[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 3rd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
010/09:34:56
900 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
Coasting Arc #1 (Orbit 2950)
---------------------------------------
Vector Time (GMT): 2019/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1856091
50 A = 6790501
43 meter
Y = 6523744
67 meter E =
0009563
Z = 211648
34 I = 52
03057
XDOT = -4486
031627 Wp = 47
80630
YDOT = -1477
699018 meter/sec RA = 104
48631 deg
ZDOT = 6039
073258 TA = 314
46109
MA = 314
53927
Ha = 221
068 n
mi
Hp = 216
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6089539
06 X = -1929931
97
Y = 21403361
79 feet Y = 6502575
68 meter
Z = 694384
30 Z = 202453
44
XDOT = -14717
951533 XDOT = -4498
508659
YDOT = -4848
093890 feet/sec YDOT = -1527
935316 meter/sec
ZDOT = 19813
232475 ZDOT = 6017
251323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22171462
41 X = -6757861
74
Y = -1915600
50 feet Y = -583875
03 meter
Z = 652135
77 Z = 198770
98
XDOT = 1796
636257 XDOT = 547
614731
YDOT = -13883
522093 feet/sec YDOT = -4231
697534 meter/sec
ZDOT = 19714
916469 ZDOT = 6009
106540
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 19002
56393925
00016717 00000-0 10270-3 0 9001
2 25544 51
6413 105
1284 0002909 226
7669 133
3241 15
53719632 29517
Satellite: ISS
Catalog Number: 25544
Epoch time: 19002
56393925 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 105
1284 deg
Eccentricity:
0002909
Arg of perigee: 226
7669 deg
Mean anomaly: 133
3241 deg
Mean motion: 15
53719632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2951
Checksum: 302
Coasting Arc #2 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2019/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2434282
98 A = 6789178
70 meter
Y = -6076158
53 meter E =
0008109
Z = -1785255
91 I = 52
03360
XDOT = 3961
913162 Wp = 163
35612
YDOT = 3257
623085 meter/sec RA = 99
54420 deg
ZDOT = -5699
059904 TA = 36
14115
MA = 36
08637
Ha = 221
030 n
mi
Hp = 216
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7986492
72 X = 2510719
14
Y = -19934903
32 feet Y = -6048509
10 meter
Z = -5857138
81 Z = -1773246
14
XDOT = 12998
402762 XDOT = 3952
873862
YDOT = 10687
739781 feet/sec YDOT = 3301
878062 meter/sec
ZDOT = -18697
703098 ZDOT = -5679
836032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21164411
50 X = 6450912
63
Y = 3727258
91 feet Y = 1136068
52 meter
Z = -5802218
38 Z = -1768516
16
XDOT = -7468
285816 XDOT = -2276
333517
YDOT = 13506
595021 feet/sec YDOT = 4116
810163 meter/sec
ZDOT = -18611
317773 ZDOT = -5672
729657
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 19003
52871953
00016717 00000-0 10270-3 0 9011
2 25544 51
6415 100
3224 0002992 230
1734 129
9155 15
53723662 29663
Satellite: ISS
Catalog Number: 25544
Epoch time: 19003
52871953 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 100
3224 deg
Eccentricity:
0002992
Arg of perigee: 230
1734 deg
Mean anomaly: 129
9155 deg
Mean motion: 15
53723662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 298
Coasting Arc #3 (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 = -2908636
14 A = 6786215
55 meter
Y = 5239026
21 meter E =
0010536
Z = 3176834
81 I = 52
02912
XDOT = -3414
654868 Wp = 93
47142
YDOT = -4851
050330 meter/sec RA = 94
59670 deg
ZDOT = 4859
192981 TA = 302
98219
MA = 303
08341
Ha = 220
919 n
mi
Hp = 216
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9542769
48 X = -2982435
44
Y = 17188406
19 feet Y = 5206086
79 meter
Z = 10422686
38 Z = 3162527
21
XDOT = -11202
935918 XDOT = -3383
758408
YDOT = -15915
519456 feet/sec YDOT = -4889
063213 meter/sec
ZDOT = 15942
234190 ZDOT = 4842
680408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18903762
21 X = -5761866
72
Y = -5523460
78 feet Y = -1683550
85 meter
