Showing default

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.

Loading next visibility...
Identifier
63492, 2025-052BN
Orbit
SSO
Country
Flag of ESES / SPN
Related 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)
Icon of a cake. It is the launch day of the satellite!2025-03-15 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.006 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 HADES-ICM
1 63492U 25052BN  26074.22212562  .00168690  00000-0  21514-2 0  9994
2 63492  97.3927 334.8766 0009113 100.0841 260.1444 15.58682409 56008
Epoch: 2026-03-15T05:19Z
TLE epoch observation values (Epoch: 2026-03-15T05:19:51.653Z)
Latitude
0.00001°
Longitude
82.07932°
Altitude
395.674 km
Speed
7.672 km/s
True Right ascension
22h 19m 30s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
04:00:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
394.55 km
Perigee altitude
382.217 km
Semi-major axis
6,766.52 km
Eccentricity
0.00091
Inclination
97.3927°
RAAN
334.8766°
Arg. of periapsis
100.0841°
True anomaly
260.04153°
Mean anomaly
260.1444°
Eccentric anomaly
260.09296°
Mean motion
3.89938 °/min
Orbital period
92.32 mins
BSTAR
0.0021514
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|