▸Orbital parameters

Orbit class	LEO
Inclination	49.9971°
Eccentricity	0.0006505
Period	96.0 min
Apogee	569 km
Perigee	560 km
Mean motion	15.00716112 rev/day
RAAN	86.7348°
Arg of perigee	248.7810°
Mean anomaly	111.2441°
B*	2.2972e-4
Rev at epoch	22,324

▸Two-line element set (TLE)

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

1 52793U 22058J 26188.15511255 .00002683 00000-0 22972-3 0 9997

2 52793 49.9971 86.7348 0006505 248.7810 111.2441 15.00716112223240

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-1 09",
  "OBJECT_ID": "2022-058J",
  "EPOCH": "2026-07-07T03:43:21.724+00:00",
  "MEAN_MOTION": 15.00716112,
  "ECCENTRICITY": 0.0006505,
  "INCLINATION": 49.9971,
  "RA_OF_ASC_NODE": 86.7348,
  "ARG_OF_PERICENTER": 248.781,
  "MEAN_ANOMALY": 111.2441,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52793,
  "REV_AT_EPOCH": 22324,
  "BSTAR": 0.00022972,
  "MEAN_MOTION_DOT": 0.00002683,
  "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 09
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/52793

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