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SPACEMOBILE-SSR02 DEB

NORAD 62370 Debris LEO 2024-163G
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
434 km
Apogee
441 km
Inclination
52.9°
Period
93.3 min
Mean Motion
15.42969574 rev/day
TLE Epoch
2026-06-20 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude438 km
Orbital Velocity27,545 km/h
Velocity7.65 km/s
Orbital Period93 minutes
Orbits / Day15.43
Eccentricity0.0005
Semi-Major Axis6,809 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2024-09-12
Launch Site
Cape Canaveral, Florida
Int'l Designator
2024-163G
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
SPACEMOBILE-SSR02 DEB is a tracked piece of space debris attributed to United States, launched on 2024-09-12 from Cape Canaveral, Florida on the BlueBird 1-1 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 434 km and 441 km with an inclination of 52.9°. It travels at approximately 27,545 km/h (7.65 km/s), completing one full orbit every 93 minutes — that’s roughly 15.43 orbits per day. 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 ~1–3 years. As orbital debris, SPACEMOBILE-SSR02 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
SPACEMOBILE-SSR02 DEB orbits at an average altitude of 438 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of SPACEMOBILE-SSR02 DEB’s average altitude, there are currently 7,625 active payloads and 145 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 43.7% of all active satellites. With an inclination of 52.9°, SPACEMOBILE-SSR02 DEB passes over latitudes between 52.9°N and 52.9°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,358 active satellites in total, of which 7,339 share a similar altitude band with SPACEMOBILE-SSR02 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
SPACEMOBILE-SSR02 DEB orbits in Low Earth Orbit (LEO) at altitudes between 434 km (perigee) and 441 km (apogee), with an average altitude of approximately 438 km. It completes one orbit every 93 minutes, travelling at approximately 27,545 km/h (17,116 mph).
SPACEMOBILE-SSR02 DEB (NORAD ID 62370) 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.
SPACEMOBILE-SSR02 DEB was launched on 2024-09-12 from Cape Canaveral, Florida, 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks SPACEMOBILE-SSR02 DEB (NORAD ID 62370) 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.
SPACEMOBILE-SSR02 DEB travels at approximately 27,545 km/h (17,116 mph) — roughly 7.65 km/s. It completes 15.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 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 7.65 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 SPACEMOBILE-SSR02 DEB. Read more about debris statistics and the Kessler syndrome.