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HERMES 4, 63833

Orbit data source: Space-Track

HERMES 4, 63833 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
63833, 2025-052BP
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, 14.5 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 HERMES 4
1 63833U 25052BP  26082.94362350  .00017518  00000-0  65620-3 0  9991
2 63833  97.3973 337.3626 0004200 124.2155 235.9482 15.27331455 56920
Epoch: 2026-03-23T22:38Z
TLE epoch observation values (Epoch: 2026-03-23T22:38:49.070Z)
Latitude
-0.00008°
Longitude
176.22978°
Altitude
488.509 km
Speed
7.62 km/s
True Right ascension
22h 29m 27s
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
03:08:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.63 km
Perigee altitude
477.868 km
Semi-major axis
6,858.886 km
Eccentricity
0.00042
Inclination
97.3973°
RAAN
337.3626°
Arg. of periapsis
124.2155°
True anomaly
235.90834°
Mean anomaly
235.9482°
Eccentric anomaly
235.92827°
Mean motion
3.82087 °/min
Orbital period
94.22 mins
BSTAR
0.0006562
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