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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 HYPSO-2
1 60531U 24149BR 26228.14758555 .00001344 00000-0 11570-3 0 9994
2 60531 97.6777 303.5338 0002453 129.1809 230.9632 14.99030705109035Epoch: 2026-08-16T03:32Z
TLE epoch observation values (Epoch: 2026-08-16T03:32:31.391Z)
Latitude
-0.00004°
Longitude
-74.14527°
Altitude
574.018 km
Speed
7.573 km/s
True Right ascension
20h 14m 08s
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
01:21:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.599 km
Perigee altitude
565.192 km
Semi-major axis
6,945.032 km
Eccentricity
0.00025
Inclination
97.6777°
RAAN
303.5338°
Arg. of periapsis
129.1809°
True anomaly
230.94137°
Mean anomaly
230.9632°
Eccentric anomaly
230.95228°
Mean motion
3.75 °/min
Orbital period
96 mins
BSTAR
0.0001157
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-16 16:56:54.949Z | 56.842° ENE | 2026-08-16 16:58:54.949Z | 87.937° E | 15.339° | 2026-08-16 17:00:54.949Z | 121.735° SE |
| 6 mins | 2026-08-16 18:31:54.949Z | 345.679° N | 2026-08-16 18:34:54.949Z | 271.009° WNW | 29.622° | 2026-08-16 18:37:54.949Z | 222.604° SW |
| 6 mins | 2026-08-17 05:18:54.949Z | 181.933° SSW | 2026-08-17 05:20:54.949Z | 239.24° WSW | 42.323° | 2026-08-17 05:24:54.949Z | 341.72° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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