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Home Library Satellite Directory OPS 9438 (DSCS 2-8)

OPS 9438 (DSCS 2-8)

NORAD 10001 Payload GEO 1977-034B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
37053 km
Apogee
37350 km
Inclination
8.9°
Period
1509.0 min
Mean Motion
0.95426623 rev/day
TLE Epoch
2026-05-08 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,202 km
Orbital Velocity10,888 km/h
Velocity3.02 km/s
Orbital Period25.1 hours
Orbits / Day0.95
Eccentricity0.0034
Semi-Major Axis43,573 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1977-05-12
Launch Site
Cape Canaveral, Florida
Int'l Designator
1977-034B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 9438 (DSCS 2-8) is an active satellite operated by United States, launched on 1977-05-12 from Cape Canaveral, Florida. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 37,053 km and 37,350 km with an inclination of 8.9°. It travels at approximately 10,888 km/h (3.02 km/s), completing one full orbit every 25.1 hours — that’s roughly 0.95 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 9438 (DSCS 2-8) 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 9438 (DSCS 2-8) occupies geostationary orbit (GEO) at approximately 35,786 km above the equator. At this precise altitude, the satellite’s orbital period matches the Earth’s rotation — so it appears to hover over a fixed point on the equator. GEO is used primarily for broadcast television, weather monitoring (Meteosat, GOES) and wideband communications. Only about 560 active satellites occupy the GEO belt, but its commercial value is immense: a single GEO slot can cover roughly one-third of the Earth’s surface. This satellite has a non-zero inclination of 8.9°, meaning it traces a small figure-of-eight pattern relative to the ground rather than remaining perfectly stationary. This can indicate an aging satellite whose stationkeeping fuel is running low, or a deliberate inclined-orbit strategy to extend operational life.
❓ Frequently Asked Questions
OPS 9438 (DSCS 2-8) orbits at approximately 37,202 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 10,888 km/h — it just keeps pace with the ground below. With an inclination of 8.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
OPS 9438 (DSCS 2-8) is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 10001. You can track OPS 9438 (DSCS 2-8) in real time on Orbital Radar’s live tracker.
OPS 9438 (DSCS 2-8) was launched on 1977-05-12 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.
Yes — Orbital Radar tracks OPS 9438 (DSCS 2-8) (NORAD ID 10001) 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.
OPS 9438 (DSCS 2-8) travels at approximately 10,888 km/h (6,766 mph) — roughly 3.02 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.
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