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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, 2025-276DZ
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 (9 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: 20 hours ago

TLE from 20 hours ago
0 LEMUR-2-VUKASIN
1 66785U 25276DZ  26238.17767113  .00004745  00000-0  37750-3 0  9993
2 66785  97.5100 306.8375 0004159 181.7289 178.3922 15.00856786 40645
Epoch: 2026-08-26T04:15Z
TLE epoch observation values (Epoch: 2026-08-26T04:15:50.785Z)
Latitude
-0.00001°
Longitude
-91.55851°
Altitude
570.201 km
Speed
7.574 km/s
True Right ascension
20h 27m 21s
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
15:16:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.135 km
Perigee altitude
558.363 km
Semi-major axis
6,939.386 km
Eccentricity
0.00042
Inclination
97.51°
RAAN
306.8375°
Arg. of periapsis
181.7289°
True anomaly
178.39354°
Mean anomaly
178.3922°
Eccentric anomaly
178.39287°
Mean motion
3.75458 °/min
Orbital period
95.88 mins
BSTAR
0.0003775
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