OBJECT J
NORAD 44887
Unknown
LEO
2019-093J
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LEO · NORAD 44887
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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
581 km
Apogee
601 km
Inclination
97.8°
Period
96.5 min
Mean Motion
14.92241050 rev/day
TLE Epoch
2026-06-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude591 km
Orbital Velocity27,240 km/h
Velocity7.57 km/s
Orbital Period97 minutes
Orbits / Day14.92
Eccentricity0.0014
Semi-Major Axis6,962 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Unknown
Launch Date
2019-12-20
Launch Site
Taiyuan, China
Int'l Designator
2019-093J
Object Type
Unknown
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OBJECT J (NORAD ID 44887) is a space object catalogued under Unknown, launched on 2019-12-20 from Taiyuan, China on the CBERS-4A launch. It orbits in Low Earth Orbit (LEO) at altitudes between 581 km and 601 km with an inclination of 97.8°. It travels at approximately 27,240 km/h (7.57 km/s), completing one full orbit every 97 minutes — that’s roughly 14.92 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 OBJECT J in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OBJECT J orbits at an average altitude of 591 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 OBJECT J’s average altitude, there are currently 2,128 active payloads and 601 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 12.2% of all active satellites. With an inclination of 97.8°, OBJECT J 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
OBJECT J is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 591 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 27,240 km/h.
OBJECT J was launched on 2019-12-20 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT J (NORAD ID 44887) 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.
OBJECT J travels at approximately 27,240 km/h (16,926 mph) — roughly 7.57 km/s. It completes 14.92 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.