Showing default

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.

Loading next visibility...
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: 10 hours ago

TLE from 10 hours ago
0 LEMUR 2 JOHNNYTRUONG
1 59146U 24043BA  25289.16627524  .00026591  00000-0  60451-3 0  9999
2 59146  97.5175  64.5293 0005734 352.0282   8.0873 15.42965066 90202
Epoch: 2025-10-16T03:59Z
TLE epoch observation values (Epoch: 2025-10-16T03:59:26.180Z)
Latitude
-0.00005°
Longitude
-20.25968°
Altitude
436.612 km
Speed
7.652 km/s
True Right ascension
04h 18m 07s
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
08:21:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
438.21 km
Perigee altitude
430.398 km
Semi-major axis
6,812.441 km
Eccentricity
0.00057
Inclination
97.5175°
RAAN
64.5293°
Arg. of periapsis
352.0282°
True anomaly
8.09655°
Mean anomaly
8.0873°
Eccentric anomaly
8.09192°
Mean motion
3.86002 °/min
Orbital period
93.26 mins
BSTAR
0.00060451
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
|