▸Orbital parameters

Orbit class	LEO
Inclination	100.1128°
Eccentricity	0.0010051
Period	109.5 min
Apogee	1,209 km
Perigee	1,194 km
Mean motion	13.15582108 rev/day
RAAN	163.6732°
Arg of perigee	44.6645°
Mean anomaly	315.5276°
B*	-6.2998e-4
Rev at epoch	60,627

▸Two-line element set (TLE)

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

1 39410U 13065A 26188.16467806 -.00000280 00000-0 -62998-3 0 9994

2 39410 100.1128 163.6732 0010051 44.6645 315.5276 13.15582108606270

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-19",
  "OBJECT_ID": "2013-065A",
  "EPOCH": "2026-07-07T03:57:08.184+00:00",
  "MEAN_MOTION": 13.15582108,
  "ECCENTRICITY": 0.0010051,
  "INCLINATION": 100.1128,
  "RA_OF_ASC_NODE": 163.6732,
  "ARG_OF_PERICENTER": 44.6645,
  "MEAN_ANOMALY": 315.5276,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 39410,
  "REV_AT_EPOCH": 60627,
  "BSTAR": -0.00062998,
  "MEAN_MOTION_DOT": -0.0000028,
  "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-19
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 20, 2013HIGHvia 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/39410

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