▸Orbital parameters

Orbit class	LEO
Inclination	50.0040°
Eccentricity	0.0012218
Period	107.3 min
Apogee	1,113 km
Perigee	1,095 km
Mean motion	13.41502889 rev/day
RAAN	255.3535°
Arg of perigee	138.8852°
Mean anomaly	221.2948°
B*	5.9237e-5
Rev at epoch	7,840

▸Two-line element set (TLE)

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

1 62186U 24226B 26188.24506080 -.00000095 00000-0 59237-4 0 9994

2 62186 50.0040 255.3535 0012218 138.8852 221.2948 13.41502889 78409

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2024-226B",
  "OBJECT_ID": "2024-226B",
  "EPOCH": "2026-07-07T05:52:53.253+00:00",
  "MEAN_MOTION": 13.41502889,
  "ECCENTRICITY": 0.0012218,
  "INCLINATION": 50.004,
  "RA_OF_ASC_NODE": 255.3535,
  "ARG_OF_PERICENTER": 138.8852,
  "MEAN_ANOMALY": 221.2948,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62186,
  "REV_AT_EPOCH": 7840,
  "BSTAR": 0.000059237,
  "MEAN_MOTION_DOT": -9.5e-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	2024-226B
Operator	China Satellite Network Group Co. Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 30, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	300HIGHvia 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/62186

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