Skip to content
Home › Library › Satellite Directory › ECHOSTAR 2

ECHOSTAR 2

NORAD 24313 Payload GEO 1996-055A ● Active
CONNECTING… GEO · NORAD 24313
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35744 km
Apogee
35824 km
Inclination
12.2°
Period
1436.0 min
Mean Motion
1.00280406 rev/day
TLE Epoch
2026-11-02 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,784 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0009
Semi-Major Axis42,155 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 Echostar (United States)
Launch Date
1996-09-11
Launch Site
Guiana Space Centre, French Guiana
Int'l Designator
1996-055A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ECHOSTAR 2 is an active satellite operated by Echostar (United States), launched on 1996-09-11 from Guiana Space Centre, French Guiana on the Echostar II launch. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,744 km and 35,824 km with an inclination of 12.2°. It travels at approximately 11,070 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 ECHOSTAR 2 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 2 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 12.2°, 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 ECHOSTAR 2’s average altitude, there are currently 730 active payloads and 57 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United States operates approximately 13,342 active satellites in total, of which 156 share a similar altitude band with ECHOSTAR 2.
❓ Frequently Asked Questions
ECHOSTAR 2 orbits at approximately 35,784 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 11,070 km/h — it just keeps pace with the ground below. With an inclination of 12.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ECHOSTAR 2 is operated by Echostar (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24313. You can track ECHOSTAR 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ECHOSTAR 2 was launched on 1996-09-11 from Guiana Space Centre, French Guiana. View the full satellite launch log.
Yes — Orbital Radar tracks ECHOSTAR 2 (NORAD ID 24313) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 2 travels at approximately 11,070 km/h (6,879 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.