▸Orbital parameters

Orbit class	LEO
Inclination	34.9975°
Eccentricity	0.0004622
Period	95.8 min
Apogee	561 km
Perigee	555 km
Mean motion	15.02829028 rev/day
RAAN	269.4716°
Arg of perigee	227.9546°
Mean anomaly	132.0769°
B*	1.5215e-4
Rev at epoch	28,256

▸Two-line element set (TLE)

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

1 48423U 21039A 26188.22706652 .00002051 00000-0 15215-3 0 9996

2 48423 34.9975 269.4716 0004622 227.9546 132.0769 15.02829028282562

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-30 09A",
  "OBJECT_ID": "2021-039A",
  "EPOCH": "2026-07-07T05:26:58.547+00:00",
  "MEAN_MOTION": 15.02829028,
  "ECCENTRICITY": 0.0004622,
  "INCLINATION": 34.9975,
  "RA_OF_ASC_NODE": 269.4716,
  "ARG_OF_PERICENTER": 227.9546,
  "MEAN_ANOMALY": 132.0769,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 48423,
  "REV_AT_EPOCH": 28256,
  "BSTAR": 0.00015215,
  "MEAN_MOTION_DOT": 0.00002051,
  "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-30 09A
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 6, 2021HIGHvia 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/48423

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