▸Orbital parameters

Orbit class	LEO
Inclination	49.9986°
Eccentricity	0.0002445
Period	97.1 min
Apogee	621 km
Perigee	617 km
Mean motion	14.83317802 rev/day
RAAN	261.7768°
Arg of perigee	164.7337°
Mean anomaly	195.3675°
B*	2.4000e-4
Rev at epoch	10,096

▸Two-line element set (TLE)

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

1 61014U 24159D 26188.12089358 .00001761 00000-0 24000-3 0 9998

2 61014 49.9986 261.7768 0002445 164.7337 195.3675 14.83317802100961

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 04",
  "OBJECT_ID": "2024-159D",
  "EPOCH": "2026-07-07T02:54:05.205+00:00",
  "MEAN_MOTION": 14.83317802,
  "ECCENTRICITY": 0.0002445,
  "INCLINATION": 49.9986,
  "RA_OF_ASC_NODE": 261.7768,
  "ARG_OF_PERICENTER": 164.7337,
  "MEAN_ANOMALY": 195.3675,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61014,
  "REV_AT_EPOCH": 10096,
  "BSTAR": 0.00024,
  "MEAN_MOTION_DOT": 0.00001761,
  "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 04
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/61014

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