[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 27th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 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 847)
---------------------------------------
Vector Time (GMT): 2015/299/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4032114
27 A = 6777315
55 meter
Y = 2120827
09 meter E =
0019210
Z = -5035090
84 I = 51
81617
XDOT = -5234
739903 Wp = 75
55250
YDOT = 5215
243714 meter/sec RA = 147
37854 deg
ZDOT = -1996
991403 TA = 175
07190
MA = 175
05296
Ha = 222
579 n
mi
Hp = 211
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13228721
37 X = 4032558
19
Y = 6958094
12 feet Y = 2165918
84 meter
Z = -16519326
90 Z = -5015502
26
XDOT = -17174
343513 XDOT = -5282
968090
YDOT = 17110
379638 feet/sec YDOT = 5156
435542 meter/sec
ZDOT = -6551
809064 ZDOT = -2022
539040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13715372
46 X = -4180445
52
Y = 6170811
07 feet Y = 1880863
21 meter
Z = -16435083
01 Z = -5009413
30
XDOT = -2391
041385 XDOT = -728
789414
YDOT = -23045
288569 feet/sec YDOT = -7024
203956 meter/sec
ZDOT = -6662
978290 ZDOT = -2030
875783
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 15299
56970807
00016717 00000-0 10270-3 0 9005
2 25544 51
6393 148
3536 0006481 75
6298 284
5574 15
54613462 8487
Satellite: ISS
Catalog Number: 25544
Epoch time: 15299
56970807 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 148
3536 deg
Eccentricity:
0006481
Arg of perigee: 75
6298 deg
Mean anomaly: 284
5574 deg
Mean motion: 15
54613462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 848
Checksum: 346
Coasting Arc #2 (Orbit 863)
---------------------------------------
Vector Time (GMT): 2015/300/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2463207
18 A = 6775965
61 meter
Y = -3382167
57 meter E =
0008885
Z = 5322288
86 I = 51
83782
XDOT = 6127
992766 Wp = 81
75592
YDOT = -4622
408086 meter/sec RA = 142
38617 deg
ZDOT = -99
931860 TA = 9
20088
MA = 9
18461
Ha = 222
707 n
mi
Hp = 211
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8081388
37 X = -2451058
28
Y = -11096350
28 feet Y = -3409644
43 meter
Z = 17461577
64 Z = 5310352
52
XDOT = 20104
963144 XDOT = 6179
711655
YDOT = -15165
380860 feet/sec YDOT = -4553
591659 meter/sec
ZDOT = -327
860434 ZDOT = -70
036463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13790555
82 X = 4203361
41
Y = 191357
34 feet Y = 58325
72 meter
Z = 17410585
11 Z = 5306746
34
XDOT = -79
781149 XDOT = -24
317294
YDOT = 24178
852656 feet/sec YDOT = 7369
714290 meter/sec
ZDOT = -197
992901 ZDOT = -60
348236
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 15300
59821194
00016717 00000-0 10270-3 0 9016
2 25544 51
6391 143
2215 0006493 79
4440 280
7444 15
54601217 8644
Satellite: ISS
Catalog Number: 25544
Epoch time: 15300
59821194 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 143
2215 deg
Eccentricity:
0006493
Arg of perigee: 79
4440 deg
Mean anomaly: 280
7444 deg
Mean motion: 15
54601217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 864
Checksum: 294
Coasting Arc #3 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2015/301/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 828862
81 A = 6777343
30 meter
Y = 4544684
85 meter E =
0018672
Z = -4975804
08 I = 51
86708
XDOT = -6412
264630 Wp = 98
52180
YDOT = 3562
071366 meter/sec RA = 137
39490 deg
ZDOT = 2189
617755 TA = 192
77866
MA = 192
82605
Ha = 222
545 n
mi
Hp = 211
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2719366
17 X = 802152
70
Y = 14910383
38 feet Y = 4553804
14 meter
Z = -16324816
54 Z = -4971842
63
XDOT = -21037
613617 XDOT = -6462
256642
YDOT = 11686
585847 feet/sec YDOT = 3490
