[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 28th 2017
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) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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
333/15:51:31
784 0
5 1
2 1
2
N/A -1
1 -0
1 221
5
000/00:03:03
567 0
2 -0
0 214
6
334/13:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
6
338/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 214
9
338/19:53:38
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
1
340/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
2
341/18:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
2
344/22:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2017/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4858321
14 A = 6779461
41 meter
Y = -528782
68 meter E =
0010796
Z = 4694691
76 I = 51
31476
XDOT = -1921
220506 Wp = 130
05402
YDOT = 6896
996181 meter/sec RA = 303
50473 deg
ZDOT = 2753
981309 TA = 292
50667
MA = 292
62092
Ha = 221
472 n
mi
Hp = 213
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15939373
81 X = 4841068
26
Y = -1734851
32 feet Y = -474550
18 meter
Z = 15402532
02 Z = 4718250
35
XDOT = -6303
216882 XDOT = -2011
579426
YDOT = 22627
940228 feet/sec YDOT = 6875
006494 meter/sec
ZDOT = 9035
371749 ZDOT = 2744
429181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4931113
34 X = -1503003
35
Y = 15150086
17 feet Y = 4617746
27 meter
Z = 15507106
42 Z = 4726566
04
XDOT = -16907
268017 XDOT = -5153
335292
YDOT = -14743
595021 feet/sec YDOT = -4493
847762 meter/sec
ZDOT = 8991
828458 ZDOT = 2740
709314
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 17331
55308095
00016717 00000-0 10270-3 0 9007
2 25544 51
6381 303
9207 0003660 159
1066 201
0237 15
54260054 7153
Satellite: ISS
Catalog Number: 25544
Epoch time: 17331
55308095 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 303
9207 deg
Eccentricity:
0003660
Arg of perigee: 159
1066 deg
Mean anomaly: 201
0237 deg
Mean motion: 15
54260054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 274
Coasting Arc #2 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2017/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157501
45 A = 6777273
86 meter
Y = -1145798
92 meter E =
0015732
Z = -5241533
36 I = 51
29029
XDOT = 3006
948222 Wp = 96
40359
YDOT = -6989
441105 meter/sec RA = 298
48199 deg
ZDOT = -861
128331 TA = 165
33317
MA = 165
28748
Ha = 221
585 n
mi
Hp = 213
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13640096
62 X = -4118918
65
Y = -3759182
81 feet Y = -1192075
13 meter
Z = -17196631
76 Z = -5261635
82
XDOT = 9865
315688 XDOT = 3089
065542
YDOT = -22931
237222 feet/sec YDOT = -6955
356196 meter/sec
ZDOT = -2825
224183 ZDOT = -846
321946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8802523
11 X = 2683009
04
Y = -10937629
86 feet Y = -3333789
58 meter
Z = -17285591
54 Z = -5268648
30
XDOT = 16357
432253 XDOT = 4985
745351
YDOT = 17503
212279 feet/sec YDOT = 5334
979103 meter/sec
ZDOT = -2758
376836 ZDOT = -840
753260
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 17332
51754064
00016717 00000-0 10270-3 0 9016
2 25544 51
6385 299
1112 0003663 160
7808 199
3483 15
54237435 7309
Satellite: ISS
Catalog Number: 25544
Epoch time: 17332
51754064 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 299
1112 deg
Eccentricity:
0003663
Arg of perigee: 160
7808 deg
Mean anomaly: 199
3483 deg
Mean motion: 15
54237435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 309
Coasting Arc #3 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2017/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3317571
