TIANPING 3B-01
NORAD 61615
Payload
LEO
2024-189B
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LEO · NORAD 61615
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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
561 km
Apogee
566 km
Inclination
97.5°
Period
95.9 min
Mean Motion
15.00990796 rev/day
TLE Epoch
2026-09-17 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude564 km
Orbital Velocity27,294 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.01
Eccentricity0.0004
Semi-Major Axis6,935 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 ZJUNI-SAT (China)
Launch Date
2024-10-22
Launch Site
Taiyuan Satellite Launch Center, China
Int'l Designator
2024-189B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TIANPING 3B-01 is an active satellite operated by ZJUNI-SAT (China), launched on 2024-10-22 from Taiyuan Satellite Launch Center, China on the Tianping-3 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 561 km and 566 km with an inclination of 97.5°. It travels at approximately 27,294 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.01 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 TIANPING 3B-01 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TIANPING 3B-01 orbits at an average altitude of 564 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 TIANPING 3B-01’s average altitude, there are currently 1,483 active payloads and 497 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-1522, STARLINK-2112. This makes it one of the more crowded altitude bands, containing roughly 7.9% of all active satellites. With an inclination of 97.5°, TIANPING 3B-01 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. China operates approximately 1,275 active satellites in total, of which 133 share a similar altitude band with TIANPING 3B-01.
❓ Frequently Asked Questions
TIANPING 3B-01 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 564 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 27,294 km/h.
TIANPING 3B-01 is operated by ZJUNI-SAT (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 61615. You can track TIANPING 3B-01 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TIANPING 3B-01 was launched on 2024-10-22 from Taiyuan Satellite Launch Center, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks TIANPING 3B-01 (NORAD ID 61615) 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.
TIANPING 3B-01 travels at approximately 27,294 km/h (16,960 mph) — roughly 7.58 km/s. It completes 15.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.