▸Orbital parameters

Orbit class	LEO
Inclination	34.9958°
Eccentricity	0.0004246
Period	95.8 min
Apogee	561 km
Perigee	555 km
Mean motion	15.02792378 rev/day
RAAN	29.1336°
Arg of perigee	169.4777°
Mean anomaly	190.6020°
B*	1.6594e-4
Rev at epoch	46,568

▸Two-line element set (TLE)

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

1 43082U 17085B 26188.04039865 .00002237 00000-0 16594-3 0 9990

2 43082 34.9958 29.1336 0004246 169.4777 190.6020 15.02792378465689

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-30 04B",
  "OBJECT_ID": "2017-085B",
  "EPOCH": "2026-07-07T00:58:10.443+00:00",
  "MEAN_MOTION": 15.02792378,
  "ECCENTRICITY": 0.0004246,
  "INCLINATION": 34.9958,
  "RA_OF_ASC_NODE": 29.1336,
  "ARG_OF_PERICENTER": 169.4777,
  "MEAN_ANOMALY": 190.602,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43082,
  "REV_AT_EPOCH": 46568,
  "BSTAR": 0.00016594,
  "MEAN_MOTION_DOT": 0.00002237,
  "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 04B
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 25, 2017HIGHvia 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/43082

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