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TIROS 2 DEB *

NORAD 5922 Debris LEO 1960-016E
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🛰️ Orbital Parameters
Perigee
969 km
Apogee
1029 km
Inclination
47.0°
Period
105.1 min
Mean Motion
13.70080229 rev/day
TLE Epoch
2026-11-02 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude999 km
Orbital Velocity26,475 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.70
Eccentricity0.0041
Semi-Major Axis7,370 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1960-11-23
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1960-016E
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TIROS 2 DEB * is a tracked piece of space debris attributed to United States, launched on 1960-11-23 from Cape Canaveral Space Force Station, United States. After more than 66 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 969 km and 1,029 km with an inclination of 47.0°. It travels at approximately 26,475 km/h (7.35 km/s), completing one full orbit every 105 minutes — that’s roughly 13.70 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, TIROS 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
TIROS 2 DEB * orbits at an average altitude of 999 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of TIROS 2 DEB *’s average altitude, there are currently 334 active payloads and 1,080 tracked debris or rocket body fragments. With an inclination of 47.0°, TIROS 2 DEB * passes over latitudes between 47.0°N and 47.0°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 13,342 active satellites in total, of which 79 share a similar altitude band with TIROS 2 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
TIROS 2 DEB * orbits in Low Earth Orbit (LEO) at altitudes between 969 km (perigee) and 1,029 km (apogee), with an average altitude of approximately 999 km. It completes one orbit every 105 minutes, travelling at approximately 26,475 km/h (16,451 mph).
TIROS 2 DEB * (NORAD ID 5922) 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.
TIROS 2 DEB * was launched on 1960-11-23 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks TIROS 2 DEB * (NORAD ID 5922) 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.
TIROS 2 DEB * travels at approximately 26,475 km/h (16,451 mph) — roughly 7.35 km/s. It completes 13.70 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.35 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 TIROS 2 DEB *. Read more about debris statistics and the Kessler syndrome.