▸Orbital parameters

Orbit class	LEO
Inclination	50.0033°
Eccentricity	0.0012982
Period	97.0 min
Apogee	625 km
Perigee	607 km
Mean motion	14.84273736 rev/day
RAAN	351.3850°
Arg of perigee	132.6096°
Mean anomaly	227.5940°
B*	2.7386e-4
Rev at epoch	9,972

▸Two-line element set (TLE)

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

1 61015U 24159E 26188.00812905 .00002093 00000-0 27386-3 0 9997

2 61015 50.0033 351.3850 0012982 132.6096 227.5940 14.84273736 99721

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 05",
  "OBJECT_ID": "2024-159E",
  "EPOCH": "2026-07-07T00:11:42.35+00:00",
  "MEAN_MOTION": 14.84273736,
  "ECCENTRICITY": 0.0012982,
  "INCLINATION": 50.0033,
  "RA_OF_ASC_NODE": 351.385,
  "ARG_OF_PERICENTER": 132.6096,
  "MEAN_ANOMALY": 227.594,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61015,
  "REV_AT_EPOCH": 9972,
  "BSTAR": 0.00027386,
  "MEAN_MOTION_DOT": 0.00002093,
  "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 05
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/61015

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