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BLOCK DM-SL R/B

NORAD 67758 Rocket Body GEO 2026-028C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
34571 km
Apogee
35409 km
Inclination
0.1°
Period
1395.6 min
Mean Motion
1.03181470 rev/day
TLE Epoch
2026-07-20 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude34,990 km
Orbital Velocity11,176 km/h
Velocity3.10 km/s
Orbital Period23 hours 16 minutes
Orbits / Day1.03
Eccentricity0.0101
Semi-Major Axis41,361 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2026-02-12
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2026-028C
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
BLOCK DM-SL R/B is a spent rocket body associated with Russia (CIS), launched on 2026-02-12 from Baikonur, Kazakhstan on the Elektro-L No. 5 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Geostationary Orbit (GEO) at altitudes between 34,571 km and 35,409 km with an inclination of 0.1°. It travels at approximately 11,176 km/h (3.10 km/s), completing one full orbit every 23 hours 16 minutes — that’s roughly 1.03 orbits per day. 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 occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. Within ±50 km of BLOCK DM-SL R/B’s average altitude, there are currently 0 active payloads and 13 tracked debris or rocket body fragments. Russia (CIS) operates approximately 1,287 active satellites in total.
🔗 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 at approximately 34,990 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,176 km/h — it just keeps pace with the ground below. Learn more about geostationary orbits.
BLOCK DM-SL R/B (NORAD ID 67758) 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.
BLOCK DM-SL R/B was launched on 2026-02-12 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks BLOCK DM-SL R/B (NORAD ID 67758) 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 11,176 km/h (6,944 mph) — roughly 3.10 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.