METOP SG-A
NORAD 65159
Payload
LEO
2025-172A
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🛰️ Orbital Parameters
Perigee
820 km
Apogee
821 km
Inclination
98.7°
Period
101.3 min
Mean Motion
14.21509720 rev/day
TLE Epoch
2026-06-16 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude821 km
Orbital Velocity26,802 km/h
Velocity7.44 km/s
Orbital Period101 minutes
Orbits / Day14.22
Eccentricity0.0001
Semi-Major Axis7,192 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
2025-08-13
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2025-172A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
METOP SG-A is an active satellite operated by ESA (European Space Agency), launched on 2025-08-13 from Guiana Space Centre, Kourou. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 820 km and 821 km with an inclination of 98.7°. It travels at approximately 26,802 km/h (7.44 km/s), completing one full orbit every 101 minutes — that’s roughly 14.22 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 ~100–500 years. Orbital Radar tracks METOP SG-A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
METOP SG-A orbits at an average altitude of 821 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 METOP SG-A’s average altitude, there are currently 397 active payloads and 2,272 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, METOP SG-A passes over latitudes between 98.7°N and 98.7°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. ESA (European Space Agency) operates approximately 93 active satellites in total, of which 8 share a similar altitude band with METOP SG-A.
❓ Frequently Asked Questions
METOP SG-A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 821 km altitude. Its 98.7° 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 101 minutes, travelling at 26,802 km/h.
METOP SG-A is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 65159. You can track METOP SG-A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
METOP SG-A was launched on 2025-08-13 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks METOP SG-A (NORAD ID 65159) 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.
METOP SG-A travels at approximately 26,802 km/h (16,654 mph) — roughly 7.44 km/s. It completes 14.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.