▸Orbital parameters

Orbit class	GEO
Inclination	0.0398°
Eccentricity	0.0000565
Period	1436.1 min
Apogee	35,790 km
Perigee	35,785 km
Mean motion	1.00269977 rev/day
RAAN	128.5414°
Arg of perigee	104.6819°
Mean anomaly	191.3321°
B*	0.0000e+0
Rev at epoch	1,404

▸Two-line element set (TLE)

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

1 53813U 22112A 26188.16118127 -.00000134 00000-0 00000-0 0 9999

2 53813 0.0398 128.5414 0000565 104.6819 191.3321 1.00269977 14042

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ZHONGXING-1E",
  "OBJECT_ID": "2022-112A",
  "EPOCH": "2026-07-07T03:52:06.062+00:00",
  "MEAN_MOTION": 1.00269977,
  "ECCENTRICITY": 0.0000565,
  "INCLINATION": 0.0398,
  "RA_OF_ASC_NODE": 128.5414,
  "ARG_OF_PERICENTER": 104.6819,
  "MEAN_ANOMALY": 191.3321,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53813,
  "REV_AT_EPOCH": 1404,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000134,
  "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	ZHONGXING-1E
Operator	Strategic Support TroopsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 13, 2022HIGHvia 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/53813

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