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: 1 day ago
TLE from 1 day ago
0 HYPERFIELD-1B
1 64552U 25135AA 25312.83158957 .00008526 00000-0 40199-3 0 9994
2 64552 97.4525 65.3045 0001450 56.0395 304.0978 15.19727617 21388Epoch: 2025-11-08T19:57Z
TLE epoch observation values (Epoch: 2025-11-08T19:57:29.338Z)
Latitude
0°
Longitude
77.6767°
Altitude
509.192 km
Speed
7.61 km/s
True Right ascension
04h 21m 13s
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
18:22:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.629 km
Perigee altitude
502.633 km
Semi-major axis
6,881.768 km
Eccentricity
0.00015
Inclination
97.4525°
RAAN
65.3045°
Arg. of periapsis
56.0395°
True anomaly
304.08404°
Mean anomaly
304.0978°
Eccentric anomaly
304.09092°
Mean motion
3.80183 °/min
Orbital period
94.69 mins
BSTAR
0.00040199
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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 | 2025-11-10 06:52:02.686Z | 117.556° SE | 2025-11-10 06:55:02.686Z | 60.587° ENE | 19.481° | 2025-11-10 06:57:02.686Z | 24.418° NE |
| 4 mins | 2025-11-10 08:27:02.686Z | 232.449° WSW | 2025-11-10 08:28:02.686Z | 254.709° W | 20.859° | 2025-11-10 08:31:02.686Z | 314.717° NW |
| 5 mins | 2025-11-10 19:57:02.686Z | 49.187° ENE | 2025-11-10 19:59:02.686Z | 100.782° ESE | 26.608° | 2025-11-10 20:02:02.686Z | 158.762° 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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