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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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: 17 hours ago
TLE from 17 hours ago
0 HYPERFIELD-1A
1 60562U 24149CY 25289.46574238 .00008820 00000-0 33588-3 0 9992
2 60562 97.4039 6.2254 0007148 95.3629 264.8425 15.26943643 64796Epoch: 2025-10-16T11:10Z
TLE epoch observation values (Epoch: 2025-10-16T11:10:40.141Z)
Latitude
-0.00009°
Longitude
173.33309°
Altitude
488.5 km
Speed
7.621 km/s
True Right ascension
00h 24m 54s
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
23:17:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.815 km
Perigee altitude
477.008 km
Semi-major axis
6,860.049 km
Eccentricity
0.00071
Inclination
97.4039°
RAAN
6.2254°
Arg. of periapsis
95.3629°
True anomaly
264.76093°
Mean anomaly
264.8425°
Eccentric anomaly
264.80171°
Mean motion
3.8199 °/min
Orbital period
94.24 mins
BSTAR
0.00033588
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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 | 2025-10-17 04:37:20.063Z | 122.775° SE | 2025-10-17 04:39:20.063Z | 83.852° E | 22.792° | 2025-10-17 04:42:20.063Z | 18.018° NNE |
| 5 mins | 2025-10-17 17:38:20.063Z | 41.839° NE | 2025-10-17 17:40:20.063Z | 94.258° ESE | 29.4° | 2025-10-17 17:43:20.063Z | 162.387° S |
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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