DODECAPOLE 2
NORAD 1510
Payload
LEO
1965-065C
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LEO · NORAD 1510
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
823 km
Apogee
883 km
Inclination
90.1°
Period
102.0 min
Mean Motion
14.11824118 rev/day
TLE Epoch
2026-10-21 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude853 km
Orbital Velocity26,741 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.12
Eccentricity0.0042
Semi-Major Axis7,224 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NRL (United States)
Launch Date
1965-08-13
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-065C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DODECAPOLE 2 is an active satellite operated by NRL (United States), launched on 1965-08-13 from Vandenberg Space Force Base, United States 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 823 km and 883 km with an inclination of 90.1°. It travels at approximately 26,741 km/h (7.43 km/s), completing one full orbit every 102 minutes — that’s roughly 14.12 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks DODECAPOLE 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
DODECAPOLE 2 orbits at an average altitude of 853 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’s average altitude, there are currently 260 active payloads and 2,304 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 90.1°, DODECAPOLE 2 passes over latitudes between 90.1°N and 90.1°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 13,279 active satellites in total, of which 62 share a similar altitude band with DODECAPOLE 2.
❓ Frequently Asked Questions
DODECAPOLE 2 orbits in Low Earth Orbit (LEO) at altitudes between 823 km (perigee) and 883 km (apogee), with an average altitude of approximately 853 km. It completes one orbit every 102 minutes, travelling at approximately 26,741 km/h (16,616 mph).
DODECAPOLE 2 is operated by NRL (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 1510. You can track DODECAPOLE 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DODECAPOLE 2 was launched on 1965-08-13 from Vandenberg Space Force Base, United States, 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 (NORAD ID 1510) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 travels at approximately 26,741 km/h (16,616 mph) — roughly 7.43 km/s. It completes 14.12 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.