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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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 HYPERFIELD-1A
1 60562U 24149CY 25353.65939848 .00005120 00000-0 18879-3 0 9993
2 60562 97.3987 69.9322 0004510 214.4613 145.6334 15.28239512 74595Epoch: 2025-12-19T15:49Z
TLE epoch observation values (Epoch: 2025-12-19T15:49:32.028Z)
Latitude
-0.00011°
Longitude
104.05139°
Altitude
486.731 km
Speed
7.62 km/s
True Right ascension
04h 39m 43s
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
21:34:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.122 km
Perigee altitude
474.937 km
Semi-major axis
6,856.167 km
Eccentricity
0.00045
Inclination
97.3987°
RAAN
69.9322°
Arg. of periapsis
214.4613°
True anomaly
145.66256°
Mean anomaly
145.6334°
Eccentric anomaly
145.64798°
Mean motion
3.82315 °/min
Orbital period
94.16 mins
BSTAR
0.00018879
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-20 04:32:43.083Z | 115.808° SE | 2025-12-20 04:34:43.083Z | 77.536° E | 19.974° | 2025-12-20 04:37:43.083Z | 19.561° NNE |
| 4 mins | 2025-12-20 06:06:43.083Z | 230.609° WSW | 2025-12-20 06:08:43.083Z | 275.444° WNW | 19.009° | 2025-12-20 06:10:43.083Z | 311.752° NW |
| 4 mins | 2025-12-20 17:33:43.083Z | 61.068° ENE | 2025-12-20 17:34:43.083Z | 88.024° E | 24.681° | 2025-12-20 17:37:43.083Z | 154.197° SSE |
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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