[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 23rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 ET - UTC (sec) : 67 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
There are no maneuvers
Coasting Arc #1 (Orbit 3363)
---------------------------------------
Vector Time (GMT): 2015/204/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4184054
54 A = 6776166
05 meter
Y = -2187269
40 meter E =
0010266
Z = -4870261
76 I = 51
26236
XDOT = 1056
912262 Wp = 105
35438
YDOT = -7220
114944 meter/sec RA = 263
44633 deg
ZDOT = 2336
068479 TA = 187
64714
MA = 187
66281
Ha = 218
801 n
mi
Hp = 213
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13727213
05 X = -4135627
30
Y = -7176080
70 feet Y = -2233787
32 meter
Z = -15978549
08 Z = -4890469
35
XDOT = 3467
559916 XDOT = 1126
223126
YDOT = -23688
041155 feet/sec YDOT = -7207
908389 meter/sec
ZDOT = 7664
266664 ZDOT = 2341
370838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13833799
76 X = -4216542
17
Y = -6766618
51 feet Y = -2062465
32 meter
Z = -16065036
60 Z = -4896623
16
XDOT = 2214
833788 XDOT = 675
081339
YDOT = -22770
247435 feet/sec YDOT = -6940
371418 meter/sec
ZDOT = 7688
405165 ZDOT = 2343
425894
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 15204
18411537
00016717 00000-0 10270-3 0 9009
2 25544 51
6398 264
2737 0001793 296
4724 63
6245 15
55161388 33644
Satellite: ISS
Catalog Number: 25544
Epoch time: 15204
18411537 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 264
2737 deg
Eccentricity:
0001793
Arg of perigee: 296
4724 deg
Mean anomaly: 63
6245 deg
Mean motion: 15
55161388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3364
Checksum: 317
Coasting Arc #2 (Orbit 3379)
---------------------------------------
Vector Time (GMT): 2015/205/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3882076
54 A = 6780419
14 meter
Y = 4135341
50 meter E =
0010163
Z = 3708407
41 I = 51
28106
XDOT = -2266
963423 Wp = 77
93931
YDOT = 5961
604121 meter/sec RA = 258
42073 deg
ZDOT = -4262
799116 TA = 57
52341
MA = 57
42520
Ha = 218
743 n
mi
Hp = 213
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12736471
60 X = 3817531
70
Y = 13567393
38 feet Y = 4178392
40 meter
Z = 12166690
97 Z = 3727109
04
XDOT = -7437
544040 XDOT = -2312
752087
YDOT = 19559
068640 feet/sec YDOT = 5935
997587 meter/sec
ZDOT = -13985
561403 ZDOT = -4273
922507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13283896
79 X = 4048931
74
Y = 12957052
45 feet Y = 3949309
59 meter
Z = 12246351
25 Z = 3732687
86
XDOT = -5473
805894 XDOT = -1668
416037
YDOT = 18913
581465 feet/sec YDOT = 5764
859631 meter/sec
ZDOT = -14034
489500 ZDOT = -4277
712400
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 15205
21226216
00016717 00000-0 10270-3 0 9013
2 25544 51
6397 259
1399 0001907 299
5424 60
5539 15
55158560 33806
Satellite: ISS
Catalog Number: 25544
Epoch time: 15205
21226216 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 259
1399 deg
Eccentricity:
0001907
Arg of perigee: 299
5424 deg
Mean anomaly: 60
5539 deg
Mean motion: 15
55158560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3380
Checksum: 313
Coasting Arc #3 (Orbit 3394)
---------------------------------------
Vector Time (GMT): 2015/206/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3333679
81 A = 6784535
63 meter
Y = -5553334
90 meter E =
0006689
Z = -2008910
12 I = 51
30277
XDOT = 3421
693921 Wp = 25
65110
YDOT = -4052
807868 meter/sec RA = 253
40971 deg
ZDOT = 5538
122618 TA = 312
04227
MA = 312
09918
Ha = 218
838 n
mi
Hp = 213
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10937269
72 X = -3261574
84
Y = -18219602
70 feet Y = -5590211
04 meter
Z = -6590912
