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SATCOM 1R

NORAD 13984 Payload GEO 1983-030A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35872 km
Apogee
35936 km
Inclination
13.2°
Period
1442.1 min
Mean Motion
0.99855118 rev/day
TLE Epoch
2026-06-17 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,904 km
Orbital Velocity11,054 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0008
Semi-Major Axis42,275 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1983-04-11
Launch Site
Cape Canaveral, Florida
Int'l Designator
1983-030A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SATCOM 1R is an active satellite operated by United States, launched on 1983-04-11 from Cape Canaveral, Florida. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,872 km and 35,936 km with an inclination of 13.2°. It travels at approximately 11,054 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 SATCOM 1R in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SATCOM 1R 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 13.2°, 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 SATCOM 1R’s average altitude, there are currently 59 active payloads and 20 tracked debris or rocket body fragments. United States operates approximately 12,360 active satellites in total, of which 18 share a similar altitude band with SATCOM 1R.
❓ Frequently Asked Questions
SATCOM 1R orbits at approximately 35,904 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 11,054 km/h — it just keeps pace with the ground below. With an inclination of 13.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
SATCOM 1R is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13984. You can track SATCOM 1R in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SATCOM 1R was launched on 1983-04-11 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 SATCOM 1R (NORAD ID 13984) 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.
SATCOM 1R travels at approximately 11,054 km/h (6,869 mph) — roughly 3.07 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.