▸Orbital parameters

Orbit class	SSO
Inclination	97.5543°
Eccentricity	0.0004206
Period	91.2 min
Apogee	335 km
Perigee	330 km
Mean motion	15.79311810 rev/day
RAAN	320.9532°
Arg of perigee	233.0820°
Mean anomaly	127.0061°
B*	6.8446e-4
Rev at epoch	21,791

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 53452U 22098J 26187.97857707 .00124150 00000-0 68446-3 0 9998

2 53452 97.5543 320.9532 0004206 233.0820 127.0061 15.79311810217911

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DONGPO 02",
  "OBJECT_ID": "2022-098J",
  "EPOCH": "2026-07-06T23:29:09.059+00:00",
  "MEAN_MOTION": 15.7931181,
  "ECCENTRICITY": 0.0004206,
  "INCLINATION": 97.5543,
  "RA_OF_ASC_NODE": 320.9532,
  "ARG_OF_PERICENTER": 233.082,
  "MEAN_ANOMALY": 127.0061,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53452,
  "REV_AT_EPOCH": 21791,
  "BSTAR": 0.00068446,
  "MEAN_MOTION_DOT": 0.0012415,
  "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 02
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/53452

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