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HUYGENS, 55093

Orbit data source: Space-Track

HUYGENS, 55093 is a Norwegian payload satellite in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
55093, 2023-001CN
Orbit
SSO
Country
Flag of NONO / NOR
Related business
Manufacturer
NanoAvionics
Mission
Operational Civil Sigint
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 HUYGENS
1 55093U 23001CN  26097.62046256  .00011210  00000-0  29348-3 0  9997
2 55093  97.3298 164.7792 0008804 347.7446  12.3584 15.38845134181514
Epoch: 2026-04-07T14:53Z
TLE epoch observation values (Epoch: 2026-04-07T14:53:27.965Z)
Latitude
-0.00001°
Longitude
105.51812°
Altitude
446.768 km
Speed
7.647 km/s
True Right ascension
10h 59m 07s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
05:59:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452.469 km
Perigee altitude
440.452 km
Semi-major axis
6,824.598 km
Eccentricity
0.00088
Inclination
97.3298°
RAAN
164.7792°
Arg. of periapsis
347.7446°
True anomaly
12.38002°
Mean anomaly
12.3584°
Eccentric anomaly
12.36921°
Mean motion
3.84971 °/min
Orbital period
93.51 mins
BSTAR
0.00029348
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Computing Atmospheric mass density...

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