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 (9 months 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: 10 hours ago

TLE from 10 hours ago
0 HERMES-2
1 63243U 25052AK  25336.24417008  .00016692  00000-0  68602-3 0  9996
2 63243  97.4104 227.6498 0007464  85.3795 274.8295 15.24226505 39956
Epoch: 2025-12-02T05:51Z
TLE epoch observation values (Epoch: 2025-12-02T05:51:36.294Z)
Latitude
-0.00003°
Longitude
68.41648°
Altitude
495.777 km
Speed
7.617 km/s
True Right ascension
15h 10m 35s
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
13:16:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.196 km
Perigee altitude
484.943 km
Semi-major axis
6,868.206 km
Eccentricity
0.00075
Inclination
97.4104°
RAAN
227.6498°
Arg. of periapsis
85.3795°
True anomaly
274.74427°
Mean anomaly
274.8295°
Eccentric anomaly
274.78688°
Mean motion
3.8131 °/min
Orbital period
94.41 mins
BSTAR
0.00068602
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
|