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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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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ALMUNTHER
1 63240U 25052AG 26306.47082992 .00015197 00000-0 43409-3 0 9993
2 63240 97.3696 201.1543 0007123 35.0874 325.0837 15.36078457 91210Epoch: 2026-11-02T11:17Z
TLE epoch observation values (Epoch: 2026-11-02T11:17:59.705Z)
Latitude
-0.00009°
Longitude
-10.09184°
Altitude
456.84 km
Speed
7.641 km/s
True Right ascension
13h 24m 37s
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
23:14:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.529 km
Perigee altitude
449.795 km
Semi-major axis
6,832.799 km
Eccentricity
0.00071
Inclination
97.3696°
RAAN
201.1543°
Arg. of periapsis
35.0874°
True anomaly
325.03695°
Mean anomaly
325.0837°
Eccentric anomaly
325.06033°
Mean motion
3.84278 °/min
Orbital period
93.68 mins
BSTAR
0.00043409
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-03 06:38:11.336Z | 325.422° NNW | 2026-11-03 06:39:11.336Z | 299.183° NW | 26.414° | 2026-11-03 06:42:11.336Z | 231.978° WSW |
| 4 mins | 2026-11-03 17:09:11.336Z | 162.092° S | 2026-11-03 17:11:11.336Z | 4.079° NNE | 65.072° | 2026-11-03 17:13:11.336Z | 350.665° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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