Skip to content
Home Library Satellite Directory OSCAR 8

OSCAR 8

NORAD 10703 Payload LEO 1978-026B ● Active
CONNECTING… LEO · NORAD 10703
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
888 km
Apogee
901 km
Inclination
99.3°
Period
102.9 min
Mean Motion
13.99782754 rev/day
TLE Epoch
2026-05-08 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude895 km
Orbital Velocity26,665 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.00
Eccentricity0.0009
Semi-Major Axis7,266 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1978-03-05
Launch Site
Vandenberg SFB, California
Int'l Designator
1978-026B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OSCAR 8 is an active satellite operated by United States, launched on 1978-03-05 from Vandenberg SFB, California. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 888 km and 901 km with an inclination of 99.3°. It travels at approximately 26,665 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.00 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 OSCAR 8 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OSCAR 8 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
OSCAR 8 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 895 km altitude. Its 99.3° 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 26,665 km/h.
OSCAR 8 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 10703. You can track OSCAR 8 in real time on Orbital Radar’s live tracker.
OSCAR 8 was launched on 1978-03-05 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: ~100–500 years.
Yes — Orbital Radar tracks OSCAR 8 (NORAD ID 10703) 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.
OSCAR 8 travels at approximately 26,665 km/h (16,569 mph) — roughly 7.41 km/s. It completes 14.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
🪐 Support Us