227 deg
Eccentricity:
0005732
Arg of perigee: 61
1257 deg
Mean anomaly: 299
0470 deg
Mean motion: 15
53284569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3787
Checksum: 324
Coasting Arc #15 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2019/057/02:28:46
144
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1677510
08 A = 6781615
89 meter
Y = 3928555
33 meter E =
0017488
Z = -5282194
99 I = 51
53304
XDOT = -7303
934350 Wp = 87
41559
YDOT = -2174
820876 meter/sec RA = 192
36726 deg
ZDOT = 704
872645 TA = 189
32343
MA = 189
35594
Ha = 224
388 n
mi
Hp = 215
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5503642
00 X = -1695657
96
Y = 12888961
05 feet Y = 3909694
47 meter
Z = -17330036
06 Z = -5290387
91
XDOT = -23963
039207 XDOT = -7282
495888
YDOT = -7135
239093 feet/sec YDOT = -2256
378661 meter/sec
ZDOT = 2312
574296 ZDOT = 669
445488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2598780
61 X = 792108
33
Y = -13724699
44 feet Y = -4183288
39 meter
Z = -17367340
23 Z = -5293565
30
XDOT = 23935
413909 XDOT = 7295
514160
YDOT = 1819
702496 feet/sec YDOT = 554
645321 meter/sec
ZDOT = 2152
709907 ZDOT = 656
145980
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 19057
11830221
00016717 00000-0 10270-3 0 9142
2 25544 51
6394 193
4798 0003642 52
3397 307
8085 15
52716656 37998
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
11830221 = yrday
fracday
Element set: 914
Inclination: 51
6394 deg
RA of node: 193
4798 deg
Eccentricity:
0003642
Arg of perigee: 52
3397 deg
Mean anomaly: 307
8085 deg
Mean motion: 15
52716656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 334
Coasting Arc #16 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2019/057/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2285616
44 A = 6782061
57 meter
Y = 3769659
52 meter E =
0016506
Z = -5168306
65 I = 51
55219
XDOT = -7134
466076 Wp = 93
21160
YDOT = -2377
978988 meter/sec RA = 189
78900 deg
ZDOT = 1423
708605 TA = 190
51065
MA = 190
54520
Ha = 224
305 n
mi
Hp = 215
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7498741
59 X = -2302495
52
Y = 12367649
34 feet Y = 3744005
52 meter
Z = -16956386
63 Z = -5179450
36
XDOT = -23407
040932 XDOT = -7114
260096
YDOT = -7801
768334 feet/sec YDOT = -2457
648520 meter/sec
ZDOT = 4670
959991 ZDOT = 1389
101686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3133270
34 X = -955020
80
Y = 14058915
84 feet Y = 4285157
55 meter
Z = -17007011
08 Z = -5183736
98
XDOT = -23676
800664 XDOT = -7216
688842
YDOT = 172
753167 feet/sec YDOT = 52
655165 meter/sec
ZDOT = 4514
804310 ZDOT = 1376
112354
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 19057
63318567
00016717 00000-0 10270-3 0 9154
2 25544 51
6401 190
9163 0003330 58
5586 301
5891 15
52729356 38074
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
63318567 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 190
9163 deg
Eccentricity:
0003330
Arg of perigee: 58
5586 deg
Mean anomaly: 301
5891 deg
Mean motion: 15
52729356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 322
Coasting Arc #17 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2019/058/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900432
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3417002
32 A = 6783808
05 meter
Y = -3467148
81 meter E =
0011092
Z = 4718548
37 I = 51
59165
XDOT = 6609
091988 Wp = 62
15615
YDOT = 2748
338731 meter/sec RA = 184
80145 deg
ZDOT = -2756
579845 TA = 55
19505
MA = 55
09074
Ha = 224
219 n
mi
Hp = 215
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11210637
53 X = 3432599
26
Y = -11375160
15 feet Y = -3428850
09 meter
Z = 15480801
74 Z = 4735184
67
XDOT = 21683
372665 XDOT = 6591
257820
YDOT = 9016
859354 feet/sec YDOT = 2822
146375 meter/sec
ZDOT = -9043
897129 ZDOT = -2724
519283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6731667
72 X = 2051812
32
Y = -14401957
02 feet Y = -4389716
50 meter
Z = 15556226
05 Z = 4741537
70
XDOT = 22450
455935 XDOT = 6842
898969
YDOT = 845
775846 feet/sec YDOT = 257
792478 meter/sec
ZDOT = -8899
250229 ZDOT = -2712
491470
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 19058
66295326
00016717 00000-0 10270-3 0 9166
2 25544 51
6405 185
7933 0003391 60
1956 299
9533 15
52749351 38230
Satellite: ISS
Catalog Number: 25544
Epoch time: 19058
66295326 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 185
7933 deg
Eccentricity:
0003391
Arg of perigee: 60
1956 deg
Mean anomaly: 299
9533 deg
Mean motion: 15
52749351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 340
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