STUDSAT
NORAD 36796
Payload
LEO
2010-035B
● Active
CONNECTING…
LEO · NORAD 36796
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
541 km
Apogee
559 km
Inclination
98.1°
Period
95.7 min
Mean Motion
15.05517918 rev/day
TLE Epoch
2026-09-17 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude550 km
Orbital Velocity27,320 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.06
Eccentricity0.0013
Semi-Major Axis6,921 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇮🇳 NMIT Bangalore (India)
Launch Date
2010-07-12
Launch Site
Satish Dhawan Space Centre, India
Int'l Designator
2010-035B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
STUDSAT is an active satellite operated by NMIT Bangalore (India), launched on 2010-07-12 from Satish Dhawan Space Centre, India on the PSLV Rideshare 03 launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 541 km and 559 km with an inclination of 98.1°. It travels at approximately 27,320 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.06 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 STUDSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
STUDSAT orbits at an average altitude of 550 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 STUDSAT’s average altitude, there are currently 1,733 active payloads and 403 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 9.3% of all active satellites. With an inclination of 98.1°, STUDSAT 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. India operates approximately 109 active satellites in total, of which 19 share a similar altitude band with STUDSAT.
❓ Frequently Asked Questions
STUDSAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 550 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 27,320 km/h.
STUDSAT is operated by NMIT Bangalore (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 36796. You can track STUDSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
STUDSAT was launched on 2010-07-12 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 STUDSAT (NORAD ID 36796) 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.
STUDSAT travels at approximately 27,320 km/h (16,976 mph) — roughly 7.59 km/s. It completes 15.06 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.