▸Orbital parameters

Orbit class	LEO
Inclination	35.0086°
Eccentricity	0.0008039
Period	94.5 min
Apogee	502 km
Perigee	491 km
Mean motion	15.23034832 rev/day
RAAN	213.6576°
Arg of perigee	232.1067°
Mean anomaly	127.8921°
B*	1.9495e-4
Rev at epoch	20,110

▸Two-line element set (TLE)

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

1 54376U 22160E 26188.20586303 .00004671 00000-0 19495-3 0 9997

2 54376 35.0086 213.6576 0008039 232.1067 127.8921 15.23034832201105

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-36 03C",
  "OBJECT_ID": "2022-160E",
  "EPOCH": "2026-07-07T04:56:26.566+00:00",
  "MEAN_MOTION": 15.23034832,
  "ECCENTRICITY": 0.0008039,
  "INCLINATION": 35.0086,
  "RA_OF_ASC_NODE": 213.6576,
  "ARG_OF_PERICENTER": 232.1067,
  "MEAN_ANOMALY": 127.8921,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54376,
  "REV_AT_EPOCH": 20110,
  "BSTAR": 0.00019495,
  "MEAN_MOTION_DOT": 0.00004671,
  "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 03C
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/54376

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