15 A = 6777426
75 meter
Y = 2814505
27 meter E =
0004401
Z = 5192840
03 I = 51
27661
XDOT = -3820
519609 Wp = 106
62490
YDOT = 6559
373380 meter/sec RA = 293
45625 deg
ZDOT = -1114
783664 TA = 354
10592
MA = 354
11110
Ha = 221
376 n
mi
Hp = 214
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10884419
78 X = 3260627
30
Y = 9233941
18 feet Y = 2851286
14 meter
Z = 17036876
73 Z = 5208817
79
XDOT = -12534
513154 XDOT = -3888
169161
YDOT = 21520
253870 feet/sec YDOT = 6516
271486 meter/sec
ZDOT = -3657
426718 ZDOT = -1133
507097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12632763
46 X = -3850466
30
Y = 6461130
92 feet Y = 1969352
70 meter
Z = 17107264
74 Z = 5214294
29
XDOT = -14690
677083 XDOT = -4477
718375
YDOT = -18820
429086 feet/sec YDOT = -5736
466785 meter/sec
ZDOT = -3741
560449 ZDOT = -1140
427625
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 17333
54629128
00016717 00000-0 10270-3 0 9023
2 25544 51
6390 293
9821 0003564 164
4155 195
7108 15
54247810 7469
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
54629128 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 293
9821 deg
Eccentricity:
0003564
Arg of perigee: 164
4155 deg
Mean anomaly: 195
7108 deg
Mean motion: 15
54247810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 316
Coasting Arc #4 (Orbit 747)
---------------------------------------
Vector Time (GMT): 2017/333/15:53:03
567
Vector Time (MET): N/A
Weight (LBS) : 933686
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2987035
10 A = 6778639
51 meter
Y = -3389862
17 meter E =
0014318
Z = -5066217
31 I = 51
27945
XDOT = 4107
666575 Wp = 115
67588
YDOT = -6223
730867 meter/sec RA = 292
64109 deg
ZDOT = 1740
259994 TA = 171
27164
MA = 171
24671
Ha = 221
468 n
mi
Hp = 214
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9799983
92 X = -2924297
09
Y = -11121595
06 feet Y = -3422914
36 meter
Z = -16621447
87 Z = -5080575
35
XDOT = 13476
596376 XDOT = 4168
503224
YDOT = -20419
064524 feet/sec YDOT = -6177
456006 meter/sec
ZDOT = 5709
514417 ZDOT = 1760
361784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3272668
52 X = 997509
36
Y = -14384619
89 feet Y = -4384432
14 meter
Z = -16684557
00 Z = -5085452
97
XDOT = 23366
727622 XDOT = 7122
178579
YDOT = -1419
270324 feet/sec YDOT = -432
593595 meter/sec
ZDOT = 5799
702976 ZDOT = 1767
749467
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 17333
67488468
00016717 00000-0 10270-3 0 9038
2 25544 51
6419 293
3416 0003204 180
2053 179
9099 15
54044206 7488
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
67488468 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 293
3416 deg
Eccentricity:
0003204
Arg of perigee: 180
2053 deg
Mean anomaly: 179
9099 deg
Mean motion: 15
54044206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 748
Checksum: 320
Coasting Arc #5 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2017/334/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933686
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4048124
83 A = 6777618
99 meter
Y = -1285716
00 meter E =
0015013
Z = -5294394
51 I = 51
26312
XDOT = 2358
390160 Wp = 101
91860
YDOT = -7285
301911 meter/sec RA = 288
16089 deg
ZDOT = -37
174963 TA = 167
74310
MA = 167
70653
Ha = 221
400 n
mi
Hp = 214
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13281249
45 X = -4007728
62
Y = -4218228
35 feet Y = -1330758
86 meter
Z = -17370060
73 Z = -5313961
39
XDOT = 7737
500526 XDOT = 2439
861659
YDOT = -23901
909157 feet/sec YDOT = -7258
473244 meter/sec
ZDOT = -121
965102 ZDOT = -25
