[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 6th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
010/09:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
3
016/05:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
2
018/18:04:49
685 2
7 2
9 2
9
N/A 0
7 0
0 220
9
000/00:07:35
370 -0
6 -0
0 217
8
Coasting Arc #1 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2019/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2907981
77 A = 6786229
75 meter
Y = 5239982
44 meter E =
0010534
Z = 3175906
37 I = 52
02920
XDOT = -3415
355615 Wp = 93
54033
YDOT = -4849
746281 meter/sec RA = 94
59674 deg
ZDOT = 4859
973238 TA = 302
90072
MA = 303
00202
Ha = 220
927 n
mi
Hp = 216
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9540622
59 X = -2981787
30
Y = 17191543
43 feet Y = 5207050
30 meter
Z = 10419640
32 Z = 3161601
94
XDOT = -11205
234958 XDOT = -3384
477475
YDOT = -15911
241081 feet/sec YDOT = -4887
767103 meter/sec
ZDOT = 15944
794087 ZDOT = 4843
457216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18906334
95 X = -5762650
89
Y = -5520646
80 feet Y = -1682693
14 meter
Z = 10354443
82 Z = 3156034
48
XDOT = 12574
039053 XDOT = 3832
567103
YDOT = -13205
083076 feet/sec YDOT = -4024
909322 meter/sec
ZDOT = 15870
822459 ZDOT = 4837
426685
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 19004
55781685
00016717 00000-0 10270-3 0 9006
2 25544 51
6423 95
1958 0002853 235
5131 124
5752 15
53743234 29822
Satellite: ISS
Catalog Number: 25544
Epoch time: 19004
55781685 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 95
1958 deg
Eccentricity:
0002853
Arg of perigee: 235
5131 deg
Mean anomaly: 124
5752 deg
Mean motion: 15
53743234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2982
Checksum: 312
Coasting Arc #2 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2019/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3338920
48 A = 6782743
55 meter
Y = -4042291
02 meter E =
0005524
Z = -4308643
53 I = 52
01787
XDOT = 2833
460849 Wp = 75
14875
YDOT = 6153
368139 meter/sec RA = 89
64192 deg
ZDOT = -3579
672330 TA = 158
51135
MA = 158
48815
Ha = 220
886 n
mi
Hp = 216
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10954463
51 X = 3404803
16
Y = -13262109
63 feet Y = -4004583
99 meter
Z = -14135969
57 Z = -4292264
92
XDOT = 9296
131394 XDOT = 2781
829468
YDOT = 20188
215678 feet/sec YDOT = 6184
765614 meter/sec
ZDOT = -11744
331791 ZDOT = -3566
033221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15530473
95 X = 4733688
46
Y = 7535710
39 feet Y = 2296884
53 meter
Z = -14061539
97 Z = -4285957
38
XDOT = -16791
868480 XDOT = -5118
161513
YDOT = 12820
404082 feet/sec YDOT = 3907
659164 meter/sec
ZDOT = -11683
510019 ZDOT = -3561
133854
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 19005
52259619
00016717 00000-0 10270-3 0 9012
2 25544 51
6412 90
3905 0002908 239
4399 120
6467 15
53718336 29970
Satellite: ISS
Catalog Number: 25544
Epoch time: 19005
52259619 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 90
3905 deg
Eccentricity:
0002908
Arg of perigee: 239
4399 deg
Mean anomaly: 120
6467 deg
Mean motion: 15
53718336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 326
Coasting Arc #3 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2019/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3713029
15 A = 6779730
93 meter
Y = 2598520
43 meter E =
0005026
Z = 5041847
20 I = 52
00758
XDOT = -2224
031891 Wp = 153
70368
YDOT = -7061
711262 meter/sec RA = 84
67785 deg
ZDOT = 1996
524940 TA = 276
97615
MA = 277
03331
Ha = 220
818 n
mi
Hp = 216
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12181854
16 X = -3766300
75
Y = 8525329
51 feet Y = 2556700
33 meter
Z = 16541493
44 Z = 5023681
84
XDOT = -7296
692557 XDOT = -2154
598443
YDOT = -23168
344035 feet/sec YDOT = -7086
193934 meter/sec
ZDOT = 6550
278675 ZDOT = 1985
