▸Orbital parameters

Orbit class	LEO
Inclination	50.0035°
Eccentricity	0.0021273
Period	97.1 min
Apogee	634 km
Perigee	604 km
Mean motion	14.83339677 rev/day
RAAN	261.6825°
Arg of perigee	84.1699°
Mean anomaly	276.1663°
B*	1.4473e-4
Rev at epoch	13,188

▸Two-line element set (TLE)

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

1 58913U 24023J 26188.15898215 .00000972 00000-0 14473-3 0 9991

2 58913 50.0035 261.6825 0021273 84.1699 276.1663 14.83339677131886

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 09",
  "OBJECT_ID": "2024-023J",
  "EPOCH": "2026-07-07T03:48:56.058+00:00",
  "MEAN_MOTION": 14.83339677,
  "ECCENTRICITY": 0.0021273,
  "INCLINATION": 50.0035,
  "RA_OF_ASC_NODE": 261.6825,
  "ARG_OF_PERICENTER": 84.1699,
  "MEAN_ANOMALY": 276.1663,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58913,
  "REV_AT_EPOCH": 13188,
  "BSTAR": 0.00014473,
  "MEAN_MOTION_DOT": 0.00000972,
  "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-2 09
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Feb 2, 2024HIGHvia 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/58913

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