[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 26th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
270/16:51:50
146 -1
0 1
5 1
5
N/A -0
9 -0
1 220
7
000/00:03:40
293 -0
5 -0
0 215
8
274/01:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
6
277/10:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2017/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3562146
60 A = 6785105
05 meter
Y = 4943221
87 meter E =
0010601
Z = 2978853
03 I = 51
27694
XDOT = -2914
665306 Wp = 79
72361
YDOT = 5088
052167 meter/sec RA = 257
30237 deg
ZDOT = -4941
015485 TA = 66
01488
MA = 65
90393
Ha = 220
412 n
mi
Hp = 215
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11686832
68 X = 3492135
43
Y = 16217919
52 feet Y = 4982665
04 meter
Z = 9773139
87 Z = 2995986
56
XDOT = -9562
550217 XDOT = -2947
343287
YDOT = 16693
084539 feet/sec YDOT = 5055
275230 meter/sec
ZDOT = -16210
680726 ZDOT = -4955
254043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12626214
25 X = -3848470
10
Y = -15450180
76 feet Y = -4709215
09 meter
Z = 9848241
60 Z = 3001744
04
XDOT = 7253
395145 XDOT = 2210
834840
YDOT = -16336
331593 feet/sec YDOT = -4979
313870 meter/sec
ZDOT = -16274
420784 ZDOT = -4960
443455
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 17268
53831645
00016717 00000-0 10270-3 0 9006
2 25544 51
6374 258
0648 0004364 323
2299 36
8554 15
54267949 37359
Satellite: ISS
Catalog Number: 25544
Epoch time: 17268
53831645 = yrday
fracday
Element set: 900
Inclination: 51
6374 deg
RA of node: 258
0648 deg
Eccentricity:
0004364
Arg of perigee: 323
2299 deg
Mean anomaly: 36
8554 deg
Mean motion: 15
54267949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3735
Checksum: 339
Coasting Arc #2 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2017/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3058877
72 A = 6788065
67 meter
Y = -5888081
87 meter E =
0010626
Z = -1402978
73 I = 51
29499
XDOT = 3789
477884 Wp = 16
39161
YDOT = -3339
061052 meter/sec RA = 252
30259 deg
ZDOT = 5772
136336 TA = 328
23606
MA = 328
30011
Ha = 220
466 n
mi
Hp = 215
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10035688
07 X = -2985993
22
Y = -19317853
91 feet Y = -5921880
92 meter
Z = -4602948
60 Z = -1417660
49
XDOT = 12432
670224 XDOT = 3798
495960
YDOT = -10954
924712 feet/sec YDOT = -3296
633639 meter/sec
ZDOT = 18937
455171 ZDOT = 5790
566839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11527610
89 X = 3513615
80
Y = 18450317
65 feet Y = 5623656
82 meter
Z = -4667077
91 Z = -1422525
35
XDOT = -10041
297092 XDOT = -3060
587354
YDOT = 11067
815774 feet/sec YDOT = 3373
470248 meter/sec
ZDOT = 19019
491527 ZDOT = 5797
141017
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 17269
50277307
00016717 00000-0 10270-3 0 9014
2 25544 51
6374 253
2569 0004107 327
1884 32
9013 15
54267314 37506
Satellite: ISS
Catalog Number: 25544
Epoch time: 17269
50277307 = yrday
fracday
Element set: 901
Inclination: 51
6374 deg
RA of node: 253
2569 deg
Eccentricity:
0004107
Arg of perigee: 327
1884 deg
Mean anomaly: 32
9013 deg
Mean motion: 15
54267314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3750
Checksum: 304
Coasting Arc #3 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2017/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2348468
35 A = 6788858
29 meter
Y = 6356700
53 meter E =
0007267
Z = -356637
34 I = 51
30946
XDOT = -4608
499536 Wp = 128
87784
YDOT = 1372
526099 meter/sec RA = 247
30773 deg
ZDOT = -5969
997953 TA = 54
98290
MA = 54
91473
Ha = 220
674 n
mi
Hp = 215
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7704948
64 X = 2278943
87
Y = 20855316
69 feet Y = 6382573
94 meter
Z = -1170070
02 Z = -345398
43
XDOT = -15119
749133 XDOT = -4594
505344
YDOT = 4503
