▸Orbital parameters

Orbit class	LEO
Inclination	49.9869°
Eccentricity	0.0005308
Period	95.7 min
Apogee	557 km
Perigee	550 km
Mean motion	15.04359909 rev/day
RAAN	204.0223°
Arg of perigee	135.1031°
Mean anomaly	225.0346°
B*	1.6022e-4
Rev at epoch	13,265

▸Two-line element set (TLE)

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

1 58910U 24023F 26188.17361382 .00001989 00000-0 16022-3 0 9991

2 58910 49.9869 204.0223 0005308 135.1031 225.0346 15.04359909132657

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 06",
  "OBJECT_ID": "2024-023F",
  "EPOCH": "2026-07-07T04:10:00.234+00:00",
  "MEAN_MOTION": 15.04359909,
  "ECCENTRICITY": 0.0005308,
  "INCLINATION": 49.9869,
  "RA_OF_ASC_NODE": 204.0223,
  "ARG_OF_PERICENTER": 135.1031,
  "MEAN_ANOMALY": 225.0346,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58910,
  "REV_AT_EPOCH": 13265,
  "BSTAR": 0.00016022,
  "MEAN_MOTION_DOT": 0.00001989,
  "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 06
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/58910

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