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: 9 hours ago
TLE from 9 hours ago
0 HYPERFIELD-1A
1 60562U 24149CY 26221.73310053 .00003928 00000-0 13116-3 0 9991
2 60562 97.3778 301.6389 0006740 113.9819 246.2129 15.31613313110231Epoch: 2026-08-09T17:35Z
TLE epoch observation values (Epoch: 2026-08-09T17:35:39.885Z)
Latitude
-0.00002°
Longitude
79.49686°
Altitude
475.97 km
Speed
7.627 km/s
True Right ascension
20h 06m 33s
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
16:33:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.562 km
Perigee altitude
463.333 km
Semi-major axis
6,846.085 km
Eccentricity
0.00067
Inclination
97.3778°
RAAN
301.6389°
Arg. of periapsis
113.9819°
True anomaly
246.14225°
Mean anomaly
246.2129°
Eccentric anomaly
246.17757°
Mean motion
3.8316 °/min
Orbital period
93.96 mins
BSTAR
0.00013116
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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 | 2026-08-10 04:42:52.517Z | 119.674° SE | 2026-08-10 04:44:52.517Z | 82.546° E | 20.24° | 2026-08-10 04:47:52.517Z | 20.192° NNE |
| 4 mins | 2026-08-10 17:41:52.517Z | 51.989° ENE | 2026-08-10 17:43:52.517Z | 106.151° ESE | 24.604° | 2026-08-10 17:45:52.517Z | 150.016° 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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