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VESPA - DEB

NORAD 100691 Debris LEO 2026-209C
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🛰️ Orbital Parameters
Perigee
654 km
Apogee
819 km
Inclination
98.6°
Period
99.5 min
Mean Motion
14.46636090 rev/day
TLE Epoch
2026-11-01 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude737 km
Orbital Velocity26,960 km/h
Velocity7.49 km/s
Orbital Period100 minutes
Orbits / Day14.47
Eccentricity0.0116
Semi-Major Axis7,108 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
2026-09-15
Launch Site
Guiana Space Centre, French Guiana
Int'l Designator
2026-209C
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
VESPA - DEB is a tracked piece of space debris attributed to ESA (European Space Agency), launched on 2026-09-15 from Guiana Space Centre, French Guiana on the Sentinel-3C/Flex launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 654 km and 819 km with an inclination of 98.6°. It travels at approximately 26,960 km/h (7.49 km/s), completing one full orbit every 100 minutes — that’s roughly 14.47 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 ~25–100 years. As orbital debris, VESPA - 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
VESPA - DEB orbits at an average altitude of 737 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 VESPA - DEB’s average altitude, there are currently 411 active payloads and 2,053 tracked debris or rocket body fragments — notable neighbours include TERRA, ONEWEB-0179, LANDSAT 9. With an inclination of 98.6°, VESPA - DEB passes over latitudes between 98.6°N and 98.6°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. ESA (European Space Agency) operates approximately 97 active satellites in total, of which 9 share a similar altitude band with VESPA - 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
VESPA - DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 737 km altitude. Its 98.6° 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 100 minutes, travelling at 26,960 km/h.
VESPA - DEB (NORAD ID 100691) is a piece of tracked orbital debris attributed to ESA (European Space Agency). 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.
VESPA - DEB was launched on 2026-09-15 from Guiana Space Centre, French Guiana. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks VESPA - DEB (NORAD ID 100691) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
VESPA - DEB travels at approximately 26,960 km/h (16,752 mph) — roughly 7.49 km/s. It completes 14.47 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.49 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 VESPA - DEB. Read more about debris statistics and the Kessler syndrome.