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
12261 km
Apogee
136573 km
Inclination
57.4°
Period
3809.2 min
Mean Motion
0.37798297 rev/day
TLE Epoch
2026-09-18 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude74,417 km
Orbital Velocity7,996 km/h
Velocity2.22 km/s
Orbital Period63.5 hours
Orbits / Day0.38
Eccentricity0.7694
Semi-Major Axis80,788 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 Space Force Station, United States
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 Space Force Station, United States on the OV-102 IUS deploy launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 12,261 km and 136,573 km with an inclination of 57.4°. It travels at approximately 7,996 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 0.7694 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 12,261 km (perigee) and 136,573 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 57.4°, CXO passes over latitudes between 57.4°N and 57.4°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 13,204 active satellites in total.
❓ Frequently Asked Questions
CXO follows a Highly Elliptical Orbit, swinging between 12,261 km (perigee) and 136,573 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 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 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 7,996 km/h (2.22 km/s), completing one revolution every 63.5 hours. Learn more about highly elliptical orbits.