SSTL S1-4
NORAD 43618
Payload
LEO
2018-071A
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
560 km
Apogee
577 km
Inclination
97.5°
Period
96.0 min
Mean Motion
14.99487944 rev/day
TLE Epoch
2026-11-02 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude569 km
Orbital Velocity27,284 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.99
Eccentricity0.0012
Semi-Major Axis6,940 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇬🇧 Surrey Satellite Technology Ltd. (United Kingdom)
Launch Date
2018-09-16
Launch Site
Satish Dhawan Space Centre, India
Int'l Designator
2018-071A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SSTL S1-4 is an active satellite operated by Surrey Satellite Technology Ltd. (United Kingdom), launched on 2018-09-16 from Satish Dhawan Space Centre, India on the PSLV Rideshare 12 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 560 km and 577 km with an inclination of 97.5°. It travels at approximately 27,284 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 SSTL S1-4 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SSTL S1-4 orbits at an average altitude of 569 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 SSTL S1-4’s average altitude, there are currently 1,094 active payloads and 529 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 5.8% of all active satellites. With an inclination of 97.5°, SSTL S1-4 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. United Kingdom operates approximately 725 active satellites in total, of which 20 share a similar altitude band with SSTL S1-4.
❓ Frequently Asked Questions
SSTL S1-4 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 569 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 96 minutes, travelling at 27,284 km/h.
SSTL S1-4 is operated by Surrey Satellite Technology Ltd. (United Kingdom). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43618. You can track SSTL S1-4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SSTL S1-4 was launched on 2018-09-16 from Satish Dhawan Space Centre, India, India’s primary launch facility on a barrier island off the coast of Andhra Pradesh. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks SSTL S1-4 (NORAD ID 43618) 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.
SSTL S1-4 travels at approximately 27,284 km/h (16,953 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.