085786 meter/sec
ZDOT = 7183
785286 ZDOT = 2158
345739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13692502
74 X = -4173474
83
Y = -6539380
31 feet Y = -1993203
12 meter
Z = -16308463
87 Z = -4970819
79
XDOT = 2565
923134 XDOT = 782
093371
YDOT = -22914
486627 feet/sec YDOT = -6984
335524 meter/sec
ZDOT = 7048
126079 ZDOT = 2148
268829
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 15301
56241926
00016717 00000-0 10270-3 0 9024
2 25544 51
6384 138
4093 0006517 83
5247 276
6648 15
54658575 8799
Satellite: ISS
Catalog Number: 25544
Epoch time: 15301
56241926 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 138
4093 deg
Eccentricity:
0006517
Arg of perigee: 83
5247 deg
Mean anomaly: 276
6648 deg
Mean motion: 15
54658575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 879
Checksum: 337
Coasting Arc #4 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2015/302/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 763341
20 A = 6781068
85 meter
Y = -5440700
39 meter E =
0017336
Z = 3961736
50 I = 51
90252
XDOT = 6188
095219 Wp = 82
48381
YDOT = -2082
756734 meter/sec RA = 132
41432 deg
ZDOT = -4035
304882 TA = 49
50885
MA = 49
35790
Ha = 222
489 n
mi
Hp = 211
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2504400
28 X = 804878
58
Y = -17850066
89 feet Y = -5431931
83 meter
Z = 12997823
18 Z = 3965545
82
XDOT = 20302
149668 XDOT = 6230
527699
YDOT = -6833
191383 feet/sec YDOT = -2013
320240 meter/sec
ZDOT = -13239
189245 ZDOT = -4005
140414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13174980
26 X = 4015733
98
Y = 12282706
85 feet Y = 3743769
05 meter
Z = 13015195
87 Z = 3967031
70
XDOT = -5295
211794 XDOT = -1613
980555
YDOT = 19630
162718 feet/sec YDOT = 5983
273596 meter/sec
ZDOT = -13108
541229 ZDOT = -3995
483367
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 15302
59089323
00016717 00000-0 10270-3 0 9030
2 25544 51
6384 133
2772 0006398 86
9358 273
2527 15
54669601 8952
Satellite: ISS
Catalog Number: 25544
Epoch time: 15302
59089323 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 133
2772 deg
Eccentricity:
0006398
Arg of perigee: 86
9358 deg
Mean anomaly: 273
2527 deg
Mean motion: 15
54669601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 895
Checksum: 336
Coasting Arc #5 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2015/303/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2108674
69 A = 6785015
12 meter
Y = 5952821
62 meter E =
0011102
Z = -2484378
96 I = 51
93738
XDOT = -5484
599787 Wp = 72
66819
YDOT = 278
216272 meter/sec RA = 127
44718 deg
ZDOT = 5344
680675 TA = 259
62388
MA = 259
74904
Ha = 222
487 n
mi
Hp = 211
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6918224
05 X = -2163015
42
Y = 19530254
67 feet Y = 5928937
16 meter
Z = -8150849
59 Z = -2494754
81
XDOT = -17994
093788 XDOT = -5513
266271
YDOT = 912
783045 feet/sec YDOT = 216
723666 meter/sec
ZDOT = 17535
041585 ZDOT = 5317
967329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12269434
05 X = -3739723
50
Y = -16673460
17 feet Y = -5082070
66 meter
Z = -8196690
46 Z = -2498351
25
XDOT = 8226
950148 XDOT = 2507
574405
YDOT = -14580
752321 feet/sec YDOT = -4444
213307 meter/sec
ZDOT = 17419
591521 ZDOT = 5309
491496
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 15303
55507489
00016717 00000-0 10270-3 0 9046
2 25544 51
6389 128
4656 0006546 91
0229 269
1674 15
54699877 9106
Satellite: ISS
Catalog Number: 25544
Epoch time: 15303
55507489 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 128
4656 deg
Eccentricity:
0006546
Arg of perigee: 91
0229 deg
Mean anomaly: 269
1674 deg
Mean motion: 15
54699877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 346
