▸Orbital parameters

Orbit class	GEO
Inclination	0.0390°
Eccentricity	0.0003890
Period	1436.1 min
Apogee	35,803 km
Perigee	35,770 km
Mean motion	1.00271009 rev/day
RAAN	182.5667°
Arg of perigee	316.7126°
Mean anomaly	248.6535°
B*	0.0000e+0
Rev at epoch	425

▸Two-line element set (TLE)

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

1 64062U 25106A 26187.82176308 -.00000030 00000-0 00000-0 0 9995

2 64062 0.0390 182.5667 0003890 316.7126 248.6535 1.00271009 4257

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CHINASAT 3B",
  "OBJECT_ID": "2025-106A",
  "EPOCH": "2026-07-06T19:43:20.33+00:00",
  "MEAN_MOTION": 1.00271009,
  "ECCENTRICITY": 0.000389,
  "INCLINATION": 0.039,
  "RA_OF_ASC_NODE": 182.5667,
  "ARG_OF_PERICENTER": 316.7126,
  "MEAN_ANOMALY": 248.6535,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64062,
  "REV_AT_EPOCH": 425,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -3e-7,
  "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 3B
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 20, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5000HIGHvia 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/64062

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