Z = 10357475
71 Z = 3156958
60
XDOT = 12578
522087 XDOT = 3833
933532
YDOT = -13203
970381 feet/sec YDOT = -4024
570172 meter/sec
ZDOT = 15868
278284 ZDOT = 4836
651221
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
55781448
00016717 00000-0 10270-3 0 9025
2 25544 51
6422 95
1957 0002841 235
7397 124
3487 15
53747257 29825
Satellite: ISS
Catalog Number: 25544
Epoch time: 19004
55781448 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 95
1957 deg
Eccentricity:
0002841
Arg of perigee: 235
7397 deg
Mean anomaly: 124
3487 deg
Mean motion: 15
53747257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2982
Checksum: 334
Coasting Arc #4 (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 = 3340177
01 A = 6782723
14 meter
Y = -4039560
30 meter E =
0005542
Z = -4310223
73 I = 52
01777
XDOT = 2831
579601 Wp = 74
97469
YDOT = 6155
651705 meter/sec RA = 89
64183 deg
ZDOT = -3577
219451 TA = 158
71414
MA = 158
69108
Ha = 220
877 n
mi
Hp = 216
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10958585
98 X = 3406036
73
Y = -13253150
59 feet Y = -4001839
35 meter
Z = -14141153
96 Z = -4293839
08
XDOT = 9289
959320 XDOT = 2779
910910
YDOT = 20195
707692 feet/sec YDOT = 6187
027933 meter/sec
ZDOT = -11736
284287 ZDOT = -3563
589571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15522777
51 X = 4731342
58
Y = 7541899
33 feet Y = 2298770
92 meter
Z = -14066697
38 Z = -4287529
36
XDOT = -16800
186814 XDOT = -5120
696941
YDOT = 12816
723680 feet/sec YDOT = 3906
537378 meter/sec
ZDOT = -11675
504454 ZDOT = -3558
693758
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
52259098
00016717 00000-0 10270-3 0 9035
2 25544 51
6411 90
3904 0002895 239
6752 120
4115 15
53723391 29973
Satellite: ISS
Catalog Number: 25544
Epoch time: 19005
52259098 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 90
3904 deg
Eccentricity:
0002895
Arg of perigee: 239
6752 deg
Mean anomaly: 120
4115 deg
Mean motion: 15
53723391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 312
Coasting Arc #5 (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 = -3714704
52 A = 6779706
74 meter
Y = 2593155
16 meter E =
0005004
Z = 5043335
74 I = 52
00748
XDOT = -2220
459705 Wp = 153
63426
YDOT = -7064
236393 meter/sec RA = 84
67768 deg
ZDOT = 1991
637116 TA = 277
09481
MA = 277
15172
Ha = 220
809 n
mi
Hp = 216
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12187350
78 X = -3767923
23
Y = 8507726
91 feet Y = 2551316
61 meter
Z = 16546377
09 Z = 5025162
37
XDOT = -7284
972785 XDOT = -2150
974543
YDOT = -23176
628585 feet/sec YDOT = -7088
678829 meter/sec
ZDOT = 6534
242505 ZDOT = 1981
019054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11384480
80 X = -3469989
75
Y = -9696671
80 feet Y = -2955545
56 meter
Z = 16464011
78 Z = 5018230
79
XDOT = 19806
026893 XDOT = 6036
876997
YDOT = -12210
218311 feet/sec YDOT = -3721
674541 meter/sec
ZDOT = 6487
178671 ZDOT = 1977
292059
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
55168115
00016717 00000-0 10270-3 0 9049
2 25544 51
6418 85
2636 0002916 245
2149 114
8701 15
53764176 30136
Satellite: ISS
Catalog Number: 25544
Epoch time: 19006
55168115 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 85
2636 deg
Eccentricity:
0002916
Arg of perigee: 245
2149 deg
Mean anomaly: 114
8701 deg
Mean motion: 15
53764176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 299
Coasting Arc #6 (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 = 4064793
15 A = 6778538
22 meter
Y = -987291
73 meter E =
0012198
Z = -5344450
66 I = 51
99838
XDOT = 1535
528471 Wp = 92
11209
YDOT = 7500
321768 meter/sec RA = 79
70786 deg
ZDOT = -218
549988 TA = 175
81775
MA = 175
80755
Ha = 220
705 n
mi
Hp = 216
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13335935
54 X = 4101491
18
Y = -3239146
11 feet Y = -941630
