Showing default

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.

Loading next visibility...
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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 HERMES-3
1 63835U 25052BR  26166.97475778  .00015354  00000-0  46924-3 0  9990
2 63835  97.3880  62.4521 0007871 122.4639 237.7365 15.33937254 69877
Epoch: 2026-06-15T23:23Z
TLE epoch observation values (Epoch: 2026-06-15T23:23:39.072Z)
Latitude
-0.00007°
Longitude
167.28587°
Altitude
470.067 km
Speed
7.629 km/s
True Right ascension
04h 09m 48s
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
14:52:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.409 km
Perigee altitude
455.642 km
Semi-major axis
6,839.162 km
Eccentricity
0.00079
Inclination
97.388°
RAAN
62.4521°
Arg. of periapsis
122.4639°
True anomaly
237.66027°
Mean anomaly
237.7365°
Eccentric anomaly
237.69838°
Mean motion
3.83742 °/min
Orbital period
93.81 mins
BSTAR
0.00046924
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|