▸Orbital parameters

Orbit class	SSO
Inclination	97.5501°
Eccentricity	0.0004641
Period	90.7 min
Apogee	314 km
Perigee	307 km
Mean motion	15.87124216 rev/day
RAAN	322.4320°
Arg of perigee	236.8144°
Mean anomaly	123.2682°
B*	7.1537e-4
Rev at epoch	21,803

▸Two-line element set (TLE)

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

1 53449U 22098F 26188.20628814 .00188435 00000-0 71537-3 0 9997

2 53449 97.5501 322.4320 0004641 236.8144 123.2682 15.87124216218038

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DONGPO 05",
  "OBJECT_ID": "2022-098F",
  "EPOCH": "2026-07-07T04:57:03.295+00:00",
  "MEAN_MOTION": 15.87124216,
  "ECCENTRICITY": 0.0004641,
  "INCLINATION": 97.5501,
  "RA_OF_ASC_NODE": 322.432,
  "ARG_OF_PERICENTER": 236.8144,
  "MEAN_ANOMALY": 123.2682,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53449,
  "REV_AT_EPOCH": 21803,
  "BSTAR": 0.00071537,
  "MEAN_MOTION_DOT": 0.00188435,
  "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 05
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/53449

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