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Home Library Satellite Directory MOS 1A (MOMO 1)

MOS 1A (MOMO 1)

NORAD 17527 Payload LEO 1987-018A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
877 km
Apogee
889 km
Inclination
98.8°
Period
102.6 min
Mean Motion
14.03208618 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude883 km
Orbital Velocity26,686 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.03
Eccentricity0.0008
Semi-Major Axis7,254 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1987-02-19
Launch Site
TNSTA
Int'l Designator
1987-018A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MOS 1A (MOMO 1) is an active satellite operated by Japan, launched on 1987-02-19 from TNSTA. With over 39 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 877 km and 889 km with an inclination of 98.8°. It travels at approximately 26,686 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.03 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 MOS 1A (MOMO 1) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MOS 1A (MOMO 1) orbits at an average altitude of 883 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 MOS 1A (MOMO 1)’s average altitude, there are currently 210 active payloads and 1,591 tracked debris or rocket body fragments. With an inclination of 98.8°, MOS 1A (MOMO 1) passes over latitudes between 98.8°N and 98.8°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. Japan operates approximately 189 active satellites in total, of which 2 share a similar altitude band with MOS 1A (MOMO 1).
❓ Frequently Asked Questions
MOS 1A (MOMO 1) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 883 km altitude. Its 98.8° 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 103 minutes, travelling at 26,686 km/h.
MOS 1A (MOMO 1) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 17527. You can track MOS 1A (MOMO 1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MOS 1A (MOMO 1) was launched on 1987-02-19 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks MOS 1A (MOMO 1) (NORAD ID 17527) 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.
MOS 1A (MOMO 1) travels at approximately 26,686 km/h (16,582 mph) — roughly 7.41 km/s. It completes 14.03 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.