HADES-ICM, 63492
Orbit data source: Space-Track
HADES-ICM, 63492 is a Spanish 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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63492 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Hydra Space
Mission
Operational Amateur Communications
Bus & Motor
PQ 1.5U, 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 HADES-ICM
1 63492U 25052BN 25287.44268133 .00049191 00000-0 16243-2 0 9995
2 63492 97.4116 180.6528 0006797 300.4489 59.6081 15.31215611 32607Epoch: 2025-10-14T10:37Z
TLE epoch observation values (Epoch: 2025-10-14T10:37:27.666Z)
Latitude
0.00002°
Longitude
-1.94352°
Altitude
472.936 km
Speed
7.631 km/s
True Right ascension
12h 02m 36s
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
05:46:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.79 km
Perigee altitude
464.481 km
Semi-major axis
6,847.272 km
Eccentricity
0.00068
Inclination
97.4116°
RAAN
180.6528°
Arg. of periapsis
300.4489°
True anomaly
59.67531°
Mean anomaly
59.6081°
Eccentric anomaly
59.6417°
Mean motion
3.8306 °/min
Orbital period
93.98 mins
BSTAR
0.0016243
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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 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 | 2025-10-15 16:33:17.670Z | 137.163° SSE | 2025-10-15 16:36:17.670Z | 70.463° E | 29.342° | 2025-10-15 16:39:17.670Z | 7.746° NNE |
| 4 mins | 2025-10-16 05:33:17.670Z | 42.486° NE | 2025-10-16 05:35:17.670Z | 125.029° SE | 33.632° | 2025-10-16 05:37:17.670Z | 167.784° S |
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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