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SPHEREX DEB

NORAD 63332 Debris LEO 2025-047F
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
621 km
Apogee
632 km
Inclination
98.0°
Period
97.2 min
Mean Motion
14.80959229 rev/day
TLE Epoch
2026-06-20 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude627 km
Orbital Velocity27,171 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.81
Eccentricity0.0008
Semi-Major Axis6,998 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2025-03-12
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-047F
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SPHEREX DEB is a tracked piece of space debris attributed to United States, launched on 2025-03-12 from Vandenberg SFB, California on the SPHEREx launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 621 km and 632 km with an inclination of 98.0°. It travels at approximately 27,171 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. As orbital debris, SPHEREX 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
SPHEREX DEB orbits at an average altitude of 627 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 SPHEREX DEB’s average altitude, there are currently 802 active payloads and 820 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050. With an inclination of 98.0°, SPHEREX DEB passes over latitudes between 98.0°N and 98.0°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 12,358 active satellites in total, of which 344 share a similar altitude band with SPHEREX 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
SPHEREX DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 627 km altitude. Its 98.0° 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 27,171 km/h.
SPHEREX DEB (NORAD ID 63332) 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.
SPHEREX DEB was launched on 2025-03-12 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks SPHEREX DEB (NORAD ID 63332) 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.
SPHEREX DEB travels at approximately 27,171 km/h (16,883 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 SPHEREX DEB. Read more about debris statistics and the Kessler syndrome.