DMC 2
NORAD 35683
Payload
LEO
2009-041C
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LEO · NORAD 35683
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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
641 km
Apogee
643 km
Inclination
97.9°
Period
97.6 min
Mean Motion
14.76039386 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude642 km
Orbital Velocity27,141 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.76
Eccentricity0.0001
Semi-Major Axis7,013 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇬🇧 UK/DMC International Imaging (DMCII) (United Kingdom)
Launch Date
2009-07-29
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2009-041C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DMC 2 is an active satellite operated by UK/DMC International Imaging (DMCII) (United Kingdom), 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 641 km and 643 km with an inclination of 97.9°. It travels at approximately 27,141 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.76 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 DMC 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
DMC 2 orbits at an average altitude of 642 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 DMC 2’s average altitude, there are currently 726 active payloads and 950 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0050. With an inclination of 97.9°, DMC 2 passes over latitudes between 97.9°N and 97.9°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. United Kingdom operates approximately 720 active satellites in total, of which 15 share a similar altitude band with DMC 2.
❓ Frequently Asked Questions
DMC 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 642 km altitude. Its 97.9° 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 27,141 km/h.
DMC 2 is operated by UK/DMC International Imaging (DMCII) (United Kingdom). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 35683. You can track DMC 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DMC 2 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 DMC 2 (NORAD ID 35683) 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.
DMC 2 travels at approximately 27,141 km/h (16,864 mph) — roughly 7.54 km/s. It completes 14.76 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.