CXO
NORAD 25867
Payload
HEO
1999-040B
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HEO · NORAD 25867
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
11167 km
Apogee
137655 km
Inclination
56.3°
Period
3808.8 min
Mean Motion
0.37807394 rev/day
TLE Epoch
2026-06-21 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude74,411 km
Orbital Velocity7,997 km/h
Velocity2.22 km/s
Orbital Period63.5 hours
Orbits / Day0.38
Eccentricity0.7829
Semi-Major Axis80,782 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 National Aeronautics and Space Administration (NASA) Goddard Space Flight Center (United States)
Launch Date
1999-07-23
Launch Site
Cape Canaveral, Florida
Int'l Designator
1999-040B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CXO is an active satellite operated by National Aeronautics and Space Administration (NASA) Goddard Space Flight Center (United States), launched on 1999-07-23 from Cape Canaveral, Florida. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 11,167 km and 137,655 km with an inclination of 56.3°. It travels at approximately 7,997 km/h (2.22 km/s), completing one full orbit every 63.5 hours — that’s roughly 0.38 orbits per day. Its orbital eccentricity of 0.7829 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks CXO in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CXO follows a Highly Elliptical Orbit, sweeping between 11,167 km (perigee) and 137,655 km (apogee). It spends most of its 63.5 hours orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. With an inclination of 56.3°, CXO passes over latitudes between 56.3°N and 56.3°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,339 active satellites in total.
❓ Frequently Asked Questions
CXO follows a Highly Elliptical Orbit, swinging between 11,167 km (perigee) and 137,655 km (apogee). It spends most of its 63.5 hours orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
CXO is operated by National Aeronautics and Space Administration (NASA) Goddard Space Flight Center (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25867. You can track CXO in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CXO was launched on 1999-07-23 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 CXO (NORAD ID 25867) 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.
CXO’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 7,997 km/h (2.22 km/s), completing one revolution every 63.5 hours. Learn more about highly elliptical orbits.