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: 7 hours ago
TLE from 7 hours ago
0 HYPERFIELD-1B
1 64552U 25135AA 26260.26284443 .00004181 00000-0 18100-3 0 9994
2 64552 97.4751 15.0538 0001419 54.9510 305.1860 15.22971334 68899Epoch: 2026-09-17T06:18Z
TLE epoch observation values (Epoch: 2026-09-17T06:18:29.758Z)
Latitude
0.00001°
Longitude
-75.77279°
Altitude
499.414 km
Speed
7.615 km/s
True Right ascension
01h 00m 12s
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
06:02:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.824 km
Perigee altitude
492.874 km
Semi-major axis
6,871.986 km
Eccentricity
0.00014
Inclination
97.4751°
RAAN
15.0538°
Arg. of periapsis
54.951°
True anomaly
305.17271°
Mean anomaly
305.186°
Eccentric anomaly
305.17935°
Mean motion
3.80995 °/min
Orbital period
94.49 mins
BSTAR
0.000181
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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 | 2026-09-17 21:04:37.660Z | 341.149° N | 2026-09-17 21:06:37.660Z | 275.134° WNW | 39.236° | 2026-09-17 21:09:37.660Z | 217.664° SW |
| 5 mins | 2026-09-18 07:40:37.660Z | 156.27° SSE | 2026-09-18 07:42:37.660Z | 113.313° SE | 65.601° | 2026-09-18 07:45:37.660Z | 354.743° N |
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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