Showing default

LEMUR 2 UNTITLED-SC, 63351

Orbit data source: Space-Track

LEMUR 2 UNTITLED-SC, 63351 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
63351, 2025-061A
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 (6 months ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 LEMUR 2 UNTITLED-SC
1 63351U 25061A   25260.92616222  .00004908  00000-0  30071-3 0  9992
2 63351  97.5318 234.3642 0021836 119.2107 241.1310 15.10435777 26446
Epoch: 2025-09-17T22:13Z
TLE epoch observation values (Epoch: 2025-09-17T22:13:40.415Z)
Latitude
-0.00006°
Longitude
-96.14929°
Altitude
545.259 km
Speed
7.585 km/s
True Right ascension
15h 37m 27s
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
04:05:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.943 km
Perigee altitude
516.765 km
Semi-major axis
6,909.991 km
Eccentricity
0.00218
Inclination
97.5318°
RAAN
234.3642°
Arg. of periapsis
119.2107°
True anomaly
240.91216°
Mean anomaly
241.131°
Eccentric anomaly
241.02155°
Mean motion
3.77857 °/min
Orbital period
95.27 mins
BSTAR
0.00030071
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
|