Skip to content
Home Library Satellite Directory SPOT 2

SPOT 2

NORAD 20436 Payload LEO 1990-005A ● Active
CONNECTING… LEO · NORAD 20436
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
557 km
Apogee
740 km
Inclination
98.7°
Period
97.7 min
Mean Motion
14.73907131 rev/day
TLE Epoch
2026-06-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude649 km
Orbital Velocity27,128 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.74
Eccentricity0.0130
Semi-Major Axis7,020 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇫🇷 CNES / Airbus (France)
Launch Date
1990-01-22
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1990-005A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SPOT 2 is an active satellite operated by CNES / Airbus (France), launched on 1990-01-22 from Guiana Space Centre, Kourou. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 557 km and 740 km with an inclination of 98.7°. It travels at approximately 27,128 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.74 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 ~10–25 years. Orbital Radar tracks SPOT 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SPOT 2 orbits at an average altitude of 649 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 SPOT 2’s average altitude, there are currently 690 active payloads and 1,026 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA. With an inclination of 98.7°, SPOT 2 passes over latitudes between 98.7°N and 98.7°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 114 active satellites in total, of which 44 share a similar altitude band with SPOT 2.
❓ Frequently Asked Questions
SPOT 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 649 km altitude. Its 98.7° 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 98 minutes, travelling at 27,128 km/h.
SPOT 2 is operated by CNES / Airbus (France). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20436. You can track SPOT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SPOT 2 was launched on 1990-01-22 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks SPOT 2 (NORAD ID 20436) 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.
SPOT 2 travels at approximately 27,128 km/h (16,857 mph) — roughly 7.54 km/s. It completes 14.74 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.