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OBJECT A

NORAD 100702 Unknown LEO 2026-211A
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🛰️ Orbital Parameters
Perigee
804 km
Apogee
807 km
Inclination
89.0°
Period
101.0 min
Mean Motion
14.25855103 rev/day
TLE Epoch
2026-10-22 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude806 km
Orbital Velocity26,830 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.26
Eccentricity0.0002
Semi-Major Axis7,177 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Yuanxin (Qianfan) (China)
Launch Date
2026-09-15
Launch Site
Yellow Sea launch area (Haiyang), China
Int'l Designator
2026-211A
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT A (NORAD ID 100702) is a space object catalogued under China, launched on 2026-09-15 from Yellow Sea launch area (Haiyang), China on the Qianfan Digui 26 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. Independent catalogue analysis identifies this object as Qianfan Jigui 26-01, attributed to Yuanxin (Qianfan). It orbits in Low Earth Orbit (LEO) at altitudes between 804 km and 807 km with an inclination of 89.0°. It travels at approximately 26,830 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.26 orbits per day. 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 ~100–500 years. Orbital Radar tracks OBJECT A 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 A orbits at an average altitude of 806 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of OBJECT A’s average altitude, there are currently 461 active payloads and 2,536 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 89.0°, OBJECT A passes over latitudes between 89.0°N and 89.0°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 1,340 active satellites in total, of which 77 share a similar altitude band with OBJECT A.
❓ Frequently Asked Questions
OBJECT A orbits in Low Earth Orbit (LEO) at altitudes between 804 km (perigee) and 807 km (apogee), with an average altitude of approximately 806 km. It completes one orbit every 101 minutes, travelling at approximately 26,830 km/h (16,671 mph).
OBJECT A was launched on 2026-09-15 from Yellow Sea launch area (Haiyang), China. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT A (NORAD ID 100702) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 A travels at approximately 26,830 km/h (16,671 mph) — roughly 7.45 km/s. It completes 14.26 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.