▸Orbital parameters

Orbit class	SSO
Inclination	97.8969°
Eccentricity	0.0001632
Period	96.9 min
Apogee	613 km
Perigee	611 km
Mean motion	14.85413386 rev/day
RAAN	211.4734°
Arg of perigee	84.2815°
Mean anomaly	6.1709°
B*	2.2197e-4
Rev at epoch	86,018

▸Two-line element set (TLE)

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

1 36834U 10038A 26188.22906426 .00001858 00000-0 22197-3 0 9998

2 36834 97.8969 211.4734 0001632 84.2815 6.1709 14.85413386860185

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-10",
  "OBJECT_ID": "2010-038A",
  "EPOCH": "2026-07-07T05:29:51.152+00:00",
  "MEAN_MOTION": 14.85413386,
  "ECCENTRICITY": 0.0001632,
  "INCLINATION": 97.8969,
  "RA_OF_ASC_NODE": 211.4734,
  "ARG_OF_PERICENTER": 84.2815,
  "MEAN_ANOMALY": 6.1709,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 36834,
  "REV_AT_EPOCH": 86018,
  "BSTAR": 0.00022197,
  "MEAN_MOTION_DOT": 0.00001858,
  "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-10
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Aug 9, 2010HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1040HIGHvia 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/36834

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