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AISAT

NORAD 40054 Payload LEO 2014-034B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
530 km
Apogee
540 km
Inclination
98.2°
Period
95.3 min
Mean Motion
15.10419118 rev/day
TLE Epoch
2026-09-17 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude535 km
Orbital Velocity27,350 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.10
Eccentricity0.0007
Semi-Major Axis6,906 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇩🇪 DLR2 (Germany)
Launch Date
2014-06-30
Launch Site
Satish Dhawan Space Centre, India
Int'l Designator
2014-034B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
AISAT is an active satellite operated by DLR2 (Germany), launched on 2014-06-30 from Satish Dhawan Space Centre, India on the PSLV Rideshare 05 launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 530 km and 540 km with an inclination of 98.2°. It travels at approximately 27,350 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.10 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks AISAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
AISAT orbits at an average altitude of 535 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 AISAT’s average altitude, there are currently 1,774 active payloads and 344 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 9.5% of all active satellites. With an inclination of 98.2°, AISAT 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. Germany operates approximately 93 active satellites in total, of which 28 share a similar altitude band with AISAT.
❓ Frequently Asked Questions
AISAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 535 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 95 minutes, travelling at 27,350 km/h.
AISAT is operated by DLR2 (Germany). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40054. You can track AISAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AISAT was launched on 2014-06-30 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 AISAT (NORAD ID 40054) 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.
AISAT travels at approximately 27,350 km/h (16,995 mph) — roughly 7.60 km/s. It completes 15.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.