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CXO

NORAD 25867 Payload HEO 1999-040B ● Active
CONNECTING… HEO · NORAD 25867
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
9890 km
Apogee
138945 km
Inclination
54.6°
Period
3809.3 min
Mean Motion
0.37802383 rev/day
TLE Epoch
2026-03-17 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude74,418 km
Orbital Velocity7,996 km/h
Velocity2.22 km/s
Orbital Period63.5 hours
Orbits / Day0.38
Eccentricity0.7987
Semi-Major Axis80,789 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 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)
🔗 Constellation / Groups
geo protected plus
📖 About This Object
CXO is an active satellite operated by 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 9,890 km and 138,945 km with an inclination of 54.6°. 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 0.7987 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. It is part of the Geo Protected Plus constellation group. 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 (HEO), which sweeps between a low-altitude perigee and a very high apogee. HEO satellites spend most of their orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest. This makes HEO ideal for high-latitude communications (Molniya and Tundra orbits), early-warning missile detection (SBIRS), and space science missions that need to sample different regions of the magnetosphere. The large difference between perigee (9,890 km) and apogee (138,945 km) for this object illustrates the characteristic elliptical shape.
❓ Frequently Asked Questions
CXO follows a Highly Elliptical Orbit, swinging between 9,890 km (perigee) and 138,945 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 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.
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.
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.
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.
CXO is a member of the Geo Protected Plus constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Geo Protected Plus satellites on Orbital Radar’s live tracker.