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IPERDRONE.0, 60520

Orbit data source: Space-Track

IPERDRONE.0, 60520 is a payload satellite owned by ASI (IT) in SSO that was launched on Fri, 16 Aug 2024 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.

Not visible in the next 10 days
Identifier
60520, 2024-149BE
Orbit
SSO
Country
Flag of ITIT
Related business
Manufacturer
TERRAN/ARGOT
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2024-08-16 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.104 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 IPERDRONE.0
1 60520U 24149BE  26042.62329197  .00048847  00000-0  81091-3 0  9999
2 60520  97.3855 131.1148 0002708 355.8969   4.2261 15.51959002 83354
Epoch: 2026-02-11T14:57Z
TLE epoch observation values (Epoch: 2026-02-11T14:57:32.426Z)
Latitude
0.00001°
Longitude
125.04294°
Altitude
412.307 km
Speed
7.665 km/s
True Right ascension
08h 44m 27s
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
04:39:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
409.767 km
Perigee altitude
406.092 km
Semi-major axis
6,786.066 km
Eccentricity
0.00027
Inclination
97.3855°
RAAN
131.1148°
Arg. of periapsis
355.8969°
True anomaly
4.22839°
Mean anomaly
4.2261°
Eccentric anomaly
4.22724°
Mean motion
3.88254 °/min
Orbital period
92.72 mins
BSTAR
0.00081091
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