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HERMES-1, 63242

Orbit data source: Space-Track

HERMES-1, 63242 is a payload satellite owned by ASI (IT) 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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Identifier
63242, 2025-052AJ
Orbit
SSO
Country
Flag of ITIT
Related business
Manufacturer
MILANP/INAFI
Mission
Operational Civil Astronomy
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2025-03-15 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 HERMES-1
1 63242U 25052AJ  25239.97099596  .00006607  00000-0  33191-3 0  9995
2 63242  97.4201 132.0443 0009555 122.2287 237.9875 15.17568062 25264
Epoch: 2025-08-27T23:18Z
TLE epoch observation values (Epoch: 2025-08-27T23:18:14.05Z)
Latitude
0.00002°
Longitude
166.04505°
Altitude
519.776 km
Speed
7.602 km/s
True Right ascension
08h 48m 10s
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
10:59:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.745 km
Perigee altitude
503.581 km
Semi-major axis
6,888.3 km
Eccentricity
0.00096
Inclination
97.4201°
RAAN
132.0443°
Arg. of periapsis
122.2287°
True anomaly
237.89472°
Mean anomaly
237.9875°
Eccentric anomaly
237.9411°
Mean motion
3.79643 °/min
Orbital period
94.83 mins
BSTAR
0.00033191
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