HYPSO-2, 60531
Orbit data source: Space-Track
HYPSO-2, 60531 is a payload satellite owned by NTNU (NO) in SSO that was launched on Fri, 16 Aug 2024 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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60531 intel report (Beta)
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Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
NanoAvionics
Mission
Operational Civil 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: 18 hours ago
TLE from 18 hours ago
0 HYPSO-2
1 60531U 24149BR 26083.93535185 .00002718 00000-0 23308-3 0 9990
2 60531 97.6844 161.4373 0000554 176.6629 183.4597 14.98343515 87433Epoch: 2026-03-24T22:26Z
TLE epoch observation values (Epoch: 2026-03-24T22:26:54.399Z)
Latitude
-0.00008°
Longitude
2.30478°
Altitude
575.451 km
Speed
7.573 km/s
True Right ascension
10h 45m 44s
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
21:57:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.406 km
Perigee altitude
568.636 km
Semi-major axis
6,947.158 km
Eccentricity
0.00006
Inclination
97.6844°
RAAN
161.4373°
Arg. of periapsis
176.6629°
True anomaly
183.45932°
Mean anomaly
183.4597°
Eccentric anomaly
183.45951°
Mean motion
3.74828 °/min
Orbital period
96.04 mins
BSTAR
0.00023308
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-25 18:14:08.423Z | 3.57° NNE | 2026-03-25 18:18:08.423Z | 273.279° WNW | 40.065° | 2026-03-25 18:21:08.423Z | 209.327° SW |
| 6 mins | 2026-03-26 05:02:08.423Z | 159.73° S | 2026-03-26 05:05:08.423Z | 33.747° NE | 43.617° | 2026-03-26 05:08:08.423Z | 351.773° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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