HYPSO-1, 51053
Orbit data source: Space-Track
HYPSO-1, 51053 is a payload satellite owned by NTNU (NO) in SSO that was launched on Thu, 13 Jan 2022 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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51053 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
NanoAvionics
Mission
Operational Amateur Imaging
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: 15 hours ago
TLE from 15 hours ago
0 HYPSO-1
1 51053U 22002BX 25287.94797306 .00029974 00000-0 56999-3 0 9991
2 51053 97.3176 357.6082 0004520 112.6277 247.5452 15.48190288208710Epoch: 2025-10-14T22:45Z
TLE epoch observation values (Epoch: 2025-10-14T22:45:04.872Z)
Latitude
-0.00002°
Longitude
-7.39118°
Altitude
426.327 km
Speed
7.655 km/s
True Right ascension
23h 50m 25s
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
08:05:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.017 km
Perigee altitude
415.872 km
Semi-major axis
6,797.082 km
Eccentricity
0.00045
Inclination
97.3176°
RAAN
357.6082°
Arg. of periapsis
112.6277°
True anomaly
247.49734°
Mean anomaly
247.5452°
Eccentric anomaly
247.52127°
Mean motion
3.87311 °/min
Orbital period
92.95 mins
BSTAR
0.00056999
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Other satellites on launch #2 in the year 2022 (2022-01-13 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.HYPSO-1 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 | 2025-10-15 17:54:52.088Z | 359.072° N | 2025-10-15 17:57:52.088Z | 280.393° WNW | 36.114° | 2025-10-15 17:59:52.088Z | 216.959° SW |
| 4 mins | 2025-10-16 04:22:52.088Z | 117.603° SE | 2025-10-16 04:23:52.088Z | 85.5° E | 28.076° | 2025-10-16 04:26:52.088Z | 9.235° 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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