FENGYUN 1A
Country: China, People's Republic of
Live Position
Ground Track · Last 90 Minutes
Upcoming Passes · Over Your Location
About This Satellite
FENGYUN 1A is listed as a payload under NORAD ID 19467 with international designator 1988-080A. According to the GCAT master catalog, it was built by Shanghai Inst. of Satellite Engineering (509 Res.Inst.), on the FY-1 platform, with a catalog mass of 757 kg, with a shape described as Box + 2 Pan. It is associated with China, People's Republic of. In the historical build snapshot (TLE epoch 2026-09-05), its LEO orbit had an apogee of about 892 km and a perigee near 871 km, with an inclination of 99.02° and a period of roughly 102.6 minutes; at apogee its speed was about 7.40 km/s. It was launched on 1988-09-06. The build snapshot uses a TLE with epoch 2026-09-05. A moving map, when available, is a prediction rather than a direct measurement.
What this identity tells us
The payload classification comes from GCAT record S19467. A catalog identifier follows a tracked physical object, not necessarily an active service. Manufacturer and owner entries describe catalog associations; ownership is not interchangeable with present-day operation. A separately sourced mission history has not yet been verified for this record.
Reading this orbital snapshot
Based on TLE epoch: 2026-09-05. Estimated altitude ranges from 871 km at perigee to 892 km at apogee, a difference of 22 km. The orbital period is about 102.6 minutes. Eccentricity 0.00151 indicates a nearly circular path. In a two-body approximation, perigee speed is 1.00 times apogee speed. These are mean-element estimates, not instantaneous measurements. Distance per orbit uses an ellipse approximation.
Saved build snapshot. If a valid TLE is retrieved, this explanation and the orbit panel update together. Otherwise this dated snapshot is retained.
Ground track is not sensor coverage
An inclination of 99.02 degrees implies approximate geocentric ground-track limits of 81.0 degrees north and south. This is a retrograde orbit, moving against the direction of Earth rotation. The plotted line marks the point beneath the object. It does not represent camera coverage, radio reception, or a guaranteed visible pass.
Accuracy and missing information
The introductory record describes the build snapshot. The orbital snapshot explanation and orbit panel share any successfully retrieved TLE; check the displayed epoch. Reentered objects retain historical data only. Mission history is not rewritten by TLE updates. TLE/SGP4 positions are predictions and can change after maneuvers or updated observations. The 14-day stale-data cutoff is a display safeguard, not an accuracy guarantee. Local passes are geometric predictions, not a visibility forecast. No verified operator or mission status means unknown, not active. Do not use this catalog for collision avoidance or operational flight decisions.
Catalog sources: CelesTrak SATCAT: NORAD 19467 · GCAT: S19467 (source update 2026 Sep 4 2345:57). Supplementary metadata: SatNOGS DB, retrieved 2026-09-05T12:57:25.375Z. Page assembled 2026-09-15. GCAT phase codes describe trajectory phases, not mission health.
Learn more: TLE data · Perigee and apogee · Ground tracks · JOT (Jewawud Live Orbital Map)