PSLV R/B
NORAD 29713
Rocket Body
LEO
2007-001E
CONNECTING…
LEO · NORAD 29713
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
557 km
Apogee
587 km
Inclination
98.0°
Period
96.1 min
Mean Motion
14.98463629 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude572 km
Orbital Velocity27,277 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.98
Eccentricity0.0022
Semi-Major Axis6,943 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2007-01-10
Launch Site
SRI
Int'l Designator
2007-001E
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
PSLV R/B is a spent rocket body associated with India, launched on 2007-01-10 from SRI on the LAPAN-TUBSAT launch. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 557 km and 587 km with an inclination of 98.0°. It travels at approximately 27,277 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.98 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 ~3–10 years. Spent rocket bodies like PSLV 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
PSLV R/B orbits at an average altitude of 572 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 R/B’s average altitude, there are currently 2,971 active payloads and 500 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-1522, STARLINK-2112. This makes it one of the more crowded altitude bands, containing roughly 17% of all active satellites. With an inclination of 98.0°, PSLV R/B passes over latitudes between 98.0°N and 98.0°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 14 share a similar altitude band with PSLV R/B.
🔗 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
PSLV R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 572 km altitude. Its 98.0° 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 96 minutes, travelling at 27,277 km/h.
PSLV R/B (NORAD ID 29713) is a spent rocket body — the upper stage of a launch vehicle attributed to India. 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.
PSLV R/B was launched on 2007-01-10 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks PSLV R/B (NORAD ID 29713) 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 R/B travels at approximately 27,277 km/h (16,949 mph) — roughly 7.58 km/s. It completes 14.98 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.