▸Orbital parameters

Orbit class	SSO
Inclination	98.4999°
Eccentricity	0.0014054
Period	101.7 min
Apogee	850 km
Perigee	830 km
Mean motion	14.15759462 rev/day
RAAN	161.1434°
Arg of perigee	330.3197°
Mean anomaly	29.7179°
B*	5.4465e-5
Rev at epoch	66,139

▸Two-line element set (TLE)

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

1 39260U 13052A 26188.18572670 .00000066 00000-0 54465-4 0 9992

2 39260 98.4999 161.1434 0014054 330.3197 29.7179 14.15759462661394

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FENGYUN 3C",
  "OBJECT_ID": "2013-052A",
  "EPOCH": "2026-07-07T04:27:26.787+00:00",
  "MEAN_MOTION": 14.15759462,
  "ECCENTRICITY": 0.0014054,
  "INCLINATION": 98.4999,
  "RA_OF_ASC_NODE": 161.1434,
  "ARG_OF_PERICENTER": 330.3197,
  "MEAN_ANOMALY": 29.7179,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39260,
  "REV_AT_EPOCH": 66139,
  "BSTAR": 0.000054465,
  "MEAN_MOTION_DOT": 6.6e-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 3C
Operator	National Satellite Meteorological CenterHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 23, 2013HIGHvia 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/39260

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