▸Orbital parameters

Orbit class	SSO
Inclination	97.6342°
Eccentricity	0.0014547
Period	95.0 min
Apogee	527 km
Perigee	507 km
Mean motion	15.16233994 rev/day
RAAN	267.8442°
Arg of perigee	76.1629°
Mean anomaly	284.1221°
B*	3.0742e-4
Rev at epoch	4,063

▸Two-line element set (TLE)

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

1 65940U 25226C 26187.67240309 .00005890 00000-0 30742-3 0 9997

2 65940 97.6342 267.8442 0014547 76.1629 284.1221 15.16233994 40638

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2025-226C",
  "OBJECT_ID": "2025-226C",
  "EPOCH": "2026-07-06T16:08:15.627+00:00",
  "MEAN_MOTION": 15.16233994,
  "ECCENTRICITY": 0.0014547,
  "INCLINATION": 97.6342,
  "RA_OF_ASC_NODE": 267.8442,
  "ARG_OF_PERICENTER": 76.1629,
  "MEAN_ANOMALY": 284.1221,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65940,
  "REV_AT_EPOCH": 4063,
  "BSTAR": 0.00030742,
  "MEAN_MOTION_DOT": 0.0000589,
  "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	2025-226C
Operator	Spacetime Daoyu Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Oct 11, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	50HIGHvia 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/65940

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