▸Orbital parameters

Orbit class	LEO
Inclination	35.0008°
Eccentricity	0.0003932
Period	93.7 min
Apogee	460 km
Perigee	454 km
Mean motion	15.36378961 rev/day
RAAN	258.5716°
Arg of perigee	114.1644°
Mean anomaly	245.9486°
B*	2.2382e-4
Rev at epoch	10,831

▸Two-line element set (TLE)

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

1 53524U 22100C 26188.21340066 .00008127 00000-0 22382-3 0 9999

2 53524 35.0008 258.5716 0003932 114.1644 245.9486 15.36378961108319

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-35 04B",
  "OBJECT_ID": "2022-100C",
  "EPOCH": "2026-07-07T05:07:17.817+00:00",
  "MEAN_MOTION": 15.36378961,
  "ECCENTRICITY": 0.0003932,
  "INCLINATION": 35.0008,
  "RA_OF_ASC_NODE": 258.5716,
  "ARG_OF_PERICENTER": 114.1644,
  "MEAN_ANOMALY": 245.9486,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53524,
  "REV_AT_EPOCH": 10831,
  "BSTAR": 0.00022382,
  "MEAN_MOTION_DOT": 0.00008127,
  "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-35 04B
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Aug 19, 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/53524

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