[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 11th 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) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
200/11:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
7
201/17:45:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 2536)
---------------------------------------
Vector Time (GMT): 2017/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1445369
59 A = 6784971
04 meter
Y = -5811261
57 meter E =
0008452
Z = -3188186
11 I = 51
28105
XDOT = 4659
336105 Wp = 44
55155
YDOT = -3772
308059 meter/sec RA = 281
29901 deg
ZDOT = 4777
287013 TA = 278
41188
MA = 278
50768
Ha = 222
164 n
mi
Hp = 213
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4742026
23 X = -1364792
70
Y = -19065818
80 feet Y = -5826973
76 meter
Z = -10459928
18 Z = -3195012
16
XDOT = 15286
535779 XDOT = 4677
967378
YDOT = -12376
338776 feet/sec YDOT = -3720
100605 meter/sec
ZDOT = 15673
513823 ZDOT = 4799
965098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16736361
04 X = -5101242
84
Y = 10260444
87 feet Y = 3127383
60 meter
Z = -10489034
62 Z = -3197057
75
XDOT = -15664
459430 XDOT = -4774
527234
YDOT = -9471
030311 feet/sec YDOT = -2886
770039 meter/sec
ZDOT = 15774
284318 ZDOT = 4808
001860
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 17191
50660012
00016717 00000-0 10270-3 0 9006
2 25544 51
6422 282
0934 0005386 15
6589 344
4729 15
54135393 25375
Satellite: ISS
Catalog Number: 25544
Epoch time: 17191
50660012 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 282
0934 deg
Eccentricity:
0005386
Arg of perigee: 15
6589 deg
Mean anomaly: 344
4729 deg
Mean motion: 15
54135393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2537
Checksum: 305
Coasting Arc #2 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2017/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 601929
88 A = 6788126
93 meter
Y = 6554688
59 meter E =
0014475
Z = 1643497
28 I = 51
28517
XDOT = -4791
148998 Wp = 94
47007
YDOT = 1875
853667 meter/sec RA = 276
29839 deg
ZDOT = -5684
346043 TA = 67
44249
MA = 67
28937
Ha = 222
295 n
mi
Hp = 213
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1974835
58 X = 520605
72
Y = 21504883
84 feet Y = 6560964
90 meter
Z = 5392051
43 Z = 1646224
39
XDOT = -15718
992774 XDOT = -4784
157874
YDOT = 6154
375548 feet/sec YDOT = 1822
315475 meter/sec
ZDOT = -18649
429276 ZDOT = -5707
602420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19744581
40 X = 6018148
41
Y = -8740357
13 feet Y = -2664060
85 meter
Z = 5402951
55 Z = 1646819
63
XDOT = 10196
442213 XDOT = 3107
875586
YDOT = 11356
293520 feet/sec YDOT = 3461
398265 meter/sec
ZDOT = -18752
416723 ZDOT = -5715
736617
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 17192
53542046
00016717 00000-0 10270-3 0 9017
2 25544 51
6411 276
9652 0005403 21
2354 338
9022 15
54147215 25533
Satellite: ISS
Catalog Number: 25544
Epoch time: 17192
53542046 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 276
9652 deg
Eccentricity:
0005403
Arg of perigee: 21
2354 deg
Mean anomaly: 338
9022 deg
Mean motion: 15
54147215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 284
Coasting Arc #3 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2017/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 180848
12 A = 6789333
87 meter
Y = -6777576
96 meter E =
0017438
Z = 33286
12 I = 51
28615
XDOT = 4796
084550 Wp = 38
94247
YDOT = 165
712817 meter/sec RA = 271
30301 deg
ZDOT = 5986
681843 TA = 321
41803
MA = 321
54252
Ha = 222
387 n
mi
Hp = 213
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 593333
73 X = 256461
65
Y = -22236144
87 feet Y = -6775131
81 meter
Z = 109206
44 Z = 34347
67
XDOT = 15735
185533 XDOT = 4764
795152
YDOT = 543
677221 feet/sec YDOT = 219
170413 meter/sec
ZDOT = 19641
344628 ZDOT = 6009
903388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21133246
22 X = -6441413
45
Y = 6941381
