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LEMUR-2-MYRA

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

Observations 0
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Falcon 9 Block 5 | Transporter 15 (Dedicated SSO Rideshare)

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
Launch
Falcon 9 Block 5 | Transporter 15 (Dedicated SSO Rideshare)
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
547.69 km
Apogee
572.36 km
Inclination
97.5°
Period
95.9 min
Semi-major axis
6938.2 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 66787U 25276EB  26282.40575663  .00004950  00000-0  38841-3 0  9997
2 66787  97.5371 349.6875 0017776 120.3651 239.9334 15.01253397 47343
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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
2026-10-13 05:58:30 STARLINK-34693
NORAD 64793 		LEMUR-2-MYRA
NORAD 66787 		2.528 6.87 1.9e-05
2026-10-13 17:28:23 STARLINK-6052
NORAD 56793 		LEMUR-2-MYRA
NORAD 66787 		4.781 14.83 2.2e-06
2026-10-13 17:39:50 EZIE-A
NORAD 63247 		LEMUR-2-MYRA
NORAD 66787 		3.662 15.00 1.2e-07
2026-10-13 20:21:28 STARLINK-5318
NORAD 55304 		LEMUR-2-MYRA
NORAD 66787 		1.463 14.81 2.4e-05
2026-10-14 02:07:39 LEMUR-2-MYRA
NORAD 66787 		RAPIDEYE 5
NORAD 33313 		1.623 6.91 1.5e-06
2026-10-14 12:14:51 LEMUR-2-MYRA
NORAD 66787 		STARLINK-36230
NORAD 67075 		3.635 15.01 3.6e-06
2026-10-15 09:21:02 LEMUR-2-MYRA
NORAD 66787 		NOAA 16 DEB
NORAD 41094 		1.934 11.64 8.1e-07
2026-10-16 01:05:32 STARLINK-5236
NORAD 55274 		LEMUR-2-MYRA
NORAD 66787 		0.388 14.95 3.2e-04
2026-10-16 12:36:58 STARLINK-6031
NORAD 56810 		LEMUR-2-MYRA
NORAD 66787 		4.714 14.58 2.5e-06

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