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: 12 hours ago
TLE from 12 hours ago
0 HUYGENS
1 55093U 23001CN 25260.32857047 .00007539 00000-0 23270-3 0 9990
2 55093 97.3652 322.7438 0010106 352.7694 7.3401 15.33802355150454Epoch: 2025-09-17T07:53Z
TLE epoch observation values (Epoch: 2025-09-17T07:53:08.488Z)
Latitude
-0.00006°
Longitude
-152.04765°
Altitude
460.73 km
Speed
7.64 km/s
True Right ascension
21h 30m 58s
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
12:32:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.338 km
Perigee altitude
454.514 km
Semi-major axis
6,839.563 km
Eccentricity
0.00101
Inclination
97.3652°
RAAN
322.7438°
Arg. of periapsis
352.7694°
True anomaly
7.35491°
Mean anomaly
7.3401°
Eccentric anomaly
7.34751°
Mean motion
3.83708 °/min
Orbital period
93.82 mins
BSTAR
0.0002327
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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 04:22:04.789Z | 171.99° S | 2025-09-18 04:25:04.789Z | 306.992° NW | 43.687° | 2025-09-18 04:28:04.789Z | 345.259° N |
| 5 mins | 2025-09-18 17:20:04.789Z | 358.962° N | 2025-09-18 17:22:04.789Z | 300.128° NW | 40.573° | 2025-09-18 17:25:04.789Z | 206.271° SW |
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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