▸Orbital parameters

Orbit class	LEO
Inclination	35.0027°
Eccentricity	0.0001457
Period	94.5 min
Apogee	498 km
Perigee	496 km
Mean motion	15.23041075 rev/day
RAAN	75.0650°
Arg of perigee	158.0332°
Mean anomaly	202.0445°
B*	2.9255e-4
Rev at epoch	15,621

▸Two-line element set (TLE)

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

1 57886U 23145A 26188.12784821 .00007025 00000-0 29255-3 0 9997

2 57886 35.0027 75.0650 0001457 158.0332 202.0445 15.23041075156215

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-39 02A",
  "OBJECT_ID": "2023-145A",
  "EPOCH": "2026-07-07T03:04:06.085+00:00",
  "MEAN_MOTION": 15.23041075,
  "ECCENTRICITY": 0.0001457,
  "INCLINATION": 35.0027,
  "RA_OF_ASC_NODE": 75.065,
  "ARG_OF_PERICENTER": 158.0332,
  "MEAN_ANOMALY": 202.0445,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 57886,
  "REV_AT_EPOCH": 15621,
  "BSTAR": 0.00029255,
  "MEAN_MOTION_DOT": 0.00007025,
  "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-39 02A
Operator	General Armaments Dept. of the PLAHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 17, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	300HIGHvia 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/57886

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