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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: 18 hours ago

TLE from 18 hours ago
0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D   25259.08111590  .00033775  00000-0  79200-3 0  9998
2 58902  97.4342 106.4539 0006705 358.2631   1.8591 15.41977831 90514
Epoch: 2025-09-16T01:56Z
TLE epoch observation values (Epoch: 2025-09-16T01:56:48.413Z)
Latitude
-0.00009°
Longitude
81.97565°
Altitude
438.822 km
Speed
7.651 km/s
True Right ascension
07h 05m 48s
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
12:47:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.78 km
Perigee altitude
432.641 km
Semi-major axis
6,815.347 km
Eccentricity
0.00067
Inclination
97.4342°
RAAN
106.4539°
Arg. of periapsis
358.2631°
True anomaly
1.86159°
Mean anomaly
1.8591°
Eccentric anomaly
1.86035°
Mean motion
3.85755 °/min
Orbital period
93.32 mins
BSTAR
0.000792
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Documentation

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