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INTERBALL AURORA

NORAD 24293 Payload MEO 1996-050C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
846 km
Apogee
19125 km
Inclination
62.7°
Period
347.2 min
Mean Motion
4.14740091 rev/day
TLE Epoch
2026-06-17 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,986 km
Orbital Velocity17,772 km/h
Velocity4.94 km/s
Orbital Period5 hours 47 minutes
Orbits / Day4.15
Eccentricity0.5588
Semi-Major Axis16,357 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1996-08-29
Launch Site
PKMTR
Int'l Designator
1996-050C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INTERBALL AURORA is an active satellite operated by Russia (CIS), launched on 1996-08-29 from PKMTR. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 846 km and 19,125 km with an inclination of 62.7°. It travels at approximately 17,772 km/h (4.94 km/s), completing one full orbit every 5 hours 47 minutes — that’s roughly 4.15 orbits per day. Its orbital eccentricity of 0.5588 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks INTERBALL AURORA in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
INTERBALL AURORA orbits at an average altitude of 9,986 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of INTERBALL AURORA’s average altitude, there are currently 2 active payloads and 4 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 62.7°, INTERBALL AURORA passes over latitudes between 62.7°N and 62.7°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Russia (CIS) operates approximately 1,285 active satellites in total.
❓ Frequently Asked Questions
INTERBALL AURORA orbits in Medium Earth Orbit (MEO) at altitudes between 846 km (perigee) and 19,125 km (apogee), with an average altitude of approximately 9,986 km. It completes one orbit every 5 hours 47 minutes, travelling at approximately 17,772 km/h (11,043 mph).
INTERBALL AURORA is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24293. You can track INTERBALL AURORA in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INTERBALL AURORA was launched on 1996-08-29 from PKMTR. 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 INTERBALL AURORA (NORAD ID 24293) 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.
INTERBALL AURORA travels at approximately 17,772 km/h (11,043 mph) — roughly 4.94 km/s. It completes 4.15 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 8 sunrises and sunsets every 24 hours.