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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.

Not visible in the next 10 days
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: 11 hours ago

TLE from 11 hours ago
0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D   25298.10050484  .00047881  00000-0  98383-3 0  9994
2 58902  97.4252 146.3015 0005694 190.8717 169.2410 15.45833340 96534
Epoch: 2025-10-25T02:24Z
TLE epoch observation values (Epoch: 2025-10-25T02:24:43.618Z)
Latitude
0.00001°
Longitude
76.38386°
Altitude
435.864 km
Speed
7.648 km/s
True Right ascension
09h 45m 12s
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
08:45:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.737 km
Perigee altitude
421.989 km
Semi-major axis
6,804 km
Eccentricity
0.00057
Inclination
97.4252°
RAAN
146.3015°
Arg. of periapsis
190.8717°
True anomaly
169.25317°
Mean anomaly
169.241°
Eccentric anomaly
169.24709°
Mean motion
3.8672 °/min
Orbital period
93.09 mins
BSTAR
0.00098383
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