▸Orbital parameters

Orbit class	LEO
Inclination	49.9996°
Eccentricity	0.0023227
Period	97.2 min
Apogee	641 km
Perigee	609 km
Mean motion	14.81460187 rev/day
RAAN	110.4847°
Arg of perigee	328.3363°
Mean anomaly	31.6176°
B*	2.0678e-4
Rev at epoch	22,289

▸Two-line element set (TLE)

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

1 52786U 22058B 26188.16994954 .00001416 00000-0 20678-3 0 9995

2 52786 49.9996 110.4847 0023227 328.3363 31.6176 14.81460187222892

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-1 02",
  "OBJECT_ID": "2022-058B",
  "EPOCH": "2026-07-07T04:04:43.64+00:00",
  "MEAN_MOTION": 14.81460187,
  "ECCENTRICITY": 0.0023227,
  "INCLINATION": 49.9996,
  "RA_OF_ASC_NODE": 110.4847,
  "ARG_OF_PERICENTER": 328.3363,
  "MEAN_ANOMALY": 31.6176,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52786,
  "REV_AT_EPOCH": 22289,
  "BSTAR": 0.00020678,
  "MEAN_MOTION_DOT": 0.00001416,
  "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 02
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/52786

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