Home Library Satellite Directory APRIZESAT 4

APRIZESAT 4

NORAD 35684 Payload LEO 2009-041D ● Active
CONNECTING… LEO · NORAD 35684
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
588 km
Apogee
647 km
Inclination
98.2°
Period
97.0 min
Mean Motion
14.83724540 rev/day
TLE Epoch
2026-03-17 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude618 km
Orbital Velocity27,188 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.84
Eccentricity0.0042
Semi-Major Axis6,989 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2009-07-29
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2009-041D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
🔗 Constellation / Groups
engineeringexperimental
📖 About This Object
APRIZESAT 4 is an active satellite operated by United States, launched on 2009-07-29 from Baikonur, Kazakhstan. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 588 km and 647 km with an inclination of 98.2°. It travels at approximately 27,188 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.84 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. It is part of the Engineering constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks APRIZESAT 4 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
APRIZESAT 4 operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
❓ Frequently Asked Questions
APRIZESAT 4 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 618 km altitude. Its 98.2° 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 97 minutes, travelling at 27,188 km/h.
APRIZESAT 4 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 35684. You can track APRIZESAT 4 in real time on Orbital Radar’s live tracker.
APRIZESAT 4 was launched on 2009-07-29 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.
Yes — Orbital Radar tracks APRIZESAT 4 (NORAD ID 35684) 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.
APRIZESAT 4 travels at approximately 27,188 km/h (16,894 mph) — roughly 7.55 km/s. It completes 14.84 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.
APRIZESAT 4 is a member of the Engineering constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Engineering satellites on Orbital Radar’s live tracker.