RROCI-2
NORAD 59106
Payload
LEO
2024-043J
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LEO · NORAD 59106
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
555 km
Apogee
577 km
Inclination
97.8°
Period
96.0 min
Mean Motion
15.00252241 rev/day
TLE Epoch
2026-09-18 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude566 km
Orbital Velocity27,289 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.00
Eccentricity0.0016
Semi-Major Axis6,937 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 USSF SSC / Orion Space Sol. (United States)
Launch Date
2024-03-04
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2024-043J
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
RROCI-2 is an active satellite operated by USSF SSC / Orion Space Sol. (United States), launched on 2024-03-04 from Vandenberg Space Force Base, United States on the Transporter-10 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 555 km and 577 km with an inclination of 97.8°. It travels at approximately 27,289 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.00 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks RROCI-2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
RROCI-2 orbits at an average altitude of 566 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 RROCI-2’s average altitude, there are currently 1,490 active payloads and 507 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-2112, STARLINK-2722. This makes it one of the more crowded altitude bands, containing roughly 8% of all active satellites. With an inclination of 97.8°, RROCI-2 passes over latitudes between 97.8°N and 97.8°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 13,204 active satellites in total, of which 935 share a similar altitude band with RROCI-2.
❓ Frequently Asked Questions
RROCI-2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 566 km altitude. Its 97.8° 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 96 minutes, travelling at 27,289 km/h.
RROCI-2 is operated by USSF SSC / Orion Space Sol. (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59106. You can track RROCI-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
RROCI-2 was launched on 2024-03-04 from Vandenberg Space Force Base, United States, 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks RROCI-2 (NORAD ID 59106) 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.
RROCI-2 travels at approximately 27,289 km/h (16,957 mph) — roughly 7.58 km/s. It completes 15.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.