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PAKTES 1A

NORAD 43529 Payload LEO 2018-056A ● Active
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🛰️ Orbital Parameters
Perigee
551 km
Apogee
585 km
Inclination
98.2°
Period
96.0 min
Mean Motion
14.99578597 rev/day
TLE Epoch
2026-11-02 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude568 km
Orbital Velocity27,285 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.00
Eccentricity0.0024
Semi-Major Axis6,939 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Pakistan Space and Upper Atmosphere Research Commission (SUPARCO) (Pakistan)
Launch Date
2018-07-09
Launch Site
Jiuquan Satellite Launch Center, China
Int'l Designator
2018-056A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
PAKTES 1A is an active satellite operated by Pakistan Space and Upper Atmosphere Research Commission (SUPARCO) (Pakistan), launched on 2018-07-09 from Jiuquan Satellite Launch Center, China on the PRSS-1 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 551 km and 585 km with an inclination of 98.2°. It travels at approximately 27,285 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.00 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 PAKTES 1A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PAKTES 1A orbits at an average altitude of 568 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 PAKTES 1A’s average altitude, there are currently 1,085 active payloads and 526 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3055. This makes it one of the more crowded altitude bands, containing roughly 5.7% of all active satellites. With an inclination of 98.2°, PAKTES 1A passes over latitudes between 98.2°N and 98.2°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. Pakistan operates approximately 8 active satellites in total, of which 2 share a similar altitude band with PAKTES 1A.
❓ Frequently Asked Questions
PAKTES 1A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 568 km altitude. Its 98.2° 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 27,285 km/h.
PAKTES 1A is operated by Pakistan Space and Upper Atmosphere Research Commission (SUPARCO) (Pakistan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43529. You can track PAKTES 1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PAKTES 1A was launched on 2018-07-09 from Jiuquan Satellite Launch Center, 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 PAKTES 1A (NORAD ID 43529) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
PAKTES 1A travels at approximately 27,285 km/h (16,954 mph) — roughly 7.58 km/s. It completes 15.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.