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)
2025-03-15 (10 months 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: 19 hours ago

TLE from 19 hours ago
0 HADES-ICM
1 63492U 25052BN  26027.22796990  .00126897  00000-0  24807-2 0  9995
2 63492  97.4022 286.4807 0003781 282.8419  77.2408 15.46968471 48717
Epoch: 2026-01-27T05:28Z
TLE epoch observation values (Epoch: 2026-01-27T05:28:16.599Z)
Latitude
-0.00003°
Longitude
77.89915°
Altitude
428.16 km
Speed
7.655 km/s
True Right ascension
19h 05m 55s
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
01:49:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
425.101 km
Perigee altitude
419.959 km
Semi-major axis
6,800.667 km
Eccentricity
0.00038
Inclination
97.4022°
RAAN
286.4807°
Arg. of periapsis
282.8419°
True anomaly
77.28306°
Mean anomaly
77.2408°
Eccentric anomaly
77.26193°
Mean motion
3.87004 °/min
Orbital period
93.02 mins
BSTAR
0.0024807
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
|