▸Orbital parameters

Orbit class	SSO
Inclination	97.0645°
Eccentricity	0.0003168
Period	93.0 min
Apogee	424 km
Perigee	420 km
Mean motion	15.48210659 rev/day
RAAN	187.9269°
Arg of perigee	18.5233°
Mean anomaly	341.6133°
B*	4.4770e-4
Rev at epoch	64,079

▸Two-line element set (TLE)

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

1 40362U 14088A 26188.17585659 .00023521 00000-0 44770-3 0 9995

2 40362 97.0645 187.9269 0003168 18.5233 341.6133 15.48210659640798

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-26",
  "OBJECT_ID": "2014-088A",
  "EPOCH": "2026-07-07T04:13:14.009+00:00",
  "MEAN_MOTION": 15.48210659,
  "ECCENTRICITY": 0.0003168,
  "INCLINATION": 97.0645,
  "RA_OF_ASC_NODE": 187.9269,
  "ARG_OF_PERICENTER": 18.5233,
  "MEAN_ANOMALY": 341.6133,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40362,
  "REV_AT_EPOCH": 64079,
  "BSTAR": 0.0004477,
  "MEAN_MOTION_DOT": 0.00023521,
  "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-26
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 27, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3000HIGHvia 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/40362

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