▸Orbital parameters

Orbit class	LEO
Inclination	35.0057°
Eccentricity	0.0002880
Period	94.6 min
Apogee	499 km
Perigee	495 km
Mean motion	15.22984060 rev/day
RAAN	213.1795°
Arg of perigee	197.1343°
Mean anomaly	162.9275°
B*	2.1410e-4
Rev at epoch	21,366

▸Two-line element set (TLE)

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

1 53760U 22109A 26188.18449417 .00005122 00000-0 21410-3 0 9999

2 53760 35.0057 213.1795 0002880 197.1343 162.9275 15.22984060213664

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-35 05A",
  "OBJECT_ID": "2022-109A",
  "EPOCH": "2026-07-07T04:25:40.296+00:00",
  "MEAN_MOTION": 15.2298406,
  "ECCENTRICITY": 0.000288,
  "INCLINATION": 35.0057,
  "RA_OF_ASC_NODE": 213.1795,
  "ARG_OF_PERICENTER": 197.1343,
  "MEAN_ANOMALY": 162.9275,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53760,
  "REV_AT_EPOCH": 21366,
  "BSTAR": 0.0002141,
  "MEAN_MOTION_DOT": 0.00005122,
  "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 05A
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/53760

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