51 feet Y = 2115733
09 meter
Z = 115050
69 Z = 35067
45
XDOT = -4243
690639 XDOT = -1293
476907
YDOT = -13334
897080 feet/sec YDOT = -4064
476630 meter/sec
ZDOT = 19743
827883 ZDOT = 6017
918739
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 17193
56423760
00016717 00000-0 10270-3 0 9023
2 25544 51
6409 271
8366 0005545 23
8358 336
3051 15
54128649 25696
Satellite: ISS
Catalog Number: 25544
Epoch time: 17193
56423760 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 271
8366 deg
Eccentricity:
0005545
Arg of perigee: 23
8358 deg
Mean anomaly: 336
3051 deg
Mean motion: 15
54128649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 323
Coasting Arc #4 (Orbit 2583)
---------------------------------------
Vector Time (GMT): 2017/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -988887
05 A = 6787913
63 meter
Y = 6483993
17 meter E =
0007275
Z = -1751832
22 I = 51
28139
XDOT = -4677
419056 Wp = 97
90896
YDOT = -2232
268807 meter/sec RA = 266
30748 deg
ZDOT = -5643
049663 TA = 101
40409
MA = 101
32236
Ha = 222
425 n
mi
Hp = 213
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3244380
10 X = -1052809
86
Y = 21272943
48 feet Y = 6472577
48 meter
Z = -5747481
03 Z = -1756790
65
XDOT = -15345
863045 XDOT = -4624
698835
YDOT = -7323
716559 feet/sec YDOT = -2284
279700 meter/sec
ZDOT = -18513
942464 ZDOT = -5665
642902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21033025
23 X = 6410866
09
Y = -4517886
25 feet Y = -1377051
73 meter
Z = -5770460
82 Z = -1758836
46
XDOT = -1801
822758 XDOT = -549
195577
YDOT = 15297
030959 feet/sec YDOT = 4662
535036 meter/sec
ZDOT = -18613
308416 ZDOT = -5673
336405
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 17194
52874805
00016717 00000-0 10270-3 0 9031
2 25544 51
6402 267
0285 0005511 27
8110 332
3337 15
54162310 25842
Satellite: ISS
Catalog Number: 25544
Epoch time: 17194
52874805 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 267
0285 deg
Eccentricity:
0005511
Arg of perigee: 27
8110 deg
Mean anomaly: 332
3337 deg
Mean motion: 15
54162310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2584
Checksum: 287
Coasting Arc #5 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2017/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1764978
44 A = 6784681
93 meter
Y = -5679024
38 meter E =
0016494
Z = 3246299
39 I = 51
27372
XDOT = 4456
726451 Wp = 71
14015
YDOT = 4092
743224 meter/sec RA = 261
30496 deg
ZDOT = 4722
237784 TA = 326
75106
MA = 326
85458
Ha = 222
425 n
mi
Hp = 213
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5790611
69 X = 1812582
87
Y = -18631969
75 feet Y = -5659021
21 meter
Z = 10650588
56 Z = 3254988
29
XDOT = 14621
805943 XDOT = 4387
691043
YDOT = 13427
635250 feet/sec YDOT = 4142
195081 meter/sec
ZDOT = 15492
906114 ZDOT = 4743
719498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19426463
90 X = -5921186
20
Y = 1566941
44 feet Y = 477603
75 meter
Z = 10689888
30 Z = 3258277
95
XDOT = 7228
941396 XDOT = 2203
381338
YDOT = -17037
490618 feet/sec YDOT = -5193
027140 meter/sec
ZDOT = 15587
065992 ZDOT = 4750
937715
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 17195
55755595
00016717 00000-0 10270-3 0 9040
2 25544 51
6402 261
8993 0005588 31
5106 328
6380 15
54177095 26002
Satellite: ISS
Catalog Number: 25544
Epoch time: 17195
55755595 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 261
8993 deg
Eccentricity:
0005588
Arg of perigee: 31
5106 deg
Mean anomaly: 328
6380 deg
Mean motion: 15
54177095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 326
Coasting Arc #6 (Orbit 2614)
---------------------------------------
Vector Time (GMT): 2017/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2570193
25 A = 6780877
60 meter
Y = 4458683
80 meter E =
0014236
Z = -4430073
91 I = 51
26578
XDOT = -4068
685438 Wp = 56
88917
YDOT = -5598
406480 meter/sec RA = 256
29309 deg
ZDOT = -3274
073974 TA = 179
86607
MA = 179
86569
Ha = 222
