DEIMOS 2
NORAD 40013
Payload
LEO
2014-033D
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LEO · NORAD 40013
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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
585 km
Apogee
587 km
Inclination
97.6°
Period
96.4 min
Mean Motion
14.93730700 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude586 km
Orbital Velocity27,250 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.94
Eccentricity0.0001
Semi-Major Axis6,957 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇪🇸 Deimos Imaging/DMC International Imaging (DMCII) (Spain)
Launch Date
2014-06-19
Launch Site
OREN
Int'l Designator
2014-033D
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DEIMOS 2 is an active satellite operated by Deimos Imaging/DMC International Imaging (DMCII) (Spain), launched on 2014-06-19 from OREN. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 585 km and 587 km with an inclination of 97.6°. It travels at approximately 27,250 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.94 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 ~3–10 years. Orbital Radar tracks DEIMOS 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
DEIMOS 2 orbits at an average altitude of 586 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 2’s average altitude, there are currently 3,199 active payloads and 585 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 18.3% of all active satellites. With an inclination of 97.6°, DEIMOS 2 passes over latitudes between 97.6°N and 97.6°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 11 share a similar altitude band with DEIMOS 2.
❓ Frequently Asked Questions
DEIMOS 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 586 km altitude. Its 97.6° 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 96 minutes, travelling at 27,250 km/h.
DEIMOS 2 is operated by Deimos Imaging/DMC International Imaging (DMCII) (Spain). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40013. You can track DEIMOS 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DEIMOS 2 was launched on 2014-06-19 from OREN. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks DEIMOS 2 (NORAD ID 40013) 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 2 travels at approximately 27,250 km/h (16,932 mph) — roughly 7.57 km/s. It completes 14.94 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.