HERMES-2
NORAD 63243
Payload
LEO
2025-052AK
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LEO · NORAD 63243
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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
471 km
Apogee
480 km
Inclination
97.4°
Period
94.1 min
Mean Motion
15.30073636 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude476 km
Orbital Velocity27,469 km/h
Velocity7.63 km/s
Orbital Period94 minutes
Orbits / Day15.30
Eccentricity0.0007
Semi-Major Axis6,847 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇮🇹 Italy
Launch Date
2025-03-15
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-052AK
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
HERMES-2 is an active satellite operated by Italy, launched on 2025-03-15 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 471 km and 480 km with an inclination of 97.4°. It travels at approximately 27,469 km/h (7.63 km/s), completing one full orbit every 94 minutes — that’s roughly 15.30 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 ~1–3 years. Orbital Radar tracks HERMES-2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HERMES-2 orbits at an average altitude of 476 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 HERMES-2’s average altitude, there are currently 7,964 active payloads and 204 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 45.7% of all active satellites. With an inclination of 97.4°, HERMES-2 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 36 share a similar altitude band with HERMES-2.
❓ Frequently Asked Questions
HERMES-2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 476 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 94 minutes, travelling at 27,469 km/h.
HERMES-2 is operated by Italy. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 63243. You can track HERMES-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HERMES-2 was launched on 2025-03-15 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks HERMES-2 (NORAD ID 63243) 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.
HERMES-2 travels at approximately 27,469 km/h (17,068 mph) — roughly 7.63 km/s. It completes 15.30 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.