589 n
mi
Hp = 213
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8432392
55 X = -2598341
46
Y = 14628227
70 feet Y = 4429785
02 meter
Z = -14534363
23 Z = -4442627
13
XDOT = -13348
705506 XDOT = -3989
876477
YDOT = -18367
475329 feet/sec YDOT = -5643
464454 meter/sec
ZDOT = -10741
712513 ZDOT = -3293
647121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16710060
34 X = 5093226
39
Y = 2056410
53 feet Y = 626793
93 meter
Z = -14590512
79 Z = -4447188
30
XDOT = -11682
770553 XDOT = -3560
908465
YDOT = 18112
663001 feet/sec YDOT = 5520
739683 meter/sec
ZDOT = -10827
213342 ZDOT = -3300
134627
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 17196
52206324
00016717 00000-0 10270-3 0 9050
2 25544 51
6392 257
0914 0005601 35
6521 324
5005 15
54159680 26157
Satellite: ISS
Catalog Number: 25544
Epoch time: 17196
52206324 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 257
0914 deg
Eccentricity:
0005601
Arg of perigee: 35
6521 deg
Mean anomaly: 324
5005 deg
Mean motion: 15
54159680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2615
Checksum: 291
Coasting Arc #7 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2017/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3342629
77 A = 6777932
69 meter
Y = -2920483
37 meter E =
0007563
Z = 5115519
17 I = 51
26548
XDOT = 3522
427755 Wp = 76
97621
YDOT = 6652
233140 meter/sec RA = 251
27129 deg
ZDOT = 1495
952106 TA = 358
55184
MA = 358
55403
Ha = 222
472 n
mi
Hp = 213
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10966633
10 X = 3350190
39
Y = -9581638
34 feet Y = -2883061
84 meter
Z = 16783199
38 Z = 5131774
74
XDOT = 11556
521505 XDOT = 3440
512372
YDOT = 21824
911875 feet/sec YDOT = 6691
165213 meter/sec
ZDOT = 4907
979350 ZDOT = 1512
864320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13130887
70 X = -4002294
57
Y = -6101189
64 feet Y = -1859642
60 meter
Z = 16855440
94 Z = 5137538
40
XDOT = 14923
747073 XDOT = 4548
758108
YDOT = -18354
565621 feet/sec YDOT = -5594
471601 meter/sec
ZDOT = 4981
576940 ZDOT = 1518
384651
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 17197
55086521
00016717 00000-0 10270-3 0 9060
2 25544 51
6397 251
9622 0005656 38
2758 321
8796 15
54187486 26312
Satellite: ISS
Catalog Number: 25544
Epoch time: 17197
55086521 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 251
9622 deg
Eccentricity:
0005656
Arg of perigee: 38
2758 deg
Mean anomaly: 321
8796 deg
Mean motion: 15
54187486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 346
Coasting Arc #8 (Orbit 2645)
---------------------------------------
Vector Time (GMT): 2017/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4080122
19 A = 6777335
54 meter
Y = 1244658
80 meter E =
0018946
Z = -5282437
48 I = 51
27494
XDOT = -2747
255106 Wp = 79
50382
YDOT = -7131
053132 meter/sec RA = 246
24542 deg
ZDOT = 446
486341 TA = 194
75604
MA = 194
81142
Ha = 222
741 n
mi
Hp = 212
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13386227
66 X = -4068077
63
Y = 4083526
26 feet Y = 1199099
83 meter
Z = -17330831
64 Z = -5302228
06
XDOT = -9013
304152 XDOT = -2669
478414
YDOT = -23395
843608 feet/sec YDOT = -7161
339959 meter/sec
ZDOT = 1464
850201 ZDOT = 433
329461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9243445
40 X = 2817402
16
Y = 10362508
61 feet Y = 3158492
62 meter
Z = -17418413
69 Z = -5309132
49
XDOT = -16748
757623 XDOT = -5105
021324
YDOT = 17280
472633 feet/sec YDOT = 5267
088058 meter/sec
ZDOT = 1407
894703 ZDOT = 429
126306
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 17198
51536576
00016717 00000-0 10270-3 0 9078
2 25544 51
6401 247
1539 0005830 41
5465 318
6130 15
54157640 26469
Satellite: ISS
Catalog Number: 25544
Epoch time: 17198
51536576 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 247
1539 deg
Eccentricity:
0005830
Arg of perigee: 41
5465 deg
Mean anomaly: 318
6130 deg
Mean motion: 15