520730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4222173
59 X = 1286918
51
Y = -13166002
27 feet Y = -4012997
49 meter
Z = -17456622
85 Z = -5320778
65
XDOT = 22940
388373 XDOT = 6992
230376
YDOT = 7434
716491 feet/sec YDOT = 2266
101587 meter/sec
ZDOT = -69
072322 ZDOT = -21
053244
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 17334
57516358
00016717 00000-0 10270-3 0 9049
2 25544 51
6397 288
8532 0003187 183
5469 176
5662 15
54038815 7622
Satellite: ISS
Catalog Number: 25544
Epoch time: 17334
57516358 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 288
8532 deg
Eccentricity:
0003187
Arg of perigee: 183
5469 deg
Mean anomaly: 176
5662 deg
Mean motion: 15
54038815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 345
Coasting Arc #6 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2017/335/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933686
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3453803
90 A = 6778717
20 meter
Y = 2950764
90 meter E =
0004121
Z = 5027841
56 I = 51
25830
XDOT = -3099
142070 Wp = 90
09030
YDOT = 6770
873632 meter/sec RA = 283
13715 deg
ZDOT = -1843
506676 TA = 17
86199
MA = 17
84751
Ha = 221
168 n
mi
Hp = 214
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11331377
61 X = 3396127
60
Y = 9680987
19 feet Y = 2989064
94 meter
Z = 16495543
18 Z = 5044479
53
XDOT = -10167
788945 XDOT = -3165
670397
YDOT = 22214
152336 feet/sec YDOT = 6735
845023 meter/sec
ZDOT = -6048
250248 ZDOT = -1858
722931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9490049
59 X = -2892567
11
Y = 11385821
85 feet Y = 3470398
50 meter
Z = 16568844
14 Z = 5050183
69
XDOT = -21552
467502 XDOT = -6569
192095
YDOT = -9056
369176 feet/sec YDOT = -2760
381325 meter/sec
ZDOT = -6116
846974 ZDOT = -1864
414958
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 17335
60404924
00016717 00000-0 10270-3 0 9050
2 25544 51
6403 283
7258 0003193 188
7039 171
4058 15
54052432 7787
Satellite: ISS
Catalog Number: 25544
Epoch time: 17335
60404924 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 283
7258 deg
Eccentricity:
0003193
Arg of perigee: 188
7039 deg
Mean anomaly: 171
4058 deg
Mean motion: 15
54052432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 311
Coasting Arc #7 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2017/336/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933686
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2821493
18 A = 6781736
06 meter
Y = -4461880
67 meter E =
0009363
Z = -4267172
13 I = 51
26283
XDOT = 3680
479612 Wp = 129
67293
YDOT = -5710
549775 meter/sec RA = 278
11665 deg
ZDOT = 3536
880621 TA = 176
62907
MA = 176
62276
Ha = 221
215 n
mi
Hp = 214
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9256867
38 X = -2750661
23
Y = -14638716
10 feet Y = -4493036
15 meter
Z = -13999908
55 Z = -4280706
70
XDOT = 12075
064345 XDOT = 3726
882141
YDOT = -18735
399524 feet/sec YDOT = -5669
132968 meter/sec
ZDOT = 11603
939045 ZDOT = 3554
871916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14317818
63 X = 4364071
12
Y = -9660118
05 feet Y = -2944403
98 meter
Z = -14059204
51 Z = -4285245
53
XDOT = 18429
486581 XDOT = 5617
307510
YDOT = 10306
511801 feet/sec YDOT = 3141
424797 meter/sec
ZDOT = 11684
664341 ZDOT = 3561
485691
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 17336
56862294
00016717 00000-0 10270-3 0 9065
2 25544 51
6410 278
9170 0003158 191
6237 168
4844 15
54067277 7937
Satellite: ISS
Catalog Number: 25544
Epoch time: 17336
56862294 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 278
9170 deg
Eccentricity:
0003158
Arg of perigee: 191
