CP4
NORAD 31132
Payload
LEO
2007-012Q
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LEO · NORAD 31132
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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
622 km
Apogee
721 km
Inclination
98.4°
Period
98.2 min
Mean Motion
14.66645732 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude672 km
Orbital Velocity27,084 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.67
Eccentricity0.0070
Semi-Major Axis7,043 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2007-04-17
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2007-012Q
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CP4 is an active satellite operated by United States, launched on 2007-04-17 from Baikonur, Kazakhstan. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 622 km and 721 km with an inclination of 98.4°. It travels at approximately 27,084 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.67 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks CP4 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CP4 orbits at an average altitude of 672 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of CP4’s average altitude, there are currently 574 active payloads and 1,214 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.4°, CP4 passes over latitudes between 98.4°N and 98.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 12,360 active satellites in total, of which 276 share a similar altitude band with CP4.
❓ Frequently Asked Questions
CP4 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 672 km altitude. Its 98.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 98 minutes, travelling at 27,084 km/h.
CP4 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 31132. You can track CP4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CP4 was launched on 2007-04-17 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks CP4 (NORAD ID 31132) 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.
CP4 travels at approximately 27,084 km/h (16,829 mph) — roughly 7.52 km/s. It completes 14.67 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.