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OPS 5390

NORAD 11389 Payload LEO 1979-050A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
786 km
Apogee
802 km
Inclination
98.6°
Period
100.8 min
Mean Motion
14.29331120 rev/day
TLE Epoch
2026-05-08 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude794 km
Orbital Velocity26,851 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.29
Eccentricity0.0011
Semi-Major Axis7,165 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1979-06-06
Launch Site
Vandenberg SFB, California
Int'l Designator
1979-050A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 5390 is an active satellite operated by United States, launched on 1979-06-06 from Vandenberg SFB, California. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 786 km and 802 km with an inclination of 98.6°. It travels at approximately 26,851 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.29 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 5390 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 5390 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 5390 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 794 km altitude. Its 98.6° 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 26,851 km/h.
OPS 5390 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 11389. You can track OPS 5390 in real time on Orbital Radar’s live tracker.
OPS 5390 was launched on 1979-06-06 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 5390 (NORAD ID 11389) 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 5390 travels at approximately 26,851 km/h (16,685 mph) — roughly 7.46 km/s. It completes 14.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
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