▸Orbital parameters

Orbit class	MEO
Inclination	54.4506°
Eccentricity	0.0001069
Period	773.2 min
Apogee	21,531 km
Perigee	21,525 km
Mean motion	1.86230146 rev/day
RAAN	301.5523°
Arg of perigee	47.5868°
Mean anomaly	303.5952°
B*	0.0000e+0
Rev at epoch	961

▸Two-line element set (TLE)

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

1 61187U 24168C 26187.57446904 -.00000062 00000-0 00000-0 0 9996

2 61187 54.4506 301.5523 0001069 47.5868 303.5952 1.86230146 9616

▸ source OMM (JSON)

{
  "OBJECT_NAME": "BEIDOU-3 M27",
  "OBJECT_ID": "2024-168C",
  "EPOCH": "2026-07-06T13:47:14.125+00:00",
  "MEAN_MOTION": 1.86230146,
  "ECCENTRICITY": 0.0001069,
  "INCLINATION": 54.4506,
  "RA_OF_ASC_NODE": 301.5523,
  "ARG_OF_PERICENTER": 47.5868,
  "MEAN_ANOMALY": 303.5952,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61187,
  "REV_AT_EPOCH": 961,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -6.2e-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 M27
Operator	China National Space AdministrationHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 19, 2024HIGHvia 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/61187

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