PSLV DEB
NORAD 27580
Debris
LEO
2001-049MY
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LEO · NORAD 27580
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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
606 km
Apogee
665 km
Inclination
98.3°
Period
97.4 min
Mean Motion
14.78136871 rev/day
TLE Epoch
2026-06-16 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude636 km
Orbital Velocity27,153 km/h
Velocity7.54 km/s
Orbital Period97 minutes
Orbits / Day14.78
Eccentricity0.0042
Semi-Major Axis7,007 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2001-10-22
Launch Site
SRI
Int'l Designator
2001-049MY
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
PSLV DEB is a tracked piece of space debris attributed to India, launched on 2001-10-22 from SRI. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 606 km and 665 km with an inclination of 98.3°. It travels at approximately 27,153 km/h (7.54 km/s), completing one full orbit every 97 minutes — that’s roughly 14.78 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 ~10–25 years. As orbital debris, PSLV DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
PSLV DEB orbits at an average altitude of 636 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 PSLV DEB’s average altitude, there are currently 769 active payloads and 888 tracked debris or rocket body fragments — notable neighbours include AQUA, ONEWEB-0050. With an inclination of 98.3°, PSLV DEB 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. India operates approximately 108 active satellites in total, of which 12 share a similar altitude band with PSLV DEB.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
PSLV DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 636 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 97 minutes, travelling at 27,153 km/h.
PSLV DEB (NORAD ID 27580) is a piece of tracked orbital debris attributed to India. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
PSLV DEB was launched on 2001-10-22 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks PSLV DEB (NORAD ID 27580) 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.
PSLV DEB travels at approximately 27,153 km/h (16,872 mph) — roughly 7.54 km/s. It completes 14.78 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.54 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like PSLV DEB. Read more about debris statistics and the Kessler syndrome.