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: 18 hours ago
TLE from 18 hours ago
0 ALMUNTHER
1 63240U 25052AG 25288.66230240 .00020010 00000-0 87502-3 0 9995
2 63240 97.4118 180.3899 0005757 308.3108 51.7610 15.22093816 32699Epoch: 2025-10-15T15:53Z
TLE epoch observation values (Epoch: 2025-10-15T15:53:42.927Z)
Latitude
-0.00003°
Longitude
-82.47212°
Altitude
500.169 km
Speed
7.616 km/s
True Right ascension
12h 01m 33s
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
04:23:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.447 km
Perigee altitude
492.532 km
Semi-major axis
6,874.626 km
Eccentricity
0.00058
Inclination
97.4118°
RAAN
180.3899°
Arg. of periapsis
308.3108°
True anomaly
51.81284°
Mean anomaly
51.761°
Eccentric anomaly
51.78692°
Mean motion
3.80776 °/min
Orbital period
94.54 mins
BSTAR
0.00087502
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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 | 2025-10-16 17:16:14.835Z | 191.021° SSW | 2025-10-16 17:19:14.835Z | 288.093° WNW | 34.853° | 2025-10-16 17:22:14.835Z | 336.066° NNW |
| 4 mins | 2025-10-17 06:20:14.835Z | 334.797° NNW | 2025-10-17 06:22:14.835Z | 277.68° WNW | 27.794° | 2025-10-17 06:24:14.835Z | 232.752° WSW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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