▸Orbital parameters

Orbit class	LEO
Inclination	49.9981°
Eccentricity	0.0022210
Period	97.0 min
Apogee	631 km
Perigee	600 km
Mean motion	14.84301029 rev/day
RAAN	350.5463°
Arg of perigee	136.6668°
Mean anomaly	223.6021°
B*	2.5344e-4
Rev at epoch	9,972

▸Two-line element set (TLE)

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

1 61019U 24159J 26188.05362469 .00001924 00000-0 25344-3 0 9995

2 61019 49.9981 350.5463 0022210 136.6668 223.6021 14.84301029 99723

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 09",
  "OBJECT_ID": "2024-159J",
  "EPOCH": "2026-07-07T01:17:13.173+00:00",
  "MEAN_MOTION": 14.84301029,
  "ECCENTRICITY": 0.002221,
  "INCLINATION": 49.9981,
  "RA_OF_ASC_NODE": 350.5463,
  "ARG_OF_PERICENTER": 136.6668,
  "MEAN_ANOMALY": 223.6021,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61019,
  "REV_AT_EPOCH": 9972,
  "BSTAR": 0.00025344,
  "MEAN_MOTION_DOT": 0.00001924,
  "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-3 09
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 5, 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/61019

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