6237 deg
Mean anomaly: 168
4844 deg
Mean motion: 15
54067277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 336
Coasting Arc #8 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2017/337/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933686
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2142100
29 A = 6785532
67 meter
Y = 5661781
25 meter E =
0012940
Z = 3049861
64 I = 51
27191
XDOT = -4153
587493 Wp = 109
63554
YDOT = 4210
867083 meter/sec RA = 273
10733 deg
ZDOT = -4887
078604 TA = 35
14170
MA = 35
05642
Ha = 221
085 n
mi
Hp = 214
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7027888
10 X = 2063814
51
Y = 18575397
80 feet Y = 5685297
64 meter
Z = 10006107
75 Z = 3060077
95
XDOT = -13627
255555 XDOT = -4176
626334
YDOT = 13815
180718 feet/sec YDOT = 4164
290521 meter/sec
ZDOT = -16033
722453 ZDOT = -4907
311367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18193883
22 X = -5545495
61
Y = 7907519
21 feet Y = 2410211
86 meter
Z = 10050500
49 Z = 3063392
55
XDOT = -13913
883357 XDOT = -4240
951647
YDOT = -11466
979305 feet/sec YDOT = -3495
135292 meter/sec
ZDOT = -16124
143686 ZDOT = -4914
638995
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 17337
59749648
00016717 00000-0 10270-3 0 9077
2 25544 51
6411 273
7894 0003122 194
8398 165
2663 15
54065178 8098
Satellite: ISS
Catalog Number: 25544
Epoch time: 17337
59749648 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 273
7894 deg
Eccentricity:
0003122
Arg of perigee: 194
8398 deg
Mean anomaly: 165
2663 deg
Mean motion: 15
54065178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 349
Coasting Arc #9 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2017/338/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 919252
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4160676
20 A = 6778283
98 meter
Y = -1604845
43 meter E =
0013551
Z = -5116745
98 I = 51
24736
XDOT = 987
825477 Wp = 114
81371
YDOT = -7439
050295 meter/sec RA = 268
16030 deg
ZDOT = 1527
588059 TA = 170
01943
MA = 169
99249
Ha = 221
023 n
mi
Hp = 214
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13650512
46 X = -4117566
16
Y = -5265240
90 feet Y = -1651131
30 meter
Z = -16787224
34 Z = -5136853
03
XDOT = 3240
897235 XDOT = 1063
517136
YDOT = -24406
332989 feet/sec YDOT = -7427
580719 meter/sec
ZDOT = 5011
771846 ZDOT = 1532
569640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5226144
06 X = 1592928
71
Y = -13555552
85 feet Y = -4131732
51 meter
Z = -16876153
54 Z = -5143851
60
XDOT = 23426
905562 XDOT = 7140
520815
YDOT = 2753
725674 feet/sec YDOT = 839
335585 meter/sec
ZDOT = 5035
065198 ZDOT = 1534
687872
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 17338
56206051
00016717 00000-0 10270-3 0 9082
2 25544 51
6414 268
9816 0003119 200
0542 160
0488 15
54078486 8249
Satellite: ISS
Catalog Number: 25544
Epoch time: 17338
56206051 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 268
9816 deg
Eccentricity:
0003119
Arg of perigee: 200
0542 deg
Mean anomaly: 160
0488 deg
Mean motion: 15
54078486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 824
Checksum: 305
Coasting Arc #10 (Orbit 828)
---------------------------------------
Vector Time (GMT): 2017/338/19:53:38
000
Vector Time (MET): N/A
Weight (LBS) : 919252
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3203097
07 A = 6781589
85 meter
Y = -4172883
04 meter E =
0010186
Z = 4276716
99 I = 51
25518
XDOT = 3161
954740 Wp = 127
36708
YDOT = 6039
383254 meter/sec RA = 266
78917 deg
ZDOT = 3512
708214 TA = 286
61231
MA = 286
72413
Ha = 220
951 n
mi
Hp = 215