Coasting Arc #6 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2015/304/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3203711
84 A = 6787320
51 meter
Y = -5942697
07 meter E =
0018760
Z = 626502
01 I = 51
96421
XDOT = 4448
400504 Wp = 116
85099
YDOT = 1752
000580 meter/sec RA = 122
49219 deg
ZDOT = -5999
315441 TA = 56
41180
MA = 56
23286
Ha = 222
365 n
mi
Hp = 211
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10510865
61 X = 3266883
05
Y = -19497037
62 feet Y = -5906517
83 meter
Z = 2055452
80 Z = 642218
83
XDOT = 14594
489841 XDOT = 4457
621551
YDOT = 5748
033398 feet/sec YDOT = 1801
797007 meter/sec
ZDOT = -19682
793442 ZDOT = -5977
683204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10533538
44 X = 3210622
52
Y = 19477402
80 feet Y = 5936712
37 meter
Z = 2124383
69 Z = 647512
15
XDOT = -11463
433276 XDOT = -3494
054462
YDOT = 8381
017716 feet/sec YDOT = 2554
534200 meter/sec
ZDOT = -19589
633462 ZDOT = -5970
920279
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 15304
58351898
00016717 00000-0 10270-3 0 9052
2 25544 51
6389 123
3332 0006416 92
6410 267
5478 15
54759646 9268
Satellite: ISS
Catalog Number: 25544
Epoch time: 15304
58351898 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 123
3332 deg
Eccentricity:
0006416
Arg of perigee: 92
6410 deg
Mean anomaly: 267
5478 deg
Mean motion: 15
54759646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 926
Checksum: 334
Coasting Arc #7 (Orbit 941)
---------------------------------------
Vector Time (GMT): 2015/305/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3919659
82 A = 6786856
54 meter
Y = 5386725
06 meter E =
0019246
Z = 1259453
32 I = 51
97986
XDOT = -3227
900380 Wp = 71
44434
YDOT = -3737
136599 meter/sec RA = 117
54141 deg
ZDOT = 5870
827230 TA = 302
19456
MA = 302
38105
Ha = 222
418 n
mi
Hp = 211
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12859776
32 X = -3985722
22
Y = 17672982
50 feet Y = 5342523
49 meter
Z = 4132064
70 Z = 1240251
53
XDOT = -10590
224345 XDOT = -3214
389612
YDOT = -12260
946846 feet/sec YDOT = -3773
157457 meter/sec
ZDOT = 19261
244193 ZDOT = 5855
179367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8049245
46 X = -2453410
02
Y = -20337261
39 feet Y = -6198797
27 meter
Z = 4048155
48 Z = 1233877
79
XDOT = 14604
250545 XDOT = 4451
375566
YDOT = -1914
755592 feet/sec YDOT = -583
617504 meter/sec
ZDOT = 19194
281789 ZDOT = 5850
417089
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 15305
61195042
00016717 00000-0 10270-3 0 9065
2 25544 51
6399 118
2014 0006563 98
7810 261
4086 15
54758970 9428
Satellite: ISS
Catalog Number: 25544
Epoch time: 15305
61195042 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 118
2014 deg
Eccentricity:
0006563
Arg of perigee: 98
7810 deg
Mean anomaly: 261
4086 deg
Mean motion: 15
54758970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 942
Checksum: 317
Coasting Arc #8 (Orbit 956)
---------------------------------------
Vector Time (GMT): 2015/306/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4341501
01 A = 6783563
11 meter
Y = -4232066
65 meter E =
0011062
Z = -3048446
45 I = 51
98344
XDOT = 1906
653138 Wp = 104
41138
YDOT = 5518
076454 meter/sec RA = 112
58590 deg
ZDOT = -4962
883286 TA = 110
35214
MA = 110
23325
Ha = 222
398 n
mi
Hp = 211
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14243769
70 X = 4403310
74
Y = -13884733
09 feet Y = -4183171
61 meter
Z = -10001464
72 Z = -3027205
75
XDOT = 6255
423681 XDOT = 1868
915092
YDOT = 18103
925374 feet/sec YDOT = 5539
186754 meter/sec
ZDOT = -16282
425480 ZDOT = -4953
712844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4423277
