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LEMUR-2-DEANANDMAEVE, 66680

Orbit data source: Space-Track

LEMUR-2-DEANANDMAEVE, 66680 is a payload satellite owned by SatRevolution (US) in SSO that was launched on Fri, 28 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
66680, 2025-276Q
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
SatRevolution
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2025-11-28 (2 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m²

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 LEMUR-2-DEANANDMAEVE
1 66680U 25276Q   26034.64154358  .00006938  00000-0  34885-3 0  9996
2 66680  97.4345 110.4235 0007490 102.7667 257.4404 15.17530061 10146
Epoch: 2026-02-03T15:23Z
TLE epoch observation values (Epoch: 2026-02-03T15:23:49.365Z)
Latitude
-0.00003°
Longitude
105.64826°
Altitude
517.521 km
Speed
7.604 km/s
True Right ascension
07h 21m 41s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
05:35:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.438 km
Perigee altitude
505.119 km
Semi-major axis
6,888.416 km
Eccentricity
0.00075
Inclination
97.4345°
RAAN
110.4235°
Arg. of periapsis
102.7667°
True anomaly
257.35664°
Mean anomaly
257.4404°
Eccentric anomaly
257.39852°
Mean motion
3.79633 °/min
Orbital period
94.83 mins
BSTAR
0.00034885
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