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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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: 15 hours ago
TLE from 15 hours ago
0 HYPERFIELD-1B
1 64552U 25135AA 26207.56298961 .00004380 00000-0 19139-3 0 9992
2 64552 97.4704 322.6378 0002208 119.9366 240.2089 15.22624415 60871Epoch: 2026-07-26T13:30Z
TLE epoch observation values (Epoch: 2026-07-26T13:30:42.302Z)
Latitude
-0.00009°
Longitude
175.70243°
Altitude
501.775 km
Speed
7.613 km/s
True Right ascension
21h 30m 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
17:28:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.411 km
Perigee altitude
493.376 km
Semi-major axis
6,873.03 km
Eccentricity
0.00022
Inclination
97.4704°
RAAN
322.6378°
Arg. of periapsis
119.9366°
True anomaly
240.18695°
Mean anomaly
240.2089°
Eccentric anomaly
240.19792°
Mean motion
3.80909 °/min
Orbital period
94.51 mins
BSTAR
0.00019139
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-27 07:00:50.700Z | 112.68° SE | 2026-07-27 07:02:50.700Z | 71.287° E | 20.814° | 2026-07-27 07:04:50.700Z | 28.73° NE |
| 4 mins | 2026-07-27 08:34:50.700Z | 229.465° WSW | 2026-07-27 08:36:50.700Z | 273.02° WNW | 19.321° | 2026-07-27 08:38:50.700Z | 310.093° NW |
| 5 mins | 2026-07-27 20:03:50.700Z | 48.521° ENE | 2026-07-27 20:05:50.700Z | 101.884° ESE | 27.061° | 2026-07-27 20:08:50.700Z | 160.179° S |
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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