889401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11400069
95 X = -3474741
32
Y = -9686803
24 feet Y = -2952537
63 meter
Z = 16459163
63 Z = 5016753
07
XDOT = 19795
698831 XDOT = 6033
729004
YDOT = -12218
380445 feet/sec YDOT = -3724
162360 meter/sec
ZDOT = 6503
135626 ZDOT = 1982
155739
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 19006
55169009
00016717 00000-0 10270-3 0 9020
2 25544 51
6419 85
2638 0002930 244
9652 115
1197 15
53758066 30134
Satellite: ISS
Catalog Number: 25544
Epoch time: 19006
55169009 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 85
2638 deg
Eccentricity:
0002930
Arg of perigee: 244
9652 deg
Mean anomaly: 115
1197 deg
Mean motion: 15
53758066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 308
Coasting Arc #4 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2019/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4063070
37 A = 6778560
11 meter
Y = -995696
55 meter E =
0012186
Z = -5344217
94 I = 51
99847
XDOT = 1541
314687 Wp = 92
12747
YDOT = 7498
905494 meter/sec RA = 79
70812 deg
ZDOT = -226
204563 TA = 175
72976
MA = 175
71935
Ha = 220
715 n
mi
Hp = 216
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13330283
38 X = 4099861
39
Y = -3266720
95 feet Y = -950054
22 meter
Z = -17533523
42 Z = -5324392
12
XDOT = 5056
806715 XDOT = 1458
444026
YDOT = 24602
708314 feet/sec YDOT = 7515
678212 meter/sec
ZDOT = -742
140955 ZDOT = -218
918070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6823324
57 X = 2079749
33
Y = 12039324
67 feet Y = 3669586
16 meter
Z = -17443889
12 Z = -5316897
40
XDOT = -21400
254326 XDOT = -6522
797519
YDOT = 11103
894361 feet/sec YDOT = 3384
467001 meter/sec
ZDOT = -710
181152 ZDOT = -216
463215
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 19007
51646522
00016717 00000-0 10270-3 0 9038
2 25544 51
6413 80
4577 0002816 251
3099 108
7748 15
53720101 30282
Satellite: ISS
Catalog Number: 25544
Epoch time: 19007
51646522 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 80
4577 deg
Eccentricity:
0002816
Arg of perigee: 251
3099 deg
Mean anomaly: 108
7748 deg
Mean motion: 15
53720101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 294
Coasting Arc #5 (Orbit 3043)
---------------------------------------
Vector Time (GMT): 2019/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4351312
85 A = 6779205
79 meter
Y = -630455
26 meter E =
0002437
Z = 5159469
48 I = 51
99408
XDOT = -772
650547 Wp = 30
80277
YDOT = -7467
876298 meter/sec RA = 74
73744 deg
ZDOT = -1561
791605 TA = 74
19023
MA = 74
16335
Ha = 220
753 n
mi
Hp = 216
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14275960
80 X = -4369000
93
Y = -2068422
77 feet Y = -679214
01 meter
Z = 16927393
31 Z = 5138289
79
XDOT = -2534
942738 XDOT = -681
499049
YDOT = -24500
906489 feet/sec YDOT = -7476
006822 meter/sec
ZDOT = -5123
988206 ZDOT = -1565
324035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2197003
97 X = -669646
81
Y = -14369417
57 feet Y = -4379798
48 meter
Z = 16831847
37 Z = 5130347
08
XDOT = 21673
608802 XDOT = 6606
115963
YDOT = -9342
547848 feet/sec YDOT = -2847
608584 meter/sec
ZDOT = -5138
993499 ZDOT = -1566
365219
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 19008
54555491
00016717 00000-0 10270-3 0 9047
2 25544 51
6412 75
3311 0002810 255
6948 104
3892 15
53769543 30447
Satellite: ISS
Catalog Number: 25544
Epoch time: 19008
54555491 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 75
3311 deg
Eccentricity:
0002810
Arg of perigee: 255
6948 deg
Mean anomaly: 104
3892 deg
Mean motion: 15
53769543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3044
Checksum: 308
Coasting Arc #6 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2019/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4569004
07 A = 6781840
67 meter
Y = 2159268
14 meter E =
0007480
Z = -4530335
32 I = 51
99188
XDOT = -107
688257 Wp = 120
72104
YDOT = 6956
