SATCOM 2R
NORAD 14328
Payload
GEO
1983-094A
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GEO · NORAD 14328
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Altitude (km)
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Speed (km/s)
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Latitude
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🛰️ Orbital Parameters
Perigee
35963 km
Apogee
36095 km
Inclination
14.3°
Period
1448.5 min
Mean Motion
0.99414651 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,029 km
Orbital Velocity11,038 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day0.99
Eccentricity0.0016
Semi-Major Axis42,400 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1983-09-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
1983-094A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SATCOM 2R is an active satellite operated by United States, launched on 1983-09-08 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 35,963 km and 36,095 km with an inclination of 14.3°. It travels at approximately 11,038 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 0.99 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 2R 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 2R 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 14.3°, 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 SATCOM 2R’s average altitude, there are currently 73 active payloads and 31 tracked debris or rocket body fragments. United States operates approximately 12,360 active satellites in total, of which 15 share a similar altitude band with SATCOM 2R.
❓ Frequently Asked Questions
SATCOM 2R orbits at approximately 36,029 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 11,038 km/h — it just keeps pace with the ground below. With an inclination of 14.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
SATCOM 2R is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 14328. You can track SATCOM 2R in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SATCOM 2R was launched on 1983-09-08 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 2R (NORAD ID 14328) 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 2R travels at approximately 11,038 km/h (6,859 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.