Showing default

LEMUR 2 BASS, 58259

Orbit data source: Space-Track

LEMUR 2 BASS, 58259 is an American payload satellite in SSO that was launched on Sat, 11 Nov 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
58259, 2023-174D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Earth Obs Sci
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2023-11-11 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 LEMUR 2 BASS
1 58259U 23174D   26024.15351560  .00026911  00000-0  71950-3 0  9990
2 58259  97.3947 107.3383 0007395 335.2179  24.8709 15.38016644123182
Epoch: 2026-01-24T03:41Z
TLE epoch observation values (Epoch: 2026-01-24T03:41:03.747Z)
Latitude
-0.00012°
Longitude
-71.40936°
Altitude
450.507 km
Speed
7.645 km/s
True Right ascension
07h 09m 21s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
12:40:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.965 km
Perigee altitude
443.868 km
Semi-major axis
6,827.053 km
Eccentricity
0.00074
Inclination
97.3947°
RAAN
107.3383°
Arg. of periapsis
335.2179°
True anomaly
24.90657°
Mean anomaly
24.8709°
Eccentric anomaly
24.88873°
Mean motion
3.84763 °/min
Orbital period
93.56 mins
BSTAR
0.0007195
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
|