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ASAP-S

NORAD 38013 Payload LEO 2011-076G ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
485 km
Apogee
496 km
Inclination
98.0°
Period
94.4 min
Mean Motion
15.25072717 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude491 km
Orbital Velocity27,439 km/h
Velocity7.62 km/s
Orbital Period94 minutes
Orbits / Day15.25
Eccentricity0.0008
Semi-Major Axis6,862 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
2011-12-17
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2011-076G
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASAP-S is an active satellite operated by France, launched on 2011-12-17 from Guiana Space Centre, Kourou. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 485 km and 496 km with an inclination of 98.0°. It travels at approximately 27,439 km/h (7.62 km/s), completing one full orbit every 94 minutes — that’s roughly 15.25 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 ASAP-S in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ASAP-S orbits at an average altitude of 491 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 ASAP-S’s average altitude, there are currently 9,165 active payloads and 232 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 52.6% of all active satellites. With an inclination of 98.0°, ASAP-S 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. France operates approximately 115 active satellites in total, of which 22 share a similar altitude band with ASAP-S.
❓ Frequently Asked Questions
ASAP-S is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 491 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 94 minutes, travelling at 27,439 km/h.
ASAP-S is operated by France. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 38013. You can track ASAP-S in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ASAP-S was launched on 2011-12-17 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks ASAP-S (NORAD ID 38013) 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.
ASAP-S travels at approximately 27,439 km/h (17,050 mph) — roughly 7.62 km/s. It completes 15.25 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.