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10508848
66 X = 3228746
86
Y = -13690561
14 feet Y = -4136920
92 meter
Z = 14031223
72 Z = 4292338
63
XDOT = 10373
867257 XDOT = 3077
122511
YDOT = 19814
249521 feet/sec YDOT = 6074
267642 meter/sec
ZDOT = 11524
633249 ZDOT = 3527
862884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7516932
98 X = 2291161
17
Y = -15472390
05 feet Y = -4715984
49 meter
Z = 14101186
77 Z = 4298041
73
XDOT = 12869
737728 XDOT = 3922
696060
YDOT = 16851
455954 feet/sec YDOT = 5136
323775 meter/sec
ZDOT = 11590
886643 ZDOT = 3532
902249
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 17338
88357909
00016717 00000-0 10270-3 0 9097
2 25544 51
6377 267
3751 0003482 201
5415 158
5592 15
54095659 8290
Satellite: ISS
Catalog Number: 25544
Epoch time: 17338
88357909 = yrday
fracday
Element set: 909
Inclination: 51
6377 deg
RA of node: 267
3751 deg
Eccentricity:
0003482
Arg of perigee: 201
5415 deg
Mean anomaly: 158
5592 deg
Mean motion: 15
54095659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 829
Checksum: 351
Coasting Arc #11 (Orbit 843)
---------------------------------------
Vector Time (GMT): 2017/339/19:53:38
000
Vector Time (MET): N/A
Weight (LBS) : 919252
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3720552
89 A = 6778510
38 meter
Y = 2589929
86 meter E =
0011676
Z = -5049767
81 I = 51
24900
XDOT = -2467
777675 Wp = 90
39354
YDOT = -7027
129570 meter/sec RA = 261
76902 deg
ZDOT = -1789
558317 TA = 162
19499
MA = 162
15404
Ha = 220
979 n
mi
Hp = 214
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12206538
34 X = -3724708
22
Y = 8497145
21 feet Y = 2548301
46 meter
Z = -16567479
71 Z = -5067851
01
XDOT = -8096
383448 XDOT = -2380
322170
YDOT = -23054
887040 feet/sec YDOT = -7054
236741 meter/sec
ZDOT = -5871
254320 ZDOT = -1801
334500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10001891
26 X = -3048576
46
Y = 10885082
90 feet Y = 3317773
27 meter
Z = -16648110
42 Z = -5074344
06
XDOT = -12005
530945 XDOT = -3659
285832
YDOT = -20071
001315 feet/sec YDOT = -6117
641201 meter/sec
ZDOT = -5922
382443 ZDOT = -1805
142168
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 17339
84813687
00016717 00000-0 10270-3 0 9106
2 25544 51
6390 262
5676 0003352 200
0133 160
0888 15
54101484 8442
Satellite: ISS
Catalog Number: 25544
Epoch time: 17339
84813687 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 262
5676 deg
Eccentricity:
0003352
Arg of perigee: 200
0133 deg
Mean anomaly: 160
0888 deg
Mean motion: 15
54101484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 844
Checksum: 302
Coasting Arc #12 (Orbit 853)
---------------------------------------
Vector Time (GMT): 2017/340/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1596879
30 A = 6789409
80 meter
Y = 6582589
65 meter E =
0013770
Z = 329848
34 I = 51
28973
XDOT = -4597
725842 Wp = 143
69169
YDOT = 1420
596756 meter/sec RA = 258
60066 deg
ZDOT = -5973
962209 TA = 32
73461
MA = 32
64936
Ha = 220
840 n
mi
Hp = 215
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5239105
31 X = 1521550
09
Y = 21596422
74 feet Y = 6600025
82 meter
Z = 1082179
58 Z = 337423
26
XDOT = -15084
402369 XDOT = -4584
250968
YDOT = 4660
750511 feet/sec YDOT = 1369
257840 meter/sec
ZDOT = -19599
613548 ZDOT = -5996
263718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21269608
95 X = -6482976
81
Y = -6433185
41 feet Y = -1960834
91 meter
Z = 1114752
29 Z = 339776
50
XDOT = 3092
540430 XDOT = 942
606323
YDOT = -13702
829968 feet/sec YDOT = -4176
622574 meter/sec
ZDOT = -19698
776300 ZDOT = -6004
187016
