▸Orbital parameters

Orbit class	LEO
Inclination	63.3863°
Eccentricity	0.0368608
Period	107.0 min
Apogee	1,365 km
Perigee	814 km
Mean motion	13.45349880 rev/day
RAAN	259.7190°
Arg of perigee	9.7128°
Mean anomaly	351.0775°
B*	5.9842e-5
Rev at epoch	56,844

▸Two-line element set (TLE)

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

1 40340U 14080C 26188.20587226 -.00000037 00000-0 59842-4 0 9994

2 40340 63.3863 259.7190 0368608 9.7128 351.0775 13.45349880568443

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-25 01C",
  "OBJECT_ID": "2014-080C",
  "EPOCH": "2026-07-07T04:56:27.363+00:00",
  "MEAN_MOTION": 13.4534988,
  "ECCENTRICITY": 0.0368608,
  "INCLINATION": 63.3863,
  "RA_OF_ASC_NODE": 259.719,
  "ARG_OF_PERICENTER": 9.7128,
  "MEAN_ANOMALY": 351.0775,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40340,
  "REV_AT_EPOCH": 56844,
  "BSTAR": 0.000059842,
  "MEAN_MOTION_DOT": -3.7e-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	YAOGAN-25 01C
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/40340

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