▸Orbital parameters

Orbit class	SSO
Inclination	98.2496°
Eccentricity	0.0002195
Period	98.3 min
Apogee	681 km
Perigee	678 km
Mean motion	14.64240301 rev/day
RAAN	322.0297°
Arg of perigee	122.2666°
Mean anomaly	237.8749°
B*	1.2796e-4
Rev at epoch	24,929

▸Two-line element set (TLE)

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

1 49383U 21099A 26188.19279961 .00000626 00000-0 12796-3 0 9999

2 49383 98.2496 322.0297 0002195 122.2666 237.8749 14.64240301249295

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAOGAN-32 02A",
  "OBJECT_ID": "2021-099A",
  "EPOCH": "2026-07-07T04:37:37.886+00:00",
  "MEAN_MOTION": 14.64240301,
  "ECCENTRICITY": 0.0002195,
  "INCLINATION": 98.2496,
  "RA_OF_ASC_NODE": 322.0297,
  "ARG_OF_PERICENTER": 122.2666,
  "MEAN_ANOMALY": 237.8749,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 49383,
  "REV_AT_EPOCH": 24929,
  "BSTAR": 0.00012796,
  "MEAN_MOTION_DOT": 0.00000626,
  "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-32 02A
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Nov 3, 2021HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	500HIGHvia 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/49383

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