▸Orbital parameters

Orbit class	LEO
Inclination	49.9922°
Eccentricity	0.0005839
Period	96.2 min
Apogee	579 km
Perigee	571 km
Mean motion	14.97271335 rev/day
RAAN	228.6325°
Arg of perigee	118.8018°
Mean anomaly	241.3513°
B*	1.2128e-4
Rev at epoch	13,232

▸Two-line element set (TLE)

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

1 58908U 24023D 26188.17635044 .00001165 00000-0 12128-3 0 9996

2 58908 49.9922 228.6325 0005839 118.8018 241.3513 14.97271335132329

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 04",
  "OBJECT_ID": "2024-023D",
  "EPOCH": "2026-07-07T04:13:56.678+00:00",
  "MEAN_MOTION": 14.97271335,
  "ECCENTRICITY": 0.0005839,
  "INCLINATION": 49.9922,
  "RA_OF_ASC_NODE": 228.6325,
  "ARG_OF_PERICENTER": 118.8018,
  "MEAN_ANOMALY": 241.3513,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58908,
  "REV_AT_EPOCH": 13232,
  "BSTAR": 0.00012128,
  "MEAN_MOTION_DOT": 0.00001165,
  "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-2 04
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Feb 2, 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/58908

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