▸Orbital parameters

Orbit class	LEO
Inclination	63.3659°
Eccentricity	0.0538945
Period	107.0 min
Apogee	1,491 km
Perigee	686 km
Mean motion	13.45703986 rev/day
RAAN	307.8018°
Arg of perigee	21.8989°
Mean anomaly	340.4152°
B*	2.6587e-5
Rev at epoch	80,259

▸Two-line element set (TLE)

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

1 36413U 10009A 26187.66913970 -.00000054 00000-0 26587-4 0 9994

2 36413 63.3659 307.8018 0538945 21.8989 340.4152 13.45703986802598

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-9 01A",
  "OBJECT_ID": "2010-009A",
  "EPOCH": "2026-07-06T16:03:33.67+00:00",
  "MEAN_MOTION": 13.45703986,
  "ECCENTRICITY": 0.0538945,
  "INCLINATION": 63.3659,
  "RA_OF_ASC_NODE": 307.8018,
  "ARG_OF_PERICENTER": 21.8989,
  "MEAN_ANOMALY": 340.4152,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 36413,
  "REV_AT_EPOCH": 80259,
  "BSTAR": 0.000026587,
  "MEAN_MOTION_DOT": -5.4e-7,
  "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-9 01A
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Mar 5, 2010HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	500HIGHvia 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/36413

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