▸Orbital parameters

Orbit class	LEO
Inclination	34.9989°
Eccentricity	0.0002474
Period	93.8 min
Apogee	462 km
Perigee	458 km
Mean motion	15.35280897 rev/day
RAAN	194.6935°
Arg of perigee	156.2605°
Mean anomaly	203.8228°
B*	2.1947e-4
Rev at epoch	20,129

▸Two-line element set (TLE)

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

1 54372U 22160A 26188.22004315 .00007689 00000-0 21947-3 0 9990

2 54372 34.9989 194.6935 0002474 156.2605 203.8228 15.35280897201291

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-36 03A",
  "OBJECT_ID": "2022-160A",
  "EPOCH": "2026-07-07T05:16:51.728+00:00",
  "MEAN_MOTION": 15.35280897,
  "ECCENTRICITY": 0.0002474,
  "INCLINATION": 34.9989,
  "RA_OF_ASC_NODE": 194.6935,
  "ARG_OF_PERICENTER": 156.2605,
  "MEAN_ANOMALY": 203.8228,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54372,
  "REV_AT_EPOCH": 20129,
  "BSTAR": 0.00021947,
  "MEAN_MOTION_DOT": 0.00007689,
  "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-36 03A
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 27, 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/54372

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