Showing default

HERMES-6, 63489

Orbit data source: Space-Track

HERMES-6, 63489 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
63489, 2025-052BK
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 (10 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 HERMES-6
1 63489U 25052BK  26027.25785584  .00013923  00000-0  63322-3 0  9992
2 63489  97.4147 281.8669 0005254 318.8910  41.1929 15.20829298 48396
Epoch: 2026-01-27T06:11Z
TLE epoch observation values (Epoch: 2026-01-27T06:11:18.744Z)
Latitude
-0.00004°
Longitude
62.49696°
Altitude
503.709 km
Speed
7.614 km/s
True Right ascension
18h 47m 28s
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
22:26:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.917 km
Perigee altitude
496.689 km
Semi-major axis
6,878.44 km
Eccentricity
0.00053
Inclination
97.4147°
RAAN
281.8669°
Arg. of periapsis
318.891°
True anomaly
41.23257°
Mean anomaly
41.1929°
Eccentric anomaly
41.21273°
Mean motion
3.80459 °/min
Orbital period
94.62 mins
BSTAR
0.00063322
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
|