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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: 7 hours ago

TLE from 7 hours ago
0 LEMUR 2 JOHNNYTRUONG
1 59146U 24043BA  26079.85976820  .00035101  00000-0  54400-3 0  9993
2 59146  97.5283 226.5822 0005423 147.6174 212.5412 15.53932105114290
Epoch: 2026-03-20T20:38Z
TLE epoch observation values (Epoch: 2026-03-20T20:38:03.972Z)
Latitude
-0.00011°
Longitude
98.67688°
Altitude
411.494 km
Speed
7.662 km/s
True Right ascension
15h 06m 19s
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
08:12:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
405.862 km
Perigee altitude
398.508 km
Semi-major axis
6,780.322 km
Eccentricity
0.00054
Inclination
97.5283°
RAAN
226.5822°
Arg. of periapsis
147.6174°
True anomaly
212.50779°
Mean anomaly
212.5412°
Eccentric anomaly
212.52449°
Mean motion
3.88748 °/min
Orbital period
92.61 mins
BSTAR
0.000544
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