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DELTA 1 DEB *

NORAD 5987 Debris MEO 1967-001S
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
472 km
Apogee
28367 km
Inclination
26.5°
Period
497.5 min
Mean Motion
2.89450811 rev/day
TLE Epoch
2026-09-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude14,420 km
Orbital Velocity15,763 km/h
Velocity4.38 km/s
Orbital Period8 hours 17 minutes
Orbits / Day2.89
Eccentricity0.6709
Semi-Major Axis20,791 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1967-01-11
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1967-001S
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DELTA 1 DEB * is a tracked piece of space debris attributed to United States, launched on 1967-01-11 from Cape Canaveral Space Force Station, United States on the INTELSAT II F-2 launch. After more than 59 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 472 km and 28,367 km with an inclination of 26.5°. It travels at approximately 15,763 km/h (4.38 km/s), completing one full orbit every 8 hours 17 minutes — that’s roughly 2.89 orbits per day. Its orbital eccentricity of 0.6709 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, DELTA 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
DELTA 1 DEB * orbits at an average altitude of 14,420 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 DELTA 1 DEB *’s average altitude, there are currently 0 active payloads and 7 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 26.5°, DELTA 1 DEB * passes over latitudes between 26.5°N and 26.5°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 13,199 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
DELTA 1 DEB * orbits in Medium Earth Orbit (MEO) at altitudes between 472 km (perigee) and 28,367 km (apogee), with an average altitude of approximately 14,420 km. It completes one orbit every 8 hours 17 minutes, travelling at approximately 15,763 km/h (9,795 mph).
DELTA 1 DEB * (NORAD ID 5987) 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.
DELTA 1 DEB * was launched on 1967-01-11 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB * (NORAD ID 5987) 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.
DELTA 1 DEB * travels at approximately 15,763 km/h (9,795 mph) — roughly 4.38 km/s. It completes 2.89 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 6 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 4.38 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 DELTA 1 DEB *. Read more about debris statistics and the Kessler syndrome.