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OBJECT R

NORAD 59066 Unknown LEO 2024-039R
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
487 km
Apogee
687 km
Inclination
95.4°
Period
96.4 min
Mean Motion
14.93530733 rev/day
TLE Epoch
2026-06-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude587 km
Orbital Velocity27,248 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.94
Eccentricity0.0144
Semi-Major Axis6,958 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Unknown
Launch Date
2024-02-29
Launch Site
Vostochny, Russia
Int'l Designator
2024-039R
Object Type
Unknown
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OBJECT R (NORAD ID 59066) is a space object catalogued under Unknown, launched on 2024-02-29 from Vostochny, Russia on the Soyuz Rideshare 12 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 487 km and 687 km with an inclination of 95.4°. It travels at approximately 27,248 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.94 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks OBJECT R in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OBJECT R orbits at an average altitude of 587 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 OBJECT R’s average altitude, there are currently 3,187 active payloads and 584 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 18.3% of all active satellites. With an inclination of 95.4°, OBJECT R passes over latitudes between 95.4°N and 95.4°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.
❓ Frequently Asked Questions
OBJECT R orbits in Low Earth Orbit (LEO) at altitudes between 487 km (perigee) and 687 km (apogee), with an average altitude of approximately 587 km. It completes one orbit every 96 minutes, travelling at approximately 27,248 km/h (16,931 mph).
OBJECT R was launched on 2024-02-29 from Vostochny, Russia. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT R (NORAD ID 59066) 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.
OBJECT R travels at approximately 27,248 km/h (16,931 mph) — roughly 7.57 km/s. It completes 14.94 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.