▸Orbital parameters

Orbit class	SSO
Inclination	98.7499°
Eccentricity	0.0002555
Period	101.4 min
Apogee	828 km
Perigee	824 km
Mean motion	14.19905767 rev/day
RAAN	191.3295°
Arg of perigee	53.1089°
Mean anomaly	307.0322°
B*	6.1979e-5
Rev at epoch	25,941

▸Two-line element set (TLE)

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

1 49008U 21062A 26188.14382683 .00000088 00000-0 61979-4 0 9994

2 49008 98.7499 191.3295 0002555 53.1089 307.0322 14.19905767259419

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FENGYUN 3E",
  "OBJECT_ID": "2021-062A",
  "EPOCH": "2026-07-07T03:27:06.638+00:00",
  "MEAN_MOTION": 14.19905767,
  "ECCENTRICITY": 0.0002555,
  "INCLINATION": 98.7499,
  "RA_OF_ASC_NODE": 191.3295,
  "ARG_OF_PERICENTER": 53.1089,
  "MEAN_ANOMALY": 307.0322,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 49008,
  "REV_AT_EPOCH": 25941,
  "BSTAR": 0.000061979,
  "MEAN_MOTION_DOT": 8.8e-7,
  "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 3E
Operator	National Satellite Meteorological CenterHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jul 4, 2021HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2450HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/49008

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