▸Orbital parameters

Orbit class	LEO
Inclination	80.3980°
Eccentricity	0.0011913
Period	103.1 min
Apogee	912 km
Perigee	894 km
Mean motion	13.97327233 rev/day
RAAN	268.3501°
Arg of perigee	177.4841°
Mean anomaly	182.6382°
B*	7.0182e-5
Rev at epoch	3,027

▸Two-line element set (TLE)

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

1 66914U 25284B 26188.16659404 .00000108 00000-0 70182-4 0 9998

2 66914 80.3980 268.3501 0011913 177.4841 182.6382 13.97327233 30270

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2025-284B",
  "OBJECT_ID": "2025-284B",
  "EPOCH": "2026-07-07T03:59:53.725+00:00",
  "MEAN_MOTION": 13.97327233,
  "ECCENTRICITY": 0.0011913,
  "INCLINATION": 80.398,
  "RA_OF_ASC_NODE": 268.3501,
  "ARG_OF_PERICENTER": 177.4841,
  "MEAN_ANOMALY": 182.6382,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66914,
  "REV_AT_EPOCH": 3027,
  "BSTAR": 0.000070182,
  "MEAN_MOTION_DOT": 0.00000108,
  "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	2025-284B
Operator	Xingyun CompanyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Dec 5, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	220HIGHvia 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/66914

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