47 Z = -2024929
53
XDOT = 11226
029924 XDOT = 3439
857116
YDOT = -13296
613740 feet/sec YDOT = -4014
442953 meter/sec
ZDOT = 18169
693629 ZDOT = 5554
788370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12043881
40 X = -3670975
05
Y = -17482086
78 feet Y = -5328540
05 meter
Z = -6658789
76 Z = -2029599
12
XDOT = 8957
480610 XDOT = 2730
240090
YDOT = -13103
424157 feet/sec YDOT = -3993
923683 meter/sec
ZDOT = 18242
101983 ZDOT = 5560
192685
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 15206
17614525
00016717 00000-0 10270-3 0 9024
2 25544 51
6402 254
3264 0001727 304
2240 55
8750 15
55175200 33959
Satellite: ISS
Catalog Number: 25544
Epoch time: 15206
17614525 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 254
3264 deg
Eccentricity:
0001727
Arg of perigee: 304
2240 deg
Mean anomaly: 55
8750 deg
Mean motion: 15
55175200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3395
Checksum: 277
Coasting Arc #4 (Orbit 3410)
---------------------------------------
Vector Time (GMT): 2015/207/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2477088
85 A = 6786144
77 meter
Y = 6312624
78 meter E =
0010174
Z = -24303
03 I = 51
31822
XDOT = -4468
007610 Wp = 134
99021
YDOT = 1736
158423 meter/sec RA = 248
41044 deg
ZDOT = -5987
012172 TA = 45
27284
MA = 45
19005
Ha = 218
838 n
mi
Hp = 213
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8126931
93 X = 2406433
52
Y = 20710711
22 feet Y = 6339930
16 meter
Z = -79734
35 Z = -12441
10
XDOT = -14658
817617 XDOT = -4458
007198
YDOT = 5696
057817 feet/sec YDOT = 1686
250522 meter/sec
ZDOT = -19642
428385 ZDOT = -6008
692355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9787081
47 X = 2983102
43
Y = 19979967
07 feet Y = 6089893
96 meter
Z = -29862
16 Z = -9101
99
XDOT = -12564
315987 XDOT = -3829
603513
YDOT = 6145
305271 feet/sec YDOT = 1873
089047 meter/sec
ZDOT = -19735
982579 ZDOT = -6015
527490
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 15207
20427968
00016717 00000-0 10270-3 0 9033
2 25544 51
6399 249
1925 0001927 313
0842 47
0150 15
55224348 34112
Satellite: ISS
Catalog Number: 25544
Epoch time: 15207
20427968 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 249
1925 deg
Eccentricity:
0001927
Arg of perigee: 313
0842 deg
Mean anomaly: 47
0150 deg
Mean motion: 15
55224348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3411
Checksum: 299
Coasting Arc #5 (Orbit 3426)
---------------------------------------
Vector Time (GMT): 2015/208/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1350022
53 A = 6784462
95 meter
Y = -6324471
81 meter E =
0013256
Z = 2028224
69 I = 51
32541
XDOT = 5277
803084 Wp = 62
36690
YDOT = 654
045355 meter/sec RA = 243
41165 deg
ZDOT = 5530
717099 TA = 320
17222
MA = 320
26944
Ha = 218
883 n
mi
Hp = 213
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4429207
79 X = -1289052
71
Y = -20749579
42 feet Y = -6339227
90 meter
Z = 6654280
48 Z = 2021814
20
XDOT = 17315
626917 XDOT = 5243
231202
YDOT = 2145
818095 feet/sec YDOT = 712
871487 meter/sec
ZDOT = 18145
397306 ZDOT = 5556
271515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6495146
88 X = -1979720
77
Y = -20207105
77 feet Y = -6159125
84 meter
Z = 6627844
29 Z = 2020166
94
XDOT = 15854
023033 XDOT = 4832
306221
YDOT = 915
179453 feet/sec YDOT = 278
946697 meter/sec
ZDOT = 18255
191482 ZDOT = 5564
182364
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 15208
23241021
00016717 00000-0 10270-3 0 9042
2 25544 51
6404 244
0585 0001671 311
2588 48
8422 15
55208339 34278
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
23241021 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 244
0585 deg
Eccentricity:
0001671
