▸Orbital parameters

Orbit class	LEO
Inclination	49.9940°
Eccentricity	0.0005668
Period	97.0 min
Apogee	620 km
Perigee	612 km
Mean motion	14.84305783 rev/day
RAAN	349.7586°
Arg of perigee	201.9054°
Mean anomaly	158.1643°
B*	2.5153e-4
Rev at epoch	9,979

▸Two-line element set (TLE)

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

1 61013U 24159C 26188.08357507 .00001905 00000-0 25153-3 0 9996

2 61013 49.9940 349.7586 0005668 201.9054 158.1643 14.84305783 99791

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 03",
  "OBJECT_ID": "2024-159C",
  "EPOCH": "2026-07-07T02:00:20.886+00:00",
  "MEAN_MOTION": 14.84305783,
  "ECCENTRICITY": 0.0005668,
  "INCLINATION": 49.994,
  "RA_OF_ASC_NODE": 349.7586,
  "ARG_OF_PERICENTER": 201.9054,
  "MEAN_ANOMALY": 158.1643,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61013,
  "REV_AT_EPOCH": 9979,
  "BSTAR": 0.00025153,
  "MEAN_MOTION_DOT": 0.00001905,
  "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 03
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/61013

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