▸Orbital parameters

Orbit class	LEO
Inclination	50.0000°
Eccentricity	0.0004016
Period	97.0 min
Apogee	619 km
Perigee	613 km
Mean motion	14.84287828 rev/day
RAAN	350.9082°
Arg of perigee	184.5960°
Mean anomaly	175.4942°
B*	2.3414e-4
Rev at epoch	9,946

▸Two-line element set (TLE)

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

1 61020U 24159K 26188.09109226 .00001757 00000-0 23414-3 0 9991

2 61020 50.0000 350.9082 0004016 184.5960 175.4942 14.84287828 99469

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 10",
  "OBJECT_ID": "2024-159K",
  "EPOCH": "2026-07-07T02:11:10.371+00:00",
  "MEAN_MOTION": 14.84287828,
  "ECCENTRICITY": 0.0004016,
  "INCLINATION": 50,
  "RA_OF_ASC_NODE": 350.9082,
  "ARG_OF_PERICENTER": 184.596,
  "MEAN_ANOMALY": 175.4942,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61020,
  "REV_AT_EPOCH": 9946,
  "BSTAR": 0.00023414,
  "MEAN_MOTION_DOT": 0.00001757,
  "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 10
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/61020

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