Arg of perigee: 311
2588 deg
Mean anomaly: 48
8422 deg
Mean motion: 15
55208339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3427
Checksum: 284
Coasting Arc #6 (Orbit 3441)
---------------------------------------
Vector Time (GMT): 2015/209/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -51733
92 A = 6780204
45 meter
Y = 5650264
22 meter E =
0005314
Z = -3753661
88 I = 51
32651
XDOT = -5723
211839 Wp = 61
15850
YDOT = -2855
458661 meter/sec RA = 238
40386 deg
ZDOT = -4221
382177 TA = 163
97512
MA = 163
95831
Ha = 218
964 n
mi
Hp = 213
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -169730
72 X = -96679
02
Y = 18537612
26 feet Y = 5649434
71 meter
Z = -12315163
66 Z = -3754021
89
XDOT = -18776
941728 XDOT = -5670
350393
YDOT = -9368
302695 feet/sec YDOT = -2919
163451 meter/sec
ZDOT = -13849
679060 ZDOT = -4249
055963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2053703
04 X = 625968
69
Y = 18422574
35 feet Y = 5615200
66 meter
Z = -12317718
57 Z = -3754440
62
XDOT = -18303
308938 XDOT = -5578
848564
YDOT = -7294
572021 feet/sec YDOT = -2223
385552 meter/sec
ZDOT = -13968
210176 ZDOT = -4257
510461
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 15209
19627674
00016717 00000-0 10270-3 0 9051
2 25544 51
6406 239
2460 0001719 319
9019 40
2007 15
55211250 34423
Satellite: ISS
Catalog Number: 25544
Epoch time: 15209
19627674 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 239
2460 deg
Eccentricity:
0001719
Arg of perigee: 319
9019 deg
Mean anomaly: 40
2007 deg
Mean motion: 15
55211250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3442
Checksum: 288
Coasting Arc #7 (Orbit 3457)
---------------------------------------
Vector Time (GMT): 2015/210/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1598387
56 A = 6775904
21 meter
Y = -4407992
05 meter E =
0005046
Z = 4888424
32 I = 51
32960
XDOT = 5697
747644 Wp = 115
67952
YDOT = 4602
928473 meter/sec RA = 233
38109 deg
ZDOT = 2283
546901 TA = 311
89031
MA = 311
93335
Ha = 218
838 n
mi
Hp = 213
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5244053
67 X = 1623814
22
Y = -14461916
18 feet Y = -4389976
06 meter
Z = 16038137
52 Z = 4896250
25
XDOT = 18693
397783 XDOT = 5634
760678
YDOT = 15101
471368 feet/sec YDOT = 4666
292056 meter/sec
ZDOT = 7491
951776 ZDOT = 2311
072421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3176586
76 X = 968223
65
Y = -15015004
44 feet Y = -4576573
35 meter
Z = 16072582
61 Z = 4898923
18
XDOT = 19390
144988 XDOT = 5910
116192
YDOT = 12261
719045 feet/sec YDOT = 3737
371965 meter/sec
ZDOT = 7609
555472 ZDOT = 2319
392508
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 15210
22439401
00016717 00000-0 10270-3 0 9067
2 25544 51
6403 234
1115 0001766 319
1112 40
9908 15
55236903 34585
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
22439401 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 234
1115 deg
Eccentricity:
0001766
Arg of perigee: 319
1112 deg
Mean anomaly: 40
9908 deg
Mean motion: 15
55236903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3458
Checksum: 276
Coasting Arc #8 (Orbit 3472)
---------------------------------------
Vector Time (GMT): 2015/211/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3175356
06 A = 6774122
16 meter
Y = 2805787
63 meter E =
0014093
Z = -5297372
56 I = 51
34380
XDOT = -5082
914816 Wp = 84
26968
YDOT = -5730
682746 meter/sec RA = 228
35078 deg
ZDOT = 12
922398 TA = 185
84586
MA = 185
86233
Ha = 219
014 n
mi
Hp = 213
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10417834
83 X = -3180762
90
Y = 9205339
99 feet Y = 2770248
85 meter
Z = -17379831
23 Z = -5312810
46
XDOT = -16676
229712 XDOT = -5018
517942
YDOT = -18801
