▸Orbital parameters

Orbit class	LEO
Inclination	49.9924°
Eccentricity	0.0022721
Period	97.2 min
Apogee	641 km
Perigee	609 km
Mean motion	14.81454983 rev/day
RAAN	110.2619°
Arg of perigee	337.9858°
Mean anomaly	22.0101°
B*	2.0736e-4
Rev at epoch	22,289

▸Two-line element set (TLE)

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

1 52785U 22058A 26188.15506757 .00001421 00000-0 20736-3 0 9994

2 52785 49.9924 110.2619 0022721 337.9858 22.0101 14.81454983222899

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-1 01",
  "OBJECT_ID": "2022-058A",
  "EPOCH": "2026-07-07T03:43:17.838+00:00",
  "MEAN_MOTION": 14.81454983,
  "ECCENTRICITY": 0.0022721,
  "INCLINATION": 49.9924,
  "RA_OF_ASC_NODE": 110.2619,
  "ARG_OF_PERICENTER": 337.9858,
  "MEAN_ANOMALY": 22.0101,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52785,
  "REV_AT_EPOCH": 22289,
  "BSTAR": 0.00020736,
  "MEAN_MOTION_DOT": 0.00001421,
  "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 01
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/52785

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