HADES-ICM, 63492 (Decayed)
Orbit data source: Space-Track
HADES-ICM, 63492 was a Spanish payload satellite in LEO 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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63492 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Hydra Space
Mission
Decayed Amateur Communications
Bus & Motor
PQ 1.5P, Unknown motor
Mass
0.375 kg wet, 0.375 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.006 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 HADES-ICM
1 63492U 25052BN 26141.26653985 .06534464 24594-5 20838-2 0 9990
2 63492 97.3646 46.2798 0012126 212.7126 147.3417 16.26141574 66567Epoch: 2026-05-21T06:23Z
TLE epoch observation values (Epoch: 2026-05-21T06:23:49.043Z)
Latitude
0.00005°
Longitude
71.41124°
Altitude
212.886 km
Speed
7.775 km/s
True Right ascension
03h 05m 07s
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
07:24:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
207.73 km
Perigee altitude
191.777 km
Semi-major axis
6,577.89 km
Eccentricity
0.00121
Inclination
97.3646°
RAAN
46.2798°
Arg. of periapsis
212.7126°
True anomaly
147.41659°
Mean anomaly
147.3417°
Eccentric anomaly
147.37915°
Mean motion
4.0683 °/min
Orbital period
88.49 mins
BSTAR
0.0020838
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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.HADES-ICM Visibility
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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. |
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| This satellite is decayed. |
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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