▸Orbital parameters

Orbit class	LEO
Inclination	34.9922°
Eccentricity	0.0002896
Period	95.8 min
Apogee	560 km
Perigee	556 km
Mean motion	15.02790683 rev/day
RAAN	208.2801°
Arg of perigee	93.0462°
Mean anomaly	267.0577°
B*	1.7980e-4
Rev at epoch	37,962

▸Two-line element set (TLE)

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

1 44449U 19045A 26188.17155257 .00002426 00000-0 17980-3 0 9994

2 44449 34.9922 208.2801 0002896 93.0462 267.0577 15.02790683379628

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-30 06A",
  "OBJECT_ID": "2019-045A",
  "EPOCH": "2026-07-07T04:07:02.142+00:00",
  "MEAN_MOTION": 15.02790683,
  "ECCENTRICITY": 0.0002896,
  "INCLINATION": 34.9922,
  "RA_OF_ASC_NODE": 208.2801,
  "ARG_OF_PERICENTER": 93.0462,
  "MEAN_ANOMALY": 267.0577,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 44449,
  "REV_AT_EPOCH": 37962,
  "BSTAR": 0.0001798,
  "MEAN_MOTION_DOT": 0.00002426,
  "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 06A
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jul 26, 2019HIGHvia 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/44449

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