▸Orbital parameters

Orbit class	SSO
Inclination	98.0508°
Eccentricity	0.0003298
Period	98.3 min
Apogee	679 km
Perigee	675 km
Mean motion	14.65077807 rev/day
RAAN	76.9419°
Arg of perigee	113.1010°
Mean anomaly	247.0542°
B*	2.1408e-4
Rev at epoch	29,465

▸Two-line element set (TLE)

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

1 47303U 20103B 26188.17331612 .00001102 00000-0 21408-3 0 9994

2 47303 98.0508 76.9419 0003298 113.1010 247.0542 14.65077807294659

▸ source OMM (JSON)

{
  "OBJECT_NAME": "WEINA 2",
  "OBJECT_ID": "2020-103B",
  "EPOCH": "2026-07-07T04:09:34.513+00:00",
  "MEAN_MOTION": 14.65077807,
  "ECCENTRICITY": 0.0003298,
  "INCLINATION": 98.0508,
  "RA_OF_ASC_NODE": 76.9419,
  "ARG_OF_PERICENTER": 113.101,
  "MEAN_ANOMALY": 247.0542,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 47303,
  "REV_AT_EPOCH": 29465,
  "BSTAR": 0.00021408,
  "MEAN_MOTION_DOT": 0.00001102,
  "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	WEINA 2
Operator	China Aerospace CorpHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 27, 2020HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia 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/47303

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