Showing default

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.

Loading next visibility...
Identifier
64552, 2025-135AA
Orbit
SSO
Country
Flag of FIFI / FIN
Related business
Manufacturer
Kuva Space
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2025-06-23 (9 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 HYPERFIELD-1B
1 64552U 25135AA  26083.51346774  .00005043  00000-0  22673-3 0  9999
2 64552  97.4556 199.5067 0001076 137.4814 222.6505 15.21577227 42006
Epoch: 2026-03-24T12:19Z
TLE epoch observation values (Epoch: 2026-03-24T12:19:23.612Z)
Latitude
-0.00007°
Longitude
-167.33172°
Altitude
504.718 km
Speed
7.612 km/s
True Right ascension
13h 18m 01s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
22:54:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.788 km
Perigee altitude
497.309 km
Semi-major axis
6,876.185 km
Eccentricity
0.00011
Inclination
97.4556°
RAAN
199.5067°
Arg. of periapsis
137.4814°
True anomaly
222.64215°
Mean anomaly
222.6505°
Eccentric anomaly
222.64632°
Mean motion
3.80646 °/min
Orbital period
94.58 mins
BSTAR
0.00022673
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|