OPS 3367 B
NORAD 735
Payload
LEO
1964-002C
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LEO · NORAD 735
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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
785 km
Apogee
808 km
Inclination
99.0°
Period
100.8 min
Mean Motion
14.28605486 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude797 km
Orbital Velocity26,846 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.29
Eccentricity0.0016
Semi-Major Axis7,168 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NRO / SAFSP (United States)
Launch Date
1964-01-19
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1964-002C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 3367 B is an active satellite operated by NRO / SAFSP (United States), launched on 1964-01-19 from Vandenberg Space Force Base, United States on the P35-6 launch. After more than 62 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 785 km and 808 km with an inclination of 99.0°. It travels at approximately 26,846 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.29 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 ~25–100 years. Orbital Radar tracks OPS 3367 B in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OPS 3367 B orbits at an average altitude of 797 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 OPS 3367 B’s average altitude, there are currently 452 active payloads and 2,488 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 99.0°, OPS 3367 B passes over latitudes between 99.0°N and 99.0°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 13,279 active satellites in total, of which 191 share a similar altitude band with OPS 3367 B.
❓ Frequently Asked Questions
OPS 3367 B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 797 km altitude. Its 99.0° 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 101 minutes, travelling at 26,846 km/h.
OPS 3367 B is operated by NRO / SAFSP (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 735. You can track OPS 3367 B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 3367 B was launched on 1964-01-19 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 3367 B (NORAD ID 735) 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.
OPS 3367 B travels at approximately 26,846 km/h (16,682 mph) — roughly 7.46 km/s. It completes 14.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.