▸Orbital parameters

Orbit class	LEO
Inclination	63.3870°
Eccentricity	0.0368376
Period	107.0 min
Apogee	1,364 km
Perigee	814 km
Mean motion	13.45413886 rev/day
RAAN	259.2177°
Arg of perigee	9.2425°
Mean anomaly	351.5141°
B*	7.5095e-5
Rev at epoch	56,835

▸Two-line element set (TLE)

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

1 40338U 14080A 26188.20079295 -.00000024 00000-0 75095-4 0 9997

2 40338 63.3870 259.2177 0368376 9.2425 351.5141 13.45413886568355

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-25 01A",
  "OBJECT_ID": "2014-080A",
  "EPOCH": "2026-07-07T04:49:08.511+00:00",
  "MEAN_MOTION": 13.45413886,
  "ECCENTRICITY": 0.0368376,
  "INCLINATION": 63.387,
  "RA_OF_ASC_NODE": 259.2177,
  "ARG_OF_PERICENTER": 9.2425,
  "MEAN_ANOMALY": 351.5141,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40338,
  "REV_AT_EPOCH": 56835,
  "BSTAR": 0.000075095,
  "MEAN_MOTION_DOT": -2.4e-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	YAOGAN-25 01A
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 10, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	500HIGHvia 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/40338

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