▸Orbital parameters

Orbit class	LEO
Inclination	100.7751°
Eccentricity	0.0006744
Period	109.5 min
Apogee	1,207 km
Perigee	1,197 km
Mean motion	13.15531480 rev/day
RAAN	339.5625°
Arg of perigee	142.3559°
Mean anomaly	217.8025°
B*	2.5509e-5
Rev at epoch	56,241

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 40275U 14063A 26187.95896034 -.00000037 00000-0 25509-4 0 9996

2 40275 100.7751 339.5625 0006744 142.3559 217.8025 13.15531480562418

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-22",
  "OBJECT_ID": "2014-063A",
  "EPOCH": "2026-07-06T23:00:54.173+00:00",
  "MEAN_MOTION": 13.1553148,
  "ECCENTRICITY": 0.0006744,
  "INCLINATION": 100.7751,
  "RA_OF_ASC_NODE": 339.5625,
  "ARG_OF_PERICENTER": 142.3559,
  "MEAN_ANOMALY": 217.8025,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40275,
  "REV_AT_EPOCH": 56241,
  "BSTAR": 0.000025509,
  "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-22
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Oct 20, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1040HIGHvia 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/40275

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