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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.

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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: 18 hours ago

TLE from 18 hours ago
0 HERMES-6
1 63489U 25052BK  26120.69953810  .00008280  00000-0  36016-3 0  9993
2 63489  97.4055  13.8801 0005941 356.0589   4.0600 15.22494316 62609
Epoch: 2026-04-30T16:47Z
TLE epoch observation values (Epoch: 2026-04-30T16:47:20.091Z)
Latitude
-0.00001°
Longitude
-96.596°
Altitude
497.338 km
Speed
7.618 km/s
True Right ascension
00h 55m 31s
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
18:12:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.366 km
Perigee altitude
491.199 km
Semi-major axis
6,873.419 km
Eccentricity
0.00059
Inclination
97.4055°
RAAN
13.8801°
Arg. of periapsis
356.0589°
True anomaly
4.06482°
Mean anomaly
4.06°
Eccentric anomaly
4.06241°
Mean motion
3.80876 °/min
Orbital period
94.52 mins
BSTAR
0.00036016
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