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ECHOSTAR 1

NORAD 23754 Payload GEO 1995-073A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36156 km
Apogee
36175 km
Inclination
8.6°
Period
1455.5 min
Mean Motion
0.98935314 rev/day
TLE Epoch
2026-06-18 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,166 km
Orbital Velocity11,020 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0002
Semi-Major Axis42,537 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1995-12-28
Launch Site
Xichang, China
Int'l Designator
1995-073A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ECHOSTAR 1 is an active satellite operated by United States, launched on 1995-12-28 from Xichang, China. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,156 km and 36,175 km with an inclination of 8.6°. It travels at approximately 11,020 km/h (3.06 km/s), completing one full orbit every 24.3 hours — 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 ECHOSTAR 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ECHOSTAR 1 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 8.6°, 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 ECHOSTAR 1’s average altitude, there are currently 152 active payloads and 11 tracked debris or rocket body fragments. United States operates approximately 12,339 active satellites in total, of which 53 share a similar altitude band with ECHOSTAR 1.
❓ Frequently Asked Questions
ECHOSTAR 1 orbits at approximately 36,166 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 11,020 km/h — it just keeps pace with the ground below. With an inclination of 8.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ECHOSTAR 1 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23754. You can track ECHOSTAR 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ECHOSTAR 1 was launched on 1995-12-28 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks ECHOSTAR 1 (NORAD ID 23754) 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.
ECHOSTAR 1 travels at approximately 11,020 km/h (6,848 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.