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LEMUR-2-VUKASIN, 66785

Orbit data source: Space-Track

LEMUR-2-VUKASIN, 66785 is an American payload satellite 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
66785, 2025-276EA
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 4U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2025-11-28 (7 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, 0.2 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 LEMUR-2-VUKASIN
1 66785U 25276EA  26192.77031164  .00002931  00000-0  23704-3 0  9997
2 66785  97.5240 262.9290 0003578  64.9856 295.1739 15.00527711 33834
Epoch: 2026-07-11T18:29Z
TLE epoch observation values (Epoch: 2026-07-11T18:29:14.925Z)
Latitude
-0.00008°
Longitude
55.93806°
Altitude
567.272 km
Speed
7.578 km/s
True Right ascension
17h 31m 42s
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
19:43:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.748 km
Perigee altitude
559.782 km
Semi-major axis
6,940.402 km
Eccentricity
0.00036
Inclination
97.524°
RAAN
262.929°
Arg. of periapsis
64.9856°
True anomaly
295.13679°
Mean anomaly
295.1739°
Eccentric anomaly
295.15534°
Mean motion
3.75376 °/min
Orbital period
95.9 mins
BSTAR
0.00023704
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