DODECAPOLE 2 DEB
NORAD 41734
Debris
LEO
1965-065U
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LEO · NORAD 41734
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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
795 km
Apogee
843 km
Inclination
90.0°
Period
101.3 min
Mean Motion
14.21805774 rev/day
TLE Epoch
2026-06-20 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude819 km
Orbital Velocity26,804 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.22
Eccentricity0.0033
Semi-Major Axis7,190 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-08-13
Launch Site
Vandenberg SFB, California
Int'l Designator
1965-065U
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DODECAPOLE 2 DEB is a tracked piece of space debris attributed to United States, launched on 1965-08-13 from Vandenberg SFB, California on the Dodecapole 2 launch. After more than 61 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 795 km and 843 km with an inclination of 90.0°. It travels at approximately 26,804 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.22 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, DODECAPOLE 2 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
DODECAPOLE 2 DEB orbits at an average altitude of 819 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of DODECAPOLE 2 DEB’s average altitude, there are currently 396 active payloads and 2,270 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 90.0°, DODECAPOLE 2 DEB passes over latitudes between 90.0°N and 90.0°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 States operates approximately 12,358 active satellites in total, of which 133 share a similar altitude band with DODECAPOLE 2 DEB.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
DODECAPOLE 2 DEB orbits in Low Earth Orbit (LEO) at altitudes between 795 km (perigee) and 843 km (apogee), with an average altitude of approximately 819 km. It completes one orbit every 101 minutes, travelling at approximately 26,804 km/h (16,656 mph).
DODECAPOLE 2 DEB (NORAD ID 41734) is a piece of tracked orbital debris attributed to United States. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
DODECAPOLE 2 DEB was launched on 1965-08-13 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks DODECAPOLE 2 DEB (NORAD ID 41734) 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.
DODECAPOLE 2 DEB travels at approximately 26,804 km/h (16,656 mph) — roughly 7.45 km/s. It completes 14.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.45 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like DODECAPOLE 2 DEB. Read more about debris statistics and the Kessler syndrome.