VOLGA R/B
NORAD 68756
Rocket Body
LEO
2026-083D
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LEO · NORAD 68756
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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
458 km
Apogee
479 km
Inclination
96.9°
Period
94.0 min
Mean Motion
15.32425374 rev/day
TLE Epoch
2026-06-26 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude469 km
Orbital Velocity27,483 km/h
Velocity7.63 km/s
Orbital Period94 minutes
Orbits / Day15.32
Eccentricity0.0015
Semi-Major Axis6,840 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2026-04-16
Launch Site
PKMTR
Int'l Designator
2026-083D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
VOLGA R/B is a spent rocket body associated with Russia (CIS), launched on 2026-04-16 from PKMTR on the Unknown launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 458 km and 479 km with an inclination of 96.9°. It travels at approximately 27,483 km/h (7.63 km/s), completing one full orbit every 94 minutes — that’s roughly 15.32 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 ~1–3 years. Spent rocket bodies like VOLGA R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
VOLGA R/B orbits at an average altitude of 469 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 VOLGA R/B’s average altitude, there are currently 8,259 active payloads and 189 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 47.2% of all active satellites. With an inclination of 96.9°, VOLGA R/B passes over latitudes between 96.9°N and 96.9°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. Russia (CIS) operates approximately 1,286 active satellites in total, of which 58 share a similar altitude band with VOLGA R/B.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
VOLGA R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 469 km altitude. Its 96.9° 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 94 minutes, travelling at 27,483 km/h.
VOLGA R/B (NORAD ID 68756) is a spent rocket body — the upper stage of a launch vehicle attributed to Russia (CIS). It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
VOLGA R/B was launched on 2026-04-16 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks VOLGA R/B (NORAD ID 68756) 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.
VOLGA R/B travels at approximately 27,483 km/h (17,077 mph) — roughly 7.63 km/s. It completes 15.32 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.