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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 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 HERMES-1
1 63242U 25052AJ  26260.46625890  .00003650  00000-0  16143-3 0  9999
2 63242  97.3749 150.3961 0006023 208.0131 152.0782 15.22300152 83837
Epoch: 2026-09-17T11:11Z
TLE epoch observation values (Epoch: 2026-09-17T11:11:24.768Z)
Latitude
-0.00006°
Longitude
-13.86019°
Altitude
505.66 km
Speed
7.609 km/s
True Right ascension
10h 01m 35s
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
14:41:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.006 km
Perigee altitude
491.726 km
Semi-major axis
6,874.003 km
Eccentricity
0.0006
Inclination
97.3749°
RAAN
150.3961°
Arg. of periapsis
208.0131°
True anomaly
152.1105°
Mean anomaly
152.0782°
Eccentric anomaly
152.09435°
Mean motion
3.80828 °/min
Orbital period
94.53 mins
BSTAR
0.00016143
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