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: 8 hours ago
TLE from 8 hours ago
0 ALMUNTHER
1 63240U 25052AG 26260.13045960 .00016327 00000-0 48846-3 0 9995
2 63240 97.3733 154.7988 0006385 161.5115 198.6361 15.34610115 84107Epoch: 2026-09-17T03:07Z
TLE epoch observation values (Epoch: 2026-09-17T03:07:51.709Z)
Latitude
-0.00005°
Longitude
111.76124°
Altitude
469.33 km
Speed
7.629 km/s
True Right ascension
10h 19m 11s
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
04:04:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.389 km
Perigee altitude
454.658 km
Semi-major axis
6,837.161 km
Eccentricity
0.00064
Inclination
97.3733°
RAAN
154.7988°
Arg. of periapsis
161.5115°
True anomaly
198.61274°
Mean anomaly
198.6361°
Eccentric anomaly
198.62442°
Mean motion
3.8391 °/min
Orbital period
93.77 mins
BSTAR
0.00048846
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 17:20:48.725Z | 183.238° SSW | 2026-09-17 17:22:48.725Z | 223.388° SW | 52.509° | 2026-09-17 17:25:48.725Z | 336.488° NNW |
| 4 mins | 2026-09-18 06:18:48.725Z | 341.349° N | 2026-09-18 06:19:48.725Z | 309.734° NW | 42.032° | 2026-09-18 06:22:48.725Z | 216.622° SW |
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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