Showing default

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.

Loading next visibility...
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 (2 years 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: 19 hours ago

TLE from 19 hours ago
0 IPERDRONE.0
1 60520U 24149BE  26257.02053492  .00199150  00000-0  81399-3 0  9998
2 60520  97.3720 355.6772 0004491 250.4169 109.6617 15.85570591116894
Epoch: 2026-09-14T00:29Z
TLE epoch observation values (Epoch: 2026-09-14T00:29:34.217Z)
Latitude
0.00001°
Longitude
-4.7222°
Altitude
318.911 km
Speed
7.716 km/s
True Right ascension
23h 42m 42s
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
12:14:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
314.6 km
Perigee altitude
308.592 km
Semi-major axis
6,689.733 km
Eccentricity
0.00045
Inclination
97.372°
RAAN
355.6772°
Arg. of periapsis
250.4169°
True anomaly
109.71015°
Mean anomaly
109.6617°
Eccentric anomaly
109.68593°
Mean motion
3.96671 °/min
Orbital period
90.76 mins
BSTAR
0.00081399
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
|