Skip to content
Home Library Satellite Directory PSLV DEB

PSLV DEB

NORAD 27153 Debris LEO 2001-049CZ
CONNECTING… LEO · NORAD 27153
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
376 km
Apogee
383 km
Inclination
97.8°
Period
92.2 min
Mean Motion
15.62711549 rev/day
TLE Epoch
2026-06-20 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude380 km
Orbital Velocity27,663 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.63
Eccentricity0.0005
Semi-Major Axis6,751 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2001-10-22
Launch Site
SRI
Int'l Designator
2001-049CZ
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PSLV DEB is a tracked piece of space debris attributed to India, launched on 2001-10-22 from SRI on the TES launch. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 376 km and 383 km with an inclination of 97.8°. It travels at approximately 27,663 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.63 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. 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 380 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 1,287 active payloads and 63 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.4% of all active satellites. With an inclination of 97.8°, PSLV DEB passes over latitudes between 97.8°N and 97.8°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 4 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 380 km altitude. Its 97.8° 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 92 minutes, travelling at 27,663 km/h.
PSLV DEB (NORAD ID 27153) 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks PSLV DEB (NORAD ID 27153) 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 27,663 km/h (17,189 mph) — roughly 7.68 km/s. It completes 15.63 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 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 7.68 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.