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HERMES-3, 63835

Orbit data source: Space-Track

HERMES-3, 63835 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
63835, 2025-052BR
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, 0.2 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 HERMES-3
1 63835U 25052BR  26120.69686945  .00022971  00000-0  74026-3 0  9996
2 63835  97.3927  16.2153 0003624 309.4756  50.6165 15.32182464 62783
Epoch: 2026-04-30T16:43Z
TLE epoch observation values (Epoch: 2026-04-30T16:43:29.520Z)
Latitude
-0.00001°
Longitude
-93.29746°
Altitude
470.835 km
Speed
7.632 km/s
True Right ascension
01h 04m 51s
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
18:12:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.732 km
Perigee altitude
463.771 km
Semi-major axis
6,844.388 km
Eccentricity
0.00036
Inclination
97.3927°
RAAN
16.2153°
Arg. of periapsis
309.4756°
True anomaly
50.64861°
Mean anomaly
50.6165°
Eccentric anomaly
50.63255°
Mean motion
3.83302 °/min
Orbital period
93.92 mins
BSTAR
0.00074026
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