[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 4th 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 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
315/12:37:22
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
4
317/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
317/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
4
Coasting Arc #1 (Orbit 340)
---------------------------------------
Vector Time (GMT): 2017/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4351484
24 A = 6787538
38 meter
Y = 4702817
43 meter E =
0009532
Z = -2238297
75 I = 51
99210
XDOT = -2372
655667 Wp = 59
56365
YDOT = 4796
258865 meter/sec RA = 63
06580 deg
ZDOT = 5486
618030 TA = 275
69241
MA = 275
80109
Ha = 222
680 n
mi
Hp = 213
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14276523
09 X = 4309445
55
Y = 15429191
03 feet Y = 4751243
54 meter
Z = -7343496
56 Z = -2217261
25
XDOT = -7784
303371 XDOT = -2452
764501
YDOT = 15735
757432 feet/sec YDOT = 4769
278538 meter/sec
ZDOT = 18000
715320 ZDOT = 5474
897255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20971133
25 X = -6392001
41
Y = -1855294
21 feet Y = -565493
67 meter
Z = -7250892
55 Z = -2210072
05
XDOT = -4813
621799 XDOT = -1467
191924
YDOT = -15447
833892 feet/sec YDOT = -4708
499770 meter/sec
ZDOT = 17947
907848 ZDOT = 5470
522312
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 17307
50438865
00016717 00000-0 10270-3 0 9004
2 25544 51
6415 63
8014 0004089 85
5267 274
6353 15
54030316 3416
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
50438865 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 63
8014 deg
Eccentricity:
0004089
Arg of perigee: 85
5267 deg
Mean anomaly: 274
6353 deg
Mean motion: 15
54030316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 341
Checksum: 294
Coasting Arc #2 (Orbit 356)
---------------------------------------
Vector Time (GMT): 2017/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3945187
29 A = 6789439
23 meter
Y = -5487041
72 meter E =
0016455
Z = 578089
94 I = 51
98256
XDOT = 3543
455017 Wp = 120
20117
YDOT = -3193
056725 meter/sec RA = 58
11825 deg
ZDOT = -6006
017101 TA = 53
58826
MA = 53
43662
Ha = 222
622 n
mi
Hp = 213
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12943527
86 X = -3886344
68
Y = -18002105
40 feet Y = -5530830
48 meter
Z = 1896620
53 Z = 559067
85
XDOT = 11625
508586 XDOT = 3608
072509
YDOT = -10475
907892 feet/sec YDOT = -3153
070212 meter/sec
ZDOT = -19704
780515 ZDOT = -5988
646520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21756664
25 X = 6631431
26
Y = 4309072
19 feet Y = 1313405
20 meter
Z = 1813102
12 Z = 552633
53
XDOT = -1121
795756 XDOT = -341
923346
YDOT = 14094
304250 feet/sec YDOT = 4295
943935 meter/sec
ZDOT = -19627
150633 ZDOT = -5982
355513
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 17308
53327297
00016717 00000-0 10270-3 0 9015
2 25544 51
6411 58
6734 0004069 91
9350 268
2269 15
54046898 3579
Satellite: ISS
Catalog Number: 25544
Epoch time: 17308
53327297 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 58
6734 deg
Eccentricity:
0004069
Arg of perigee: 91
9350 deg
Mean anomaly: 268
2269 deg
Mean motion: 15
54046898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 357
Checksum: 328
Coasting Arc #3 (Orbit 372)
---------------------------------------
Vector Time (GMT): 2017/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3296814
84 A = 6789005
99 meter
Y = 5825587
42 meter E =
0017148
Z = 1090522
99 I = 51
96474
XDOT = -4646
956383 Wp = 64
93759
YDOT = 1510
779039 meter/sec RA = 53
