▸Orbital parameters

Orbit class	SSO
Inclination	97.8147°
Eccentricity	0.0001701
Period	96.6 min
Apogee	596 km
Perigee	594 km
Mean motion	14.90863710 rev/day
RAAN	217.8760°
Arg of perigee	77.4604°
Mean anomaly	282.6805°
B*	1.9749e-4
Rev at epoch	885

▸Two-line element set (TLE)

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

1 32289U 07055A 26188.19581397 .00001890 00000-0 19749-3 0 9990

2 32289 97.8147 217.8760 0001701 77.4604 282.6805 14.90863710 8851

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-3",
  "OBJECT_ID": "2007-055A",
  "EPOCH": "2026-07-07T04:41:58.327+00:00",
  "MEAN_MOTION": 14.9086371,
  "ECCENTRICITY": 0.0001701,
  "INCLINATION": 97.8147,
  "RA_OF_ASC_NODE": 217.876,
  "ARG_OF_PERICENTER": 77.4604,
  "MEAN_ANOMALY": 282.6805,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 32289,
  "REV_AT_EPOCH": 885,
  "BSTAR": 0.00019749,
  "MEAN_MOTION_DOT": 0.0000189,
  "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-3
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 11, 2007HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2700HIGHvia 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/32289

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