ISIS 2 DEB
NORAD 27658
Debris
LEO
1971-024D
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LEO · NORAD 27658
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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
1314 km
Apogee
1389 km
Inclination
88.2°
Period
112.7 min
Mean Motion
12.77490781 rev/day
TLE Epoch
2026-06-15 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,352 km
Orbital Velocity25,864 km/h
Velocity7.18 km/s
Orbital Period113 minutes
Orbits / Day12.77
Eccentricity0.0049
Semi-Major Axis7,723 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇨🇦 Canada
Launch Date
1971-04-01
Launch Site
Vandenberg SFB, California
Int'l Designator
1971-024D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ISIS 2 DEB is a tracked piece of space debris attributed to Canada, launched on 1971-04-01 from Vandenberg SFB, California. After more than 55 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 1,314 km and 1,389 km with an inclination of 88.2°. It travels at approximately 25,864 km/h (7.18 km/s), completing one full orbit every 113 minutes — that’s roughly 12.77 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, ISIS 2 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
ISIS 2 DEB orbits at an average altitude of 1,352 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of ISIS 2 DEB’s average altitude, there are currently 36 active payloads and 145 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 88.2°, ISIS 2 DEB passes over latitudes between 88.2°N and 88.2°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. Canada operates approximately 66 active satellites in total.
🔗 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
ISIS 2 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,314 km (perigee) and 1,389 km (apogee), with an average altitude of approximately 1,352 km. It completes one orbit every 113 minutes, travelling at approximately 25,864 km/h (16,071 mph).
ISIS 2 DEB (NORAD ID 27658) is a piece of tracked orbital debris attributed to Canada. 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.
ISIS 2 DEB was launched on 1971-04-01 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks ISIS 2 DEB (NORAD ID 27658) 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.
ISIS 2 DEB travels at approximately 25,864 km/h (16,071 mph) — roughly 7.18 km/s. It completes 12.77 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.18 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 ISIS 2 DEB. Read more about debris statistics and the Kessler syndrome.