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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: 14 hours ago

TLE from 14 hours ago
0 LEMUR 2 JOHNNYTRUONG
1 59146U 24043BA  26132.40004082  .00024172  00000-0  32562-3 0  9997
2 59146  97.5345 281.9716 0003458 307.6688  52.4253 15.57835141122468
Epoch: 2026-05-12T09:36Z
TLE epoch observation values (Epoch: 2026-05-12T09:36:03.526Z)
Latitude
-0.00007°
Longitude
-92.21805°
Altitude
395.634 km
Speed
7.674 km/s
True Right ascension
18h 47m 53s
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
07:47:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
393.186 km
Perigee altitude
388.504 km
Semi-major axis
6,768.982 km
Eccentricity
0.00035
Inclination
97.5345°
RAAN
281.9716°
Arg. of periapsis
307.6688°
True anomaly
52.45671°
Mean anomaly
52.4253°
Eccentric anomaly
52.44101°
Mean motion
3.89725 °/min
Orbital period
92.37 mins
BSTAR
0.00032562
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