HYPERFIELD-1B, 64552
Orbit data source: Space-Track
HYPERFIELD-1B, 64552 is a payload satellite owned by Kuva Space (FI) in SSO that was launched on Mon, 23 Jun 2025 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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64552 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-1B
1 64552U 25135AA 25269.29937866 .00009672 00000-0 46521-3 0 9997
2 64552 97.4480 22.3597 0002139 113.2309 246.9151 15.18996770 14778Epoch: 2025-09-26T07:11Z
TLE epoch observation values (Epoch: 2025-09-26T07:11:06.316Z)
Latitude
0.00001°
Longitude
-90.76476°
Altitude
512.537 km
Speed
7.607 km/s
True Right ascension
01h 29m 26s
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
17:06:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.313 km
Perigee altitude
504.368 km
Semi-major axis
6,883.977 km
Eccentricity
0.00021
Inclination
97.448°
RAAN
22.3597°
Arg. of periapsis
113.2309°
True anomaly
246.89255°
Mean anomaly
246.9151°
Eccentric anomaly
246.90383°
Mean motion
3.8 °/min
Orbital period
94.74 mins
BSTAR
0.00046521
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-1B 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 | 2025-09-27 07:02:24.139Z | 126.677° SE | 2025-09-27 07:05:24.139Z | 62.352° ENE | 24.816° | 2025-09-27 07:07:24.139Z | 20.437° NNE |
| 5 mins | 2025-09-27 20:07:24.139Z | 33.967° NE | 2025-09-27 20:09:24.139Z | 78.098° E | 32.69° | 2025-09-27 20:12:24.139Z | 164.636° 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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