74 X = 1348215
06
Y = 19440878
60 feet Y = 5925579
80 meter
Z = -9908932
24 Z = -3020242
55
XDOT = -17352
224122 XDOT = -5288
957913
YDOT = -4301
448303 feet/sec YDOT = -1311
081443 meter/sec
ZDOT = -16243
767100 ZDOT = -4951
100212
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 15306
57609028
00016717 00000-0 10270-3 0 9076
2 25544 51
6403 113
3901 0006573 100
6641 259
5253 15
54780124 9577
Satellite: ISS
Catalog Number: 25544
Epoch time: 15306
57609028 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 113
3901 deg
Eccentricity:
0006573
Arg of perigee: 100
6641 deg
Mean anomaly: 259
5253 deg
Mean motion: 15
54780124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 957
Checksum: 297
Coasting Arc #9 (Orbit 972)
---------------------------------------
Vector Time (GMT): 2015/307/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4436477
33 A = 6779240
73 meter
Y = 2627522
05 meter E =
0015994
Z = 4391103
95 I = 51
98093
XDOT = -641
073816 Wp = 107
63383
YDOT = -6837
169881 meter/sec RA = 107
61884 deg
ZDOT = 3428
530633 TA = 307
75237
MA = 307
89717
Ha = 222
368 n
mi
Hp = 211
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14555371
83 X = -4486859
79
Y = 8620479
17 feet Y = 2577628
91 meter
Z = 14406509
02 Z = 4369429
66
XDOT = -2103
260550 XDOT = -581
225984
YDOT = -22431
659714 feet/sec YDOT = -6844
004017 meter/sec
ZDOT = 11248
460082 ZDOT = 3425
562040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -42451
94 X = -12939
35
Y = -16996268
63 feet Y = -5180462
68 meter
Z = 14312374
46 Z = 4362411
74
XDOT = 19218
046997 XDOT = 5857
660725
YDOT = 9456
013037 feet/sec YDOT = 2882
192774 meter/sec
ZDOT = 11236
843155 ZDOT = 3424
989794
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 15307
60449028
00016717 00000-0 10270-3 0 9084
2 25544 51
6405 108
2579 0006465 105
5545 254
6322 15
54815792 9731
Satellite: ISS
Catalog Number: 25544
Epoch time: 15307
60449028 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 108
2579 deg
Eccentricity:
0006465
Arg of perigee: 105
5545 deg
Mean anomaly: 254
6322 deg
Mean motion: 15
54815792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 973
Checksum: 319
Coasting Arc #10 (Orbit 987)
---------------------------------------
Vector Time (GMT): 2015/308/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4314149
80 A = 6775991
02 meter
Y = -652366
65 meter E =
0019856
Z = -5201463
81 I = 51
97964
XDOT = -556
067099 Wp = 88
33693
YDOT = 7503
998203 meter/sec RA = 102
64119 deg
ZDOT = -1406
423214 TA = 168
19965
MA = 168
15305
Ha = 222
261 n
mi
Hp = 211
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14154034
78 X = 4346391
16
Y = -2140310
54 feet Y = -603942
99 meter
Z = -17065170
00 Z = -5180427
91
XDOT = -1824
367124 XDOT = -633
105348
YDOT = 24619
416678 feet/sec YDOT = 7497
349073 meter/sec
ZDOT = -4614
249390 ZDOT = -1409
312035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5124766
58 X = -1562028
85
Y = 13481581
51 feet Y = 4109186
05 meter
Z = -16974138
69 Z = -5173717
47
XDOT = -19595
246448 XDOT = -5972
631117
YDOT = -13258
910204 feet/sec YDOT = -4041
315830 meter/sec
ZDOT = -4628
076482 ZDOT = -1410
637712
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 15308
56860254
00016717 00000-0 10270-3 0 9099
2 25544 51
6413 103
4476 0006545 107
5659 252
6210 15
54824787 9884
Satellite: ISS
Catalog Number: 25544
Epoch time: 15308
56860254 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 103
4476 deg
Eccentricity:
0006545
Arg of perigee: 107
5659 deg
Mean anomaly: 252
6210 deg
Mean motion: 15
54824787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 988
Checksum: 327
