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: 1 day ago
TLE from 1 day ago
0 HYPERFIELD-1A
1 60562U 24149CY 26296.97869139 .00006158 00000-0 19938-3 0 9999
2 60562 97.3724 16.5415 0004517 192.7139 167.3990 15.32387007121751Epoch: 2026-10-23T23:29Z
TLE epoch observation values (Epoch: 2026-10-23T23:29:18.936Z)
Latitude
0.00003°
Longitude
-8.17888°
Altitude
474.82 km
Speed
7.627 km/s
True Right ascension
01h 06m 09s
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
02:18:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.732 km
Perigee altitude
462.549 km
Semi-major axis
6,843.778 km
Eccentricity
0.00045
Inclination
97.3724°
RAAN
16.5415°
Arg. of periapsis
192.7139°
True anomaly
167.41029°
Mean anomaly
167.399°
Eccentric anomaly
167.40464°
Mean motion
3.83353 °/min
Orbital period
93.91 mins
BSTAR
0.00019938
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-25 18:21:38.756Z | 9.778° NNE | 2026-10-25 18:24:38.756Z | 269.834° W | 82.287° | 2026-10-25 18:27:38.756Z | 195.809° SSW |
| 4 mins | 2026-10-26 04:55:38.756Z | 116.385° SE | 2026-10-26 04:57:38.756Z | 60.995° ENE | 28.249° | 2026-10-26 04:59:38.756Z | 18.132° NNE |
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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