OPS 9346 (IDSCS 24)
NORAD 3289
Payload
GEO
1968-050F
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GEO · NORAD 3289
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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
33738 km
Apogee
34118 km
Inclination
7.3°
Period
1342.2 min
Mean Motion
1.07287523 rev/day
TLE Epoch
2026-10-21 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude33,928 km
Orbital Velocity11,322 km/h
Velocity3.15 km/s
Orbital Period22 hours 22 minutes
Orbits / Day1.07
Eccentricity0.0047
Semi-Major Axis40,299 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 SAMSO (United States)
Launch Date
1968-06-13
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1968-050F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 9346 (IDSCS 24) is an active satellite operated by SAMSO (United States), launched on 1968-06-13 from Cape Canaveral Space Force Station, United States on the IDCSP 20 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 33,738 km and 34,118 km with an inclination of 7.3°. It travels at approximately 11,322 km/h (3.15 km/s), completing one full orbit every 22 hours 22 minutes — that’s roughly 1.07 orbits per day. Orbital Radar tracks OPS 9346 (IDSCS 24) 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 9346 (IDSCS 24) 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 7.3°, 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 OPS 9346 (IDSCS 24)’s average altitude, there are currently 5 active payloads and 1 tracked debris or rocket body fragment. United States operates approximately 13,279 active satellites in total, of which 5 share a similar altitude band with OPS 9346 (IDSCS 24).
❓ Frequently Asked Questions
OPS 9346 (IDSCS 24) orbits at approximately 33,928 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 11,322 km/h — it just keeps pace with the ground below. With an inclination of 7.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
OPS 9346 (IDSCS 24) is operated by SAMSO (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 3289. You can track OPS 9346 (IDSCS 24) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 9346 (IDSCS 24) was launched on 1968-06-13 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 OPS 9346 (IDSCS 24) (NORAD ID 3289) 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 9346 (IDSCS 24) travels at approximately 11,322 km/h (7,035 mph) — roughly 3.15 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.