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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 (1 year 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: 15 hours ago

TLE from 15 hours ago
0 HERMES-1
1 63242U 25052AJ  26083.43316279  .00005552  00000-0  25498-3 0  9993
2 63242  97.3998 336.5869 0008954 115.3930 244.8233 15.20760668 56910
Epoch: 2026-03-24T10:23Z
TLE epoch observation values (Epoch: 2026-03-24T10:23:45.265Z)
Latitude
-0.00004°
Longitude
-1.26259°
Altitude
509.263 km
Speed
7.608 km/s
True Right ascension
22h 26m 20s
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
06:58:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.669 km
Perigee altitude
494.35 km
Semi-major axis
6,878.646 km
Eccentricity
0.0009
Inclination
97.3998°
RAAN
336.5869°
Arg. of periapsis
115.393°
True anomaly
244.73049°
Mean anomaly
244.8233°
Eccentric anomaly
244.77689°
Mean motion
3.80442 °/min
Orbital period
94.63 mins
BSTAR
0.00025498
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