▸Orbital parameters

Orbit class	SSO
Inclination	97.5609°
Eccentricity	0.0002790
Period	91.3 min
Apogee	342 km
Perigee	338 km
Mean motion	15.76606216 rev/day
RAAN	321.6518°
Arg of perigee	219.9478°
Mean anomaly	140.1583°
B*	6.0141e-4
Rev at epoch	21,790

▸Two-line element set (TLE)

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

1 53453U 22098K 26188.18995993 .00096376 00000-0 60141-3 0 9995

2 53453 97.5609 321.6518 0002790 219.9478 140.1583 15.76606216217903

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DONGPO 01",
  "OBJECT_ID": "2022-098K",
  "EPOCH": "2026-07-07T04:33:32.538+00:00",
  "MEAN_MOTION": 15.76606216,
  "ECCENTRICITY": 0.000279,
  "INCLINATION": 97.5609,
  "RA_OF_ASC_NODE": 321.6518,
  "ARG_OF_PERICENTER": 219.9478,
  "MEAN_ANOMALY": 140.1583,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53453,
  "REV_AT_EPOCH": 21790,
  "BSTAR": 0.00060141,
  "MEAN_MOTION_DOT": 0.00096376,
  "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	DONGPO 01
Operator	Chang Guang Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Aug 10, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	42HIGHvia 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/53453

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