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OV2-1

NORAD 1641 Payload LEO 1965-082C ● Active
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🛰️ Orbital Parameters
Perigee
696 km
Apogee
723 km
Inclination
32.3°
Period
99.0 min
Mean Motion
14.54858115 rev/day
TLE Epoch
2026-10-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude710 km
Orbital Velocity27,011 km/h
Velocity7.50 km/s
Orbital Period99 minutes
Orbits / Day14.55
Eccentricity0.0019
Semi-Major Axis7,081 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF SSD (United States)
Launch Date
1965-10-15
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1965-082C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OV2-1 is an active satellite operated by USAF SSD (United States), launched on 1965-10-15 from Cape Canaveral Space Force Station, United States on the LCS 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 696 km and 723 km with an inclination of 32.3°. It travels at approximately 27,011 km/h (7.50 km/s), completing one full orbit every 99 minutes — that’s roughly 14.55 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks OV2-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OV2-1 orbits at an average altitude of 710 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of OV2-1’s average altitude, there are currently 282 active payloads and 1,709 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 32.3°, OV2-1 passes over latitudes between 32.3°N and 32.3°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 13,279 active satellites in total, of which 85 share a similar altitude band with OV2-1.
❓ Frequently Asked Questions
OV2-1 orbits in Low Earth Orbit (LEO) at altitudes between 696 km (perigee) and 723 km (apogee), with an average altitude of approximately 710 km. It completes one orbit every 99 minutes, travelling at approximately 27,011 km/h (16,784 mph).
OV2-1 is operated by USAF SSD (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 1641. You can track OV2-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OV2-1 was launched on 1965-10-15 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks OV2-1 (NORAD ID 1641) 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.
OV2-1 travels at approximately 27,011 km/h (16,784 mph) — roughly 7.50 km/s. It completes 14.55 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.