▸Orbital parameters

Orbit class	LEO
Inclination	34.9950°
Eccentricity	0.0002265
Period	92.1 min
Apogee	379 km
Perigee	375 km
Mean motion	15.63712496 rev/day
RAAN	287.7023°
Arg of perigee	98.9437°
Mean anomaly	261.1546°
B*	8.4542e-4
Rev at epoch	22,575

▸Two-line element set (TLE)

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

1 52908U 22068B 26187.72472551 .00082454 00000-0 84542-3 0 9998

2 52908 34.9950 287.7023 0002265 98.9437 261.1546 15.63712496225750

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-35 02B",
  "OBJECT_ID": "2022-068B",
  "EPOCH": "2026-07-06T17:23:36.284+00:00",
  "MEAN_MOTION": 15.63712496,
  "ECCENTRICITY": 0.0002265,
  "INCLINATION": 34.995,
  "RA_OF_ASC_NODE": 287.7023,
  "ARG_OF_PERICENTER": 98.9437,
  "MEAN_ANOMALY": 261.1546,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52908,
  "REV_AT_EPOCH": 22575,
  "BSTAR": 0.00084542,
  "MEAN_MOTION_DOT": 0.00082454,
  "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 02B
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/52908

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