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: 11 hours ago
TLE from 11 hours ago
0 HYPSO-2
1 60531U 24149BR 26175.94504404 .00002377 00000-0 20196-3 0 9996
2 60531 97.6810 252.0919 0000682 126.4168 233.7118 14.98820099101210Epoch: 2026-06-24T22:40Z
TLE epoch observation values (Epoch: 2026-06-24T22:40:51.805Z)
Latitude
0.00002°
Longitude
-1.21894°
Altitude
573.875 km
Speed
7.574 km/s
True Right ascension
16h 48m 22s
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
20:56:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.02 km
Perigee altitude
567.073 km
Semi-major axis
6,945.684 km
Eccentricity
0.00007
Inclination
97.681°
RAAN
252.0919°
Arg. of periapsis
126.4168°
True anomaly
233.7055°
Mean anomaly
233.7118°
Eccentric anomaly
233.70865°
Mean motion
3.74948 °/min
Orbital period
96.01 mins
BSTAR
0.00020196
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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 | 2026-06-25 16:54:03.259Z | 61.007° ENE | 2026-06-25 16:56:03.259Z | 92.265° ESE | 14.323° | 2026-06-25 16:58:03.259Z | 123.63° SE |
| 6 mins | 2026-06-25 18:29:03.259Z | 345.472° N | 2026-06-25 18:31:03.259Z | 299.352° NW | 31.979° | 2026-06-25 18:35:03.259Z | 218.871° SW |
| 6 mins | 2026-06-26 05:16:03.259Z | 178.345° S | 2026-06-26 05:18:03.259Z | 252.189° W | 43.735° | 2026-06-26 05:22:03.259Z | 343.697° 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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