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IPERDRONE.0

NORAD 60520 Payload LEO 2024-149BE ● Active
CONNECTING… LEO · NORAD 60520
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
366 km
Apogee
371 km
Inclination
97.4°
Period
91.9 min
Mean Motion
15.66905166 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude369 km
Orbital Velocity27,686 km/h
Velocity7.69 km/s
Orbital Period92 minutes
Orbits / Day15.67
Eccentricity0.0004
Semi-Major Axis6,740 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇮🇹 Italy
Launch Date
2024-08-16
Launch Site
Vandenberg SFB, California
Int'l Designator
2024-149BE
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
IPERDRONE.0 is an active satellite operated by Italy, launched on 2024-08-16 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 366 km and 371 km with an inclination of 97.4°. It travels at approximately 27,686 km/h (7.69 km/s), completing one full orbit every 92 minutes — that’s roughly 15.67 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Orbital Radar tracks IPERDRONE.0 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IPERDRONE.0 orbits at an average altitude of 369 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of IPERDRONE.0’s average altitude, there are currently 1,305 active payloads and 52 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.5% of all active satellites. With an inclination of 97.4°, IPERDRONE.0 passes over latitudes between 97.4°N and 97.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Italy operates approximately 88 active satellites in total, of which 3 share a similar altitude band with IPERDRONE.0.
❓ Frequently Asked Questions
IPERDRONE.0 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 369 km altitude. Its 97.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 92 minutes, travelling at 27,686 km/h.
IPERDRONE.0 is operated by Italy. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 60520. You can track IPERDRONE.0 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IPERDRONE.0 was launched on 2024-08-16 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks IPERDRONE.0 (NORAD ID 60520) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
IPERDRONE.0 travels at approximately 27,686 km/h (17,203 mph) — roughly 7.69 km/s. It completes 15.67 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.