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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: 7 hours ago

TLE from 7 hours ago
0 HERMES-1
1 63242U 25052AJ  26129.94474806  .00003280  00000-0  14991-3 0  9993
2 63242  97.3945  22.2588 0006194 332.0857  28.0046 15.21247363 63981
Epoch: 2026-05-09T22:40Z
TLE epoch observation values (Epoch: 2026-05-09T22:40:26.232Z)
Latitude
0.00001°
Longitude
174.39459°
Altitude
501.407 km
Speed
7.616 km/s
True Right ascension
01h 29m 02s
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
13:32:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.3 km
Perigee altitude
494.781 km
Semi-major axis
6,877.178 km
Eccentricity
0.00062
Inclination
97.3945°
RAAN
22.2588°
Arg. of periapsis
332.0857°
True anomaly
28.03795°
Mean anomaly
28.0046°
Eccentric anomaly
28.02127°
Mean motion
3.80564 °/min
Orbital period
94.6 mins
BSTAR
0.00014991
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