66 meter
Z = -17534286
95 Z = -5324616
70
XDOT = 5037
823067 XDOT = 1452
605222
YDOT = 24607
354883 feet/sec YDOT = 7517
029485 meter/sec
ZDOT = -717
027519 ZDOT = -211
291729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6798350
69 X = 2072137
29
Y = 12052312
27 feet Y = 3673544
78 meter
Z = -17444616
93 Z = -5317119
24
XDOT = -21409
019267 XDOT = -6525
469073
YDOT = 11088
567845 feet/sec YDOT = 3379
795479 meter/sec
ZDOT = -685
195367 ZDOT = -208
847548
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
51645215
00016717 00000-0 10270-3 0 9058
2 25544 51
6412 80
4575 0002801 251
5956 108
4892 15
53727259 30285
Satellite: ISS
Catalog Number: 25544
Epoch time: 19007
51645215 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 80
4575 deg
Eccentricity:
0002801
Arg of perigee: 251
5956 deg
Mean anomaly: 108
4892 deg
Mean motion: 15
53727259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 307
Coasting Arc #7 (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 = -4352497
06 A = 6779192
57 meter
Y = -642035
87 meter E =
0002480
Z = 5157008
58 I = 51
99404
XDOT = -764
056021 Wp = 31
05378
YDOT = -7466
632850 meter/sec RA = 74
73710 deg
ZDOT = -1572
035829 TA = 74
03999
MA = 74
01266
Ha = 220
742 n
mi
Hp = 216
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14279845
98 X = -4370043
59
Y = -2106416
91 feet Y = -690807
07 meter
Z = 16919319
50 Z = 5135823
48
XDOT = -2506
745476 XDOT = -672
869307
YDOT = -24496
826937 feet/sec YDOT = -7474
667066 meter/sec
ZDOT = -5157
597863 ZDOT = -1575
526424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2161755
74 X = -658903
15
Y = -14384109
06 feet Y = -4384276
44 meter
Z = 16823750
61 Z = 5127879
19
XDOT = 21676
882914 XDOT = 6607
113912
YDOT = -9316
736933 feet/sec YDOT = -2839
741417 meter/sec
ZDOT = -5172
414434 ZDOT = -1576
551919
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
54553676
00016717 00000-0 10270-3 0 9062
2 25544 51
6412 75
3309 0002794 255
9900 104
0942 15
53777739 30445
Satellite: ISS
Catalog Number: 25544
Epoch time: 19008
54553676 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 75
3309 deg
Eccentricity:
0002794
Arg of perigee: 255
9900 deg
Mean anomaly: 104
0942 deg
Mean motion: 15
53777739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3044
Checksum: 321
Coasting Arc #8 (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 = 4568771
19 A = 6781838
14 meter
Y = 2173332
67 meter E =
0007447
Z = -4523802
27 I = 51
99188
XDOT = -119
463476 Wp = 120
62727
YDOT = 6950
685256 meter/sec RA = 69
76995 deg
ZDOT = 3218
847716 TA = 181
59797
MA = 181
60035
Ha = 220
665 n
mi
Hp = 216
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14989406
78 X = 4566102
54
Y = 7130356
51 feet Y = 2224409
23 meter
Z = -14841870
95 Z = -4501615
62
XDOT = -391
940538 XDOT = -212
814206
YDOT = 22804
085485 feet/sec YDOT = 6948
827157 meter/sec
ZDOT = 10560
524001 ZDOT = 3218
041162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2159985
57 X = -658363
60
Y = 16547328
40 feet Y = 5043625
69 meter
Z = -14741974
71 Z = -4493353
89
XDOT = -20641
721411 XDOT = -6291
596686
YDOT = 6709
165778 feet/sec YDOT = 2044
953729 meter/sec
ZDOT = 10555
995654 ZDOT = 3217
467475
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
51030414
00016717 00000-0 10270-3 0 9071
2 25544 51
6401 70
5245 0002569 259
1481 100
9382 15
53765778 30598
Satellite: ISS
Catalog Number: 25544
Epoch time: 19009
51030414 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 70
5245 deg
Eccentricity:
0002569
Arg of perigee: 259
1481 deg
Mean anomaly: 100
9382 deg
Mean motion: 15
53765778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 303
Coasting Arc #9 (Orbit 3072)
---------------------------------------
Vector Time (GMT): 2019/010/09:34:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4650407