17161 deg
ZDOT = 5912
452196 TA = 306
84226
MA = 306
99939
Ha = 222
614 n
mi
Hp = 213
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10816321
65 X = 3226129
14
Y = 19112819
63 feet Y = 5862059
42 meter
Z = 3577831
33 Z = 1106366
74
XDOT = -15245
919893 XDOT = -4692
225642
YDOT = 4956
624144 feet/sec YDOT = 1458
560451 meter/sec
ZDOT = 19397
809043 ZDOT = 5889
768064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21045084
04 X = -6414541
61
Y = -6236677
88 feet Y = -1900939
42 meter
Z = 3647170
45 Z = 1111657
55
XDOT = 7149
161246 XDOT = 2179
064348
YDOT = -12716
401541 feet/sec YDOT = -3875
959190 meter/sec
ZDOT = 19296
871045 ZDOT = 5881
686295
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 17309
56215277
00016717 00000-0 10270-3 0 9024
2 25544 51
6427 53
5457 0004110 93
3334 266
8289 15
54061080 3731
Satellite: ISS
Catalog Number: 25544
Epoch time: 17309
56215277 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 53
5457 deg
Eccentricity:
0004110
Arg of perigee: 93
3334 deg
Mean anomaly: 266
8289 deg
Mean motion: 15
54061080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 373
Checksum: 299
Coasting Arc #4 (Orbit 387)
---------------------------------------
Vector Time (GMT): 2017/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2324995
51 A = 6786391
98 meter
Y = -5776520
55 meter E =
0008702
Z = -2700804
69 I = 51
93554
XDOT = 5618
124043 Wp = 110
95927
YDOT = 166
220470 meter/sec RA = 48
21969 deg
ZDOT = -5208
428572 TA = 99
39923
MA = 99
30084
Ha = 222
580 n
mi
Hp = 213
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7627938
02 X = -2247108
56
Y = -18951839
07 feet Y = -5802084
68 meter
Z = -8860907
77 Z = -2711910
08
XDOT = 18432
165495 XDOT = 5641
148464
YDOT = 545
342750 feet/sec YDOT = 229
175040 meter/sec
ZDOT = -17088
020248 ZDOT = -5181
080775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18757721
35 X = 5717353
47
Y = 8040347
66 feet Y = 2450697
97 meter
Z = -8909210
32 Z = -2715527
30
XDOT = -12904
994764 XDOT = -3933
442404
YDOT = 11366
350501 feet/sec YDOT = 3464
463633 meter/sec
ZDOT = -16966
665732 ZDOT = -5171
439715
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 17310
52672329
00016717 00000-0 10270-3 0 9038
2 25544 51
6425 48
7383 0004083 96
8818 263
2799 15
54062387 3881
Satellite: ISS
Catalog Number: 25544
Epoch time: 17310
52672329 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 48
7383 deg
Eccentricity:
0004083
Arg of perigee: 96
8818 deg
Mean anomaly: 263
2799 deg
Mean motion: 15
54062387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 388
Checksum: 333
Coasting Arc #5 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2017/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1127654
02 A = 6782619
85 meter
Y = 5358567
90 meter E =
0014954
Z = 3991661
44 I = 51
90072
XDOT = -6335
819153 Wp = 100
50528
YDOT = -1656
740461 meter/sec RA = 43
25758 deg
ZDOT = 3998
615462 TA = 307
95853
MA = 308
09355
Ha = 222
515 n
mi
Hp = 213
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3699652
30 X = 1048259
29
Y = 17580603
33 feet Y = 5370734
03 meter
Z = 13096002
10 Z = 3996946
71
XDOT = -20786
808246 XDOT = -6336
245901
YDOT = -5435
500199 feet/sec YDOT = -1727
594446 meter/sec
ZDOT = 13118
817132 ZDOT = 3967
836214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15159440
38 X = -4620597
43
Y = -9610710
96 feet Y = -2929344
70 meter
Z = 13118533
23 Z = 3998528
93
XDOT = 17705
263202 XDOT = 5396
564224
YDOT = -10137
791334 feet/sec YDOT = -3089
998799 meter/sec
ZDOT = 12982
489552 ZDOT = 3957
062815
