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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: 6 hours ago

TLE from 6 hours ago
0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D   26074.54575238  .00092667  00000-0  87329-3 0  9994
2 58902  97.4054 292.9089 0004516  53.9452 306.2226 15.66770697118519
Epoch: 2026-03-15T13:05Z
TLE epoch observation values (Epoch: 2026-03-15T13:05:53.005Z)
Latitude
-0.00005°
Longitude
-76.71298°
Altitude
369.505 km
Speed
7.689 km/s
True Right ascension
19h 31m 38s
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
23:16:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
368.1 km
Perigee altitude
362.01 km
Semi-major axis
6,743.192 km
Eccentricity
0.00045
Inclination
97.4054°
RAAN
292.9089°
Arg. of periapsis
53.9452°
True anomaly
306.18084°
Mean anomaly
306.2226°
Eccentric anomaly
306.20172°
Mean motion
3.91963 °/min
Orbital period
91.85 mins
BSTAR
0.00087329
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