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CUBEBUG 2

NORAD 39440 Payload LEO 2013-066AA ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
546 km
Apogee
626 km
Inclination
97.9°
Period
96.4 min
Mean Motion
14.93833268 rev/day
TLE Epoch
2026-06-26 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude586 km
Orbital Velocity27,250 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.94
Eccentricity0.0057
Semi-Major Axis6,957 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Argentinian Ministry of Science, Technology and Productive Innovation/Radio Club Bariloche (Argentina)
Launch Date
2013-11-21
Launch Site
OREN
Int'l Designator
2013-066AA
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CUBEBUG 2 is an active satellite operated by Argentinian Ministry of Science, Technology and Productive Innovation/Radio Club Bariloche (Argentina), launched on 2013-11-21 from OREN on the Dnepr Rideshare 8 launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 546 km and 626 km with an inclination of 97.9°. 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks CUBEBUG 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
CUBEBUG 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 CUBEBUG 2’s average altitude, there are currently 3,034 active payloads and 589 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 17.3% of all active satellites. With an inclination of 97.9°, CUBEBUG 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. Argentina operates approximately 34 active satellites in total, of which 6 share a similar altitude band with CUBEBUG 2.
❓ Frequently Asked Questions
CUBEBUG 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 586 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 96 minutes, travelling at 27,250 km/h.
CUBEBUG 2 is operated by Argentinian Ministry of Science, Technology and Productive Innovation/Radio Club Bariloche (Argentina). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39440. You can track CUBEBUG 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CUBEBUG 2 was launched on 2013-11-21 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 CUBEBUG 2 (NORAD ID 39440) 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.
CUBEBUG 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.