ISIS 1 DEB
NORAD 31999
Debris
MEO
1969-009C
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MEO · NORAD 31999
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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
559 km
Apogee
2492 km
Inclination
88.4°
Period
116.5 min
Mean Motion
12.35510286 rev/day
TLE Epoch
2026-06-20 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,526 km
Orbital Velocity25,577 km/h
Velocity7.10 km/s
Orbital Period117 minutes
Orbits / Day12.36
Eccentricity0.1224
Semi-Major Axis7,897 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇨🇦 Canada
Launch Date
1969-01-30
Launch Site
Vandenberg SFB, California
Int'l Designator
1969-009C
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ISIS 1 DEB is a tracked piece of space debris attributed to Canada, launched on 1969-01-30 from Vandenberg SFB, California on the Isis A launch. After more than 57 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 559 km and 2,492 km with an inclination of 88.4°. It travels at approximately 25,577 km/h (7.10 km/s), completing one full orbit every 117 minutes — that’s roughly 12.36 orbits per day. Its orbital eccentricity of 0.1224 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, ISIS 1 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 1 DEB orbits at an average altitude of 1,526 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of ISIS 1 DEB’s average altitude, there are currently 163 active payloads and 262 tracked debris or rocket body fragments. With an inclination of 88.4°, ISIS 1 DEB passes over latitudes between 88.4°N and 88.4°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 67 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 1 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 559 km (perigee) and 2,492 km (apogee), with an average altitude of approximately 1,526 km. It completes one orbit every 117 minutes, travelling at approximately 25,577 km/h (15,893 mph).
ISIS 1 DEB (NORAD ID 31999) 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 1 DEB was launched on 1969-01-30 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 1 DEB (NORAD ID 31999) 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 1 DEB travels at approximately 25,577 km/h (15,893 mph) — roughly 7.10 km/s. It completes 12.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.10 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 1 DEB. Read more about debris statistics and the Kessler syndrome.