▸Orbital parameters

Orbit class	LEO
Inclination	50.0042°
Eccentricity	0.0033399
Period	97.2 min
Apogee	648 km
Perigee	601 km
Mean motion	14.81487521 rev/day
RAAN	110.5898°
Arg of perigee	223.6772°
Mean anomaly	136.1521°
B*	1.8128e-4
Rev at epoch	22,289

▸Two-line element set (TLE)

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

1 52790U 22058F 26188.17763977 .00001219 00000-0 18128-3 0 9998

2 52790 50.0042 110.5898 0033399 223.6772 136.1521 14.81487521222897

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-1 06",
  "OBJECT_ID": "2022-058F",
  "EPOCH": "2026-07-07T04:15:48.076+00:00",
  "MEAN_MOTION": 14.81487521,
  "ECCENTRICITY": 0.0033399,
  "INCLINATION": 50.0042,
  "RA_OF_ASC_NODE": 110.5898,
  "ARG_OF_PERICENTER": 223.6772,
  "MEAN_ANOMALY": 136.1521,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52790,
  "REV_AT_EPOCH": 22289,
  "BSTAR": 0.00018128,
  "MEAN_MOTION_DOT": 0.00001219,
  "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 06
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/52790

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