▸Orbital parameters

Orbit class	SSO
Inclination	97.6102°
Eccentricity	0.0017518
Period	95.3 min
Apogee	544 km
Perigee	520 km
Mean motion	15.11320130 rev/day
RAAN	9.4539°
Arg of perigee	90.2816°
Mean anomaly	270.0421°
B*	1.4813e-4
Rev at epoch	7,131

▸Two-line element set (TLE)

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

1 63348U 25059E 26188.15537006 .00002438 00000-0 14813-3 0 9994

2 63348 97.6102 9.4539 0017518 90.2816 270.0421 15.11320130 71314

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YUNYAO-1 47",
  "OBJECT_ID": "2025-059E",
  "EPOCH": "2026-07-07T03:43:43.973+00:00",
  "MEAN_MOTION": 15.1132013,
  "ECCENTRICITY": 0.0017518,
  "INCLINATION": 97.6102,
  "RA_OF_ASC_NODE": 9.4539,
  "ARG_OF_PERICENTER": 90.2816,
  "MEAN_ANOMALY": 270.0421,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63348,
  "REV_AT_EPOCH": 7131,
  "BSTAR": 0.00014813,
  "MEAN_MOTION_DOT": 0.00002438,
  "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	YUNYAO-1 47
Operator	Yunyao Aerospace Tech Co. (Tianjin) Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Mar 21, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	50HIGHvia 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/63348

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