BLOCK DM-SL R/B
NORAD 27446
Rocket Body
HEO
2002-030B
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HEO · NORAD 27446
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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
365 km
Apogee
40773 km
Inclination
0.9°
Period
733.7 min
Mean Motion
1.96259526 rev/day
TLE Epoch
2026-06-25 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,569 km
Orbital Velocity13,848 km/h
Velocity3.85 km/s
Orbital Period12 hours 14 minutes
Orbits / Day1.96
Eccentricity0.7500
Semi-Major Axis26,940 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
Sea Launch
Launch Date
2002-06-15
Launch Site
Sea Launch (ocean platform)
Int'l Designator
2002-030B
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 2002-06-15 from Sea Launch (ocean platform) on the Galaxy III-C launch. With over 24 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 365 km and 40,773 km with an inclination of 0.9°. It travels at approximately 13,848 km/h (3.85 km/s), completing one full orbit every 12 hours 14 minutes — that’s roughly 1.96 orbits per day. Its orbital eccentricity of 0.7500 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 follows a Highly Elliptical Orbit, sweeping between 365 km (perigee) and 40,773 km (apogee). It spends most of its 12 hours 14 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of BLOCK DM-SL R/B’s average altitude, there are currently 0 active payloads and 8 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 0.9°, BLOCK DM-SL R/B passes over latitudes between 0.9°N and 0.9°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 follows a Highly Elliptical Orbit, swinging between 365 km (perigee) and 40,773 km (apogee). It spends most of its 12 hours 14 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
BLOCK DM-SL R/B (NORAD ID 27446) 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 2002-06-15 from Sea Launch (ocean platform). 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 BLOCK DM-SL R/B (NORAD ID 27446) 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’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 13,848 km/h (3.85 km/s), completing one revolution every 12 hours 14 minutes. Learn more about highly elliptical orbits.