▸Orbital parameters

Orbit class	LEO
Inclination	142.0399°
Eccentricity	0.0001004
Period	104.1 min
Apogee	953 km
Perigee	952 km
Mean motion	13.83243126 rev/day
RAAN	312.4231°
Arg of perigee	282.5463°
Mean anomaly	77.5144°
B*	1.1664e-4
Rev at epoch	2,420

▸Two-line element set (TLE)

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

1 67433U 26006A 26188.18963360 .00000317 00000-0 11664-3 0 9990

2 67433 142.0399 312.4231 0001004 282.5463 77.5144 13.83243126 24203

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-50 01",
  "OBJECT_ID": "2026-006A",
  "EPOCH": "2026-07-07T04:33:04.343+00:00",
  "MEAN_MOTION": 13.83243126,
  "ECCENTRICITY": 0.0001004,
  "INCLINATION": 142.0399,
  "RA_OF_ASC_NODE": 312.4231,
  "ARG_OF_PERICENTER": 282.5463,
  "MEAN_ANOMALY": 77.5144,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67433,
  "REV_AT_EPOCH": 2420,
  "BSTAR": 0.00011664,
  "MEAN_MOTION_DOT": 0.00000317,
  "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	YAOGAN-50 01
Operator	China Satellite Network Group Co. Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jan 13, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1500HIGHvia 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/67433

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