87 A = 6780623
79 meter
Y = 1091378
53 meter E =
0009065
Z = -4821083
77 I = 51
97848
XDOT = 1031
671492 Wp = 116
13202
YDOT = 7128
057330 meter/sec RA = 65
31323 deg
ZDOT = 2608
682133 TA = 179
48147
MA = 179
48053
Ha = 220
597 n
mi
Hp = 216
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15257243
68 X = 4661275
89
Y = 3580638
23 feet Y = 1143443
66 meter
Z = -15817203
98 Z = -4798467
77
XDOT = 3384
748990 XDOT = 939
215567
YDOT = 23386
014861 feet/sec YDOT = 7139
077106 meter/sec
ZDOT = 8558
668415 ZDOT = 2613
469346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8038746
66 X = -2450209
98
Y = 13571971
66 feet Y = 4136736
96 meter
Z = -15715232
54 Z = -4790002
88
XDOT = -22313
642934 XDOT = -6801
198366
YDOT = -3281
940141 feet/sec YDOT = -1000
335355 meter/sec
ZDOT = 8579
365831 ZDOT = 2614
990705
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
41074951
00016717 00000-0 10270-3 0 9087
2 25544 51
6417 66
0371 0002655 260
4164 99
6689 15
53783292 30735
Satellite: ISS
Catalog Number: 25544
Epoch time: 19010
41074951 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 66
0371 deg
Eccentricity:
0002655
Arg of perigee: 260
4164 deg
Mean anomaly: 99
6689 deg
Mean motion: 15
53783292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3073
Checksum: 316
Coasting Arc #10 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2019/011/09:34:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4942495
95 A = 6783986
09 meter
Y = -2496561
26 meter E =
0008658
Z = 3913328
41 I = 51
97473
XDOT = 10
636759 Wp = 79
21760
YDOT = -6475
775951 meter/sec RA = 60
34894 deg
ZDOT = -4108
611130 TA = 53
67262
MA = 53
59272
Ha = 220
725 n
mi
Hp = 216
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16215537
89 X = -4933219
85
Y = -8190817
78 feet Y = -2551779
98 meter
Z = 12839003
97 Z = 3889342
42
XDOT = 34
897502 XDOT = 103
006957
YDOT = -21245
984091 feet/sec YDOT = -6475
140368 meter/sec
ZDOT = -13479
695310 ZDOT = -4108
335370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12490896
60 X = 3807225
28
Y = -13295544
16 feet Y = -4052481
86 meter
Z = 12731032
79 Z = 3880418
79
XDOT = 19363
044133 XDOT = 5901
855852
YDOT = 5256
472013 feet/sec YDOT = 1602
172670 meter/sec
ZDOT = -13477
609271 ZDOT = -4107
975306
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
43982801
00016717 00000-0 10270-3 0 9093
2 25544 51
6417 60
9100 0002603 267
4635 92
6220 15
53770111 30898
Satellite: ISS
Catalog Number: 25544
Epoch time: 19011
43982801 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 60
9100 deg
Eccentricity:
0002603
Arg of perigee: 267
4635 deg
Mean anomaly: 92
6220 deg
Mean motion: 15
53770111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 285
Coasting Arc #11 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2019/012/09:34:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5058488
16 A = 6787489
54 meter
Y = 3649494
75 meter E =
0003278
Z = -2672961
93 I = 51
96800
XDOT = -1190
497669 Wp = 23
01390
YDOT = 5476
226977 meter/sec RA = 55
39287 deg
ZDOT = 5229
016214 TA = 306
98178
MA = 307
01178
Ha = 220
634 n
mi
Hp = 216
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16596089
77 X = 5030286
13
Y = 11973407
98 feet Y = 3705904
68 meter
Z = -8769560
14 Z = -2648458
39
XDOT = -3905
832247 XDOT = -1277
045230
YDOT = 17966
623939 feet/sec YDOT = 5462
429928 meter/sec
ZDOT = 17155
565005 ZDOT = 5223
023255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15999487
19 X = -4876643
70
Y = 12834675
79 feet Y = 3912009
18 meter
Z = -8659410
28 Z = -2639388
25
XDOT = -15296
319175 XDOT = -4662
318085
YDOT = -7523
625052 feet/sec YDOT = -2293
200916 meter/sec
ZDOT = 17127
789624 ZDOT = 5220
550277
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
40458778
00016717 00000-0 10270-3 0 9104
