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EWS-G2 (GOES 15)

NORAD 36411 Payload GEO 2010-008A ● Active
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🛰️ Orbital Parameters
Perigee
35771 km
Apogee
35804 km
Inclination
1.6°
Period
1436.1 min
Mean Motion
1.00269832 rev/day
TLE Epoch
2026-11-01 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,788 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0004
Semi-Major Axis42,159 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 NOAA (National Oceanographic and Atmospheric Administration) (United States)
Launch Date
2010-03-04
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
2010-008A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
goes
📖 About This Object
EWS-G2 (GOES 15) is an active satellite operated by NOAA (National Oceanographic and Atmospheric Administration) (United States), launched on 2010-03-04 from Cape Canaveral Space Force Station, United States on the GOES P launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,771 km and 35,804 km with an inclination of 1.6°. 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. It is part of the Goes constellation group. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks EWS-G2 (GOES 15) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
EWS-G2 (GOES 15) 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 1.6°, 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 EWS-G2 (GOES 15)’s average altitude, there are currently 730 active payloads and 60 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United States operates approximately 13,340 active satellites in total, of which 154 share a similar altitude band with EWS-G2 (GOES 15).
❓ Frequently Asked Questions
EWS-G2 (GOES 15) orbits at approximately 35,788 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 1.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EWS-G2 (GOES 15) is operated by NOAA (National Oceanographic and Atmospheric Administration) (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 36411. You can track EWS-G2 (GOES 15) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EWS-G2 (GOES 15) was launched on 2010-03-04 from Cape Canaveral Space Force Station, United States, 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 EWS-G2 (GOES 15) (NORAD ID 36411) 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.
EWS-G2 (GOES 15) travels at approximately 11,070 km/h (6,878 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.
EWS-G2 (GOES 15) is a member of the Goes constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Goes satellites on Orbital Radar’s live tracker.