▸Orbital parameters

Orbit class	MEO
Inclination	54.3974°
Eccentricity	0.0008559
Period	773.2 min
Apogee	21,552 km
Perigee	21,504 km
Mean motion	1.86229378 rev/day
RAAN	182.0557°
Arg of perigee	359.0397°
Mean anomaly	0.9657°
B*	0.0000e+0
Rev at epoch	4,616

▸Two-line element set (TLE)

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

1 44542U 19061A 26188.10973588 .00000118 00000-0 00000-0 0 9992

2 44542 54.3974 182.0557 0008559 359.0397 0.9657 1.86229378 46164

▸ source OMM (JSON)

{
  "OBJECT_NAME": "BEIDOU-3 M24",
  "OBJECT_ID": "2019-061A",
  "EPOCH": "2026-07-07T02:38:01.18+00:00",
  "MEAN_MOTION": 1.86229378,
  "ECCENTRICITY": 0.0008559,
  "INCLINATION": 54.3974,
  "RA_OF_ASC_NODE": 182.0557,
  "ARG_OF_PERICENTER": 359.0397,
  "MEAN_ANOMALY": 0.9657,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 44542,
  "REV_AT_EPOCH": 4616,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000118,
  "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 M24
Operator	China National Space AdministrationHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 22, 2019HIGHvia 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/44542

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