▸Orbital parameters

Orbit class	LEO
Inclination	34.9911°
Eccentricity	0.0009219
Period	95.8 min
Apogee	565 km
Perigee	552 km
Mean motion	15.02789479 rev/day
RAAN	207.5421°
Arg of perigee	250.7351°
Mean anomaly	109.2360°
B*	1.2205e-4
Rev at epoch	37,967

▸Two-line element set (TLE)

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

1 44450U 19045B 26188.21548014 .00001638 00000-0 12205-3 0 9997

2 44450 34.9911 207.5421 0009219 250.7351 109.2360 15.02789479379676

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-30 06B",
  "OBJECT_ID": "2019-045B",
  "EPOCH": "2026-07-07T05:10:17.484+00:00",
  "MEAN_MOTION": 15.02789479,
  "ECCENTRICITY": 0.0009219,
  "INCLINATION": 34.9911,
  "RA_OF_ASC_NODE": 207.5421,
  "ARG_OF_PERICENTER": 250.7351,
  "MEAN_ANOMALY": 109.236,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 44450,
  "REV_AT_EPOCH": 37967,
  "BSTAR": 0.00012205,
  "MEAN_MOTION_DOT": 0.00001638,
  "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 06B
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/44450

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