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 17311
55559353
00016717 00000-0 10270-3 0 9044
2 25544 51
6425 43
6105 0004079 100
2962 259
8650 15
54101803 4045
Satellite: ISS
Catalog Number: 25544
Epoch time: 17311
55559353 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 43
6105 deg
Eccentricity:
0004079
Arg of perigee: 100
2962 deg
Mean anomaly: 259
8650 deg
Mean motion: 15
54101803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 404
Checksum: 283
Coasting Arc #6 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2017/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 308275
56 A = 6779320
36 meter
Y = -4673348
06 meter E =
0015642
Z = -4915696
24 I = 51
86425
XDOT = 6676
710520 Wp = 80
15096
YDOT = 2913
998142 meter/sec RA = 38
28365 deg
ZDOT = -2355
392740 TA = 166
84455
MA = 166
80371
Ha = 222
530 n
mi
Hp = 213
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1011402
75 X = 384389
74
Y = -15332506
75 feet Y = -4669474
96 meter
Z = -16127612
35 Z = -4914014
00
XDOT = 21905
218242 XDOT = 6655
070731
YDOT = 9560
361358 feet/sec YDOT = 2988
540764 meter/sec
ZDOT = -7727
666469 ZDOT = -2323
011228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10452022
15 X = 3185776
35
Y = 11275239
23 feet Y = 3436692
92 meter
Z = -16119329
76 Z = -4913171
71
XDOT = -21143
338918 XDOT = -6444
489702
YDOT = 8774
440772 feet/sec YDOT = 2674
449547 meter/sec
ZDOT = -7584
448723 ZDOT = -2311
739971
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 17312
52015732
00016717 00000-0 10270-3 0 9051
2 25544 51
6420 38
8033 0003953 103
4965 256
6628 15
54061383 4198
Satellite: ISS
Catalog Number: 25544
Epoch time: 17312
52015732 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 38
8033 deg
Eccentricity:
0003953
Arg of perigee: 103
4965 deg
Mean anomaly: 256
6628 deg
Mean motion: 15
54061383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 419
Checksum: 293
Coasting Arc #7 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2017/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1827586
06 A = 6777436
15 meter
Y = 3790548
39 meter E =
0006651
Z = 5307378
88 I = 51
83296
XDOT = -6604
582011 Wp = 106
28241
YDOT = -3876
047621 meter/sec RA = 33
30015 deg
ZDOT = 491
681422 TA = 339
02938
MA = 339
05665
Ha = 222
512 n
mi
Hp = 213
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5996017
26 X = -1895618
16
Y = 12436182
38 feet Y = 3769730
56 meter
Z = 17412660
35 Z = 5298335
75
XDOT = -21668
576153 XDOT = -6563
136523
YDOT = -12716
691670 feet/sec YDOT = -3949
672843 meter/sec
ZDOT = 1613
128025 ZDOT = 459
698534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5150658
49 X = -1569920
71
Y = -12864715
23 feet Y = -3921165
20 meter
Z = 17371856
98 Z = 5294942
01
XDOT = 23020
246088 XDOT = 7016
571007
YDOT = -7218
777806 feet/sec YDOT = -2200
283475 meter/sec
ZDOT = 1471
852735 ZDOT = 448
620714
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 17313
54901737
00016717 00000-0 10270-3 0 9064
2 25544 51
6428 33
6747 0003967 104
9550 255
2042 15
54118995 4357
Satellite: ISS
Catalog Number: 25544
Epoch time: 17313
54901737 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 33
6747 deg
Eccentricity:
0003967
Arg of perigee: 104
9550 deg
Mean anomaly: 255
2042 deg
Mean motion: 15
54118995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 315
Coasting Arc #8 (Orbit 449)
---------------------------------------
Vector Time (GMT): 2017/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3354511
68 A = 6778170
14 meter
Y = -2825337
30 meter E =
0017776
Z = -5183792
37 I = 51
