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 (1 year 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: 5 hours ago

TLE from 5 hours ago
0 HERMES-6
1 63489U 25052BK  26121.29104832  .00010953  00000-0  47508-3 0  9990
2 63489  97.4053  14.4629 0005861 354.0047   6.1118 15.22509698 62696
Epoch: 2026-05-01T06:59Z
TLE epoch observation values (Epoch: 2026-05-01T06:59:06.574Z)
Latitude
-0.00008°
Longitude
50.4601°
Altitude
497.359 km
Speed
7.618 km/s
True Right ascension
00h 57m 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
19:21:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.264 km
Perigee altitude
491.207 km
Semi-major axis
6,873.373 km
Eccentricity
0.00059
Inclination
97.4053°
RAAN
14.4629°
Arg. of periapsis
354.0047°
True anomaly
6.11896°
Mean anomaly
6.1118°
Eccentric anomaly
6.11538°
Mean motion
3.8088 °/min
Orbital period
94.52 mins
BSTAR
0.00047508
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
|