▸Orbital parameters

Orbit class	SSO
Inclination	97.6385°
Eccentricity	0.0013765
Period	95.4 min
Apogee	549 km
Perigee	530 km
Mean motion	15.09018660 rev/day
RAAN	266.6983°
Arg of perigee	81.2680°
Mean anomaly	279.0107°
B*	1.3238e-4
Rev at epoch	4,059

▸Two-line element set (TLE)

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

1 65939U 25226B 26188.19479226 .00002033 00000-0 13238-3 0 9992

2 65939 97.6385 266.6983 0013765 81.2680 279.0107 15.09018660 40599

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2025-226B",
  "OBJECT_ID": "2025-226B",
  "EPOCH": "2026-07-07T04:40:30.051+00:00",
  "MEAN_MOTION": 15.0901866,
  "ECCENTRICITY": 0.0013765,
  "INCLINATION": 97.6385,
  "RA_OF_ASC_NODE": 266.6983,
  "ARG_OF_PERICENTER": 81.268,
  "MEAN_ANOMALY": 279.0107,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65939,
  "REV_AT_EPOCH": 4059,
  "BSTAR": 0.00013238,
  "MEAN_MOTION_DOT": 0.00002033,
  "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	2025-226B
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/65939

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