038384 feet/sec YDOT = 1321
068522 meter/sec
ZDOT = -19586
607457 ZDOT = -5992
350960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9711434
55 X = -2960045
25
Y = -20002760
23 feet Y = -6096841
32 meter
Z = -1121228
77 Z = -341750
53
XDOT = 13021
326853 XDOT = 3968
900425
YDOT = -5235
110717 feet/sec YDOT = -1595
661747 meter/sec
ZDOT = -19685
725816 ZDOT = -6000
209229
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 17270
53151964
00016717 00000-0 10270-3 0 9020
2 25544 51
6383 248
1267 0004351 331
8803 28
2114 15
54272269 37660
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
53151964 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 248
1267 deg
Eccentricity:
0004351
Arg of perigee: 331
8803 deg
Mean anomaly: 28
2114 deg
Mean motion: 15
54272269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 304
Coasting Arc #4 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/270/16:53:40
293
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2416064
91 A = 6779744
59 meter
Y = 4117226
12 meter E =
0010529
Z = -4823802
08 I = 51
28215
XDOT = -4613
126583 Wp = 49
57250
YDOT = -5596
867277 meter/sec RA = 246
30303 deg
ZDOT = -2463
365773 TA = 196
06933
MA = 196
10275
Ha = 220
655 n
mi
Hp = 215
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7926722
15 X = -2438493
36
Y = 13507959
71 feet Y = 4090082
28 meter
Z = -15826122
31 Z = -4835593
47
XDOT = -15134
929733 XDOT = -4538
232120
YDOT = -18362
425449 feet/sec YDOT = -5648
035823 meter/sec
ZDOT = -8081
908703 ZDOT = -2485
592822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11805284
23 X = -3598250
63
Y = -10210792
13 feet Y = -3112249
44 meter
Z = -15878886
47 Z = -4839884
60
XDOT = 20115
131588 XDOT = 6131
092108
YDOT = -10520
282358 feet/sec YDOT = -3206
582063 meter/sec
ZDOT = -8179
489470 ZDOT = -2493
108390
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 17270
72441108
00016717 00000-0 10270-3 0 9034
2 25544 51
6415 247
1661 0004518 316
9115 43
1683 15
54015970 37692
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
72441108 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 247
1661 deg
Eccentricity:
0004518
Arg of perigee: 316
9115 deg
Mean anomaly: 43
1683 deg
Mean motion: 15
54015970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 300
Coasting Arc #5 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2017/271/16:53:40
293
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3345818
20 A = 6777790
42 meter
Y = -2663796
00 meter E =
0002113
Z = 5258157
59 I = 51
28911
XDOT = 4116
353509 Wp = 353
56186
YDOT = 6438
173908 meter/sec RA = 241
28187 deg
ZDOT = 644
406879 TA = 90
26818
MA = 90
24397
Ha = 220
584 n
mi
Hp = 215
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10977093
84 X = 3349815
05
Y = -8739488
19 feet Y = -2626358
06 meter
Z = 17251173
18 Z = 5274420
56
XDOT = 13505
096814 XDOT = 4040
923960
YDOT = 21122
617807 feet/sec YDOT = 6483
784074 meter/sec
ZDOT = 2114
195798 ZDOT = 664
219344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6762816
00 X = 2061306
32
Y = 12191721
52 feet Y = 3716036
72 meter
Z = 17323523
47 Z = 5280209
95
XDOT = -22220
736227 XDOT = -6772
880402
YDOT = 9208
218037 feet/sec YDOT = 2806
664858 meter/sec
ZDOT = 2200
991306 ZDOT = 670
862150
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 17271
75333042
00016717 00000-0 10270-3 0 9046
2 25544 51
6407 242
0380 0004514 319
4661 40
6155 15
54027147 37858
Satellite: ISS
Catalog Number: 25544
Epoch time: 17271
75333042 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 242
0380 deg
Eccentricity:
0004514
Arg of perigee: 319
4661 deg
Mean anomaly: 40
6155 deg
Mean motion: 15
54027147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3785
Checksum: 288
