▸Orbital parameters

Orbit class	LEO
Inclination	34.9955°
Eccentricity	0.0022368
Period	94.9 min
Apogee	531 km
Perigee	500 km
Mean motion	15.16764690 rev/day
RAAN	318.6314°
Arg of perigee	276.7406°
Mean anomaly	83.0761°
B*	2.1623e-4
Rev at epoch	16,384

▸Two-line element set (TLE)

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

1 57454U 23106C 26187.79352632 .00004338 00000-0 21623-3 0 9993

2 57454 34.9955 318.6314 0022368 276.7406 83.0761 15.16764690163843

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-36 05B",
  "OBJECT_ID": "2023-106C",
  "EPOCH": "2026-07-06T19:02:40.674+00:00",
  "MEAN_MOTION": 15.1676469,
  "ECCENTRICITY": 0.0022368,
  "INCLINATION": 34.9955,
  "RA_OF_ASC_NODE": 318.6314,
  "ARG_OF_PERICENTER": 276.7406,
  "MEAN_ANOMALY": 83.0761,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 57454,
  "REV_AT_EPOCH": 16384,
  "BSTAR": 0.00021623,
  "MEAN_MOTION_DOT": 0.00004338,
  "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 05B
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jul 26, 2023HIGHvia 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/57454

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