▸Orbital parameters

Orbit class	LEO
Inclination	50.0033°
Eccentricity	0.0009569
Period	97.2 min
Apogee	631 km
Perigee	618 km
Mean motion	14.81470218 rev/day
RAAN	110.9168°
Arg of perigee	227.2239°
Mean anomaly	132.7894°
B*	2.1009e-4
Rev at epoch	22,288

▸Two-line element set (TLE)

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

1 52788U 22058D 26188.13990155 .00001441 00000-0 21009-3 0 9990

2 52788 50.0033 110.9168 0009569 227.2239 132.7894 14.81470218222887

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-1 04",
  "OBJECT_ID": "2022-058D",
  "EPOCH": "2026-07-07T03:21:27.494+00:00",
  "MEAN_MOTION": 14.81470218,
  "ECCENTRICITY": 0.0009569,
  "INCLINATION": 50.0033,
  "RA_OF_ASC_NODE": 110.9168,
  "ARG_OF_PERICENTER": 227.2239,
  "MEAN_ANOMALY": 132.7894,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52788,
  "REV_AT_EPOCH": 22288,
  "BSTAR": 0.00021009,
  "MEAN_MOTION_DOT": 0.00001441,
  "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	GEESAT-1 04
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jun 2, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	130HIGHvia 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/52788

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