OPS 5644
NORAD 10033
Payload
LEO
1977-044A
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LEO · NORAD 10033
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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
760 km
Apogee
814 km
Inclination
99.1°
Period
100.6 min
Mean Motion
14.31444090 rev/day
TLE Epoch
2026-05-08 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude787 km
Orbital Velocity26,864 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.31
Eccentricity0.0038
Semi-Major Axis7,158 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1977-06-05
Launch Site
Vandenberg SFB, California
Int'l Designator
1977-044A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 5644 is an active satellite operated by United States, launched on 1977-06-05 from Vandenberg SFB, California. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 760 km and 814 km with an inclination of 99.1°. It travels at approximately 26,864 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.31 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks OPS 5644 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OPS 5644 operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
❓ Frequently Asked Questions
OPS 5644 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 787 km altitude. Its 99.1° 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 26,864 km/h.
OPS 5644 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 10033. You can track OPS 5644 in real time on Orbital Radar’s live tracker.
OPS 5644 was launched on 1977-06-05 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: ~25–100 years.
Yes — Orbital Radar tracks OPS 5644 (NORAD ID 10033) 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.
OPS 5644 travels at approximately 26,864 km/h (16,693 mph) — roughly 7.46 km/s. It completes 14.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.