OV2-5
NORAD 3428
Payload
GEO
1968-081A
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GEO · NORAD 3428
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35099 km
Apogee
35761 km
Inclination
2.3°
Period
1417.9 min
Mean Motion
1.01557312 rev/day
TLE Epoch
2026-10-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,430 km
Orbital Velocity11,117 km/h
Velocity3.09 km/s
Orbital Period23 hours 38 minutes
Orbits / Day1.02
Eccentricity0.0079
Semi-Major Axis41,801 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 SAMSO (United States)
Launch Date
1968-09-26
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1968-081A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OV2-5 is an active satellite operated by SAMSO (United States), launched on 1968-09-26 from Cape Canaveral Space Force Station, United States on the OV2-5 launch. After more than 58 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 35,099 km and 35,761 km with an inclination of 2.3°. It travels at approximately 11,117 km/h (3.09 km/s), completing one full orbit every 23 hours 38 minutes — that’s roughly 1.02 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks OV2-5 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OV2-5 occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 2.3°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of OV2-5’s average altitude, there are currently 2 active payloads and 18 tracked debris or rocket body fragments. United States operates approximately 13,279 active satellites in total, of which 2 share a similar altitude band with OV2-5.
❓ Frequently Asked Questions
OV2-5 orbits at approximately 35,430 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,117 km/h — it just keeps pace with the ground below. With an inclination of 2.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
OV2-5 is operated by SAMSO (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 3428. You can track OV2-5 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OV2-5 was launched on 1968-09-26 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. View the full satellite launch log.
Yes — Orbital Radar tracks OV2-5 (NORAD ID 3428) 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.
OV2-5 travels at approximately 11,117 km/h (6,908 mph) — roughly 3.09 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.