▸Orbital parameters

Orbit class	GEO
Inclination	2.3699°
Eccentricity	0.0008127
Period	1436.1 min
Apogee	35,820 km
Perigee	35,752 km
Mean motion	1.00273257 rev/day
RAAN	80.0689°
Arg of perigee	157.8567°
Mean anomaly	218.8708°
B*	0.0000e+0
Rev at epoch	3,513

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 41882U 16077A 26188.13308638 -.00000343 00000-0 00000-0 0 9992

2 41882 2.3699 80.0689 0008127 157.8567 218.8708 1.00273257 35135

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FENGYUN 4A",
  "OBJECT_ID": "2016-077A",
  "EPOCH": "2026-07-07T03:11:38.663+00:00",
  "MEAN_MOTION": 1.00273257,
  "ECCENTRICITY": 0.0008127,
  "INCLINATION": 2.3699,
  "RA_OF_ASC_NODE": 80.0689,
  "ARG_OF_PERICENTER": 157.8567,
  "MEAN_ANOMALY": 218.8708,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41882,
  "REV_AT_EPOCH": 3513,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000343,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	FENGYUN 4A
Operator	National Satellite Meteorological CenterHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	People's Republic of ChinaMEDIUMvia Wikidata
Launch date	Dec 10, 2016HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5380HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/41882

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.