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LEMUR 2 OBA-NI-JESU, 58902

Orbit data source: Space-Track

LEMUR 2 OBA-NI-JESU, 58902 is an American payload satellite in SSO that was launched on Wed, 31 Jan 2024 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
58902, 2024-022D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Early Warn
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~25 kg wet, ~25 kg dry
Launch date (UTC)
2024-01-31 (2 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.146 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 OBA-NI-JESU
1 58902U 24022D   25351.52750001  .00043734  00000-0  72036-3 0  9992
2 58902  97.4153 201.2228 0007240  23.2268 336.9311 15.52179114104803
Epoch: 2025-12-17T12:39Z
TLE epoch observation values (Epoch: 2025-12-17T12:39:36.000Z)
Latitude
0.00002°
Longitude
-75.07328°
Altitude
408.976 km
Speed
7.668 km/s
True Right ascension
13h 24m 53s
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
00:52:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
412.201 km
Perigee altitude
402.376 km
Semi-major axis
6,785.425 km
Eccentricity
0.00072
Inclination
97.4153°
RAAN
201.2228°
Arg. of periapsis
23.2268°
True anomaly
336.89856°
Mean anomaly
336.9311°
Eccentric anomaly
336.91483°
Mean motion
3.88309 °/min
Orbital period
92.71 mins
BSTAR
0.00072036
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