Showing default

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.

Loading next visibility...
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 (3 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: 14 hours ago

TLE from 14 hours ago
0 LEMUR 2 NIMBUS2000
1 58899U 24022A   26255.57226110  .00019246  00000-0  43245-3 0  9996
2 58899  97.3997 106.8469 0008722 151.9869 208.1850 15.43354462145738
Epoch: 2026-09-12T13:44Z
TLE epoch observation values (Epoch: 2026-09-12T13:44:03.359Z)
Latitude
0.00002°
Longitude
-90.74644°
Altitude
444.581 km
Speed
7.642 km/s
True Right ascension
07h 07m 23s
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
20:03:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
439.093 km
Perigee altitude
427.211 km
Semi-major axis
6,811.289 km
Eccentricity
0.00087
Inclination
97.3997°
RAAN
106.8469°
Arg. of periapsis
151.9869°
True anomaly
208.13784°
Mean anomaly
208.185°
Eccentric anomaly
208.16141°
Mean motion
3.86099 °/min
Orbital period
93.24 mins
BSTAR
0.00043245
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|