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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 (7 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: 11 hours ago

TLE from 11 hours ago
0 LEMUR 2 ESPERANZA
1 63352U 25061B   25309.86078388  .00005133  00000-0  30727-3 0  9994
2 63352  97.5403 282.6015 0017999 318.9783  41.0092 15.11326129 33831
Epoch: 2025-11-05T20:39Z
TLE epoch observation values (Epoch: 2025-11-05T20:39:31.727Z)
Latitude
-0.00004°
Longitude
-72.60808°
Altitude
525.851 km
Speed
7.605 km/s
True Right ascension
18h 50m 24s
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
04:03:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.57 km
Perigee altitude
516.705 km
Semi-major axis
6,907.275 km
Eccentricity
0.0018
Inclination
97.5403°
RAAN
282.6015°
Arg. of periapsis
318.9783°
True anomaly
41.14477°
Mean anomaly
41.0092°
Eccentric anomaly
41.07696°
Mean motion
3.78079 °/min
Orbital period
95.22 mins
BSTAR
0.00030727
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