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TERRA

NORAD 25994 Payload LEO 1999-068A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
688 km
Apogee
692 km
Inclination
98.0°
Period
98.6 min
Mean Motion
14.61023383 rev/day
TLE Epoch
2026-03-17 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude690 km
Orbital Velocity27,048 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.61
Eccentricity0.0003
Semi-Major Axis7,061 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 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)
🔗 Constellation / Groups
resourcevisualtdrss
📖 About This Object
TERRA is an active satellite operated by 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 692 km with an inclination of 98.0°. It travels at approximately 27,048 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. It is part of the Resource constellation group. 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 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
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 27,048 km/h.
TERRA is operated by 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.
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.
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.
TERRA travels at approximately 27,048 km/h (16,807 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.
TERRA is a member of the Resource constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Resource satellites on Orbital Radar’s live tracker.