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LEMUR 2 NIMBUS2000, 58899

Orbit data source: Space-Track

LEMUR 2 NIMBUS2000, 58899 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
58899, 2024-022A
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 NIMBUS2000
1 58899U 24022A   25306.50959907  .00016411  00000-0  53947-3 0  9993
2 58899  97.4321 149.6398 0009950 202.5936 157.4868 15.31573047 97479
Epoch: 2025-11-02T12:13Z
TLE epoch observation values (Epoch: 2025-11-02T12:13:49.359Z)
Latitude
-0.00009°
Longitude
-75.84015°
Altitude
480.522 km
Speed
7.622 km/s
True Right ascension
09h 58m 33s
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
19:22:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.882 km
Perigee altitude
461.258 km
Semi-major axis
6,846.207 km
Eccentricity
0.001
Inclination
97.4321°
RAAN
149.6398°
Arg. of periapsis
202.5936°
True anomaly
157.53041°
Mean anomaly
157.4868°
Eccentric anomaly
157.50861°
Mean motion
3.83149 °/min
Orbital period
93.96 mins
BSTAR
0.00053947
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