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PETREL

NORAD 69503 Payload LEO 2026-132B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
559 km
Apogee
580 km
Inclination
97.7°
Period
96.0 min
Mean Motion
14.99250862 rev/day
TLE Epoch
2026-08-05 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude570 km
Orbital Velocity27,282 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.99
Eccentricity0.0015
Semi-Major Axis6,941 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2026-06-12
Launch Site
TNSTA
Int'l Designator
2026-132B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PETREL is an active satellite operated by Japan, launched on 2026-06-12 from TNSTA on the VEP-5 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 559 km and 580 km with an inclination of 97.7°. It travels at approximately 27,282 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.99 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 PETREL in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PETREL orbits at an average altitude of 570 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 PETREL’s average altitude, there are currently 2,160 active payloads and 481 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-1522, STARLINK-2112. This makes it one of the more crowded altitude bands, containing roughly 12.1% of all active satellites. With an inclination of 97.7°, PETREL passes over latitudes between 97.7°N and 97.7°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 200 active satellites in total, of which 51 share a similar altitude band with PETREL.
❓ Frequently Asked Questions
PETREL is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 570 km altitude. Its 97.7° 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 27,282 km/h.
PETREL is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69503. You can track PETREL in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PETREL was launched on 2026-06-12 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks PETREL (NORAD ID 69503) 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.
PETREL travels at approximately 27,282 km/h (16,952 mph) — roughly 7.58 km/s. It completes 14.99 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.