Coasting Arc #6 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2017/272/16:53:40
293
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4229662
85 A = 6778142
41 meter
Y = 1139916
25 meter E =
0011210
Z = -5181829
84 I = 51
30704
XDOT = -3338
905380 Wp = 83
20782
YDOT = -6782
606710 meter/sec RA = 236
25993 deg
ZDOT = 1236
928469 TA = 198
71104
MA = 198
75228
Ha = 220
776 n
mi
Hp = 215
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13876846
62 X = -4216924
40
Y = 3739882
70 feet Y = 1092688
11 meter
Z = -17000754
08 Z = -5202345
50
XDOT = -10954
413977 XDOT = -3268
820740
YDOT = -22252
646686 feet/sec YDOT = -6819
552667 meter/sec
ZDOT = 4058
164269 ZDOT = 1220
879743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1586643
12 X = -483608
82
Y = -14175149
88 feet Y = -4320585
68 meter
Z = -17091720
91 Z = -5209556
53
XDOT = 22637
644718 XDOT = 6899
954110
YDOT = -7328
259130 feet/sec YDOT = -2233
653383 meter/sec
ZDOT = 3988
055218 ZDOT = 1215
559230
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 17272
71793873
00016717 00000-0 10270-3 0 9056
2 25544 51
6409 237
2308 0004605 322
6003 37
4828 15
54025101 38000
Satellite: ISS
Catalog Number: 25544
Epoch time: 17272
71793873 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 237
2308 deg
Eccentricity:
0004605
Arg of perigee: 322
6003 deg
Mean anomaly: 37
4828 deg
Mean motion: 15
54025101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 290
Coasting Arc #7 (Orbit 3815)
---------------------------------------
Vector Time (GMT): 2017/273/16:53:40
293
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4991840
54 A = 6780522
19 meter
Y = 373208
31 meter E =
0009003
Z = 4572911
64 I = 51
33492
XDOT = 2269
289371 Wp = 34
50040
YDOT = 6676
313533 meter/sec RA = 231
24261 deg
ZDOT = -3011
847246 TA = 85
75372
MA = 85
65084
Ha = 220
806 n
mi
Hp = 215
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16377429
59 X = 4965083
16
Y = 1224436
73 feet Y = 428881
27 meter
Z = 15002990
95 Z = 4597095
54
XDOT = 7445
175102 XDOT = 2209
094540
YDOT = 21903
915790 feet/sec YDOT = 6701
353443 meter/sec
ZDOT = -9881
388604 ZDOT = -3000
970479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3429832
33 X = -1045412
89
Y = 15960369
38 feet Y = 4864720
59 meter
Z = 15109998
10 Z = 4605527
42
XDOT = -21557
549299 XDOT = -6570
741026
YDOT = 4709
005297 feet/sec YDOT = 1435
304815 meter/sec
ZDOT = -9834
140040 ZDOT = -2997
445884
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 17273
74684601
00016717 00000-0 10270-3 0 9069
2 25544 51
6414 232
1025 0004752 326
6065 33
4787 15
54063844 38164
Satellite: ISS
Catalog Number: 25544
Epoch time: 17273
74684601 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 232
1025 deg
Eccentricity:
0004752
Arg of perigee: 326
6065 deg
Mean anomaly: 33
4787 deg
Mean motion: 15
54063844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3816
Checksum: 307
Coasting Arc #8 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2017/274/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3495673
76 A = 6788955
85 meter
Y = -5665510
40 meter E =
0014172
Z = 1287243
65 I = 51
36947
XDOT = 4744
584954 Wp = 42
18794
YDOT = -1600
652714 meter/sec RA = 229
43560 deg
ZDOT = 5812
652401 TA = 331
87703
MA = 331
95351
Ha = 220
863 n
mi
Hp = 215
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11468745
95 X = -3438313
54
Y = -18587632
55 feet Y = -5704280
57 meter
Z = 4223240
31 Z = 1270402
52
XDOT = 15566
223602 XDOT = 4733
896118
YDOT = -5251
485282 feet/sec YDOT = -1547
654754 meter/sec
ZDOT = 19070
381894 ZDOT = 5835
674403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20020892
01 X = -6102367
89
Y = -8764357
39 feet Y = -2671376
13 meter
Z = 4149445
57 Z = 1264751
01
XDOT = 9084
756427 XDOT = 2769
033759
YDOT = -11633
