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LEMUR 2 JOHNNYTRUONG, 59146

Orbit data source: Space-Track

LEMUR 2 JOHNNYTRUONG, 59146 is an American payload satellite in SSO that was launched on Mon, 04 Mar 2024 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.

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Identifier
59146, 2024-043BA
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
2024-03-04 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 1.4 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 LEMUR 2 JOHNNYTRUONG
1 59146U 24043BA  26186.41798977  .00047528  00000-0  54499-3 0  9993
2 59146  97.5395 339.2692 0004469 123.0348 237.1339 15.61947714130886
Epoch: 2026-07-05T10:01Z
TLE epoch observation values (Epoch: 2026-07-05T10:01:54.316Z)
Latitude
-0.00002°
Longitude
-94.62473°
Altitude
386.815 km
Speed
7.677 km/s
True Right ascension
22h 37m 04s
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
23:27:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
381.967 km
Perigee altitude
375.928 km
Semi-major axis
6,757.084 km
Eccentricity
0.00045
Inclination
97.5395°
RAAN
339.2692°
Arg. of periapsis
123.0348°
True anomaly
237.0909°
Mean anomaly
237.1339°
Eccentric anomaly
237.1124°
Mean motion
3.90755 °/min
Orbital period
92.13 mins
BSTAR
0.00054499
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