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 17340
49117195
00016717 00000-0 10270-3 0 9111
2 25544 51
6402 259
3655 0003042 207
2809 152
8185 15
54084976 8548
Satellite: ISS
Catalog Number: 25544
Epoch time: 17340
49117195 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 259
3655 deg
Eccentricity:
0003042
Arg of perigee: 207
2809 deg
Mean anomaly: 152
8185 deg
Mean motion: 15
54084976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 854
Checksum: 313
Coasting Arc #13 (Orbit 869)
---------------------------------------
Vector Time (GMT): 2017/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -814257
58 A = 6788645
65 meter
Y = -6598482
57 meter E =
0011183
Z = 1349133
96 I = 51
29382
XDOT = 5000
404488 Wp = 67
43239
YDOT = 572
712226 meter/sec RA = 253
60697 deg
ZDOT = 5784
766521 TA = 307
33180
MA = 307
43365
Ha = 220
750 n
mi
Hp = 215
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2671448
75 X = -746964
49
Y = -21648564
86 feet Y = -6607212
02 meter
Z = 4426292
52 Z = 1345341
41
XDOT = 16405
526536 XDOT = 4965
529090
YDOT = 1878
977118 feet/sec YDOT = 628
434648 meter/sec
ZDOT = 18978
892784 ZDOT = 5808
972266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20177111
25 X = 6149983
51
Y = 8295834
71 feet Y = 2528570
42 meter
Z = 4410484
42 Z = 1344315
65
XDOT = -9039
603296 XDOT = -2755
271085
YDOT = 11778
939135 feet/sec YDOT = 3590
220648 meter/sec
ZDOT = 19086
202548 ZDOT = 5817
474537
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 17341
52002351
00016717 00000-0 10270-3 0 9124
2 25544 51
6392 254
2375 0003080 212
1454 147
9511 15
54100799 8700
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
52002351 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 254
2375 deg
Eccentricity:
0003080
Arg of perigee: 212
1454 deg
Mean anomaly: 147
9511 deg
Mean motion: 15
54100799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 870
Checksum: 278
Coasting Arc #14 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2017/341/18:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1555477
44 A = 6782918
93 meter
Y = 5338102
11 meter E =
0004678
Z = -3888186
89 I = 51
27522
XDOT = -4823
673948 Wp = 101
98515
YDOT = -4358
112732 meter/sec RA = 252
13857 deg
ZDOT = -4058
650968 TA = 125
28523
MA = 125
24147
Ha = 220
705 n
mi
Hp = 215
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5103272
45 X = -1596167
04
Y = 17513458
35 feet Y = 5320480
51 meter
Z = -12756518
67 Z = -3895841
30
XDOT = -15825
701928 XDOT = -4754
866948
YDOT = -14298
270117 feet/sec YDOT = -4411
669290 meter/sec
ZDOT = -13315
784017 ZDOT = -4081
916095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8807736
19 X = -2684597
99
Y = 15946779
17 feet Y = 4860578
29 meter
Z = -12791301
69 Z = -3898788
76
XDOT = -10979
362789 XDOT = -3346
509778
YDOT = -16813
905168 feet/sec YDOT = -5124
878295 meter/sec
ZDOT = -13418
341908 ZDOT = -4089
910614
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 17341
77723436
00016717 00000-0 10270-3 0 9136
2 25544 51
6369 252
9527 0003184 211
3130 148
7834 15
54117230 8744
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
77723436 = yrday
fracday
Element set: 913
Inclination: 51
6369 deg
RA of node: 252
9527 deg
Eccentricity:
0003184
Arg of perigee: 211
3130 deg
Mean anomaly: 148
7834 deg
Mean motion: 15
54117230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 304
Coasting Arc #15 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2017/342/18:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2475232
07 A = 6779500
56 meter
Y = -4074071
14 meter E =
0007463
Z = 4819202
