▸Orbital parameters

Orbit class	SSO
Inclination	97.7471°
Eccentricity	0.0010276
Period	96.4 min
Apogee	596 km
Perigee	581 km
Mean motion	14.93024467 rev/day
RAAN	116.4973°
Arg of perigee	293.2138°
Mean anomaly	66.7998°
B*	2.0279e-4
Rev at epoch	3,312

▸Two-line element set (TLE)

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

1 66650U 25274A 26187.72361913 .00002054 00000-0 20279-3 0 9993

2 66650 97.7471 116.4973 0010276 293.2138 66.7998 14.93024467 33129

▸ source OMM (JSON)

{
  "OBJECT_NAME": "BEE-1000",
  "OBJECT_ID": "2025-274A",
  "EPOCH": "2026-07-06T17:22:00.693+00:00",
  "MEAN_MOTION": 14.93024467,
  "ECCENTRICITY": 0.0010276,
  "INCLINATION": 97.7471,
  "RA_OF_ASC_NODE": 116.4973,
  "ARG_OF_PERICENTER": 293.2138,
  "MEAN_ANOMALY": 66.7998,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66650,
  "REV_AT_EPOCH": 3312,
  "BSTAR": 0.00020279,
  "MEAN_MOTION_DOT": 0.00002054,
  "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	BEE-1000
Operator	Space LintechHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	South Korea
Launch date	Nov 26, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	11HIGHvia 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/66650

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