Showing default

ALMUNTHER, 63240

Orbit data source: Space-Track

ALMUNTHER, 63240 is a Bahraini payload satellite in SSO that was launched on Sat, 15 Mar 2025 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
63240, 2025-052AG
Orbit
SSO
Country
Flag of BHBH / BHR
Related business
Manufacturer
AMAN/BNSSA
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
2025-03-15 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 ALMUNTHER
1 63240U 25052AG  26083.50449424  .00017154  00000-0  61126-3 0  9997
2 63240  97.3978 338.6825 0008787  89.7113 270.5133 15.28951792 57062
Epoch: 2026-03-24T12:06Z
TLE epoch observation values (Epoch: 2026-03-24T12:06:28.302Z)
Latitude
-0.0001°
Longitude
-24.91661°
Altitude
481.999 km
Speed
7.624 km/s
True Right ascension
22h 34m 43s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
08:47:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.921 km
Perigee altitude
469.875 km
Semi-major axis
6,854.035 km
Eccentricity
0.00088
Inclination
97.3978°
RAAN
338.6825°
Arg. of periapsis
89.7113°
True anomaly
270.41261°
Mean anomaly
270.5133°
Eccentric anomaly
270.46296°
Mean motion
3.82493 °/min
Orbital period
94.12 mins
BSTAR
0.00061126
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
|