Coasting Arc #11 (Orbit 1003)
---------------------------------------
Vector Time (GMT): 2015/309/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3978208
91 A = 6775522
78 meter
Y = -1429738
25 meter E =
0008940
Z = 5287291
16 I = 51
98426
XDOT = 1627
745748 Wp = 94
92253
YDOT = -7460
394272 meter/sec RA = 97
65607 deg
ZDOT = -792
236960 TA = 2
60647
MA = 2
60181
Ha = 222
387 n
mi
Hp = 211
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13051866
50 X = -3987609
60
Y = -4690742
30 feet Y = -1474277
45 meter
Z = 17346755
77 Z = 5267942
77
XDOT = 5340
373190 XDOT = 1714
897164
YDOT = -24476
359160 feet/sec YDOT = -7441
704501 meter/sec
ZDOT = -2599
202624 ZDOT = -784
117434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10380007
95 X = 3163826
42
Y = -9353878
39 feet Y = -2851062
13 meter
Z = 17263389
36 Z = 5261881
08
XDOT = 18309
947985 XDOT = 5580
872146
YDOT = 15586
337120 feet/sec YDOT = 4750
715554 meter/sec
ZDOT = -2562
763343 ZDOT = -781
130267
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 15309
59697364
00016717 00000-0 10270-3 0 9105
2 25544 51
6413 98
3144 0006523 110
6804 249
5049 15
54822061 10049
Satellite: ISS
Catalog Number: 25544
Epoch time: 15309
59697364 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 98
3144 deg
Eccentricity:
0006523
Arg of perigee: 110
6804 deg
Mean anomaly: 249
5049 deg
Mean motion: 15
54822061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1004
Checksum: 298
Coasting Arc #12 (Orbit 1018)
---------------------------------------
Vector Time (GMT): 2015/310/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3513562
12 A = 6777965
22 meter
Y = 3420206
58 meter E =
0017005
Z = -4696063
91 I = 51
99656
XDOT = -2570
222903 Wp = 111
42247
YDOT = 6606
544626 meter/sec RA = 92
67614 deg
ZDOT = 2890
975751 TA = 187
20056
MA = 187
22502
Ha = 222
115 n
mi
Hp = 211
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11527434
79 X = 3497867
50
Y = 11221150
20 feet Y = 3459409
49 meter
Z = -15407033
81 Z = -4679033
76
XDOT = -8432
489840 XDOT = -2657
951384
YDOT = 21675
015177 feet/sec YDOT = 6577
312366 meter/sec
ZDOT = 9484
828580 ZDOT = 2878
276384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15309627
65 X = -4666374
51
Y = 5162833
22 feet Y = 1573631
57 meter
Z = -15334050
66 Z = -4673818
64
XDOT = -14964
598914 XDOT = -4561
209749
YDOT = -16394
326303 feet/sec YDOT = -4996
990657 meter/sec
ZDOT = 9428
735992 ZDOT = 2873
878730
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 15310
56105537
00016717 00000-0 10270-3 0 9111
2 25544 51
6418 93
5036 0006427 114
4483 245
7341 15
54859852 10196
Satellite: ISS
Catalog Number: 25544
Epoch time: 15310
56105537 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 93
5036 deg
Eccentricity:
0006427
Arg of perigee: 114
4483 deg
Mean anomaly: 245
7341 deg
Mean motion: 15
54859852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1019
Checksum: 301
Coasting Arc #13 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2015/311/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2885003
29 A = 6782240
37 meter
Y = -5076920
20 meter E =
0018399
Z = 3431013
10 I = 52
01175
XDOT = 3415
427817 Wp = 99
40560
YDOT = -5082
338146 meter/sec RA = 87
70591 deg
ZDOT = -4630
393356 TA = 40
59575
MA = 40
45870
Ha = 222
177 n
mi
Hp = 211
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9465233
89 X = -2844684
41
Y = -16656562
33 feet Y = -5108956
55 meter
Z = 11256604
66 Z = 3417096
30
XDOT = 11205
471842 XDOT = 3494
499079
YDOT = -16674
337750 feet/sec YDOT = -5043
702762 meter/sec
ZDOT = -15191
579252 ZDOT = -4613
609160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19158985
07 X = 5839658
