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SL-4 R/B

NORAD 68753 Rocket Body LEO 2026-083A
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
453 km
Apogee
541 km
Inclination
98.3°
Period
94.6 min
Mean Motion
15.22804267 rev/day
TLE Epoch
2026-07-16 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude497 km
Orbital Velocity27,426 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.23
Eccentricity0.0064
Semi-Major Axis6,868 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
2026-083A
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
SL-4 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 453 km and 541 km with an inclination of 98.3°. It travels at approximately 27,426 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.23 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 SL-4 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
SL-4 R/B orbits at an average altitude of 497 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 SL-4 R/B’s average altitude, there are currently 9,440 active payloads and 215 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 53.6% of all active satellites. With an inclination of 98.3°, SL-4 R/B passes over latitudes between 98.3°N and 98.3°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 1,288 active satellites in total, of which 59 share a similar altitude band with SL-4 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
SL-4 R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 497 km altitude. Its 98.3° 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 95 minutes, travelling at 27,426 km/h.
SL-4 R/B (NORAD ID 68753) 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.
SL-4 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 SL-4 R/B (NORAD ID 68753) 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.
SL-4 R/B travels at approximately 27,426 km/h (17,041 mph) — roughly 7.62 km/s. It completes 15.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.