▸Orbital parameters

Orbit class	GEO
Inclination	0.0415°
Eccentricity	0.0003067
Period	1436.1 min
Apogee	35,800 km
Perigee	35,774 km
Mean motion	1.00271958 rev/day
RAAN	234.1816°
Arg of perigee	234.9939°
Mean anomaly	326.9513°
B*	0.0000e+0
Rev at epoch	434

▸Two-line element set (TLE)

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

1 64470U 25132A 26188.16326131 -.00000232 00000-0 00000-0 0 9990

2 64470 0.0415 234.1816 0003067 234.9939 326.9513 1.00271958 4346

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CHINASAT 9C",
  "OBJECT_ID": "2025-132A",
  "EPOCH": "2026-07-07T03:55:05.777+00:00",
  "MEAN_MOTION": 1.00271958,
  "ECCENTRICITY": 0.0003067,
  "INCLINATION": 0.0415,
  "RA_OF_ASC_NODE": 234.1816,
  "ARG_OF_PERICENTER": 234.9939,
  "MEAN_ANOMALY": 326.9513,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64470,
  "REV_AT_EPOCH": 434,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000232,
  "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	CHINASAT 9C
Operator	Chinese Academy of Space Technology, Beijing (CASC 5th Acad)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jun 20, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5500HIGHvia 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/64470

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