54157640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2646
Checksum: 311
Coasting Arc #9 (Orbit 2661)
---------------------------------------
Vector Time (GMT): 2017/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4698754
24 A = 6778950
50 meter
Y = 468850
58 meter E =
0012521
Z = 4857895
02 I = 51
29410
XDOT = 1740
664460 Wp = 52
82737
YDOT = 7091
543807 meter/sec RA = 241
22250 deg
ZDOT = -2356
425422 TA = 60
41047
MA = 60
28577
Ha = 222
601 n
mi
Hp = 212
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15415860
37 X = 4669564
99
Y = 1538223
69 feet Y = 521231
60 meter
Z = 15937975
78 Z = 4880649
21
XDOT = 5710
841405 XDOT = 1672
681913
YDOT = 23266
219839 feet/sec YDOT = 7110
629193 meter/sec
ZDOT = -7731
054533 ZDOT = -2348
134321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5233198
14 X = -1595078
79
Y = -14471281
94 feet Y = -4410846
73 meter
Z = 16038378
69 Z = 4888497
83
XDOT = 17430
737508 XDOT = 5312
888792
YDOT = -14874
404239 feet/sec YDOT = -4533
718412 meter/sec
ZDOT = -7695
564021 ZDOT = -2345
607914
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 17199
54416236
00016717 00000-0 10270-3 0 9083
2 25544 51
6393 242
0256 0005834 45
5056 314
6573 15
54205935 26629
Satellite: ISS
Catalog Number: 25544
Epoch time: 17199
54416236 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 242
0256 deg
Eccentricity:
0005834
Arg of perigee: 45
5056 deg
Mean anomaly: 314
6573 deg
Mean motion: 15
54205935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2662
Checksum: 316
Coasting Arc #10 (Orbit 2676)
---------------------------------------
Vector Time (GMT): 2017/200/11:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4625309
27 A = 6778654
80 meter
Y = 234816
04 meter E =
0016651
Z = -4964200
92 I = 51
31002
XDOT = -2590
907237 Wp = 88
28194
YDOT = -6893
575912 meter/sec RA = 236
23525 deg
ZDOT = 2094
552064 TA = 202
19888
MA = 202
27105
Ha = 222
831 n
mi
Hp = 212
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15174899
19 X = -4603477
72
Y = 770393
85 feet Y = 183215
29 meter
Z = -16286748
44 Z = -4986616
12
XDOT = -8500
351827 XDOT = -2523
803162
YDOT = -22616
718870 feet/sec YDOT = -6922
174215 meter/sec
ZDOT = 6871
889975 ZDOT = 2082
128537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7118442
49 X = 2169701
27
Y = 13302758
66 feet Y = 4054680
84 meter
Z = -16385775
39 Z = -4994384
34
XDOT = -15846
095292 XDOT = -4829
889845
YDOT = 16851
160657 feet/sec YDOT = 5136
233768 meter/sec
ZDOT = 6818
105644 ZDOT = 2078
158600
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 17200
50865827
00016717 00000-0 10270-3 0 9097
2 25544 51
6400 237
2169 0005932 48
7400 311
4263 15
54172544 26770
Satellite: ISS
Catalog Number: 25544
Epoch time: 17200
50865827 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 237
2169 deg
Eccentricity:
0005932
Arg of perigee: 48
7400 deg
Mean anomaly: 311
4263 deg
Mean motion: 15
54172544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2677
Checksum: 301
Coasting Arc #11 (Orbit 2692)
---------------------------------------
Vector Time (GMT): 2017/201/11:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5247325
90 A = 6781876
35 meter
Y = 1319559
32 meter E =
0016175
Z = 4080104
10 I = 51
33962
XDOT = 1334
378030 Wp = 67
95409
YDOT = 6525
390212 meter/sec RA = 231
22058 deg
ZDOT = -3808
392509 TA = 61
59775
MA = 61
43480
Ha = 222
753 n
mi
Hp = 212
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17215636
17 X = 5212361
25
Y = 4329262
85 feet Y = 1378042
49 meter
Z = 13386168
31 Z = 4105509
04
XDOT = 4377
880676 XDOT = 1279
809394
YDOT = 21408
760537 feet/sec YDOT = 6540
007472 meter/sec
ZDOT = -12494
726081 ZDOT = -3802
042323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3681227
15 X = -1122038
04
Y = -17278833
93 feet Y = -5266588
58 meter
Z = 13498170
70 Z = 4114242
43
XDOT = 15975
552373 XDOT = 4869
348363
YDOT = -13189
334785 feet/sec YDOT = -4020
109242 meter/sec