80598
XDOT = 6012
634238 Wp = 101
87136
YDOT = 4516
907347 meter/sec RA = 28
31373 deg
ZDOT = 1429
588134 TA = 181
87167
MA = 181
87833
Ha = 222
496 n
mi
Hp = 213
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11005615
76 X = 3411036
67
Y = -9269479
35 feet Y = -2787508
78 meter
Z = -17007192
80 Z = -5167359
72
XDOT = 19726
490282 XDOT = 5954
733778
YDOT = 14819
249826 feet/sec YDOT = 4583
820978 meter/sec
ZDOT = 4690
249783 ZDOT = 1458
655396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -304485
31 X = -92807
12
Y = 14472265
53 feet Y = 4411146
53 meter
Z = -16933760
71 Z = -5161410
26
XDOT = -23053
244532 XDOT = -7026
628933
YDOT = 5150
736219 feet/sec YDOT = 1569
944399 meter/sec
ZDOT = 4818
465204 ZDOT = 1468
668194
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 17314
51357157
00016717 00000-0 10270-3 0 9074
2 25544 51
6416 28
8673 0004035 106
1723 253
9874 15
54095472 4500
Satellite: ISS
Catalog Number: 25544
Epoch time: 17314
51357157 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 28
8673 deg
Eccentricity:
0004035
Arg of perigee: 106
1723 deg
Mean anomaly: 253
9874 deg
Mean motion: 15
54095472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 450
Checksum: 308
Coasting Arc #9 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2017/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4725398
67 A = 6780824
13 meter
Y = 1820518
77 meter E =
0012308
Z = 4500164
60 I = 51
78632
XDOT = -4957
899285 Wp = 80
49435
YDOT = -4895
697064 meter/sec RA = 23
32946 deg
ZDOT = -3216
047742 TA = 41
78648
MA = 41
69257
Ha = 222
511 n
mi
Hp = 213
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15503276
48 X = -4767264
85
Y = 5972830
61 feet Y = 1767442
09 meter
Z = 14764319
57 Z = 4477108
10
XDOT = -16266
073771 XDOT = -4887
163638
YDOT = -16061
998242 feet/sec YDOT = -4950
744205 meter/sec
ZDOT = -10551
337735 ZDOT = -3239
960113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5463579
80 X = 1665299
12
Y = -15785948
50 feet Y = -4811557
10 meter
Z = 14661669
25 Z = 4468876
79
XDOT = 21566
265570 XDOT = 6573
397746
YDOT = -2462
509890 feet/sec YDOT = -750
573015 meter/sec
ZDOT = -10656
600049 ZDOT = -3248
131695
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 17315
54242356
00016717 00000-0 10270-3 0 9083
2 25544 51
6420 23
7387 0003941 110
3214 249
8362 15
54135013 4667
Satellite: ISS
Catalog Number: 25544
Epoch time: 17315
54242356 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 23
7387 deg
Eccentricity:
0003941
Arg of perigee: 110
3214 deg
Mean anomaly: 249
8362 deg
Mean motion: 15
54135013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 284
Coasting Arc #10 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2017/315/12:37:22
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1383325
20 A = 6777527
10 meter
Y = -3974131
16 meter E =
0018633
Z = -5329001
51 I = 51
77299
XDOT = 7109
319858 Wp = 92
48707
YDOT = 2825
333520 meter/sec RA = 23
22594 deg
ZDOT = -263
121901 TA = 175
01434
MA = 174
99575
Ha = 222
500 n
mi
Hp = 213
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4538468
51 X = 1453548
17
Y = -13038488
05 feet Y = -3958269
28 meter
Z = -17483600
76 Z = -5322111
06
XDOT = 23324
540217 XDOT = 7078
475975
YDOT = 9269
466928 feet/sec YDOT = 2904
662329 meter/sec
ZDOT = -863
260831 ZDOT = -228
661558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8840812
77 X = 2694679
73
Y = 10655177
02 feet Y = 3247697
95 meter
Z = -17452317
75 Z = -5319466
45
XDOT = -19098
337523 XDOT = -5821
173277
YDOT = 14690
525380 feet/sec YDOT = 4477
