▸Orbital parameters

Orbit class	LEO
Inclination	49.9947°
Eccentricity	0.0018949
Period	97.0 min
Apogee	629 km
Perigee	603 km
Mean motion	14.84296790 rev/day
RAAN	351.1252°
Arg of perigee	133.0539°
Mean anomaly	227.1990°
B*	2.4882e-4
Rev at epoch	9,974

▸Two-line element set (TLE)

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

1 61012U 24159B 26188.06143138 .00001883 00000-0 24882-3 0 9999

2 61012 49.9947 351.1252 0018949 133.0539 227.1990 14.84296790 99747

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-3 02",
  "OBJECT_ID": "2024-159B",
  "EPOCH": "2026-07-07T01:28:27.671+00:00",
  "MEAN_MOTION": 14.8429679,
  "ECCENTRICITY": 0.0018949,
  "INCLINATION": 49.9947,
  "RA_OF_ASC_NODE": 351.1252,
  "ARG_OF_PERICENTER": 133.0539,
  "MEAN_ANOMALY": 227.199,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61012,
  "REV_AT_EPOCH": 9974,
  "BSTAR": 0.00024882,
  "MEAN_MOTION_DOT": 0.00001883,
  "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 02
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/61012

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