Showing default

LEMUR 2 THERMORAPTOR, 63354

Orbit data source: Space-Track

LEMUR 2 THERMORAPTOR, 63354 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.

Loading next visibility...
Identifier
63354, 2025-061D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 8U, 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: 3 days ago

TLE from 3 days ago
0 LEMUR 2 THERMORAPTOR
1 63354U 25061D   26154.98900498  .00004355  00000-0  24289-3 0  9995
2 63354  97.5694 131.1285 0017367 304.9847  54.9753 15.13981450 65611
Epoch: 2026-06-03T23:44Z
TLE epoch observation values (Epoch: 2026-06-03T23:44:10.030Z)
Latitude
-0.00004°
Longitude
-117.353°
Altitude
520.283 km
Speed
7.607 km/s
True Right ascension
08h 44m 30s
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
00:56:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.035 km
Perigee altitude
509.072 km
Semi-major axis
6,899.19 km
Eccentricity
0.00174
Inclination
97.5694°
RAAN
131.1285°
Arg. of periapsis
304.9847°
True anomaly
55.13847°
Mean anomaly
54.9753°
Eccentric anomaly
55.05687°
Mean motion
3.78744 °/min
Orbital period
95.05 mins
BSTAR
0.00024289
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|