031422 feet/sec YDOT = -3545
747977 meter/sec
ZDOT = 19172
513895 ZDOT = 5843
782235
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 17274
13268617
00016717 00000-0 10270-3 0 9079
2 25544 51
6407 230
1743 0004160 326
2490 33
8397 15
54025346 38225
Satellite: ISS
Catalog Number: 25544
Epoch time: 17274
13268617 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 230
1743 deg
Eccentricity:
0004160
Arg of perigee: 326
2490 deg
Mean anomaly: 33
8397 deg
Mean motion: 15
54025346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 298
Coasting Arc #9 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2017/275/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2501546
51 A = 6786224
09 meter
Y = 5633500
40 meter E =
0002307
Z = -2842197
32 I = 51
38197
XDOT = -5758
594793 Wp = 57
10374
YDOT = 7
769802 meter/sec RA = 224
44381 deg
ZDOT = -5054
764017 TA = 155
30291
MA = 155
29186
Ha = 220
931 n
mi
Hp = 215
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8207173
58 X = 2452171
34
Y = 18482612
87 feet Y = 5661198
01 meter
Z = -9324794
36 Z = -2830166
08
XDOT = -18893
027537 XDOT = -5733
700017
YDOT = 25
491475 feet/sec YDOT = -56
488098 meter/sec
ZDOT = -16583
871447 ZDOT = -5082
677133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17482810
33 X = 5328760
59
Y = 10212383
45 feet Y = 3112734
48 meter
Z = -9272272
29 Z = -2826188
59
XDOT = -14513
071006 XDOT = -4423
584043
YDOT = 9681
108794 feet/sec YDOT = 2950
801960 meter/sec
ZDOT = -16707
453279 ZDOT = -5092
431760
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 17275
09727970
00016717 00000-0 10270-3 0 9088
2 25544 51
6403 225
3671 0004139 328
4443 31
6461 15
54031898 38378
Satellite: ISS
Catalog Number: 25544
Epoch time: 17275
09727970 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 225
3671 deg
Eccentricity:
0004139
Arg of perigee: 328
4443 deg
Mean anomaly: 31
6461 deg
Mean motion: 15
54031898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 320
Coasting Arc #10 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2017/276/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1243344
99 A = 6782391
31 meter
Y = -5256038
91 meter E =
0008428
Z = 4094218
46 I = 51
39438
XDOT = 6509
593401 Wp = 81
76926
YDOT = 1425
322876 meter/sec RA = 219
44398 deg
ZDOT = 3801
110545 TA = 328
85733
MA = 328
90725
Ha = 220
935 n
mi
Hp = 215
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4079215
86 X = -1204365
98
Y = -17244222
14 feet Y = -5269724
38 meter
Z = 13432475
27 Z = 4088273
98
XDOT = 21356
933731 XDOT = 6474
707214
YDOT = 4676
256155 feet/sec YDOT = 1497
923013 meter/sec
ZDOT = 12470
835123 ZDOT = 3832
647397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13624851
15 X = -4152854
63
Y = -11360223
63 feet Y = -3462596
16 meter
Z = 13406839
35 Z = 4086404
63
XDOT = 19041
140643 XDOT = 5803
739668
YDOT = -7933
371850 feet/sec YDOT = -2418
091740 meter/sec
ZDOT = 12610
285394 ZDOT = 3843
614988
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 17276
12617147
00016717 00000-0 10270-3 0 9098
2 25544 51
6410 220
2387 0004136 331
5255 28
5671 15
54076511 38534
Satellite: ISS
Catalog Number: 25544
Epoch time: 17276
12617147 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 220
2387 deg
Eccentricity:
0004136
Arg of perigee: 331
5255 deg
Mean anomaly: 28
5671 deg
Mean motion: 15
54076511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 296
Coasting Arc #11 (Orbit 3867)
---------------------------------------
Vector Time (GMT): 2017/277/01:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -223927
74 A = 6779208
06 meter
Y = 4637177
09 meter E =
0012442
Z = -4951249
27 I = 51
40969
XDOT = -6865
253105 Wp = 54
43321
YDOT = -2628
658388 meter/sec RA = 214
43644 deg
ZDOT = -2148
144669 TA = 194