53 I = 51
27477
XDOT = 4534
945272 Wp = 145
57761
YDOT = 5674
069429 meter/sec RA = 247
12200 deg
ZDOT = 2459
604922 TA = 280
10577
MA = 280
18995
Ha = 220
589 n
mi
Hp = 215
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8120840
13 X = 2497196
18
Y = -13366375
12 feet Y = -4046268
89 meter
Z = 15811031
91 Z = 4831279
51
XDOT = 14878
429370 XDOT = 4459
211725
YDOT = 18615
713350 feet/sec YDOT = 5724
358682 meter/sec
ZDOT = 8069
569955 ZDOT = 2481
450655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10607131
95 X = 3233053
82
Y = -11418394
81 feet Y = -3480326
74 meter
Z = 15865237
79 Z = 4835724
48
XDOT = 9822
323099 XDOT = 2993
844081
YDOT = 20506
183513 feet/sec YDOT = 6250
284735 meter/sec
ZDOT = 8165
650632 ZDOT = 2488
890312
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 17342
80608009
00016717 00000-0 10270-3 0 9140
2 25544 51
6370 247
8232 0003241 217
2285 142
8643 15
54096470 8905
Satellite: ISS
Catalog Number: 25544
Epoch time: 17342
80608009 = yrday
fracday
Element set: 914
Inclination: 51
6370 deg
RA of node: 247
8232 deg
Eccentricity:
0003241
Arg of perigee: 217
2285 deg
Mean anomaly: 142
8643 deg
Mean motion: 15
54096470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 299
Coasting Arc #16 (Orbit 904)
---------------------------------------
Vector Time (GMT): 2017/343/18:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3420744
49 A = 6777493
70 meter
Y = 2566255
51 meter E =
0012857
Z = -5269047
34 I = 51
28230
XDOT = -3984
087838 Wp = 96
36555
YDOT = -6514
950545 meter/sec RA = 242
09894 deg
ZDOT = -589
177106 TA = 167
99184
MA = 167
96116
Ha = 220
619 n
mi
Hp = 215
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11222914
99 X = -3423592
37
Y = 8419473
44 feet Y = 2527986
72 meter
Z = -17286900
73 Z = -5285671
05
XDOT = -13071
154325 XDOT = -3908
077875
YDOT = -21374
509663 feet/sec YDOT = -6559
078314 meter/sec
ZDOT = -1932
995756 ZDOT = -608
346256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12505586
55 X = -3811702
78
Y = 6154868
18 feet Y = 1876003
82 meter
Z = -17361053
92 Z = -5291649
24
XDOT = -8312
016747 XDOT = -2533
502704
YDOT = -22553
803849 feet/sec YDOT = -6874
399413 meter/sec
ZDOT = -2017
094596 ZDOT = -614
810433
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 17343
77061792
00016717 00000-0 10270-3 0 9150
2 25544 51
6373 243
0149 0003183 215
4965 144
5976 15
54124227 9050
Satellite: ISS
Catalog Number: 25544
Epoch time: 17343
77061792 = yrday
fracday
Element set: 915
Inclination: 51
6373 deg
RA of node: 243
0149 deg
Eccentricity:
0003183
Arg of perigee: 215
4965 deg
Mean anomaly: 144
5976 deg
Mean motion: 15
54124227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 905
Checksum: 314
Coasting Arc #17 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2017/344/18:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4289630
74 A = 6778048
03 meter
Y = -974590
82 meter E =
0001492
Z = 5155352
31 I = 51
29901
XDOT = 3164
685382 Wp = 93
37767
YDOT = 6857
331764 meter/sec RA = 237
07463 deg
ZDOT = -1336
660490 TA = 9
52740
MA = 9
52457
Ha = 220
483 n
mi
Hp = 215
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14073591
68 X = 4275167
83
Y = -3197476
44 feet Y = -926702
30 meter
Z = 16913885
52 Z = 5176154
89
XDOT = 10382
826057 XDOT = 3094
262509
YDOT = 22497
807624 feet/sec YDOT = 6892
327733 meter/sec
ZDOT = -4385
369063 ZDOT = -1321
458171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14304446
52 X = 4359995
30
Y = -732240
96 feet Y = -223187
04 meter
Z = 17006351
60 Z = 5183535
97
XDOT = 6308
733917 XDOT = 1922
902098
YDOT = 22916