2 25544 51
6409 56
1038 0002741 271
1359 88
9480 15
53744890 31043
Satellite: ISS
Catalog Number: 25544
Epoch time: 19012
40458778 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 56
1038 deg
Eccentricity:
0002741
Arg of perigee: 271
1359 deg
Mean anomaly: 88
9480 deg
Mean motion: 15
53744890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 311
Coasting Arc #12 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2019/013/09:38:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4153255
55 A = 6790348
80 meter
Y = -5358582
32 meter E =
0009705
Z = -269011
04 I = 51
95807
XDOT = 3881
562458 Wp = 147
02322
YDOT = -2711
201447 meter/sec RA = 50
44277 deg
ZDOT = -6031
282325 TA = 35
86243
MA = 35
79731
Ha = 220
609 n
mi
Hp = 216
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13626166
51 X = -4091719
01
Y = -17580650
64 feet Y = -5404682
83 meter
Z = -882582
16 Z = -289036
49
XDOT = 12734
784967 XDOT = 3940
887725
YDOT = -8895
017871 feet/sec YDOT = -2667
463240 meter/sec
ZDOT = -19787
671671 ZDOT = -6012
283318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20284508
01 X = 6182718
04
Y = -9117239
19 feet Y = -2778934
51 meter
Z = -972278
77 Z = -296350
57
XDOT = 4966
120949 XDOT = 1513
673665
YDOT = 13114
996579 feet/sec YDOT = 3997
450957 meter/sec
ZDOT = -19701
538923 ZDOT = -6005
029064
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
43366305
00016717 00000-0 10270-3 0 9113
2 25544 51
6409 50
9769 0002620 275
1201 84
9653 15
53764794 31203
Satellite: ISS
Catalog Number: 25544
Epoch time: 19013
43366305 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 50
9769 deg
Eccentricity:
0002620
Arg of perigee: 275
1201 deg
Mean anomaly: 84
9653 deg
Mean motion: 15
53764794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 300
Coasting Arc #13 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/014/09:38:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3448195
23 A = 6788969
04 meter
Y = 5548000
46 meter E =
0011996
Z = 1825737
24 I = 51
93184
XDOT = -5010
532462 Wp = 58
60159
YDOT = 1240
369273 meter/sec RA = 45
49366 deg
ZDOT = 5672
678661 TA = 321
39180
MA = 321
47752
Ha = 220
684 n
mi
Hp = 216
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11312976
48 X = 3377031
30
Y = 18202101
23 feet Y = 5586162
61 meter
Z = 5989951
57 Z = 1842314
50
XDOT = -16438
754796 XDOT = -5051
584758
YDOT = 4069
452994 feet/sec YDOT = 1184
108287 meter/sec
ZDOT = 18611
150461 ZDOT = 5648
239873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20220448
77 X = -6163192
79
Y = 7038484
96 feet Y = 2145330
21 meter
Z = 6064043
78 Z = 1848320
54
XDOT = 146
776157 XDOT = 44
737373
YDOT = -15577
170107 feet/sec YDOT = -4747
921449 meter/sec
ZDOT = 18500
657365 ZDOT = 5639
000365
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
46273533
00016717 00000-0 10270-3 0 9128
2 25544 51
6414 45
8495 0002560 283
2134 76
8733 15
53755488 31362
Satellite: ISS
Catalog Number: 25544
Epoch time: 19014
46273533 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 45
8495 deg
Eccentricity:
0002560
Arg of perigee: 283
2134 deg
Mean anomaly: 76
8733 deg
Mean motion: 15
53755488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 314
Coasting Arc #14 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2019/015/09:38:56
900
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2448272
90 A = 6785888
83 meter
Y = -5437534
94 meter E =
0002180
Z = -3240417
60 I = 51
89682
XDOT = 5976
200364 Wp = 87
56738
YDOT = 164
427095 meter/sec RA = 40
53830 deg
ZDOT = -4793
875963 TA = 129
78789
MA = 129
76869
Ha = 220
705 n
mi
Hp = 216
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8032391
40 X = -2371546
83
Y = -17839681
55 feet Y = -5464484
08 meter
Z = -10631291
33 Z = -3252124
22
XDOT = 19606
956576 XDOT = 5997
203401
YDOT = 539
