▸Orbital parameters

Orbit class	LEO
Inclination	34.9901°
Eccentricity	0.0005979
Period	94.7 min
Apogee	506 km
Perigee	498 km
Mean motion	15.21235990 rev/day
RAAN	95.9429°
Arg of perigee	115.8770°
Mean anomaly	244.2561°
B*	2.2879e-4
Rev at epoch	19,817

▸Two-line element set (TLE)

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

1 54746U 22171A 26188.19815894 .00005201 00000-0 22879-3 0 9998

2 54746 34.9901 95.9429 0005979 115.8770 244.2561 15.21235990198178

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-36 04A",
  "OBJECT_ID": "2022-171A",
  "EPOCH": "2026-07-07T04:45:20.932+00:00",
  "MEAN_MOTION": 15.2123599,
  "ECCENTRICITY": 0.0005979,
  "INCLINATION": 34.9901,
  "RA_OF_ASC_NODE": 95.9429,
  "ARG_OF_PERICENTER": 115.877,
  "MEAN_ANOMALY": 244.2561,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54746,
  "REV_AT_EPOCH": 19817,
  "BSTAR": 0.00022879,
  "MEAN_MOTION_DOT": 0.00005201,
  "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 04A
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 14, 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/54746

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