OBJECT A
NORAD 69472
Unknown
LEO
2026-128A
CONNECTING…
LEO · NORAD 69472
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
402 km
Apogee
416 km
Inclination
55.0°
Period
92.7 min
Mean Motion
15.52805922 rev/day
TLE Epoch
2026-10-19 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude409 km
Orbital Velocity27,603 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.53
Eccentricity0.0010
Semi-Major Axis6,780 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Yuanxin (Qianfan) (China)
Launch Date
2026-06-09
Launch Site
Jiuquan Satellite Launch Center, China
Int'l Designator
2026-128A
Object Type
Unknown
RCS Size
Large (>1 m²)
📖 About This Object
OBJECT A (NORAD ID 69472) is a space object catalogued under China, launched on 2026-06-09 from Jiuquan Satellite Launch Center, China on the Qianfan DTC1 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. Independent catalogue analysis identifies this object as Qianfan DTC 01, attributed to Yuanxin (Qianfan). It orbits in Low Earth Orbit (LEO) at altitudes between 402 km and 416 km with an inclination of 55.0°. It travels at approximately 27,603 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.53 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 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 409 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of OBJECT A’s average altitude, there are currently 1,000 active payloads and 96 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1008, STARLINK-1012. This makes it one of the more crowded altitude bands, containing roughly 5.3% of all active satellites. With an inclination of 55.0°, OBJECT A passes over latitudes between 55.0°N and 55.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,330 active satellites in total, of which 52 share a similar altitude band with OBJECT A.
❓ Frequently Asked Questions
OBJECT A orbits in Low Earth Orbit (LEO) at altitudes between 402 km (perigee) and 416 km (apogee), with an average altitude of approximately 409 km. It completes one orbit every 93 minutes, travelling at approximately 27,603 km/h (17,152 mph).
OBJECT A was launched on 2026-06-09 from Jiuquan Satellite Launch Center, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks OBJECT A (NORAD ID 69472) 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 27,603 km/h (17,152 mph) — roughly 7.67 km/s. It completes 15.53 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.