ZDOT = -12467
692528 ZDOT = -3800
152682
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 17201
53744816
00016717 00000-0 10270-3 0 9107
2 25544 51
6394 232
0882 0006030 52
3158 307
8536 15
54220650 26930
Satellite: ISS
Catalog Number: 25544
Epoch time: 17201
53744816 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 232
0882 deg
Eccentricity:
0006030
Arg of perigee: 52
3158 deg
Mean anomaly: 307
8536 deg
Mean motion: 15
54220650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2693
Checksum: 291
Coasting Arc #12 (Orbit 2696)
---------------------------------------
Vector Time (GMT): 2017/201/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73207
54 A = 6781253
17 meter
Y = -5247364
48 meter E =
0014100
Z = 4282126
40 I = 51
34163
XDOT = 6147
915354 Wp = 87
18131
YDOT = 2961
434436 meter/sec RA = 230
05041 deg
ZDOT = 3514
525350 TA = 326
87658
MA = 326
96479
Ha = 222
787 n
mi
Hp = 212
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 240182
21 X = 111079
21
Y = -17215762
72 feet Y = -5246334
58 meter
Z = 14048971
12 Z = 4282573
37
XDOT = 20170
325963 XDOT = 6097
271189
YDOT = 9715
992243 feet/sec YDOT = 3029
901006 meter/sec
ZDOT = 11530
594981 ZDOT = 3544
267130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6923120
84 X = 2110167
23
Y = 15761733
43 feet Y = 4804176
35 meter
Z = 14051758
62 Z = 4282976
03
XDOT = -21162
466247 XDOT = -6450
319712
YDOT = -1128
364037 feet/sec YDOT = -343
925359 meter/sec
ZDOT = 11661
502376 ZDOT = 3554
425924
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 17201
79464574
00016717 00000-0 10270-3 0 9116
2 25544 51
6387 230
8064 0005938 51
9403 308
2285 15
54224183 26979
Satellite: ISS
Catalog Number: 25544
Epoch time: 17201
79464574 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 230
8064 deg
Eccentricity:
0005938
Arg of perigee: 51
9403 deg
Mean anomaly: 308
2285 deg
Mean motion: 15
54224183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2697
Checksum: 319
Coasting Arc #13 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2017/202/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1464801
24 A = 6778206
32 meter
Y = 4272272
30 meter E =
0019012
Z = -5071565
21 I = 51
35227
XDOT = -6161
736688 Wp = 70
11369
YDOT = -4190
107885 meter/sec RA = 225
03533 deg
ZDOT = -1749
087171 TA = 182
86722
MA = 182
87814
Ha = 222
939 n
mi
Hp = 212
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4805778
34 X = -1487831
20
Y = 14016641
42 feet Y = 4255763
75 meter
Z = -16638993
47 Z = -5078736
08
XDOT = -20215
671547 XDOT = -6105
927752
YDOT = -13747
073115 feet/sec YDOT = -4258
700349 meter/sec
ZDOT = -5738
474970 ZDOT = -1778
883542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1715498
46 X = -522883
93
Y = -14681341
88 feet Y = -4474873
00 meter
Z = -16671326
03 Z = -5081420
17
XDOT = 23039
615199 XDOT = 7022
474713
YDOT = 3976
513135 feet/sec YDOT = 1212
041203 meter/sec
ZDOT = -5869
458893 ZDOT = -1789
011071
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 17202
75913572
00016717 00000-0 10270-3 0 9121
2 25544 51
6381 225
9977 0006103 55
0477 305
1248 15
54203175 27123
Satellite: ISS
Catalog Number: 25544
Epoch time: 17202
75913572 = yrday
fracday
Element set: 912
Inclination: 51
6381 deg
RA of node: 225
9977 deg
Eccentricity:
0006103
Arg of perigee: 55
0477 deg
Mean anomaly: 305
1248 deg
Mean motion: 15
54203175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 298
Coasting Arc #14 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2017/203/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2887560
95 A = 6777045
93 meter
Y = -3092573
59 meter E =
0008183
Z = 5287660
25 I = 51
37275
XDOT = 5774
403884 Wp = 64
91512
YDOT = 5051
766143 meter/sec RA = 220
01681 deg
ZDOT = -195
116316 TA = 26
97102
MA = 26
92851
Ha = 222
737 n
mi
Hp = 212
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9473625
15 X = 2896243
93
Y = -10146238
82 feet Y = -3060234
