THEA
NORAD 43796
Payload
LEO
2018-099AQ
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LEO · NORAD 43796
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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
457 km
Apogee
465 km
Inclination
97.4°
Period
93.8 min
Mean Motion
15.35084249 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude461 km
Orbital Velocity27,498 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.35
Eccentricity0.0006
Semi-Major Axis6,832 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 SpaceQuest, Ltd. (United States)
Launch Date
2018-12-03
Launch Site
Vandenberg SFB, California
Int'l Designator
2018-099AQ
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
THEA is an active satellite operated by SpaceQuest, Ltd. (United States), launched on 2018-12-03 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 457 km and 465 km with an inclination of 97.4°. It travels at approximately 27,498 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.35 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 ~1–3 years. Orbital Radar tracks THEA in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
THEA orbits at an average altitude of 461 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 THEA’s average altitude, there are currently 7,969 active payloads and 173 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 45.7% of all active satellites. With an inclination of 97.4°, THEA passes over latitudes between 97.4°N and 97.4°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 7,439 share a similar altitude band with THEA.
❓ Frequently Asked Questions
THEA is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 461 km altitude. Its 97.4° 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 94 minutes, travelling at 27,498 km/h.
THEA is operated by SpaceQuest, Ltd. (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43796. You can track THEA in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
THEA was launched on 2018-12-03 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks THEA (NORAD ID 43796) 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.
THEA travels at approximately 27,498 km/h (17,086 mph) — roughly 7.64 km/s. It completes 15.35 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.