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LEMUR-2-MYRA

In orbit NORAD 66787 PTFX-4430-4038-7458-5782

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-MYRA
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
547.27 km
Apogee
572.34 km
Inclination
97.5°
Period
95.9 min
Semi-major axis
6937.9 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 66787U 25276EB  26287.13798982  .00006912  00000-0  53940-3 0  9990
2 66787 97.5366 354.2798 0018063 105.1837 255.1387 15.01325187 48054
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-15 14:16:04 TRITON-1
NORAD 39427
LEMUR-2-MYRA
NORAD 66787
4.128 14.79 1.0e-07
2026-10-16 01:05:31 STARLINK-5236
NORAD 55274
LEMUR-2-MYRA
NORAD 66787
3.632 14.95 3.7e-06
2026-10-16 07:59:41 LEMUR-2-MYRA
NORAD 66787
IKONOS 2
NORAD 25919
3.820 14.97 1.4e-07
2026-10-16 09:17:08 LEMUR-2-MYRA
NORAD 66787
OBJECT K
NORAD 100964
4.160 3.74 2.5e-07
2026-10-16 14:05:03 LEMUR-2-MYRA
NORAD 66787
OBJECT M
NORAD 100966
3.844 3.74 2.9e-07
2026-10-17 11:05:34 STARLINK-5599
NORAD 55766
LEMUR-2-MYRA
NORAD 66787
4.054 5.02 7.7e-06
2026-10-17 13:49:02 STARLINK-5260
NORAD 55275
LEMUR-2-MYRA
NORAD 66787
4.225 15.02 2.6e-06
2026-10-18 05:51:56 LEMUR-2-MYRA
NORAD 66787
STARLINK-36225
NORAD 67207
1.867 4.78 3.7e-05
2026-10-18 07:46:32 LEMUR-2-MYRA
NORAD 66787
STARLINK-35715
NORAD 66841
4.546 13.95 3.2e-06
2026-10-18 08:07:37 RISAT-2B
NORAD 44233
LEMUR-2-MYRA
NORAD 66787
4.759 7.78 1.7e-07
2026-10-18 10:31:31 RISAT-2B
NORAD 44233
LEMUR-2-MYRA
NORAD 66787
3.628 7.78 2.9e-07
2026-10-18 11:40:35 LEMUR-2-MYRA
NORAD 66787
OBJECT H
NORAD 67000
2.837 1.09 5.5e-07
2026-10-18 17:33:43 LEMUR-2-MYRA
NORAD 66787
STARLINK-35784
NORAD 67093
3.678 15.02 3.5e-06
2026-10-18 17:49:05 YAOGAN-30 06A
NORAD 44449
LEMUR-2-MYRA
NORAD 66787
1.523 9.84 1.5e-06
2026-10-19 12:28:56 SKYCRAFT-4A
NORAD 64897
LEMUR-2-MYRA
NORAD 66787
3.678 0.64 3.3e-07
2026-10-19 15:32:19 LEMUR-2-MYRA
NORAD 66787
COSMOS 2251 DEB
NORAD 35442
4.956 14.93 6.5e-08
2026-10-20 00:49:57 LEMUR-2-MYRA
NORAD 66787
THOR ABLESTAR DEB
NORAD 122
4.234 15.02 8.8e-08
2026-10-20 07:18:36 HAWK-9C
NORAD 59448
LEMUR-2-MYRA
NORAD 66787
4.341 6.74 2.1e-07
2026-10-20 08:54:41 HAWK-9C
NORAD 59448
LEMUR-2-MYRA
NORAD 66787
1.671 6.75 1.4e-06
2026-10-20 09:10:10 LEMUR-2-MYRA
NORAD 66787
ORBCOMM FM01
NORAD 23545
3.500 9.67 8.5e-07
2026-10-20 10:30:45 HAWK-9C
NORAD 59448
LEMUR-2-MYRA
NORAD 66787
2.272 6.75 7.8e-07
2026-10-20 10:57:17 LEMUR-2-MYRA
NORAD 66787
STARLINK-35982
NORAD 66828
4.245 13.57 3.9e-06
2026-10-20 20:26:52 LEMUR-2-MYRA
NORAD 66787
PEGASUS DEB
NORAD 25442
3.558 15.05 1.2e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite