▸Orbital parameters

Orbit class	LEO
Inclination	49.9925°
Eccentricity	0.0020260
Period	97.2 min
Apogee	639 km
Perigee	611 km
Mean motion	14.81456609 rev/day
RAAN	109.3686°
Arg of perigee	6.0505°
Mean anomaly	354.0674°
B*	2.1460e-4
Rev at epoch	22,289

▸Two-line element set (TLE)

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

1 52792U 22058H 26188.14745735 .00001477 00000-0 21460-3 0 9998

2 52792 49.9925 109.3686 0020260 6.0505 354.0674 14.81456609222890

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-1 08",
  "OBJECT_ID": "2022-058H",
  "EPOCH": "2026-07-07T03:32:20.315+00:00",
  "MEAN_MOTION": 14.81456609,
  "ECCENTRICITY": 0.002026,
  "INCLINATION": 49.9925,
  "RA_OF_ASC_NODE": 109.3686,
  "ARG_OF_PERICENTER": 6.0505,
  "MEAN_ANOMALY": 354.0674,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52792,
  "REV_AT_EPOCH": 22289,
  "BSTAR": 0.0002146,
  "MEAN_MOTION_DOT": 0.00001477,
  "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 08
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/52792

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