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.
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63240 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
BH / BHRRelated business
Manufacturer
AMAN/BNSSA
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 ALMUNTHER
1 63240U 25052AG 25311.26974583 .00022305 00000-0 94686-3 0 9993
2 63240 97.4097 202.6898 0006050 199.0819 161.0192 15.23079559 36135Epoch: 2025-11-07T06:28Z
TLE epoch observation values (Epoch: 2025-11-07T06:28:26.039Z)
Latitude
-0.00004°
Longitude
58.86518°
Altitude
503.587 km
Speed
7.61 km/s
True Right ascension
13h 30m 45s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
22:44:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.677 km
Perigee altitude
489.363 km
Semi-major axis
6,871.657 km
Eccentricity
0.00061
Inclination
97.4097°
RAAN
202.6898°
Arg. of periapsis
199.0819°
True anomaly
161.04173°
Mean anomaly
161.0192°
Eccentric anomaly
161.03047°
Mean motion
3.81023 °/min
Orbital period
94.48 mins
BSTAR
0.00094686
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Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ALMUNTHER Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-08 05:06:57.674Z | 38.966° NE | 2025-11-08 05:09:57.674Z | 97.558° ESE | 23.594° | 2025-11-08 05:12:57.674Z | 154.372° SSE |
| 5 mins | 2025-11-08 17:17:57.674Z | 195.883° SSW | 2025-11-08 17:19:57.674Z | 253.046° W | 35.531° | 2025-11-08 17:22:57.674Z | 331.764° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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