▸Orbital parameters

Orbit class	SSO
Inclination	99.0142°
Eccentricity	0.0001977
Period	101.4 min
Apogee	828 km
Perigee	825 km
Mean motion	14.19743400 rev/day
RAAN	163.0182°
Arg of perigee	29.6498°
Mean anomaly	330.4789°
B*	3.6062e-5
Rev at epoch	44,783

▸Two-line element set (TLE)

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

1 43010U 17072A 26188.23264601 .00000030 00000-0 36062-4 0 9998

2 43010 99.0142 163.0182 0001977 29.6498 330.4789 14.19743400447831

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FENGYUN 3D",
  "OBJECT_ID": "2017-072A",
  "EPOCH": "2026-07-07T05:35:00.615+00:00",
  "MEAN_MOTION": 14.197434,
  "ECCENTRICITY": 0.0001977,
  "INCLINATION": 99.0142,
  "RA_OF_ASC_NODE": 163.0182,
  "ARG_OF_PERICENTER": 29.6498,
  "MEAN_ANOMALY": 330.4789,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43010,
  "REV_AT_EPOCH": 44783,
  "BSTAR": 0.000036062,
  "MEAN_MOTION_DOT": 3e-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 3D
Operator	National Satellite Meteorological CenterHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	People's Republic of ChinaMEDIUMvia Wikidata
Launch date	Nov 14, 2017HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2450HIGHvia 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/43010

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