51956
MA = 194
55533
Ha = 221
112 n
mi
Hp = 215
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -734671
06 X = -251714
28
Y = 15213835
60 feet Y = 4634516
94 meter
Z = -16244256
14 Z = -4952405
17
XDOT = -22523
796275 XDOT = -6824
913776
YDOT = -8624
207309 feet/sec YDOT = -2705
205077 meter/sec
ZDOT = -7047
718729 ZDOT = -2181
395898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8779478
35 X = 2675985
00
Y = 12439276
40 feet Y = 3791491
45 meter
Z = -16249970
93 Z = -4952991
14
XDOT = -22166
261435 XDOT = -6756
276485
YDOT = 6231
963992 feet/sec YDOT = 1899
502625 meter/sec
ZDOT = -7194
618850 ZDOT = -2192
919825
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 17277
09075257
00016717 00000-0 10270-3 0 9107
2 25544 51
6414 215
4315 0004285 335
0062 25
0882 15
54040662 38685
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
09075257 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 215
4315 deg
Eccentricity:
0004285
Arg of perigee: 335
0062 deg
Mean anomaly: 25
0882 deg
Mean motion: 15
54040662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3868
Checksum: 296
Coasting Arc #12 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2017/277/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 596522
81 A = 6780117
12 meter
Y = 4843545
08 meter E =
0011868
Z = -4718028
92 I = 51
42122
XDOT = -6917
064789 Wp = 48
02482
YDOT = -1819
029460 meter/sec RA = 212
51844 deg
ZDOT = -2738
649017 TA = 194
73708
MA = 194
77170
Ha = 221
322 n
mi
Hp = 215
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1957095
82 X = 565234
78
Y = 15890895
94 feet Y = 4850040
21 meter
Z = -15479097
52 Z = -4715207
83
XDOT = -22693
782116 XDOT = -6882
906668
YDOT = -5967
944422 feet/sec YDOT = -1896
190189 meter/sec
ZDOT = -8985
068954 ZDOT = -2772
167108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1072835
43 X = -327000
24
Y = -15986469
70 feet Y = -4872675
97 meter
Z = -15467225
62 Z = -4714410
37
XDOT = 21056
539733 XDOT = 6418
033311
YDOT = 7434
106929 feet/sec YDOT = 2265
915792 meter/sec
ZDOT = -9133
260166 ZDOT = -2783
817699
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 17277
47658341
00016717 00000-0 10270-3 0 9111
2 25544 51
6393 213
5099 0004671 341
6908 18
4076 15
54063529 38745
Satellite: ISS
Catalog Number: 25544
Epoch time: 17277
47658341 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 213
5099 deg
Eccentricity:
0004671
Arg of perigee: 341
6908 deg
Mean anomaly: 18
4076 deg
Mean motion: 15
54063529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 330
Coasting Arc #13 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2017/278/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1006636
53 A = 6777741
87 meter
Y = -4181660
14 meter E =
0003169
Z = 5236308
97 I = 51
44186
XDOT = 7061
526649 Wp = 32
58040
YDOT = 2849
907056 meter/sec RA = 207
50883 deg
ZDOT = 920
744813 TA = 48
60300
MA = 48
57576
Ha = 221
272 n
mi
Hp = 215
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3302613
30 X = 1027886
35
Y = -13719357
40 feet Y = -4170283
71 meter
Z = 17179491
37 Z = 5241251
15
XDOT = 23167
738351 XDOT = 7024
660804
YDOT = 9350
088765 feet/sec YDOT = 2928
667863 meter/sec
ZDOT = 3020
816314 ZDOT = 954
958106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3798665
25 X = -1157833
17
Y = 13561983
93 feet Y = 4133692
70 meter
Z = 17201909
19 Z = 5243141
92
XDOT = -21718
274502 XDOT = -6619
730068
YDOT = -10096
709531 feet/sec YDOT = -3077
477065 meter/sec
ZDOT = 3171
968659 ZDOT = 966
816047
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 17278
50545737
00016717 00000-0 10270-3 0 9121
2 25544 51
6394 208
3825 0004733 343
9357 16
1645 15
54098346 38907
Satellite: ISS
Catalog Number: 25544
Epoch time: 17278
