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DEIMOS 1

NORAD 35681 Payload LEO 2009-041A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
643 km
Apogee
646 km
Inclination
97.7°
Period
97.6 min
Mean Motion
14.75240356 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude645 km
Orbital Velocity27,136 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.75
Eccentricity0.0002
Semi-Major Axis7,016 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇪🇸 Deimos Imaging/DMC International Imaging (DMCII) (Spain)
Launch Date
2009-07-29
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2009-041A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DEIMOS 1 is an active satellite operated by Deimos Imaging/DMC International Imaging (DMCII) (Spain), launched on 2009-07-29 from Baikonur, Kazakhstan. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 643 km and 646 km with an inclination of 97.7°. It travels at approximately 27,136 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.75 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 ~10–25 years. Orbital Radar tracks DEIMOS 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
DEIMOS 1 orbits at an average altitude of 645 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 DEIMOS 1’s average altitude, there are currently 691 active payloads and 986 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0050. With an inclination of 97.7°, DEIMOS 1 passes over latitudes between 97.7°N and 97.7°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. Spain operates approximately 53 active satellites in total, of which 4 share a similar altitude band with DEIMOS 1.
❓ Frequently Asked Questions
DEIMOS 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 645 km altitude. Its 97.7° 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 27,136 km/h.
DEIMOS 1 is operated by Deimos Imaging/DMC International Imaging (DMCII) (Spain). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 35681. You can track DEIMOS 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DEIMOS 1 was launched on 2009-07-29 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks DEIMOS 1 (NORAD ID 35681) 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.
DEIMOS 1 travels at approximately 27,136 km/h (16,861 mph) — roughly 7.54 km/s. It completes 14.75 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.