BLOCK DM-SL R/B
NORAD 34811
Rocket Body
MEO
2009-020B
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MEO · NORAD 34811
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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
8598 km
Apogee
35427 km
Inclination
2.6°
Period
793.4 min
Mean Motion
1.81487099 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude22,013 km
Orbital Velocity13,491 km/h
Velocity3.75 km/s
Orbital Period13 hours 13 minutes
Orbits / Day1.81
Eccentricity0.4726
Semi-Major Axis28,384 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
Sea Launch
Launch Date
2009-04-20
Launch Site
Sea Launch (ocean platform)
Int'l Designator
2009-020B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
BLOCK DM-SL R/B is a spent rocket body associated with Sea Launch, launched on 2009-04-20 from Sea Launch (ocean platform) on the SICRAL 1B launch. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 8,598 km and 35,427 km with an inclination of 2.6°. It travels at approximately 13,491 km/h (3.75 km/s), completing one full orbit every 13 hours 13 minutes — that’s roughly 1.81 orbits per day. Its orbital eccentricity of 0.4726 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like BLOCK DM-SL 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
BLOCK DM-SL R/B orbits at an average altitude of 22,013 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 BLOCK DM-SL R/B’s average altitude, there are currently 0 active payloads and 14 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 2.6°, BLOCK DM-SL R/B passes over latitudes between 2.6°N and 2.6°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones.
🔗 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
BLOCK DM-SL R/B orbits in Medium Earth Orbit (MEO) at altitudes between 8,598 km (perigee) and 35,427 km (apogee), with an average altitude of approximately 22,013 km. It completes one orbit every 13 hours 13 minutes, travelling at approximately 13,491 km/h (8,383 mph).
BLOCK DM-SL R/B (NORAD ID 34811) is a spent rocket body — the upper stage of a launch vehicle attributed to Sea Launch. 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.
BLOCK DM-SL R/B was launched on 2009-04-20 from Sea Launch (ocean platform). View the full satellite launch log.
Yes — Orbital Radar tracks BLOCK DM-SL R/B (NORAD ID 34811) 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.
BLOCK DM-SL R/B travels at approximately 13,491 km/h (8,383 mph) — roughly 3.75 km/s. It completes 1.81 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.