SUNSAT
NORAD 25636
Payload
LEO
1999-008C
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LEO · NORAD 25636
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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
637 km
Apogee
837 km
Inclination
96.5°
Period
99.5 min
Mean Motion
14.46473022 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude737 km
Orbital Velocity26,959 km/h
Velocity7.49 km/s
Orbital Period100 minutes
Orbits / Day14.46
Eccentricity0.0141
Semi-Major Axis7,108 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
South Africa
Launch Date
1999-02-23
Launch Site
Vandenberg SFB, California
Int'l Designator
1999-008C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SUNSAT is an active satellite operated by South Africa, launched on 1999-02-23 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 637 km and 837 km with an inclination of 96.5°. It travels at approximately 26,959 km/h (7.49 km/s), completing one full orbit every 100 minutes — that’s roughly 14.46 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 ~25–100 years. Orbital Radar tracks SUNSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SUNSAT orbits at an average altitude of 737 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 SUNSAT’s average altitude, there are currently 364 active payloads and 1,876 tracked debris or rocket body fragments — notable neighbours include TERRA, LANDSAT 9. With an inclination of 96.5°, SUNSAT passes over latitudes between 96.5°N and 96.5°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. South Africa operates approximately 3 active satellites in total.
❓ Frequently Asked Questions
SUNSAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 737 km altitude. Its 96.5° 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 100 minutes, travelling at 26,959 km/h.
SUNSAT is operated by South Africa. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25636. You can track SUNSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SUNSAT was launched on 1999-02-23 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks SUNSAT (NORAD ID 25636) 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.
SUNSAT travels at approximately 26,959 km/h (16,751 mph) — roughly 7.49 km/s. It completes 14.46 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.