▸Orbital parameters

Orbit class	LEO
Inclination	34.9770°
Eccentricity	0.0003752
Period	93.5 min
Apogee	450 km
Perigee	445 km
Mean motion	15.39648185 rev/day
RAAN	180.1984°
Arg of perigee	343.5737°
Mean anomaly	16.4860°
B*	2.2094e-4
Rev at epoch	21,395

▸Two-line element set (TLE)

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

1 53761U 22109B 26188.19578013 .00008930 00000-0 22094-3 0 9995

2 53761 34.9770 180.1984 0003752 343.5737 16.4860 15.39648185213959

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-35 05B",
  "OBJECT_ID": "2022-109B",
  "EPOCH": "2026-07-07T04:41:55.403+00:00",
  "MEAN_MOTION": 15.39648185,
  "ECCENTRICITY": 0.0003752,
  "INCLINATION": 34.977,
  "RA_OF_ASC_NODE": 180.1984,
  "ARG_OF_PERICENTER": 343.5737,
  "MEAN_ANOMALY": 16.486,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53761,
  "REV_AT_EPOCH": 21395,
  "BSTAR": 0.00022094,
  "MEAN_MOTION_DOT": 0.0000893,
  "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-35 05B
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 6, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	300HIGHvia 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/53761

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