▸Orbital parameters

Orbit class	LEO
Inclination	50.0057°
Eccentricity	0.0027805
Period	97.0 min
Apogee	635 km
Perigee	596 km
Mean motion	14.84305455 rev/day
RAAN	350.6721°
Arg of perigee	169.9443°
Mean anomaly	190.2058°
B*	2.5792e-4
Rev at epoch	9,973

▸Two-line element set (TLE)

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

1 61018U 24159H 26188.11337814 .00001967 00000-0 25792-3 0 9991

2 61018 50.0057 350.6721 0027805 169.9443 190.2058 14.84305455 99739

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 08",
  "OBJECT_ID": "2024-159H",
  "EPOCH": "2026-07-07T02:43:15.871+00:00",
  "MEAN_MOTION": 14.84305455,
  "ECCENTRICITY": 0.0027805,
  "INCLINATION": 50.0057,
  "RA_OF_ASC_NODE": 350.6721,
  "ARG_OF_PERICENTER": 169.9443,
  "MEAN_ANOMALY": 190.2058,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61018,
  "REV_AT_EPOCH": 9973,
  "BSTAR": 0.00025792,
  "MEAN_MOTION_DOT": 0.00001967,
  "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 08
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/61018

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