374214 feet/sec YDOT = 6984
910860 meter/sec
ZDOT = -4318
905465 ZDOT = -1316
402386
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 17344
79945597
00016717 00000-0 10270-3 0 9168
2 25544 51
6363 237
8857 0003235 219
0867 141
0052 15
54084893 9214
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
79945597 = yrday
fracday
Element set: 916
Inclination: 51
6363 deg
RA of node: 237
8857 deg
Eccentricity:
0003235
Arg of perigee: 219
0867 deg
Mean anomaly: 141
0052 deg
Mean motion: 15
54084893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 921
Checksum: 336
Coasting Arc #18 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2017/344/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 553067
59 A = 6781624
77 meter
Y = -5266188
98 meter E =
0009123
Z = 4234164
53 I = 51
31943
XDOT = 5802
420238 Wp = 126
80552
YDOT = 3502
554111 meter/sec RA = 236
19014 deg
ZDOT = 3587
596246 TA = 286
32521
MA = 286
42552
Ha = 220
446 n
mi
Hp = 215
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1814526
20 X = 591346
86
Y = -17277522
92 feet Y = -5259790
33 meter
Z = 13891615
93 Z = 4236943
95
XDOT = 19036
811803 XDOT = 5745
395654
YDOT = 11491
319261 feet/sec YDOT = 3567
121760 meter/sec
ZDOT = 11770
328891 ZDOT = 3615
644322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13449391
94 X = -4099374
66
Y = -10979748
29 feet Y = -3346627
28 meter
Z = 13904721
52 Z = 4238159
12
XDOT = 19252
015649 XDOT = 5868
014370
YDOT = -8474
799162 feet/sec YDOT = -2583
118785 meter/sec
ZDOT = 11894
297383 ZDOT = 3625
381842
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 17344
99235952
00016717 00000-0 10270-3 0 9178
2 25544 51
6409 236
9253 0003521 221
5048 138
5838 15
54158302 9245
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
99235952 = yrday
fracday
Element set: 917
Inclination: 51
6409 deg
RA of node: 236
9253 deg
Eccentricity:
0003521
Arg of perigee: 221
5048 deg
Mean anomaly: 138
5838 deg
Mean motion: 15
54158302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 317
Coasting Arc #19 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2017/345/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 940422
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1814765
88 A = 6778583
01 meter
Y = 4171558
46 meter E =
0010051
Z = -5034246
74 I = 51
32802
XDOT = -5725
671872 Wp = 85
69300
YDOT = -4736
390985 meter/sec RA = 231
17503 deg
ZDOT = -1863
213975 TA = 166
17006
MA = 166
14251
Ha = 220
351 n
mi
Hp = 215
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5953956
30 X = -1836824
44
Y = 13686215
41 feet Y = 4151141
36 meter
Z = -16516557
55 Z = -5043115
78
XDOT = -18785
012704 XDOT = -5663
232099
YDOT = -15539
340502 feet/sec YDOT = -4800
070167 meter/sec
ZDOT = -6112
906741 ZDOT = -1890
876212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8391172
33 X = 2557629
33
Y = 12289363
04 feet Y = 3745797
86 meter
Z = -16556525
72 Z = -5046429
04
XDOT = -22287
374485 XDOT = -6793
191743
YDOT = 6828
818040 feet/sec YDOT = 2081
423739 meter/sec
ZDOT = -6234
999845 ZDOT = -1900
427953
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 17345
95689075
00016717 00000-0 10270-3 0 9185
2 25544 51
6410 232
1176 0003513 227
5119 132
5737 15
54116422 9390
Satellite: ISS
Catalog Number: 25544
Epoch time: 17345
95689075 = yrday
fracday
Element set: 918
Inclination: 51
6410 deg
RA of node: 232
1176 deg
Eccentricity:
0003513
Arg of perigee: 227
5119 deg
Mean anomaly: 132
5737 deg
Mean motion: 15
54116422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 309
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