264989 meter/sec RA = 69
77033 deg
ZDOT = 3207
123718 TA = 181
37304
MA = 181
37509
Ha = 220
675 n
mi
Hp = 216
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14990170
85 X = 4566524
41
Y = 7084213
06 feet Y = 2210348
37 meter
Z = -14863304
87 Z = -4508147
09
XDOT = -353
307930 XDOT = -201
045309
YDOT = 22822
391697 feet/sec YDOT = 6954
538534 meter/sec
ZDOT = 10522
059441 ZDOT = 3206
374348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2115784
74 X = -644891
19
Y = 16534044
08 feet Y = 5039576
64 meter
Z = -14763399
66 Z = -4499884
22
XDOT = -20648
189030 XDOT = -6293
568016
YDOT = 6748
570045 feet/sec YDOT = 2056
964150 meter/sec
ZDOT = 10517
788569 ZDOT = 3205
821956
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 19009
51032767
00016717 00000-0 10270-3 0 9052
2 25544 51
6402 70
5248 0002586 258
8473 101
2389 15
53756415 30597
Satellite: ISS
Catalog Number: 25544
Epoch time: 19009
51032767 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 70
5248 deg
Eccentricity:
0002586
Arg of perigee: 258
8473 deg
Mean anomaly: 101
2389 deg
Mean motion: 15
53756415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 313
Coasting Arc #7 (Orbit 3072)
---------------------------------------
Vector Time (GMT): 2019/010/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4651025
91 A = 6780658
97 meter
Y = 1095645
90 meter E =
0009049
Z = -4819553
60 I = 51
97859
XDOT = 1028
133093 Wp = 116
30297
YDOT = 7127
225288 meter/sec RA = 65
31343 deg
ZDOT = 2612
327804 TA = 179
34903
MA = 179
34785
Ha = 220
608 n
mi
Hp = 216
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15259271
37 X = 4661838
73
Y = 3594638
78 feet Y = 1147717
63 meter
Z = -15812183
71 Z = -4796934
72
XDOT = 3373
140068 XDOT = 935
669026
YDOT = 23383
285067 feet/sec YDOT = 7138
205450 meter/sec
ZDOT = 8570
629277 ZDOT = 2617
097809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8049630
61 X = -2453527
41
Y = 13571477
87 feet Y = 4136586
45 meter
Z = -15710199
87 Z = -4788468
92
XDOT = -22308
433610 XDOT = -6799
610564
YDOT = -3286
204449 feet/sec YDOT = -1001
635116 meter/sec
ZDOT = 8591
249108 ZDOT = 2618
612728
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 19010
41077858
00016717 00000-0 10270-3 0 9064
2 25544 51
6418 66
0374 0002674 260
1158 99
9693 15
53773369 30732
Satellite: ISS
Catalog Number: 25544
Epoch time: 19010
41077858 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 66
0374 deg
Eccentricity:
0002674
Arg of perigee: 260
1158 deg
Mean anomaly: 99
9693 deg
Mean motion: 15
53773369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3073
Checksum: 330
Coasting Arc #8 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2019/011/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4942501
20 A = 6784017
40 meter
Y = -2496675
14 meter E =
0008638
Z = 3913306
01 I = 51
97482
XDOT = 10
750119 Wp = 79
29831
YDOT = -6475
714359 meter/sec RA = 60
34925 deg
ZDOT = -4108
671649 TA = 53
59264
MA = 53
51300
Ha = 220
736 n
mi
Hp = 216
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16215555
11 X = -4933223
71
Y = -8191191
40 feet Y = -2551893
91 meter
Z = 12838930
47 Z = 3889319
99
XDOT = 35
269418 XDOT = 103
119914
YDOT = -21245
782019 feet/sec YDOT = -6475
077511 meter/sec
ZDOT = -13479
893861 ZDOT = -4108
395339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12488253
70 X = 3806419
73
Y = -13298277
23 feet Y = -4053314
90 meter
Z = 12730959
19 Z = 3880396
36
XDOT = 19363
938608 XDOT = 5902
128488
YDOT = 5252
368634 feet/sec YDOT = 1600
921960 meter/sec
ZDOT = -13477
805349 ZDOT = -4108
035070
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 19011
43986395
00016717 00000-0 10270-3 0 9073
2 25544 51
6418 60
9103 0002622 267
1431 92
9421 15
53759400 30898
Satellite: ISS
Catalog Number: 25544
Epoch time: 19011
43986395 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 60
9103 deg
Eccentricity:
0002622
