SATMAR
NORAD 64551
Payload
LEO
2025-135Z
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LEO · NORAD 64551
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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
487 km
Apogee
488 km
Inclination
97.5°
Period
94.4 min
Mean Motion
15.26141829 rev/day
TLE Epoch
2026-09-18 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude488 km
Orbital Velocity27,445 km/h
Velocity7.62 km/s
Orbital Period94 minutes
Orbits / Day15.26
Eccentricity0.0001
Semi-Major Axis6,859 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇪🇸 ALENSP (Spain)
Launch Date
2025-06-23
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2025-135Z
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SATMAR is an active satellite operated by ALENSP (Spain), launched on 2025-06-23 from Vandenberg Space Force Base, United States on the Transporter-14 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 487 km and 488 km with an inclination of 97.5°. It travels at approximately 27,445 km/h (7.62 km/s), completing one full orbit every 94 minutes — that’s roughly 15.26 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 SATMAR in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SATMAR orbits at an average altitude of 488 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 SATMAR’s average altitude, there are currently 10,213 active payloads and 207 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 54.6% of all active satellites. With an inclination of 97.5°, SATMAR passes over latitudes between 97.5°N and 97.5°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. Spain operates approximately 56 active satellites in total, of which 19 share a similar altitude band with SATMAR.
❓ Frequently Asked Questions
SATMAR is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 488 km altitude. Its 97.5° 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 27,445 km/h.
SATMAR is operated by ALENSP (Spain). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 64551. You can track SATMAR in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SATMAR was launched on 2025-06-23 from Vandenberg Space Force Base, United States, 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 SATMAR (NORAD ID 64551) 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.
SATMAR travels at approximately 27,445 km/h (17,053 mph) — roughly 7.62 km/s. It completes 15.26 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.