96 meter
Z = 17347966
70 Z = 5301707
62
XDOT = 18944
894633 XDOT = 5718
432302
YDOT = 16574
035902 feet/sec YDOT = 5116
026512 meter/sec
ZDOT = -640
145393 ZDOT = -167
201949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3924494
62 X = -1196185
96
Y = 13233312
67 feet Y = 4033513
70 meter
Z = 17410498
61 Z = 5306719
98
XDOT = -23351
816316 XDOT = -7117
633613
YDOT = -6228
620253 feet/sec YDOT = -1898
483453 meter/sec
ZDOT = -517
579391 ZDOT = -157
758198
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 17203
78791984
00016717 00000-0 10270-3 0 9137
2 25544 51
6382 220
8694 0005908 57
4204 302
7519 15
54233105 27287
Satellite: ISS
Catalog Number: 25544
Epoch time: 17203
78791984 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 220
8694 deg
Eccentricity:
0005908
Arg of perigee: 57
4204 deg
Mean anomaly: 302
7519 deg
Mean motion: 15
54233105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 318
Coasting Arc #15 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2017/204/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4234968
68 A = 6778555
05 meter
Y = 1873224
33 meter E =
0017527
Z = -4965615
88 I = 51
40363
XDOT = -4899
384841 Wp = 91
72853
YDOT = -5489
789436 meter/sec RA = 214
99881 deg
ZDOT = 2113
480028 TA = 198
92374
MA = 198
98896
Ha = 222
968 n
mi
Hp = 212
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13894254
21 X = -4231480
83
Y = 6145749
13 feet Y = 1825885
99 meter
Z = -16291390
69 Z = -4986178
96
XDOT = -16074
097249 XDOT = -4847
898462
YDOT = -18011
120197 feet/sec YDOT = -5544
289996 meter/sec
ZDOT = 6933
989592 ZDOT = 2089
805409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9461704
36 X = 2883927
49
Y = -11760895
28 feet Y = -3584720
88 meter
Z = -16382534
48 Z = -4993396
51
XDOT = 21705
992666 XDOT = 6615
986565
YDOT = 7975
442370 feet/sec YDOT = 2430
914834 meter/sec
ZDOT = 6830
195255 ZDOT = 2081
843514
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 17204
75240322
00016717 00000-0 10270-3 0 9141
2 25544 51
6387 216
0598 0006101 61
3029 298
8737 15
54209282 27430
Satellite: ISS
Catalog Number: 25544
Epoch time: 17204
75240322 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 216
0598 deg
Eccentricity:
0006101
Arg of perigee: 61
3029 deg
Mean anomaly: 298
8737 deg
Mean motion: 15
54209282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 305
Coasting Arc #16 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2017/205/17:45:30
000
Vector Time (MET): N/A
Weight (LBS) : 887557
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5376580
10 A = 6781939
14 meter
Y = -645195
05 meter E =
0016552
Z = 4072793
25 I = 51
44200
XDOT = 3587
635491 Wp = 72
80992
YDOT = 5597
031120 meter/sec RA = 209
99124 deg
ZDOT = -3831
758478 TA = 56
95592
MA = 56
79704
Ha = 222
919 n
mi
Hp = 212
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17639698
50 X = 5363612
08
Y = -2116781
65 feet Y = -585143
25 meter
Z = 13362182
58 Z = 4098878
87
XDOT = 11770
457648 XDOT = 3543
393748
YDOT = 18362
962993 feet/sec YDOT = 5636
903373 meter/sec
ZDOT = -12571
386083 ZDOT = -3814
438349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14477877
14 X = -4412856
95
Y = 10145644
75 feet Y = 3092392
52 meter
Z = 13477559
77 Z = 4107960
22
XDOT = -18373
238187 XDOT = -5600
163000
YDOT = -9542
875959 feet/sec YDOT = -2908
668592 meter/sec
ZDOT = -12495
664913 ZDOT = -3808
678665
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 17205
78118210
00016717 00000-0 10270-3 0 9156
2 25544 51
6384 210
9312 0006121 65
2993 294
8796 15
54205900 27590
Satellite: ISS
Catalog Number: 25544
Epoch time: 17205
78118210 = yrday
fracday
Element set: 915
Inclination: 51
6384 deg
RA of node: 210
9312 deg
Eccentricity:
0006121
Arg of perigee: 65
2993 deg
Mean anomaly: 294
8796 deg
Mean motion: 15
54205900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 310
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