Arg of perigee: 267
1431 deg
Mean anomaly: 92
9421 deg
Mean motion: 15
53759400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 305
Coasting Arc #9 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2019/012/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5059202
44 A = 6787515
81 meter
Y = 3646256
33 meter E =
0003246
Z = -2676121
10 I = 51
96806
XDOT = -1186
630268 Wp = 22
89530
YDOT = 5479
007067 meter/sec RA = 55
39326 deg
ZDOT = 5226
943500 TA = 307
06147
MA = 307
09115
Ha = 220
644 n
mi
Hp = 216
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16598433
22 X = 5031051
92
Y = 11962783
22 feet Y = 3702674
53 meter
Z = -8779924
87 Z = -2651613
97
XDOT = -3893
143923 XDOT = -1273
199136
YDOT = 17975
744971 feet/sec YDOT = 5465
253148 meter/sec
ZDOT = 17148
764763 ZDOT = 5220
969275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15986994
56 X = -4872835
94
Y = 12843463
07 feet Y = 3914687
54 meter
Z = -8669758
36 Z = -2642542
35
XDOT = -15309
840754 XDOT = -4666
439462
YDOT = -7511
041588 feet/sec YDOT = -2289
365476 meter/sec
ZDOT = 17121
073600 ZDOT = 5218
503233
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 19012
40463066
00016717 00000-0 10270-3 0 9087
2 25544 51
6410 56
1043 0002760 270
8212 89
2625 15
53733454 31045
Satellite: ISS
Catalog Number: 25544
Epoch time: 19012
40463066 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 56
1043 deg
Eccentricity:
0002760
Arg of perigee: 270
8212 deg
Mean anomaly: 89
2625 deg
Mean motion: 15
53733454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 276
Coasting Arc #10 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2019/013/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4924638
76 A = 6789852
23 meter
Y = -4514460
68 meter E =
0011394
Z = 1178141
01 I = 51
95659
XDOT = 2473
025266 Wp = 128
25861
YDOT = -4243
050008 meter/sec RA = 50
44355 deg
ZDOT = -5889
833343 TA = 39
00184
MA = 38
91973
Ha = 220
640 n
mi
Hp = 216
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16156951
30 X = -4879513
48
Y = -14811222
70 feet Y = -4569279
14 meter
Z = 3865292
02 Z = 1154328
67
XDOT = 8113
599954 XDOT = 2548
897705
YDOT = -13920
767742 feet/sec YDOT = -4214
970527 meter/sec
ZDOT = -19323
600206 ZDOT = -5877
636267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18401928
89 X = 5608907
92
Y = -11941667
19 feet Y = -3639820
16 meter
Z = 3758387
13 Z = 1145556
40
XDOT = 10533
616276 XDOT = 3210
646241
YDOT = 10134
360791 feet/sec YDOT = 3088
953169 meter/sec
ZDOT = -19267
972432 ZDOT = -5872
877997
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 19013
43371379
00016717 00000-0 10270-3 0 9097
2 25544 51
6412 50
9774 0002633 275
3666 84
7186 15
53757893 31205
Satellite: ISS
Catalog Number: 25544
Epoch time: 19013
43371379 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 50
9774 deg
Eccentricity:
0002633
Arg of perigee: 275
3666 deg
Mean anomaly: 84
7186 deg
Mean motion: 15
53757893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 326
Coasting Arc #11 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/014/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4517269
12 A = 6790436
16 meter
Y = 5045268
41 meter E =
0011542
Z = 402074
37 I = 51
93651
XDOT = -3770
519576 Wp = 38
63642
YDOT = 2889
425816 meter/sec RA = 45
49558 deg
ZDOT = 6020
528975 TA = 325
68077
MA = 325
75529
Ha = 220
750 n
mi
Hp = 216
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14820436
75 X = 4458562
74
Y = 16552717
89 feet Y = 5095455
40 meter
Z = 1319141
63 Z = 423875
00
XDOT = -12370
471049 XDOT = -3831
793898
YDOT = 9479
743492 feet/sec YDOT = 2846
918439 meter/sec
ZDOT = 19752
391651 ZDOT = 6002
064602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19565420
67 X = -5963540
22
Y = 10514975
51 feet Y = 3204964
54 meter
Z = 1416881
69 Z = 431865
54
XDOT = -5517
054570 XDOT = -1681
598233
YDOT = -12950
643853 feet/sec YDOT = -3947