452578 feet/sec YDOT = -5787
163170 meter/sec
ZDOT = 42
396320 ZDOT = -11
612929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8812035
26 X = -2685908
35
Y = 10643649
85 feet Y = 3244184
47 meter
Z = -17446743
34 Z = -5317767
37
XDOT = -18527
969034 XDOT = -5647
324961
YDOT = -15449
037830 feet/sec YDOT = -4708
866731 meter/sec
ZDOT = -62
168349 ZDOT = -18
948913
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 15211
18824996
00016717 00000-0 10270-3 0 9071
2 25544 51
6407 229
2997 0001685 328
8919 31
2135 15
55240058 34732
Satellite: ISS
Catalog Number: 25544
Epoch time: 15211
18824996 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 229
2997 deg
Eccentricity:
0001685
Arg of perigee: 328
8919 deg
Mean anomaly: 31
2135 deg
Mean motion: 15
55240058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3473
Checksum: 327
Coasting Arc #9 (Orbit 3488)
---------------------------------------
Vector Time (GMT): 2015/212/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4581745
33 A = 6775980
88 meter
Y = -1039674
56 meter E =
0006988
Z = 4880181
88 I = 51
37148
XDOT = 3879
645762 Wp = 45
09639
YDOT = 6200
658149 meter/sec RA = 223
31935 deg
ZDOT = -2314
524490 TA = 67
65797
MA = 67
58392
Ha = 219
010 n
mi
Hp = 213
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15031972
88 X = 4569325
14
Y = -3411005
77 feet Y = -988508
17 meter
Z = 16011095
42 Z = 4902408
40
XDOT = 12728
496593 XDOT = 3821
263007
YDOT = 20343
366631 feet/sec YDOT = 6243
716573 meter/sec
ZDOT = -7593
584285 ZDOT = -2295
819835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14151944
70 X = 4313512
74
Y = -5851498
24 feet Y = -1783536
66 meter
Z = 16106916
99 Z = 4909388
30
XDOT = 15563
472215 XDOT = 4743
746331
YDOT = 16895
139728 feet/sec YDOT = 5149
638589 meter/sec
ZDOT = -7514
165856 ZDOT = -2290
317753
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 15212
21635743
00016717 00000-0 10270-3 0 9087
2 25544 51
6406 224
1645 0001649 334
0651 26
0419 15
55196389 34898
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
21635743 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 224
1645 deg
Eccentricity:
0001649
Arg of perigee: 334
0651 deg
Mean anomaly: 26
0419 deg
Mean motion: 15
55196389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3489
Checksum: 309
Coasting Arc #10 (Orbit 3503)
---------------------------------------
Vector Time (GMT): 2015/213/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5625133
93 A = 6780118
85 meter
Y = -645942
50 meter E =
0005006
Z = -3733764
61 I = 51
41000
XDOT = -2130
551041 Wp = 86
50947
YDOT = -6009
139776 meter/sec RA = 218
30165 deg
ZDOT = 4254
622012 TA = 228
71650
MA = 228
75962
Ha = 219
042 n
mi
Hp = 213
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18455163
82 X = -5599355
97
Y = -2119233
93 feet Y = -708702
21 meter
Z = -12249883
88 Z = -3761027
18
XDOT = -6989
996854 XDOT = -2083
863920
YDOT = -19715
025513 feet/sec YDOT = -6032
704069 meter/sec
ZDOT = 13958
733635 ZDOT = 4244
385684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18453474
40 X = -5624619
00
Y = 1291513
06 feet Y = 393653
18 meter
Z = -12367099
73 Z = -3769492
00
XDOT = -10485
624900 XDOT = -3196
018470
YDOT = -16732
223560 feet/sec YDOT = -5099
981741 meter/sec
ZDOT = 13915
704340 ZDOT = 4241
506683
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 15213
18019985
00016717 00000-0 10270-3 0 9099
2 25544 51
6412 219
3517 0001847 334
0605 26
0456 15
55222869 35040
Satellite: ISS
Catalog Number: 25544
Epoch time: 15213
18019985 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 219
3517 deg
Eccentricity:
0001847
Arg of perigee: 334
0605 deg
Mean anomaly: 26
0456 deg
