LIDE
NORAD 64869
Payload
LEO
2025-154A
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LEO · NORAD 64869
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
581 km
Apogee
587 km
Inclination
97.7°
Period
96.4 min
Mean Motion
14.94370508 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude584 km
Orbital Velocity27,254 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.94
Eccentricity0.0004
Semi-Major Axis6,955 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇮🇹 Italy
Launch Date
2025-07-23
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-154A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LIDE is an active satellite operated by Italy, launched on 2025-07-23 from Vandenberg SFB, California. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 581 km and 587 km with an inclination of 97.7°. It travels at approximately 27,254 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.94 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 ~3–10 years. Orbital Radar tracks LIDE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
LIDE orbits at an average altitude of 584 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 LIDE’s average altitude, there are currently 3,208 active payloads and 575 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 18.4% of all active satellites. With an inclination of 97.7°, LIDE passes over latitudes between 97.7°N and 97.7°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 37 share a similar altitude band with LIDE.
❓ Frequently Asked Questions
LIDE is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 584 km altitude. Its 97.7° 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 96 minutes, travelling at 27,254 km/h.
LIDE is operated by Italy. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 64869. You can track LIDE in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LIDE was launched on 2025-07-23 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks LIDE (NORAD ID 64869) 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.
LIDE travels at approximately 27,254 km/h (16,935 mph) — roughly 7.57 km/s. It completes 14.94 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.