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EO 1

NORAD 26619 Payload LEO 2000-075A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
656 km
Apogee
671 km
Inclination
98.1°
Period
98.0 min
Mean Motion
14.69201163 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude664 km
Orbital Velocity27,099 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.69
Eccentricity0.0011
Semi-Major Axis7,035 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2000-11-21
Launch Site
Vandenberg SFB, California
Int'l Designator
2000-075A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EO 1 is an active satellite operated by United States, launched on 2000-11-21 from Vandenberg SFB, California. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 656 km and 671 km with an inclination of 98.1°. It travels at approximately 27,099 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.69 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 ~10–25 years. Orbital Radar tracks EO 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
EO 1 orbits at an average altitude of 664 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 EO 1’s average altitude, there are currently 644 active payloads and 1,129 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.1°, EO 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 280 share a similar altitude band with EO 1.
❓ Frequently Asked Questions
EO 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 664 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 27,099 km/h.
EO 1 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26619. You can track EO 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EO 1 was launched on 2000-11-21 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 EO 1 (NORAD ID 26619) 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.
EO 1 travels at approximately 27,099 km/h (16,839 mph) — roughly 7.53 km/s. It completes 14.69 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.