Mean motion: 15
55222869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3504
Checksum: 303
Coasting Arc #11 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2015/214/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6122220
18 A = 6784370
93 meter
Y = 2129387
28 meter E =
0012834
Z = 1984663
39 I = 51
45015
XDOT = -26
657593 Wp = 106
09530
YDOT = 5284
176370 meter/sec RA = 213
30012 deg
ZDOT = -5560
822875 TA = 51
92054
MA = 51
80485
Ha = 219
093 n
mi
Hp = 213
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20086024
21 X = 6088313
31
Y = 6986178
76 feet Y = 2197660
37 meter
Z = 6511362
84 Z = 2014320
94
XDOT = -87
459293 XDOT = -58
732752
YDOT = 17336
536648 feet/sec YDOT = 5283
698954 meter/sec
ZDOT = -18244
169538 ZDOT = -5561
030248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21038167
17 X = 6412433
35
Y = 2824315
66 feet Y = 860851
41 meter
Z = 6638649
83 Z = 2023460
47
XDOT = 3711
283686 XDOT = 1131
199267
YDOT = 15442
644508 feet/sec YDOT = 4706
918046 meter/sec
ZDOT = -18245
951411 ZDOT = -5561
365990
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 15214
20829433
00016717 00000-0 10270-3 0 9102
2 25544 51
6415 214
2171 0001728 338
6988 21
4093 15
55237712 35202
Satellite: ISS
Catalog Number: 25544
Epoch time: 15214
20829433 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 214
2171 deg
Eccentricity:
0001728
Arg of perigee: 338
6988 deg
Mean anomaly: 21
4093 deg
Mean motion: 15
55237712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 288
Coasting Arc #12 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2015/215/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5951282
04 A = 6786073
54 meter
Y = -3245905
15 meter E =
0013175
Z = 44207
32 I = 51
48406
XDOT = 2327
544419 Wp = 38
82327
YDOT = -4172
656325 meter/sec RA = 208
31123 deg
ZDOT = 6002
591657 TA = 321
65426
MA = 321
74786
Ha = 219
158 n
mi
Hp = 213
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19525203
54 X = -5914757
97
Y = -10649295
11 feet Y = -3312252
08 meter
Z = 145037
14 Z = 15386
45
XDOT = 7636
300588 XDOT = 2344
873298
YDOT = -13689
817338 feet/sec YDOT = -4146
531237 meter/sec
ZDOT = 19693
542182 ZDOT = 6013
940334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21373907
14 X = -6514766
90
Y = -6149611
84 feet Y = -1874401
69 meter
Z = 21522
71 Z = 6560
12
XDOT = 3906
681360 XDOT = 1190
756479
YDOT = -13434
831116 feet/sec YDOT = -4094
936524 meter/sec
ZDOT = 19743
086410 ZDOT = 6017
692738
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 15215
23638228
00016717 00000-0 10270-3 0 9117
2 25544 51
6426 209
0830 0001899 345
4714 14
6384 15
55250235 35369
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
23638228 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 209
0830 deg
Eccentricity:
0001899
Arg of perigee: 345
4714 deg
Mean anomaly: 14
6384 deg
Mean motion: 15
55250235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 300
Coasting Arc #13 (Orbit 3550)
---------------------------------------
Vector Time (GMT): 2015/216/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5057880
18 A = 6784185
72 meter
Y = 4001393
47 meter E =
0004989
Z = -2102175
02 I = 51
50652
XDOT = -4519
548275 Wp = 129
39816
YDOT = 2823
854949 meter/sec RA = 203
32473 deg
ZDOT = -5510
913579 TA = 73
92749
MA = 73
87256
Ha = 219
195 n
mi
Hp = 213
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16594095
08 X = 5022971
15
Y = 13127931
32 feet Y = 4057758
78 meter
Z = -6896899
68 Z = -2077690
06
XDOT = -14827
914288 XDOT = -4524
019853
YDOT = 9264
615976 feet/sec YDOT = 2773
289290 meter/sec
ZDOT = -18080
425127 ZDOT = -5532
879245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19249075
