▸Orbital parameters

Orbit class	SSO
Inclination	97.6435°
Eccentricity	0.0014937
Period	94.9 min
Apogee	526 km
Perigee	506 km
Mean motion	15.16700770 rev/day
RAAN	268.2975°
Arg of perigee	82.8420°
Mean anomaly	277.4510°
B*	3.2283e-4
Rev at epoch	4,065

▸Two-line element set (TLE)

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

1 65938U 25226A 26187.68748212 .00006274 00000-0 32283-3 0 9990

2 65938 97.6435 268.2975 0014937 82.8420 277.4510 15.16700770 40659

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2025-226A",
  "OBJECT_ID": "2025-226A",
  "EPOCH": "2026-07-06T16:29:58.455+00:00",
  "MEAN_MOTION": 15.1670077,
  "ECCENTRICITY": 0.0014937,
  "INCLINATION": 97.6435,
  "RA_OF_ASC_NODE": 268.2975,
  "ARG_OF_PERICENTER": 82.842,
  "MEAN_ANOMALY": 277.451,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65938,
  "REV_AT_EPOCH": 4065,
  "BSTAR": 0.00032283,
  "MEAN_MOTION_DOT": 0.00006274,
  "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	2025-226A
Operator	Chang Guang Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Oct 11, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	230HIGHvia 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/65938

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