HYPERFIELD-1A, 60562
Orbit data source: Space-Track
HYPERFIELD-1A, 60562 is a payload satellite owned by Kuva Space (FI) 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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60562 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated business
Manufacturer
Kuva Space
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.092 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 HYPERFIELD-1A
1 60562U 24149CY 26129.19037918 .00005324 00000-0 18272-3 0 9994
2 60562 97.3796 209.5637 0006814 91.0468 269.1554 15.30554557 96075Epoch: 2026-05-09T04:34Z
TLE epoch observation values (Epoch: 2026-05-09T04:34:08.761Z)
Latitude
0.00003°
Longitude
-85.98418°
Altitude
477.334 km
Speed
7.627 km/s
True Right ascension
13h 58m 15s
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
03:48:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.774 km
Perigee altitude
466.44 km
Semi-major axis
6,849.244 km
Eccentricity
0.00068
Inclination
97.3796°
RAAN
209.5637°
Arg. of periapsis
91.0468°
True anomaly
269.07733°
Mean anomaly
269.1554°
Eccentric anomaly
269.11636°
Mean motion
3.82895 °/min
Orbital period
94.02 mins
BSTAR
0.00018272
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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.HYPERFIELD-1A 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 | 2026-05-10 05:49:11.214Z | 209.626° SW | 2026-05-10 05:51:11.214Z | 282.113° WNW | 30.739° | 2026-05-10 05:53:11.214Z | 325.615° NNW |
| 4 mins | 2026-05-10 18:48:11.214Z | 328.697° NNW | 2026-05-10 18:49:11.214Z | 302.289° NW | 25.522° | 2026-05-10 18:52:11.214Z | 230.539° WSW |
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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