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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 (1 year 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   26139.37162257  .00002092  00000-0  12068-3 0  9990
2 63352  97.5633 115.0390 0018721   9.9175 350.2422 15.13339645 63235
Epoch: 2026-05-19T08:55Z
TLE epoch observation values (Epoch: 2026-05-19T08:55:08.190Z)
Latitude
0.00002°
Longitude
104.20839°
Altitude
516.36 km
Speed
7.612 km/s
True Right ascension
07h 40m 09s
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
04:53:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.925 km
Perigee altitude
510.086 km
Semi-major axis
6,901.142 km
Eccentricity
0.00187
Inclination
97.5633°
RAAN
115.039°
Arg. of periapsis
9.9175°
True anomaly
350.20576°
Mean anomaly
350.2422°
Eccentric anomaly
350.22399°
Mean motion
3.78584 °/min
Orbital period
95.09 mins
BSTAR
0.00012068
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