▸Orbital parameters

Orbit class	SSO
Inclination	98.6885°
Eccentricity	0.0009864
Period	101.4 min
Apogee	834 km
Perigee	820 km
Mean motion	14.19575331 rev/day
RAAN	128.3188°
Arg of perigee	73.3980°
Mean anomaly	286.8279°
B*	5.3635e-5
Rev at epoch	93,819

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 32958U 08026A 26187.85317918 .00000070 00000-0 53635-4 0 9992

2 32958 98.6885 128.3188 0009864 73.3980 286.8279 14.19575331938192

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FENGYUN 3A",
  "OBJECT_ID": "2008-026A",
  "EPOCH": "2026-07-06T20:28:34.681+00:00",
  "MEAN_MOTION": 14.19575331,
  "ECCENTRICITY": 0.0009864,
  "INCLINATION": 98.6885,
  "RA_OF_ASC_NODE": 128.3188,
  "ARG_OF_PERICENTER": 73.398,
  "MEAN_ANOMALY": 286.8279,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 32958,
  "REV_AT_EPOCH": 93819,
  "BSTAR": 0.000053635,
  "MEAN_MOTION_DOT": 7e-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 3A
Operator	National Satellite Meteorological CenterHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 27, 2008HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2200HIGHvia 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/32958

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