▸Orbital parameters

Orbit class	LEO
Inclination	50.0007°
Eccentricity	0.0002532
Period	97.0 min
Apogee	618 km
Perigee	614 km
Mean motion	14.84315103 rev/day
RAAN	350.8673°
Arg of perigee	317.6123°
Mean anomaly	42.4620°
B*	2.2998e-4
Rev at epoch	9,963

▸Two-line element set (TLE)

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

1 61011U 24159A 26188.06864073 .00001723 00000-0 22998-3 0 9995

2 61011 50.0007 350.8673 0002532 317.6123 42.4620 14.84315103 99635

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 01",
  "OBJECT_ID": "2024-159A",
  "EPOCH": "2026-07-07T01:38:50.559+00:00",
  "MEAN_MOTION": 14.84315103,
  "ECCENTRICITY": 0.0002532,
  "INCLINATION": 50.0007,
  "RA_OF_ASC_NODE": 350.8673,
  "ARG_OF_PERICENTER": 317.6123,
  "MEAN_ANOMALY": 42.462,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61011,
  "REV_AT_EPOCH": 9963,
  "BSTAR": 0.00022998,
  "MEAN_MOTION_DOT": 0.00001723,
  "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 01
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/61011

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