356246 meter/sec
ZDOT = 19668
648248 ZDOT = 5995
003986
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 19014
46279550
00016717 00000-0 10270-3 0 9101
2 25544 51
6415 45
8501 0002626 284
8161 75
2700 15
53721480 31363
Satellite: ISS
Catalog Number: 25544
Epoch time: 19014
46279550 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 45
8501 deg
Eccentricity:
0002626
Arg of perigee: 284
8161 deg
Mean anomaly: 75
2700 deg
Mean motion: 15
53721480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 288
Coasting Arc #12 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2019/015/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3789375
53 A = 6788709
63 meter
Y = -5273978
63 meter E =
0004866
Z = -1969992
07 I = 51
90636
XDOT = 5004
326451 Wp = 156
23080
YDOT = -1504
304164 meter/sec RA = 40
54582 deg
ZDOT = -5607
954797 TA = 45
41387
MA = 45
37416
Ha = 220
704 n
mi
Hp = 216
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12432334
42 X = -3720549
71
Y = -17303079
48 feet Y = -5315969
14 meter
Z = -6463228
57 Z = -1988232
41
XDOT = 16418
393868 XDOT = 5048
016263
YDOT = -4935
381117 feet/sec YDOT = -1448
097763 meter/sec
ZDOT = -18398
801828 ZDOT = -5583
539731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19586695
14 X = 5970024
68
Y = -8322204
90 feet Y = -2536608
05 meter
Z = -6544853
05 Z = -1994871
21
XDOT = 608
234791 XDOT = 185
389964
YDOT = 15790
778887 feet/sec YDOT = 4813
029405 meter/sec
ZDOT = -18288
382830 ZDOT = -5574
299087
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 19015
42755708
00016717 00000-0 10270-3 0 9113
2 25544 51
6407 41
0442 0002515 286
4189 73
6686 15
53760593 31511
Satellite: ISS
Catalog Number: 25544
Epoch time: 19015
42755708 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 41
0442 deg
Eccentricity:
0002515
Arg of perigee: 286
4189 deg
Mean anomaly: 73
6686 deg
Mean motion: 15
53760593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 308
Coasting Arc #13 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2019/016/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5933484
33 A = 6786992
06 meter
Y = -1551674
54 meter E =
0010853
Z = 2895423
82 I = 51
87919
XDOT = -995
556540 Wp = 98
30255
YDOT = -5671
742482 meter/sec RA = 36
39891 deg
ZDOT = -5065
011632 TA = 48
83234
MA = 48
73877
Ha = 220
797 n
mi
Hp = 216
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19466812
10 X = -5929756
38
Y = -5090795
73 feet Y = -1618006
22 meter
Z = 9499421
98 Z = 2866610
27
XDOT = -3266
261613 XDOT = -907
456629
YDOT = -18608
079009 feet/sec YDOT = -5682
382588 meter/sec
ZDOT = -16617
492231 ZDOT = -5069
634013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20178359
74 X = 6150364
05
Y = -396196
25 feet Y = -120760
62 meter
Z = 9369568
77 Z = 2855844
56
XDOT = 8054
112353 XDOT = 2454
893445
YDOT = 15585
127012 feet/sec YDOT = 4750
346713 meter/sec
ZDOT = -16637
579813 ZDOT = -5071
134327
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19016
26368433
00016717 00000-0 10270-3 0 9122
2 25544 51
6410 36
8758 0002487 281
7041 78
3832 15
53743824 31647
Satellite: ISS
Catalog Number: 25544
Epoch time: 19016
26368433 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 36
8758 deg
Eccentricity:
0002487
Arg of perigee: 281
7041 deg
Mean anomaly: 78
3832 deg
Mean motion: 15
53743824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 313
Coasting Arc #14 (Orbit 3178)
---------------------------------------
Vector Time (GMT): 2019/017/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6165026
29 A = 6789589
89 meter
Y = 2433934
62 meter E =
0008216
Z = -1451025
71 I = 51
86186
XDOT = -601
575415 Wp = 19
98271
YDOT = 4973
661075 meter/sec RA = 31
44175 deg
ZDOT = 5804
031271 TA = 324
23993
MA = 324
29492
Ha = 220
830 n
mi
Hp = 216
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20226464
21 X = 6144399
39
Y = 7985349
79 feet Y = 2502761
