R5-S10
NORAD 100801
Payload
LEO
2026-067DA
● Active
CONNECTING…
LEO · NORAD 100801
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
486 km
Apogee
501 km
Inclination
97.5°
Period
94.5 min
Mean Motion
15.24105865 rev/day
TLE Epoch
2026-09-24 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude494 km
Orbital Velocity27,433 km/h
Velocity7.62 km/s
Orbital Period94 minutes
Orbits / Day15.24
Eccentricity0.0011
Semi-Major Axis6,865 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-03-30
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2026-067DA
Object Type
Payload
RCS Size
Unknown
📖 About This Object
R5-S10 is an active satellite operated by United States, launched on 2026-03-30 from Vandenberg Space Force Base, United States on the Transporter-16 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 486 km and 501 km with an inclination of 97.5°. It travels at approximately 27,433 km/h (7.62 km/s), completing one full orbit every 94 minutes — that’s roughly 15.24 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 ~1–3 years. Orbital Radar tracks R5-S10 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
R5-S10 orbits at an average altitude of 494 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 R5-S10’s average altitude, there are currently 10,458 active payloads and 216 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 55.8% of all active satellites. With an inclination of 97.5°, R5-S10 passes over latitudes between 97.5°N and 97.5°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 13,219 active satellites in total, of which 9,833 share a similar altitude band with R5-S10.
❓ Frequently Asked Questions
R5-S10 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 494 km altitude. Its 97.5° 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 94 minutes, travelling at 27,433 km/h.
R5-S10 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 100801. You can track R5-S10 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
R5-S10 was launched on 2026-03-30 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks R5-S10 (NORAD ID 100801) 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.
R5-S10 travels at approximately 27,433 km/h (17,046 mph) — roughly 7.62 km/s. It completes 15.24 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.