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DOJO

NORAD 65302 Payload LEO 2025-185F ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
621 km
Apogee
641 km
Inclination
98.0°
Period
97.3 min
Mean Motion
14.79395693 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude631 km
Orbital Velocity27,162 km/h
Velocity7.54 km/s
Orbital Period97 minutes
Orbits / Day14.79
Eccentricity0.0014
Semi-Major Axis7,002 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
RWA
Launch Date
2025-08-23
Launch Site
RLLC
Int'l Designator
2025-185F
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DOJO is an active satellite operated by RWA, launched on 2025-08-23 from RLLC. 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 641 km with an inclination of 98.0°. It travels at approximately 27,162 km/h (7.54 km/s), completing one full orbit every 97 minutes — that’s roughly 14.79 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 ~10–25 years. Orbital Radar tracks DOJO in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
DOJO orbits at an average altitude of 631 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 DOJO’s average altitude, there are currently 790 active payloads and 843 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050. With an inclination of 98.0°, DOJO 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. RWA operates approximately 7 active satellites in total, of which 5 share a similar altitude band with DOJO.
❓ Frequently Asked Questions
DOJO is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 631 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 27,162 km/h.
DOJO is operated by RWA. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 65302. You can track DOJO in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DOJO was launched on 2025-08-23 from RLLC. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks DOJO (NORAD ID 65302) 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.
DOJO travels at approximately 27,162 km/h (16,878 mph) — roughly 7.54 km/s. It completes 14.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.