02 meter
Z = -4760583
05 Z = -1421128
39
XDOT = -1973
672623 XDOT = -685
340184
YDOT = 16317
785679 feet/sec YDOT = 4966
465019 meter/sec
ZDOT = 19042
097346 ZDOT = 5800
906008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21698555
35 X = -6613719
67
Y = -1819875
26 feet Y = -554697
98 meter
Z = -4625966
52 Z = -1409994
59
XDOT = -2815
267678 XDOT = -858
093588
YDOT = -14651
406940 feet/sec YDOT = -4465
748835 meter/sec
ZDOT = 19027
299989 ZDOT = 5799
521037
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19017
22844329
00016717 00000-0 10270-3 0 9133
2 25544 51
6422 32
0694 0002535 291
3858 68
7023 15
53748016 31793
Satellite: ISS
Catalog Number: 25544
Epoch time: 19017
22844329 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 32
0694 deg
Eccentricity:
0002535
Arg of perigee: 291
3858 deg
Mean anomaly: 68
7023 deg
Mean motion: 15
53748016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3179
Checksum: 310
Coasting Arc #15 (Orbit 3194)
---------------------------------------
Vector Time (GMT): 2019/018/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6018636
31 A = 6790381
49 meter
Y = -3129886
69 meter E =
0009499
Z = -148863
26 I = 51
83485
XDOT = 2299
582849 Wp = 141
43087
YDOT = -4145
568749 meter/sec RA = 26
48770 deg
ZDOT = -6025
966528 TA = 40
16809
MA = 40
09792
Ha = 220
781 n
mi
Hp = 216
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19746182
13 X = -5982466
64
Y = -10268657
11 feet Y = -3196989
02 meter
Z = -488396
52 Z = -178011
75
XDOT = 7544
563152 XDOT = 2375
039399
YDOT = -13600
947338 feet/sec YDOT = -4119
430722 meter/sec
ZDOT = -19770
231390 ZDOT = -6014
613246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21930204
41 X = 6684326
31
Y = 3778607
67 feet Y = 1151719
62 meter
Z = -619529
85 Z = -188832
70
XDOT = -2900
810018 XDOT = -884
166894
YDOT = 13693
423649 feet/sec YDOT = 4173
755528 meter/sec
ZDOT = -19718
403894 ZDOT = -6010
169507
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19018
25751862
00016717 00000-0 10270-3 0 9147
2 25544 51
6413 26
9426 0002470 293
2973 66
7919 15
53761010 31954
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
25751862 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 26
9426 deg
Eccentricity:
0002470
Arg of perigee: 293
2973 deg
Mean anomaly: 66
7919 deg
Mean motion: 15
53761010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3195
Checksum: 315
Coasting Arc #16 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/018/18:08:37
370
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1664383
97 A = 6779971
69 meter
Y = -3855313
68 meter E =
0010548
Z = -5332067
23 I = 51
77907
XDOT = 7015
323942 Wp = 83
96205
YDOT = 3074
381624 meter/sec RA = 23
85382 deg
ZDOT = -32
076778 TA = 185
72649
MA = 185
73856
Ha = 220
914 n
mi
Hp = 217
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5460577
34 X = 1733271
41
Y = -12648666
94 feet Y = -3836315
66 meter
Z = -17493658
90 Z = -5323815
45
XDOT = 23016
154664 XDOT = 6980
579761
YDOT = 10086
553885 feet/sec YDOT = 3152
637597 meter/sec
ZDOT = -105
238774 ZDOT = 1
916595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1286652
01 X = -392171
53
Y = -13764879
40 feet Y = -4195535
24 meter
Z = -17455870
18 Z = -5320549
23
XDOT = 24011
382140 XDOT = 7318
669276
YDOT = -2300
723681 feet/sec YDOT = -701
260578 meter/sec
ZDOT = 47
768900 ZDOT = 14
559961
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19018
77205864
00016717 00000-0 10270-3 0 9151
2 25544 51
6414 24
3827 0004498 283
6396 76
4255 15
53229932 32039
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
77205864 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 24
3827 deg
Eccentricity:
0004498
Arg of perigee: 283
6396 deg
Mean anomaly: 76
4255 deg
Mean motion: 15
53229932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 324
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