▸Orbital parameters

Orbit class	MEO
Inclination	56.6428°
Eccentricity	0.0005603
Period	773.2 min
Apogee	21,544 km
Perigee	21,512 km
Mean motion	1.86231621 rev/day
RAAN	62.0271°
Arg of perigee	6.4444°
Mean anomaly	353.6283°
B*	0.0000e+0
Rev at epoch	5,300

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 43623U 18072B 26187.19473721 -.00000040 00000-0 00000-0 0 9999

2 43623 56.6428 62.0271 0005603 6.4444 353.6283 1.86231621 53003

▸ source OMM (JSON)

{
  "OBJECT_NAME": "BEIDOU-3 M14",
  "OBJECT_ID": "2018-072B",
  "EPOCH": "2026-07-06T04:40:25.295+00:00",
  "MEAN_MOTION": 1.86231621,
  "ECCENTRICITY": 0.00056028,
  "INCLINATION": 56.6428,
  "RA_OF_ASC_NODE": 62.0271,
  "ARG_OF_PERICENTER": 6.4444,
  "MEAN_ANOMALY": 353.6283,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43623,
  "REV_AT_EPOCH": 5300,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -4e-7,
  "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	BEIDOU-3 M14
Operator	China National Space AdministrationHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 19, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1014HIGHvia 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/43623

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