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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Edit Public Description
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: 6 hours ago
TLE from 6 hours ago
0 HYPSO-2
1 60531U 24149BR 25289.92117532 .00005469 00000-0 48258-3 0 9995
2 60531 97.7076 4.7134 0001907 83.0022 277.1417 14.96799611 63634Epoch: 2025-10-16T22:06Z
TLE epoch observation values (Epoch: 2025-10-16T22:06:29.547Z)
Latitude
0.00002°
Longitude
7.41632°
Altitude
579.678 km
Speed
7.571 km/s
True Right ascension
00h 18m 51s
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
23:18:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.128 km
Perigee altitude
572.477 km
Semi-major axis
6,951.939 km
Eccentricity
0.00019
Inclination
97.7076°
RAAN
4.7134°
Arg. of periapsis
83.0022°
True anomaly
277.12002°
Mean anomaly
277.1417°
Eccentric anomaly
277.13086°
Mean motion
3.74442 °/min
Orbital period
96.14 mins
BSTAR
0.00048258
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-17 04:39:52.020Z | 136.274° SSE | 2025-10-17 04:42:52.020Z | 65.063° ENE | 32.968° | 2025-10-17 04:45:52.020Z | 6.293° NNE |
| 6 mins | 2025-10-17 17:56:52.020Z | 16.739° NNE | 2025-10-17 17:58:52.020Z | 64.038° ENE | 44.538° | 2025-10-17 18:02:52.020Z | 190.327° SSW |
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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