672136 meter/sec
ZDOT = -710
819231 ZDOT = -216
657702
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 17315
54242497
00016717 00000-0 10270-3 0 9090
2 25544 51
6409 23
7392 0004012 110
2848 249
8736 15
54076521 4665
Satellite: ISS
Catalog Number: 25544
Epoch time: 17315
54242497 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 23
7392 deg
Eccentricity:
0004012
Arg of perigee: 110
2848 deg
Mean anomaly: 249
8736 deg
Mean motion: 15
54076521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 309
Coasting Arc #11 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2017/316/12:37:22
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3033974
11 A = 6778282
67 meter
Y = 3244978
67 meter E =
0008034
Z = 5113151
50 I = 51
74641
XDOT = -6598
108875 Wp = 79
24609
YDOT = -3550
384411 meter/sec RA = 18
23521 deg
ZDOT = -1658
231675 TA = 26
74675
MA = 26
70534
Ha = 222
481 n
mi
Hp = 213
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9953983
29 X = -3094872
36
Y = 10646255
47 feet Y = 3210710
31 meter
Z = 16775431
44 Z = 5098265
20
XDOT = -21647
338829 XDOT = -6549
862151
YDOT = -11648
242818 feet/sec YDOT = -3623
899246 meter/sec
ZDOT = -5440
392635 ZDOT = -1690
166423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4264411
02 X = -1299792
48
Y = -14016799
43 feet Y = -4272320
47 meter
Z = 16708793
23 Z = 5092840
18
XDOT = 19802
077601 XDOT = 6035
673253
YDOT = -12692
359268 feet/sec YDOT = -3868
631105 meter/sec
ZDOT = -5581
486855 ZDOT = -1701
237193
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 17316
57127111
00016717 00000-0 10270-3 0 9101
2 25544 51
6417 18
6107 0003968 112
7819 247
3753 15
54135025 4820
Satellite: ISS
Catalog Number: 25544
Epoch time: 17316
57127111 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 18
6107 deg
Eccentricity:
0003968
Arg of perigee: 112
7819 deg
Mean anomaly: 247
3753 deg
Mean motion: 15
54135025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 295
Coasting Arc #12 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2017/317/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5333985
93 A = 6786600
99 meter
Y = -3349728
45 meter E =
0009228
Z = -2525602
68 I = 51
74564
XDOT = 4513
147345 Wp = 123
09537
YDOT = -3203
038923 meter/sec RA = 13
69807 deg
ZDOT = -5302
329129 TA = 85
19530
MA = 85
08993
Ha = 222
401 n
mi
Hp = 213
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17499953
83 X = -5283863
59
Y = -10989922
75 feet Y = -3409096
55 meter
Z = -8286098
03 Z = -2551392
13
XDOT = 14806
913862 XDOT = 4574
385703
YDOT = -10508
657883 feet/sec YDOT = -3152
227574 meter/sec
ZDOT = -17396
092942 ZDOT = -5280
256456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20618246
72 X = 6284441
60
Y = 122501
44 feet Y = 37338
44 meter
Z = -8399946
57 Z = -2560303
72
XDOT = -7113
033036 XDOT = -2168
052469
YDOT = 15300
425811 feet/sec YDOT = 4663
569787 meter/sec
ZDOT = -17297
575111 ZDOT = -5272
300894
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 17317
47150984
00016717 00000-0 10270-3 0 9116
2 25544 51
6420 14
1227 0004101 116
9655 243
1917 15
54109549 4965
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
47150984 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 14
1227 deg
Eccentricity:
0004101
Arg of perigee: 116
9655 deg
Mean anomaly: 243
1917 deg
Mean motion: 15
54109549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 295
Coasting Arc #13 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2017/317/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4948175
95 A = 6782478
58 meter
Y = -2273395
