▸Orbital parameters

Orbit class	SSO
Inclination	97.5573°
Eccentricity	0.0004371
Period	91.4 min
Apogee	345 km
Perigee	339 km
Mean motion	15.75802715 rev/day
RAAN	320.5096°
Arg of perigee	251.3832°
Mean anomaly	108.6959°
B*	6.1945e-4
Rev at epoch	21,786

▸Two-line element set (TLE)

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

1 53444U 22098A 26187.98086271 .00095870 00000-0 61945-3 0 9993

2 53444 97.5573 320.5096 0004371 251.3832 108.6959 15.75802715217865

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DONGPO 07",
  "OBJECT_ID": "2022-098A",
  "EPOCH": "2026-07-06T23:32:26.538+00:00",
  "MEAN_MOTION": 15.75802715,
  "ECCENTRICITY": 0.0004371,
  "INCLINATION": 97.5573,
  "RA_OF_ASC_NODE": 320.5096,
  "ARG_OF_PERICENTER": 251.3832,
  "MEAN_ANOMALY": 108.6959,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53444,
  "REV_AT_EPOCH": 21786,
  "BSTAR": 0.00061945,
  "MEAN_MOTION_DOT": 0.0009587,
  "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 07
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/53444

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