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.
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55093 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
NanoAvionics
Mission
Operational Civil Sigint
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 HUYGENS
1 55093U 23001CN 25311.84525531 .00016232 00000-0 47625-3 0 9994
2 55093 97.3563 14.1243 0011615 152.6834 207.5023 15.35178414158355Epoch: 2025-11-07T20:17Z
TLE epoch observation values (Epoch: 2025-11-07T20:17:10.058Z)
Latitude
-0°
Longitude
22.54902°
Altitude
470.552 km
Speed
7.627 km/s
True Right ascension
00h 56m 29s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:42:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.273 km
Perigee altitude
449.395 km
Semi-major axis
6,835.471 km
Eccentricity
0.00116
Inclination
97.3563°
RAAN
14.1243°
Arg. of periapsis
152.6834°
True anomaly
207.44092°
Mean anomaly
207.5023°
Eccentric anomaly
207.4716°
Mean motion
3.84052 °/min
Orbital period
93.74 mins
BSTAR
0.00047625
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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.HUYGENS Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-08 17:11:07.484Z | 10.959° NNE | 2025-11-08 17:14:07.484Z | 200.037° SSW | 42.627° | 2025-11-08 17:16:07.484Z | 194.187° SSW |
| 4 mins | 2025-11-09 03:44:07.484Z | 105.617° ESE | 2025-11-09 03:45:07.484Z | 78.866° E | 23.514° | 2025-11-09 03:48:07.484Z | 14.941° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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