Skip to content
Home Library Satellite Directory PROBA-3 CSC

PROBA-3 CSC

NORAD 62256 Payload HEO 2024-233A ● Active
CONNECTING… HEO · NORAD 62256
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
978 km
Apogee
60232 km
Inclination
59.7°
Period
1179.7 min
Mean Motion
1.22073990 rev/day
TLE Epoch
2026-06-16 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude30,605 km
Orbital Velocity11,820 km/h
Velocity3.28 km/s
Orbital Period19 hours 40 minutes
Orbits / Day1.22
Eccentricity0.8012
Semi-Major Axis36,976 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
2024-12-05
Launch Site
SRI
Int'l Designator
2024-233A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
PROBA-3 CSC is an active satellite operated by ESA (European Space Agency), launched on 2024-12-05 from SRI. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 978 km and 60,232 km with an inclination of 59.7°. It travels at approximately 11,820 km/h (3.28 km/s), completing one full orbit every 19 hours 40 minutes — that’s roughly 1.22 orbits per day. Its orbital eccentricity of 0.8012 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks PROBA-3 CSC in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PROBA-3 CSC follows a Highly Elliptical Orbit, sweeping between 978 km (perigee) and 60,232 km (apogee). It spends most of its 19 hours 40 minutes 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. Within ±50 km of PROBA-3 CSC’s average altitude, there are currently 2 active payloads and 0 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 59.7°, PROBA-3 CSC passes over latitudes between 59.7°N and 59.7°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. ESA (European Space Agency) operates approximately 93 active satellites in total, of which 2 share a similar altitude band with PROBA-3 CSC.
❓ Frequently Asked Questions
PROBA-3 CSC follows a Highly Elliptical Orbit, swinging between 978 km (perigee) and 60,232 km (apogee). It spends most of its 19 hours 40 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
PROBA-3 CSC is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 62256. You can track PROBA-3 CSC in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PROBA-3 CSC was launched on 2024-12-05 from SRI. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks PROBA-3 CSC (NORAD ID 62256) 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.
PROBA-3 CSC’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 11,820 km/h (3.28 km/s), completing one revolution every 19 hours 40 minutes. Learn more about highly elliptical orbits.