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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 LEO 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.

Not visible in the next 10 days
Identifier
58902, 2024-022D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Decayed 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: 3 days ago

TLE from 3 days ago
0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D   26164.26942669  .07840474  25257-5  90464-3 0  9993
2 58902  97.3603  29.4721 0009182 248.5343 111.4976 16.36778297132706
Epoch: 2026-06-13T06:27Z
TLE epoch observation values (Epoch: 2026-06-13T06:27:58.466Z)
Latitude
0.00001°
Longitude
30.89155°
Altitude
179.845 km
Speed
7.797 km/s
True Right ascension
01h 57m 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
14:56:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
177.21 km
Perigee altitude
165.183 km
Semi-major axis
6,549.334 km
Eccentricity
0.00092
Inclination
97.3603°
RAAN
29.4721°
Arg. of periapsis
248.5343°
True anomaly
111.59546°
Mean anomaly
111.4976°
Eccentric anomaly
111.54653°
Mean motion
4.09494 °/min
Orbital period
87.91 mins
BSTAR
0.00090464
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Documentation

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