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LEMUR 2 ESPERANZA, 63352

Orbit data source: Space-Track

LEMUR 2 ESPERANZA, 63352 is a payload satellite owned by OroraTech (US) in SSO that was launched on Wed, 26 Mar 2025 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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
63352, 2025-061B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
2025-03-26 (9 months ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 LEMUR 2 ESPERANZA
1 63352U 25061B   25354.41038388  .00003213  00000-0  19079-3 0  9995
2 63352  97.5449 326.5643 0019533 155.3994 204.8173 15.11877742 40568
Epoch: 2025-12-20T09:50Z
TLE epoch observation values (Epoch: 2025-12-20T09:50:57.167Z)
Latitude
0.00004°
Longitude
89.58851°
Altitude
545.805 km
Speed
7.582 km/s
True Right ascension
21h 46m 15s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
16:16:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.945 km
Perigee altitude
513.968 km
Semi-major axis
6,905.593 km
Eccentricity
0.00195
Inclination
97.5449°
RAAN
326.5643°
Arg. of periapsis
155.3994°
True anomaly
204.72356°
Mean anomaly
204.8173°
Eccentric anomaly
204.77041°
Mean motion
3.78218 °/min
Orbital period
95.18 mins
BSTAR
0.00019079
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