50545737 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 208
3825 deg
Eccentricity:
0004733
Arg of perigee: 343
9357 deg
Mean anomaly: 16
1645 deg
Mean motion: 15
54098346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 332
Coasting Arc #14 (Orbit 3904)
---------------------------------------
Vector Time (GMT): 2017/279/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2630255
67 A = 6777787
27 meter
Y = 3423357
09 meter E =
0013589
Z = -5236178
69 I = 51
47175
XDOT = -6676
353722 Wp = 78
72028
YDOT = -3619
819740 meter/sec RA = 202
49674 deg
ZDOT = 991
882522 TA = 200
78089
MA = 200
83619
Ha = 221
438 n
mi
Hp = 214
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8629447
72 X = -2642905
78
Y = 11231486
52 feet Y = 3393872
39 meter
Z = -17179063
94 Z = -5248987
06
XDOT = -21904
047643 XDOT = -6640
197904
YDOT = -11876
049016 feet/sec YDOT = -3694
277002 meter/sec
ZDOT = 3254
207749 ZDOT = 959
538503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8821315
35 X = 2688736
92
Y = -10992310
02 feet Y = -3350456
09 meter
Z = -17236223
81 Z = -5253601
02
XDOT = 20789
447980 XDOT = 6336
623744
YDOT = 11829
295552 feet/sec YDOT = 3605
569284 meter/sec
ZDOT = 3111
417363 ZDOT = 948
360012
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 17279
47002062
00016717 00000-0 10270-3 0 9138
2 25544 51
6398 203
5744 0004695 347
8996 12
2043 15
54081951 39057
Satellite: ISS
Catalog Number: 25544
Epoch time: 17279
47002062 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 203
5744 deg
Eccentricity:
0004695
Arg of perigee: 347
8996 deg
Mean anomaly: 12
2043 deg
Mean motion: 15
54081951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3905
Checksum: 319
Coasting Arc #15 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2017/280/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166329
04 A = 6780021
44 meter
Y = -2588112
69 meter E =
0010420
Z = 4679260
14 I = 51
51058
XDOT = 5779
002038 Wp = 38
04310
YDOT = 4175
778681 meter/sec RA = 197
49059 deg
ZDOT = -2824
482310 TA = 80
08522
MA = 79
96761
Ha = 221
446 n
mi
Hp = 214
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13669058
55 X = 4172230
28
Y = -8491183
35 feet Y = -2541488
45 meter
Z = 15351903
34 Z = 4699513
95
XDOT = 18959
980441 XDOT = 5745
598125
YDOT = 13700
061290 feet/sec YDOT = 4240
216348 meter/sec
ZDOT = -9266
674247 ZDOT = -2796
490655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13654138
29 X = -4161781
35
Y = 8350764
17 feet Y = 2545312
92 meter
Z = 15441940
87 Z = 4706703
58
XDOT = -18270
371454 XDOT = -5568
809219
YDOT = -12897
368698 feet/sec YDOT = -3931
117979 meter/sec
ZDOT = -9143
217948 ZDOT = -2786
852831
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 17280
49887710
00016717 00000-0 10270-3 0 9144
2 25544 51
6403 198
4464 0004745 351
7248 8
3826 15
54097350 39218
Satellite: ISS
Catalog Number: 25544
Epoch time: 17280
49887710 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 198
4464 deg
Eccentricity:
0004745
Arg of perigee: 351
7248 deg
Mean anomaly: 8
3826 deg
Mean motion: 15
54097350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 326
Coasting Arc #16 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2017/281/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5429123
48 A = 6783596
34 meter
Y = 1774010
29 meter E =
0006409
Z = -3661062
03 I = 51
55337
XDOT = -4405
045885 Wp = 54
95499
YDOT = -4515
998369 meter/sec RA = 192
49464 deg
ZDOT = 4353
127778 TA = 261
49137
MA = 261
56400
Ha = 221
560 n
mi
Hp = 214
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17812084
90 X = -5430773
35
Y = 5820243
74 feet Y = 1713288
58 meter
Z = -12011358
37 Z = -3687439
83
XDOT = -14452
250280 XDOT = -4375
365269
YDOT = -14816
267616 feet/sec YDOT = -4565
092264 meter/sec
ZDOT = 14281