99 meter E =
0011075
Z = -4055126
90 I = 51
71732
XDOT = 5106
971922 Wp = 108
91981
YDOT = 4163
757941 meter/sec RA = 11
32152 deg
ZDOT = 3902
587365 TA = 201
53785
MA = 201
58448
Ha = 222
437 n
mi
Hp = 213
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16234173
06 X = 4992928
09
Y = -7458648
26 feet Y = -2217812
00 meter
Z = -13304222
11 Z = -4030980
99
XDOT = 16755
157226 XDOT = 5041
074899
YDOT = 13660
623165 feet/sec YDOT = 4220
499254 meter/sec
ZDOT = 12803
764320 ZDOT = 3927
235727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12573303
95 X = 3832343
04
Y = -12803983
53 feet Y = -3902654
18 meter
Z = -13196672
61 Z = -4022345
81
XDOT = 19520
647391 XDOT = 5949
893325
YDOT = 5878
335226 feet/sec YDOT = 1791
716577 meter/sec
ZDOT = 12912
399669 ZDOT = 3935
699419
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 17317
92162853
00016717 00000-0 10270-3 0 9125
2 25544 51
6425 11
8811 0004063 112
0427 248
1158 15
54129522 5038
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
92162853 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 11
8811 deg
Eccentricity:
0004063
Arg of perigee: 112
0427 deg
Mean anomaly: 248
1158 deg
Mean motion: 15
54129522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 277
Coasting Arc #14 (Orbit 518)
---------------------------------------
Vector Time (GMT): 2017/318/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6023163
03 A = 6786340
56 meter
Y = 1495545
82 meter E =
0017483
Z = 2724692
04 I = 51
69734
XDOT = -3463
703453 Wp = 104
88811
YDOT = -4492
061838 meter/sec RA = 6
34503 deg
ZDOT = -5167
902605 TA = 44
29695
MA = 44
15717
Ha = 222
502 n
mi
Hp = 213
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19761033
55 X = -6052674
47
Y = 4906646
39 feet Y = 1428025
76 meter
Z = 8939278
34 Z = 2695361
02
XDOT = -11363
856473 XDOT = -3388
110901
YDOT = -14737
735690 feet/sec YDOT = -4530
372807 meter/sec
ZDOT = -16955
061041 ZDOT = -5184
544846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16549678
49 X = -5044342
01
Y = 11958106
32 feet Y = 3644830
81 meter
Z = 8808868
14 Z = 2684943
01
XDOT = -15072
910509 XDOT = -4594
223123
YDOT = -8259
738167 feet/sec YDOT = -2517
568193 meter/sec
ZDOT = -17028
103023 ZDOT = -5190
165801
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 17318
95046719
00016717 00000-0 10270-3 0 9132
2 25544 51
6421 6
7535 0004061 117
2969 242
8589 15
54105664 5193
Satellite: ISS
Catalog Number: 25544
Epoch time: 17318
95046719 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 6
7535 deg
Eccentricity:
0004061
Arg of perigee: 117
2969 deg
Mean anomaly: 242
8589 deg
Mean motion: 15
54105664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 519
Checksum: 319
Coasting Arc #15 (Orbit 533)
---------------------------------------
Vector Time (GMT): 2017/319/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6645682
78 A = 6788759
83 meter
Y = -751197
63 meter E =
0010726
Z = -1151571
05 I = 51
67431
XDOT = 1538
632319 Wp = 58
83265
YDOT = 4680
168559 meter/sec RA = 1
37365 deg
ZDOT = 5872
298822 TA = 288
67551
MA = 288
79191
Ha = 222
323 n
mi
Hp = 213
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21803421
20 X = 6659182
86
Y = -2464559
14 feet Y = -676805
59 meter
Z = -3778120
24 Z = -1119254
79
XDOT = 5048
006297 XDOT = 1457
657621
YDOT = 15354
883724 feet/sec YDOT = 4696
921929 meter/sec
ZDOT = 19266
072252 ZDOT = 5879
576453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19142864
12 X = 5834744
98
Y = -10773940
86 feet Y = -3283897
17 meter
Z = -3634607
57 Z = -1107828
39
XDOT = 9729
