Showing default

STRIX-4, 60352

Orbit data source: Space-Track

STRIX-4, 60352 is a payload satellite owned by Synspective (JP) in LEO that was launched on Fri, 02 Aug 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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
60352, 2024-137A
Orbit
LEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
Synspective
Mission
Operational Commercial Radar Imaging
Bus & Motor
STRIX, Unknown motor
Mass
150 kg wet, 150 kg dry
Launch date (UTC)
2024-08-02 (1 year ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.052 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 STRIX-4
1 60352U 24137A   25342.93526789  .00030785  00000-0  11988-2 0  9990
2 60352  43.0207 281.6675 0016117 135.1852 225.0304 15.25320179 74899
Epoch: 2025-12-08T22:26Z
TLE epoch observation values (Epoch: 2025-12-08T22:26:47.145Z)
Latitude
-0°
Longitude
-132.9561°
Altitude
497.433 km
Speed
7.613 km/s
True Right ascension
18h 46m 40s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
05:17:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.836 km
Perigee altitude
480.692 km
Semi-major axis
6,869.901 km
Eccentricity
0.00161
Inclination
43.0207°
RAAN
281.6675°
Arg. of periapsis
135.1852°
True anomaly
224.89992°
Mean anomaly
225.0304°
Eccentric anomaly
224.96514°
Mean motion
3.81169 °/min
Orbital period
94.45 mins
BSTAR
0.0011988
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...
Other satellites on launch #137 in the year 2024 (2024-08-02 UTC)

Documentation

Showing up to 5 results
|