65
Y = -1137820
67 feet Y = -346807
74 meter
Z = 11197389
19 Z = 3412964
23
XDOT = 9829
201094 XDOT = 2995
940493
YDOT = 16140
640143 feet/sec YDOT = 4919
667116 meter/sec
ZDOT = -15118
098310 ZDOT = -4607
996365
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 15311
58939524
00016717 00000-0 10270-3 0 9126
2 25544 51
6421 88
3706 0006494 118
0006 242
1805 15
54864727 10352
Satellite: ISS
Catalog Number: 25544
Epoch time: 15311
58939524 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 88
3706 deg
Eccentricity:
0006494
Arg of perigee: 118
0006 deg
Mean anomaly: 242
1805 deg
Mean motion: 15
54864727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1035
Checksum: 302
Coasting Arc #14 (Orbit 1049)
---------------------------------------
Vector Time (GMT): 2015/312/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2154869
83 A = 6785835
00 meter
Y = 6196300
42 meter E =
0010579
Z = -1736513
06 I = 52
02278
XDOT = -4113
384138 Wp = 74
36802
YDOT = 3023
515331 meter/sec RA = 82
74934 deg
ZDOT = 5715
897310 TA = 266
68913
MA = 266
81015
Ha = 221
991 n
mi
Hp = 211
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7069782
92 X = 2093856
65
Y = 20329069
63 feet Y = 6220056
35 meter
Z = -5697221
32 Z = -1726193
44
XDOT = -13495
354785 XDOT = -4174
654424
YDOT = 9919
669720 feet/sec YDOT = 2977
174507 meter/sec
ZDOT = 18752
943930 ZDOT = 5695
765838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21411084
57 X = -6526098
58
Y = -2304677
68 feet Y = -702465
76 meter
Z = -5653773
22 Z = -1723270
08
XDOT = -3287
204576 XDOT = -1001
939955
YDOT = -14993
809193 feet/sec YDOT = -4570
113042 meter/sec
ZDOT = 18665
367823 ZDOT = 5689
204113
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 15312
55344791
00016717 00000-0 10270-3 0 9131
2 25544 51
6429 83
5591 0006325 119
7528 240
4255 15
54894803 10504
Satellite: ISS
Catalog Number: 25544
Epoch time: 15312
55344791 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 83
5591 deg
Eccentricity:
0006325
Arg of perigee: 119
7528 deg
Mean anomaly: 240
4255 deg
Mean motion: 15
54894803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1050
Checksum: 309
Coasting Arc #15 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2015/313/13:12:05
841
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1235839
06 A = 6786972
91 meter
Y = -6660792
17 meter E =
0017828
Z = -255621
96 I = 52
02216
XDOT = 4684
898160 Wp = 132
07119
YDOT = -648
148901 meter/sec RA = 77
80091 deg
ZDOT = -6041
107254 TA = 50
67063
MA = 50
51274
Ha = 221
906 n
mi
Hp = 211
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4054590
10 X = -1160022
86
Y = -21852992
69 feet Y = -6674188
24 meter
Z = -838654
72 Z = -261441
10
XDOT = 15370
400788 XDOT = 4721
143900
YDOT = -2126
472771 feet/sec YDOT = -595
556906 meter/sec
ZDOT = -19819
905689 ZDOT = -6018
260286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21571563
56 X = 6575012
57
Y = 5349765
22 feet Y = 1630608
44 meter
Z = -862548
55 Z = -262904
80
XDOT = -4080
199343 XDOT = -1243
644760
YDOT = 13416
870399 feet/sec YDOT = 4089
462098 meter/sec
ZDOT = -19721
033992 ZDOT = -6010
971161
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 15313
58175608
00016717 00000-0 10270-3 0 9145
2 25544 51
6431 78
4265 0006350 124
0374 236
1383 15
54930007 10662
Satellite: ISS
Catalog Number: 25544
Epoch time: 15313
58175608 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 78
4265 deg
Eccentricity:
0006350
Arg of perigee: 124
0374 deg
Mean anomaly: 236
1383 deg
Mean motion: 15
54930007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1066
Checksum: 291
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