Skip to content
Home Library Satellite Directory HJ-1A

HJ-1A

NORAD 33320 Payload LEO 2008-041A ● Active
CONNECTING… LEO · NORAD 33320
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
603 km
Apogee
631 km
Inclination
97.7°
Period
97.0 min
Mean Motion
14.83992801 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude617 km
Orbital Velocity27,189 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.84
Eccentricity0.0020
Semi-Major Axis6,988 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 National Remote Sensing Center (NRSCC) (China)
Launch Date
2008-09-06
Launch Site
Taiyuan, China
Int'l Designator
2008-041A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
HJ-1A is an active satellite operated by National Remote Sensing Center (NRSCC) (China), launched on 2008-09-06 from Taiyuan, China. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 603 km and 631 km with an inclination of 97.7°. It travels at approximately 27,189 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.84 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 HJ-1A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HJ-1A orbits at an average altitude of 617 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 HJ-1A’s average altitude, there are currently 1,555 active payloads and 745 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3090, STARLINK-3077. This makes it one of the more crowded altitude bands, containing roughly 8.9% of all active satellites. With an inclination of 97.7°, HJ-1A passes over latitudes between 97.7°N and 97.7°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 1,218 active satellites in total, of which 135 share a similar altitude band with HJ-1A.
❓ Frequently Asked Questions
HJ-1A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 617 km altitude. Its 97.7° 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 27,189 km/h.
HJ-1A is operated by National Remote Sensing Center (NRSCC) (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33320. You can track HJ-1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HJ-1A was launched on 2008-09-06 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks HJ-1A (NORAD ID 33320) 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.
HJ-1A travels at approximately 27,189 km/h (16,895 mph) — roughly 7.55 km/s. It completes 14.84 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.