TERRA
NORAD 25994
Payload
LEO
1999-068A
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LEO · NORAD 25994
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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
688 km
Apogee
691 km
Inclination
98.0°
Period
98.6 min
Mean Motion
14.61104930 rev/day
TLE Epoch
2026-06-19 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude690 km
Orbital Velocity27,049 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.61
Eccentricity0.0002
Semi-Major Axis7,061 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Earth Sciences Enterprise (NASA) (United States)
Launch Date
1999-12-18
Launch Site
Vandenberg SFB, California
Int'l Designator
1999-068A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TERRA is an active satellite operated by Earth Sciences Enterprise (NASA) (United States), launched on 1999-12-18 from Vandenberg SFB, California. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 688 km and 691 km with an inclination of 98.0°. It travels at approximately 27,049 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.61 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 TERRA in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TERRA orbits at an average altitude of 690 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 TERRA’s average altitude, there are currently 307 active payloads and 1,350 tracked debris or rocket body fragments — notable neighbours include AQUA, LANDSAT 9. With an inclination of 98.0°, TERRA passes over latitudes between 98.0°N and 98.0°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 70 share a similar altitude band with TERRA.
❓ Frequently Asked Questions
TERRA is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 690 km altitude. Its 98.0° 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 99 minutes, travelling at 27,049 km/h.
TERRA is operated by Earth Sciences Enterprise (NASA) (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25994. You can track TERRA in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TERRA was launched on 1999-12-18 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 TERRA (NORAD ID 25994) 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.
TERRA travels at approximately 27,049 km/h (16,808 mph) — roughly 7.51 km/s. It completes 14.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.