▸Orbital parameters

Orbit class	SSO
Inclination	98.1519°
Eccentricity	0.0013952
Period	97.6 min
Apogee	651 km
Perigee	632 km
Mean motion	14.76112428 rev/day
RAAN	325.7220°
Arg of perigee	195.5480°
Mean anomaly	164.5302°
B*	1.2670e-4
Rev at epoch	62,667

▸Two-line element set (TLE)

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

1 40310U 14072A 26188.21411899 .00000823 00000-0 12670-3 0 9994

2 40310 98.1519 325.7220 0013952 195.5480 164.5302 14.76112428626670

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-24",
  "OBJECT_ID": "2014-072A",
  "EPOCH": "2026-07-07T05:08:19.881+00:00",
  "MEAN_MOTION": 14.76112428,
  "ECCENTRICITY": 0.0013952,
  "INCLINATION": 98.1519,
  "RA_OF_ASC_NODE": 325.722,
  "ARG_OF_PERICENTER": 195.548,
  "MEAN_ANOMALY": 164.5302,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40310,
  "REV_AT_EPOCH": 62667,
  "BSTAR": 0.0001267,
  "MEAN_MOTION_DOT": 0.00000823,
  "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-24
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 20, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	800HIGHvia 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/40310

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