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ORIGAMISAT-2

NORAD 68795 Payload LEO 2026-088D ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
529 km
Apogee
551 km
Inclination
97.5°
Period
95.4 min
Mean Motion
15.08780628 rev/day
TLE Epoch
2026-06-19 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude540 km
Orbital Velocity27,340 km/h
Velocity7.59 km/s
Orbital Period95 minutes
Orbits / Day15.09
Eccentricity0.0016
Semi-Major Axis6,911 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2026-04-23
Launch Site
RLLC
Int'l Designator
2026-088D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ORIGAMISAT-2 is an active satellite operated by Japan, launched on 2026-04-23 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 529 km and 551 km with an inclination of 97.5°. It travels at approximately 27,340 km/h (7.59 km/s), completing one full orbit every 95 minutes — that’s roughly 15.09 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 ORIGAMISAT-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
ORIGAMISAT-2 orbits at an average altitude of 540 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 ORIGAMISAT-2’s average altitude, there are currently 3,504 active payloads and 327 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 20.1% of all active satellites. With an inclination of 97.5°, ORIGAMISAT-2 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. Japan operates approximately 189 active satellites in total, of which 51 share a similar altitude band with ORIGAMISAT-2.
❓ Frequently Asked Questions
ORIGAMISAT-2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 540 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 95 minutes, travelling at 27,340 km/h.
ORIGAMISAT-2 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 68795. You can track ORIGAMISAT-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ORIGAMISAT-2 was launched on 2026-04-23 from RLLC. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks ORIGAMISAT-2 (NORAD ID 68795) 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.
ORIGAMISAT-2 travels at approximately 27,340 km/h (16,988 mph) — roughly 7.59 km/s. It completes 15.09 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.