▸Orbital parameters

Orbit class	LEO
Inclination	34.9935°
Eccentricity	0.0011085
Period	94.5 min
Apogee	500 km
Perigee	485 km
Mean motion	15.24427307 rev/day
RAAN	14.6370°
Arg of perigee	256.8262°
Mean anomaly	103.1216°
B*	2.3130e-4
Rev at epoch	22,489

▸Two-line element set (TLE)

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

1 52907U 22068A 26187.84749041 .00005791 00000-0 23130-3 0 9996

2 52907 34.9935 14.6370 0011085 256.8262 103.1216 15.24427307224899

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-35 02A",
  "OBJECT_ID": "2022-068A",
  "EPOCH": "2026-07-06T20:20:23.171+00:00",
  "MEAN_MOTION": 15.24427307,
  "ECCENTRICITY": 0.0011085,
  "INCLINATION": 34.9935,
  "RA_OF_ASC_NODE": 14.637,
  "ARG_OF_PERICENTER": 256.8262,
  "MEAN_ANOMALY": 103.1216,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52907,
  "REV_AT_EPOCH": 22489,
  "BSTAR": 0.0002313,
  "MEAN_MOTION_DOT": 0.00005791,
  "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 02A
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jun 23, 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/52907

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