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GEOEYE 1

NORAD 33331 Payload LEO 2008-042A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
674 km
Apogee
682 km
Inclination
98.1°
Period
98.3 min
Mean Motion
14.64727786 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude678 km
Orbital Velocity27,071 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.65
Eccentricity0.0006
Semi-Major Axis7,049 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 DigitalGlobe Corporation (United States)
Launch Date
2008-09-06
Launch Site
Vandenberg SFB, California
Int'l Designator
2008-042A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GEOEYE 1 is an active satellite operated by DigitalGlobe Corporation (United States), launched on 2008-09-06 from Vandenberg SFB, California. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 674 km and 682 km with an inclination of 98.1°. It travels at approximately 27,071 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.65 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 ~10–25 years. Orbital Radar tracks GEOEYE 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
GEOEYE 1 orbits at an average altitude of 678 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 GEOEYE 1’s average altitude, there are currently 524 active payloads and 1,255 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.1°, GEOEYE 1 passes over latitudes between 98.1°N and 98.1°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. United States operates approximately 12,360 active satellites in total, of which 267 share a similar altitude band with GEOEYE 1.
❓ Frequently Asked Questions
GEOEYE 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 678 km altitude. Its 98.1° 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 98 minutes, travelling at 27,071 km/h.
GEOEYE 1 is operated by DigitalGlobe Corporation (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33331. You can track GEOEYE 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GEOEYE 1 was launched on 2008-09-06 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks GEOEYE 1 (NORAD ID 33331) 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.
GEOEYE 1 travels at approximately 27,071 km/h (16,821 mph) — roughly 7.52 km/s. It completes 14.65 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.