458973 feet/sec YDOT = 231
374781 meter/sec
ZDOT = -15727
939510 ZDOT = -4764
794948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19076286
06 X = 5814451
99
Y = -4214047
96 feet Y = -1284441
82 meter
Z = -10683399
02 Z = -3256300
02
XDOT = -4795
397919 XDOT = -1461
637286
YDOT = 17810
294699 feet/sec YDOT = 5428
577824 meter/sec
ZDOT = -15596
684108 ZDOT = -4753
869316
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
42748947
00016717 00000-0 10270-3 0 9132
2 25544 51
6405 41
0436 0002492 285
9289 74
1589 15
53766462 31510
Satellite: ISS
Catalog Number: 25544
Epoch time: 19015
42748947 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 41
0436 deg
Eccentricity:
0002492
Arg of perigee: 285
9289 deg
Mean anomaly: 74
1589 deg
Mean motion: 15
53766462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 326
Coasting Arc #15 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2019/016/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5939772
18 A = 6787028
66 meter
Y = -1588412
68 meter E =
0010915
Z = 2862406
59 I = 51
87937
XDOT = -946
330198 Wp = 98
87916
YDOT = -5658
724901 meter/sec RA = 36
39808 deg
ZDOT = -5088
994094 TA = 48
67690
MA = 48
58301
Ha = 220
782 n
mi
Hp = 216
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19487441
55 X = -5935472
57
Y = -5211327
70 feet Y = -1654811
48 meter
Z = 9391097
75 Z = 2833563
89
XDOT = -3104
757869 XDOT = -858
263020
YDOT = -18565
370411 feet/sec YDOT = -5668
814706 meter/sec
ZDOT = -16696
174850 ZDOT = -5093
377432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20230204
53 X = 6166166
34
Y = -285569
81 feet Y = -87041
68 meter
Z = 9261117
97 Z = 2822788
76
XDOT = 7894
644785 XDOT = 2406
287731
YDOT = 15584
177409 feet/sec YDOT = 4750
057274 meter/sec
ZDOT = -16715
185160 ZDOT = -5094
788437
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
26360886
00016717 00000-0 10270-3 0 9148
2 25544 51
6409 36
8751 0002464 281
9968 78
0908 15
53758596 31646
Satellite: ISS
Catalog Number: 25544
Epoch time: 19016
26360886 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 36
8751 deg
Eccentricity:
0002464
Arg of perigee: 281
9968 deg
Mean anomaly: 78
0908 deg
Mean motion: 15
53758596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 348
Coasting Arc #16 (Orbit 3178)
---------------------------------------
Vector Time (GMT): 2019/017/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929891
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6160400
41 A = 6789593
61 meter
Y = 2470185
85 meter E =
0008350
Z = -1408457
02 I = 51
86194
XDOT = -659
204460 Wp = 20
44533
YDOT = 4950
739890 meter/sec RA = 31
44101 deg
ZDOT = 5817
461442 TA = 324
25154
MA = 324
30741
Ha = 220
815 n
mi
Hp = 216
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20211287
43 X = 6139161
71
Y = 8104284
29 feet Y = 2538957
10 meter
Z = -4620921
98 Z = -1378583
65
XDOT = -2162
744290 XDOT = -742
773870
YDOT = 16242
584942 feet/sec YDOT = 4942
900477 meter/sec
ZDOT = 19086
159586 ZDOT = 5814
056713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21717344
12 X = -6619446
49
Y = -1938426
21 feet Y = -590832
31 meter
Z = -4486418
60 Z = -1367460
39
XDOT = -2620
923073 XDOT = -798
857353
YDOT = -14632
491960 feet/sec YDOT = -4459
983549 meter/sec
ZDOT = 19070
103919 ZDOT = 5812
567675
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
22835850
00016717 00000-0 10270-3 0 9154
2 25544 51
6422 32
0686 0002510 291
6942 68
3943 15
53763967 31793
Satellite: ISS
Catalog Number: 25544
Epoch time: 19017
22835850 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 32
0686 deg
Eccentricity:
0002510
Arg of perigee: 291
6942 deg
Mean anomaly: 68
3943 deg
Mean motion: 15
53763967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3179
Checksum: 321
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