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NEE 01 PEGASUS

NORAD 39151 Payload LEO 2013-018B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
577 km
Apogee
596 km
Inclination
98.1°
Period
96.4 min
Mean Motion
14.93668156 rev/day
TLE Epoch
2026-06-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude587 km
Orbital Velocity27,249 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.94
Eccentricity0.0014
Semi-Major Axis6,958 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Ecuador
Launch Date
2013-04-26
Launch Site
Jiuquan, China
Int'l Designator
2013-018B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
NEE 01 PEGASUS is an active satellite operated by Ecuador, launched on 2013-04-26 from Jiuquan, China. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 577 km and 596 km with an inclination of 98.1°. It travels at approximately 27,249 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.94 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 NEE 01 PEGASUS in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
NEE 01 PEGASUS orbits at an average altitude of 587 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 NEE 01 PEGASUS’s average altitude, there are currently 3,232 active payloads and 591 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 18.6% of all active satellites. With an inclination of 98.1°, NEE 01 PEGASUS passes over latitudes between 98.1°N and 98.1°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. Ecuador operates approximately 2 active satellites in total, of which 2 share a similar altitude band with NEE 01 PEGASUS.
❓ Frequently Asked Questions
NEE 01 PEGASUS is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 587 km altitude. Its 98.1° 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 27,249 km/h.
NEE 01 PEGASUS is operated by Ecuador. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39151. You can track NEE 01 PEGASUS in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
NEE 01 PEGASUS was launched on 2013-04-26 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks NEE 01 PEGASUS (NORAD ID 39151) 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.
NEE 01 PEGASUS travels at approximately 27,249 km/h (16,932 mph) — roughly 7.57 km/s. It completes 14.94 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.