THOR ALTAIR DEB
NORAD 2177
Debris
LEO
1966-026D
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LEO · NORAD 2177
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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
537 km
Apogee
714 km
Inclination
99.0°
Period
97.2 min
Mean Motion
14.81209408 rev/day
TLE Epoch
2026-09-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude626 km
Orbital Velocity27,173 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.81
Eccentricity0.0126
Semi-Major Axis6,997 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-03-31
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-026D
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
THOR ALTAIR DEB is a tracked piece of space debris attributed to United States, launched on 1966-03-31 from Vandenberg Space Force Base, United States on the DAPP 15 launch. After more than 60 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 537 km and 714 km with an inclination of 99.0°. It travels at approximately 27,173 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.81 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 ~10–25 years. As orbital debris, THOR ALTAIR 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
THOR ALTAIR DEB orbits at an average altitude of 626 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 THOR ALTAIR DEB’s average altitude, there are currently 1,022 active payloads and 880 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 5.5% of all active satellites. With an inclination of 99.0°, THOR ALTAIR DEB passes over latitudes between 99.0°N and 99.0°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. United States operates approximately 13,198 active satellites in total, of which 523 share a similar altitude band with THOR ALTAIR 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
THOR ALTAIR DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 626 km altitude. Its 99.0° 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 97 minutes, travelling at 27,173 km/h.
THOR ALTAIR DEB (NORAD ID 2177) is a piece of tracked orbital debris attributed to United States. 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.
THOR ALTAIR DEB was launched on 1966-03-31 from Vandenberg Space Force Base, United States, 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks THOR ALTAIR DEB (NORAD ID 2177) 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.
THOR ALTAIR DEB travels at approximately 27,173 km/h (16,884 mph) — roughly 7.55 km/s. It completes 14.81 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 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 7.55 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 THOR ALTAIR DEB. Read more about debris statistics and the Kessler syndrome.