TIGRISAT
NORAD 40043
Payload
LEO
2014-033AK
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LEO · NORAD 40043
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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
577 km
Apogee
647 km
Inclination
97.8°
Period
96.9 min
Mean Motion
14.85443852 rev/day
TLE Epoch
2026-09-18 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude612 km
Orbital Velocity27,199 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.85
Eccentricity0.0050
Semi-Major Axis6,983 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
La Sapienza University of Rome (Iraq)
Launch Date
2014-06-19
Launch Site
Yasny / Dombarovsky, Russia
Int'l Designator
2014-033AK
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TIGRISAT is an active satellite operated by La Sapienza University of Rome (Iraq), launched on 2014-06-19 from Yasny / Dombarovsky, Russia on the Dnepr Rideshare 9 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 577 km and 647 km with an inclination of 97.8°. It travels at approximately 27,199 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.85 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 ~10–25 years. Orbital Radar tracks TIGRISAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TIGRISAT orbits at an average altitude of 612 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 TIGRISAT’s average altitude, there are currently 1,594 active payloads and 767 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 8.5% of all active satellites. With an inclination of 97.8°, TIGRISAT passes over latitudes between 97.8°N and 97.8°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.
❓ Frequently Asked Questions
TIGRISAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 612 km altitude. Its 97.8° 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 97 minutes, travelling at 27,199 km/h.
TIGRISAT is operated by La Sapienza University of Rome (Iraq). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40043. You can track TIGRISAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TIGRISAT was launched on 2014-06-19 from Yasny / Dombarovsky, Russia. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks TIGRISAT (NORAD ID 40043) 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.
TIGRISAT travels at approximately 27,199 km/h (16,901 mph) — roughly 7.56 km/s. It completes 14.85 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.