558908 XDOT = 2965
569555
YDOT = 10829
969127 feet/sec YDOT = 3300
974590 meter/sec
ZDOT = 19297
523788 ZDOT = 5881
885251
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 17319
91499791
00016717 00000-0 10270-3 0 9142
2 25544 51
6432 1
9451 0003898 119
9233 240
2307 15
54143345 5344
Satellite: ISS
Catalog Number: 25544
Epoch time: 17319
91499791 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 1
9451 deg
Eccentricity:
0003898
Arg of perigee: 119
9233 deg
Mean anomaly: 240
2307 deg
Mean motion: 15
54143345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 534
Checksum: 310
Coasting Arc #16 (Orbit 549)
---------------------------------------
Vector Time (GMT): 2017/320/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6757275
28 A = 6789239
63 meter
Y = -42819
47 meter E =
0014604
Z = -589292
12 I = 51
64234
XDOT = 542
760668 Wp = 134
86935
YDOT = -4774
022014 meter/sec RA = 356
40569 deg
ZDOT = -5977
607389 TA = 51
49157
MA = 51
36070
Ha = 222
324 n
mi
Hp = 213
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22169538
33 X = -6753431
68
Y = -140483
82 feet Y = -118362
45 meter
Z = -1933373
09 Z = -622108
39
XDOT = 1780
710852 XDOT = 625
141764
YDOT = -15662
801884 feet/sec YDOT = -4767
491867 meter/sec
ZDOT = -19611
572797 ZDOT = -5974
770665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20311294
52 X = -6190882
57
Y = 8852986
52 feet Y = 2698390
29 meter
Z = -2078951
97 Z = -633664
56
XDOT = -3958
789218 XDOT = -1206
638954
YDOT = -13612
625069 feet/sec YDOT = -4149
128121 meter/sec
ZDOT = -19598
130720 ZDOT = -5973
510244
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 17320
94382869
00016717 00000-0 10270-3 0 9155
2 25544 51
6426 356
8170 0003993 124
6252 235
5277 15
54100575 5506
Satellite: ISS
Catalog Number: 25544
Epoch time: 17320
94382869 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 356
8170 deg
Eccentricity:
0003993
Arg of perigee: 124
6252 deg
Mean anomaly: 235
5277 deg
Mean motion: 15
54100575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 550
Checksum: 315
Coasting Arc #17 (Orbit 565)
---------------------------------------
Vector Time (GMT): 2017/321/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6354499
02 A = 6787161
08 meter
Y = 821957
37 meter E =
0016410
Z = 2220125
96 I = 51
60252
XDOT = -2533
518683 Wp = 82
21379
YDOT = 4756
246354 meter/sec RA = 351
43206 deg
ZDOT = 5458
190769 TA = 302
47854
MA = 302
63707
Ha = 222
205 n
mi
Hp = 213
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20848093
90 X = 6334050
82
Y = 2696710
54 feet Y = 892903
34 meter
Z = 7283877
82 Z = 2250945
32
XDOT = -8312
069170 XDOT = -2613
029925
YDOT = 15604
482788 feet/sec YDOT = 4727
470135 meter/sec
ZDOT = 17907
450031 ZDOT = 5445
690361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20001998
28 X = 6096609
08
Y = -6310874
95 feet Y = -1923554
69 meter
Z = 7420449
13 Z = 2261752
90
XDOT = -1535
449262 XDOT = -468
004935
YDOT = 16245
887980 feet/sec YDOT = 4951
746656 meter/sec
ZDOT = 17851
139645 ZDOT = 5441
027364
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 17321
97265555
00016717 00000-0 10270-3 0 9162
2 25544 51
6420 351
6882 0003810 125
6769 234
4739 15
54129765 5665
Satellite: ISS
Catalog Number: 25544
Epoch time: 17321
97265555 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 351
6882 deg
Eccentricity:
0003810
Arg of perigee: 125
6769 deg
Mean anomaly: 234
4739 deg
Mean motion: 15
54129765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 566
Checksum: 331
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