OPS 9444 (DSCS 2-14)
NORAD 11622
Payload
GEO
1979-098B
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GEO · NORAD 11622
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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
36320 km
Apogee
36347 km
Inclination
8.5°
Period
1464.1 min
Mean Motion
0.98351138 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,334 km
Orbital Velocity10,999 km/h
Velocity3.06 km/s
Orbital Period24.4 hours
Orbits / Day0.98
Eccentricity0.0003
Semi-Major Axis42,705 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1979-11-21
Launch Site
Cape Canaveral, Florida
Int'l Designator
1979-098B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 9444 (DSCS 2-14) is an active satellite operated by United States, launched on 1979-11-21 from Cape Canaveral, Florida. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,320 km and 36,347 km with an inclination of 8.5°. It travels at approximately 10,999 km/h (3.06 km/s), completing one full orbit every 24.4 hours — that’s roughly 0.98 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 OPS 9444 (DSCS 2-14) 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 9444 (DSCS 2-14) 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 8.5°, 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 9444 (DSCS 2-14)’s average altitude, there are currently 43 active payloads and 10 tracked debris or rocket body fragments. United States operates approximately 12,339 active satellites in total, of which 11 share a similar altitude band with OPS 9444 (DSCS 2-14).
❓ Frequently Asked Questions
OPS 9444 (DSCS 2-14) orbits at approximately 36,334 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 10,999 km/h — it just keeps pace with the ground below. With an inclination of 8.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
OPS 9444 (DSCS 2-14) is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 11622. You can track OPS 9444 (DSCS 2-14) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 9444 (DSCS 2-14) was launched on 1979-11-21 from Cape Canaveral, Florida, 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 9444 (DSCS 2-14) (NORAD ID 11622) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. 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 9444 (DSCS 2-14) travels at approximately 10,999 km/h (6,834 mph) — roughly 3.06 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.