915281 ZDOT = 4331
801399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17691860
22 X = 5392479
00
Y = -5942858
20 feet Y = -1811383
18 meter
Z = -12128431
64 Z = -3696745
96
XDOT = 14215
310012 XDOT = 4332
826492
YDOT = 13423
118860 feet/sec YDOT = 4091
366629 meter/sec
ZDOT = 14188
014863 ZDOT = 4324
506930
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 17281
46342136
00016717 00000-0 10270-3 0 9151
2 25544 51
6395 193
6386 0004797 355
6848 4
4263 15
54106793 39364
Satellite: ISS
Catalog Number: 25544
Epoch time: 17281
46342136 = yrday
fracday
Element set: 915
Inclination: 51
6395 deg
RA of node: 193
6386 deg
Eccentricity:
0004797
Arg of perigee: 355
6848 deg
Mean anomaly: 4
4263 deg
Mean motion: 15
54106793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 339
Coasting Arc #17 (Orbit 3951)
---------------------------------------
Vector Time (GMT): 2017/282/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6336860
80 A = 6787156
72 meter
Y = -946286
22 meter E =
0013079
Z = 2228639
12 I = 51
59784
XDOT = 2630
105458 Wp = 88
31736
YDOT = 4705
881321 meter/sec RA = 187
51133 deg
ZDOT = -5452
189283 TA = 66
89727
MA = 66
75947
Ha = 221
647 n
mi
Hp = 214
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20790225
73 X = 6336145
57
Y = -3104613
58 feet Y = -875426
97 meter
Z = 7311808
12 Z = 2259420
66
XDOT = 8628
954915 XDOT = 2603
772241
YDOT = 15439
243179 feet/sec YDOT = 4735
145356 meter/sec
ZDOT = -17887
760116 ZDOT = -5439
477023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20660694
37 X = -6297379
64
Y = 3604600
69 feet Y = 1098682
29 meter
Z = 7448302
59 Z = 2270242
63
XDOT = -8853
978994 XDOT = -2698
692797
YDOT = -13715
188979 feet/sec YDOT = -4180
389601 meter/sec
ZDOT = -17832
037041 ZDOT = -5435
204890
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 17282
49226046
00016717 00000-0 10270-3 0 9167
2 25544 51
6399 188
5103 0004766 358
8612 1
2529 15
54125086 39522
Satellite: ISS
Catalog Number: 25544
Epoch time: 17282
49226046 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 188
5103 deg
Eccentricity:
0004766
Arg of perigee: 358
8612 deg
Mean anomaly: 1
2529 deg
Mean motion: 15
54125086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 323
Coasting Arc #18 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2017/283/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904841
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6752831
67 A = 6789151
63 meter
Y = 170800
31 meter E =
0014776
Z = -593257
06 I = 51
63693
XDOT = -639
104355 Wp = 29
22132
YDOT = -4764
979366 meter/sec RA = 182
53737 deg
ZDOT = 5978
227756 TA = 324
37234
MA = 324
47088
Ha = 221
703 n
mi
Hp = 214
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22154959
54 X = -6751357
91
Y = 560368
47 feet Y = 95293
75 meter
Z = -1946381
41 Z = -626057
31
XDOT = -2096
799066 XDOT = -614
813470
YDOT = -15633
134403 feet/sec YDOT = -4771
990152 meter/sec
ZDOT = 19613
608123 ZDOT = 5975
182359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22099579
75 X = 6735951
91
Y = -1475748
82 feet Y = -449808
24 meter
Z = -2091742
35 Z = -637563
07
XDOT = 2762
615326 XDOT = 842
045151
YDOT = 13914
536164 feet/sec YDOT = 4241
150623 meter/sec
ZDOT = 19600
720333 ZDOT = 5974
299557
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 17283
45678763
00016717 00000-0 10270-3 0 9172
2 25544 51
6398 183
7020 0004834 1
7024 358
4145 15
54130585 39670
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
45678763 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 183
7020 deg
Eccentricity:
0004834
Arg of perigee: 1
7024 deg
Mean anomaly: 358
4145 deg
Mean motion: 15
54130585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 326
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