▸Orbital parameters

Orbit class	LEO
Inclination	49.9942°
Eccentricity	0.0011222
Period	97.0 min
Apogee	624 km
Perigee	608 km
Mean motion	14.84291710 rev/day
RAAN	350.5886°
Arg of perigee	109.9729°
Mean anomaly	250.2419°
B*	2.3588e-4
Rev at epoch	9,910

▸Two-line element set (TLE)

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

1 61017U 24159G 26188.09841205 .00001771 00000-0 23588-3 0 9995

2 61017 49.9942 350.5886 0011222 109.9729 250.2419 14.84291710 99103

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 07",
  "OBJECT_ID": "2024-159G",
  "EPOCH": "2026-07-07T02:21:42.801+00:00",
  "MEAN_MOTION": 14.8429171,
  "ECCENTRICITY": 0.0011222,
  "INCLINATION": 49.9942,
  "RA_OF_ASC_NODE": 350.5886,
  "ARG_OF_PERICENTER": 109.9729,
  "MEAN_ANOMALY": 250.2419,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61017,
  "REV_AT_EPOCH": 9910,
  "BSTAR": 0.00023588,
  "MEAN_MOTION_DOT": 0.00001771,
  "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 07
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/61017

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