Showing default

HERMES-2, 63243

Orbit data source: Space-Track

HERMES-2, 63243 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
63243, 2025-052AK
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: 1 day ago

TLE from 1 day ago
0 HERMES-2
1 63243U 25052AK  26206.20065874  .00016017  00000-0  54083-3 0  9998
2 63243  97.3851 100.9276 0004261   9.7157 350.4165 15.30749924 75831
Epoch: 2026-07-25T04:48Z
TLE epoch observation values (Epoch: 2026-07-25T04:48:56.915Z)
Latitude
-0.00006°
Longitude
85.77411°
Altitude
473.8 km
Speed
7.631 km/s
True Right ascension
06h 43m 42s
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
20:20:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.442 km
Perigee altitude
467.606 km
Semi-major axis
6,848.661 km
Eccentricity
0.00043
Inclination
97.3851°
RAAN
100.9276°
Arg. of periapsis
9.7157°
True anomaly
350.40837°
Mean anomaly
350.4165°
Eccentric anomaly
350.41243°
Mean motion
3.82943 °/min
Orbital period
94.01 mins
BSTAR
0.00054083
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
|