Showing default

LEMUR 2 CAEL, 58903

Orbit data source: Space-Track

LEMUR 2 CAEL, 58903 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
58903, 2024-022E
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: 15 hours ago

TLE from 15 hours ago
0 LEMUR 2 CAEL
1 58903U 24022E   26166.52642514  .00014546  00000-0  35495-3 0  9994
2 58903  97.4085  17.4317 0009286 102.4687 257.7599 15.40929139132087
Epoch: 2026-06-15T12:38Z
TLE epoch observation values (Epoch: 2026-06-15T12:38:03.132Z)
Latitude
0.00001°
Longitude
-75.8929°
Altitude
447.833 km
Speed
7.643 km/s
True Right ascension
01h 09m 43s
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
14:03:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.636 km
Perigee altitude
433.972 km
Semi-major axis
6,818.441 km
Eccentricity
0.00093
Inclination
97.4085°
RAAN
17.4317°
Arg. of periapsis
102.4687°
True anomaly
257.65593°
Mean anomaly
257.7599°
Eccentric anomaly
257.70791°
Mean motion
3.85492 °/min
Orbital period
93.39 mins
BSTAR
0.00035495
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
|