76 X = 5867118
29
Y = 8866421
65 feet Y = 2702485
32 meter
Z = -6792160
70 Z = -2070250
58
XDOT = -11487
720332 XDOT = -3501
457157
YDOT = 11046
816332 feet/sec YDOT = 3367
069618 meter/sec
ZDOT = -18175
448710 ZDOT = -5539
876767
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 15216
20020870
00016717 00000-0 10270-3 0 9124
2 25544 51
6428 204
2702 0001841 347
8176 12
2933 15
55271439 35511
Satellite: ISS
Catalog Number: 25544
Epoch time: 15216
20020870 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 204
2702 deg
Eccentricity:
0001841
Arg of perigee: 347
8176 deg
Mean anomaly: 12
2933 deg
Mean motion: 15
55271439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3551
Checksum: 279
Coasting Arc #14 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2015/217/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3522488
47 A = 6779823
26 meter
Y = -4355987
09 meter E =
0011171
Z = 3808862
88 I = 51
52227
XDOT = 6279
754886 Wp = 88
17553
YDOT = -1416
914815 meter/sec RA = 198
32870 deg
ZDOT = 4176
909087 TA = 317
73223
MA = 317
81827
Ha = 219
238 n
mi
Hp = 212
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11556720
71 X = -3492018
79
Y = -14291296
24 feet Y = -4395207
45 meter
Z = 12496269
28 Z = 3791825
58
XDOT = 20602
870361 XDOT = 6274
842819
YDOT = -4648
670652 feet/sec YDOT = -1346
717872 meter/sec
ZDOT = 13703
769969 ZDOT = 4207
402657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14848793
46 X = -4525912
25
Y = -10914311
72 feet Y = -3326682
21 meter
Z = 12423639
56 Z = 3786725
34
XDOT = 17897
441125 XDOT = 5455
140055
YDOT = -8562
222157 feet/sec YDOT = -2609
765313 meter/sec
ZDOT = 13835
281905 ZDOT = 4216
993925
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 15217
22828331
00016717 00000-0 10270-3 0 9136
2 25544 51
6433 199
1360 0001860 352
1060 8
0064 15
55302753 35670
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
22828331 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 199
1360 deg
Eccentricity:
0001860
Arg of perigee: 352
1060 deg
Mean anomaly: 8
0064 deg
Mean motion: 15
55302753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3567
Checksum: 280
Coasting Arc #15 (Orbit 3581)
---------------------------------------
Vector Time (GMT): 2015/218/04:07:52
577
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1489438
78 A = 6775668
24 meter
Y = 4393556
16 meter E =
0012773
Z = -4950262
21 I = 51
53846
XDOT = -7344
529159 Wp = 65
59979
YDOT = 37
315736 meter/sec RA = 193
32042 deg
ZDOT = -2175
976458 TA = 183
12541
MA = 183
13340
Ha = 219
252 n
mi
Hp = 212
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4886610
17 X = 1464244
58
Y = 14414554
32 feet Y = 4410071
14 meter
Z = -16241017
75 Z = -4943088
09
XDOT = -24096
224274 XDOT = -7333
830588
YDOT = 122
426955 feet/sec YDOT = -44
755804 meter/sec
ZDOT = -7139
030374 ZDOT = -2211
628451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8663247
27 X = 2640557
77
Y = 12553303
07 feet Y = 3826246
78 meter
Z = -16210851
97 Z = -4941067
68
XDOT = -22226
045002 XDOT = -6774
498517
YDOT = 5918
160583 feet/sec YDOT = 1803
855346 meter/sec
ZDOT = -7292
538040 ZDOT = -2222
765595
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 15218
19209930
00016717 00000-0 10270-3 0 9142
2 25544 51
6432 194
3238 0001936 353
1634 6
9492 15
55271106 35828
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
19209930 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 194
3238 deg
Eccentricity:
0001936
Arg of perigee: 353
1634 deg
Mean anomaly: 6
9492 deg
Mean motion: 15
55271106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3582
Checksum: 304
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