MAQSAT H
NORAD 25023
Payload
MEO
1997-066A
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MEO · NORAD 25023
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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
570 km
Apogee
26330 km
Inclination
7.9°
Period
463.1 min
Mean Motion
3.10947707 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude13,450 km
Orbital Velocity16,144 km/h
Velocity4.48 km/s
Orbital Period7 hours 43 minutes
Orbits / Day3.11
Eccentricity0.6498
Semi-Major Axis19,821 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
1997-10-30
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1997-066A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MAQSAT H is an active satellite operated by ESA (European Space Agency), launched on 1997-10-30 from Guiana Space Centre, Kourou. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 570 km and 26,330 km with an inclination of 7.9°. It travels at approximately 16,144 km/h (4.48 km/s), completing one full orbit every 7 hours 43 minutes — that’s roughly 3.11 orbits per day. Its orbital eccentricity of 0.6498 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MAQSAT H in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MAQSAT H orbits at an average altitude of 13,450 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of MAQSAT H’s average altitude, there are currently 2 active payloads and 6 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 7.9°, MAQSAT H passes over latitudes between 7.9°N and 7.9°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. ESA (European Space Agency) operates approximately 93 active satellites in total.
❓ Frequently Asked Questions
MAQSAT H orbits in Medium Earth Orbit (MEO) at altitudes between 570 km (perigee) and 26,330 km (apogee), with an average altitude of approximately 13,450 km. It completes one orbit every 7 hours 43 minutes, travelling at approximately 16,144 km/h (10,031 mph).
MAQSAT H is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25023. You can track MAQSAT H in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MAQSAT H was launched on 1997-10-30 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks MAQSAT H (NORAD ID 25023) 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.
MAQSAT H travels at approximately 16,144 km/h (10,031 mph) — roughly 4.48 km/s. It completes 3.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 6 sunrises and sunsets every 24 hours.