▸Orbital parameters

Orbit class	LEO
Inclination	34.9898°
Eccentricity	0.0008500
Period	92.9 min
Apogee	421 km
Perigee	409 km
Mean motion	15.50525486 rev/day
RAAN	305.3869°
Arg of perigee	46.0706°
Mean anomaly	314.0718°
B*	6.1704e-4
Rev at epoch	20,826

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 54045U 22133D 26187.76699083 .00036512 00000-0 61704-3 0 9999

2 54045 34.9898 305.3869 0008500 46.0706 314.0718 15.50525486208264

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-36 02C",
  "OBJECT_ID": "2022-133D",
  "EPOCH": "2026-07-06T18:24:28.008+00:00",
  "MEAN_MOTION": 15.50525486,
  "ECCENTRICITY": 0.00085,
  "INCLINATION": 34.9898,
  "RA_OF_ASC_NODE": 305.3869,
  "ARG_OF_PERICENTER": 46.0706,
  "MEAN_ANOMALY": 314.0718,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 54045,
  "REV_AT_EPOCH": 20826,
  "BSTAR": 0.00061704,
  "MEAN_MOTION_DOT": 0.00036512,
  "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 02C
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Oct 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/54045

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