▸Orbital parameters

Orbit class	LEO
Inclination	50.0047°
Eccentricity	0.0010130
Period	97.1 min
Apogee	626 km
Perigee	612 km
Mean motion	14.83322636 rev/day
RAAN	262.0908°
Arg of perigee	138.4775°
Mean anomaly	221.6934°
B*	1.5495e-4
Rev at epoch	13,188

▸Two-line element set (TLE)

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

1 58911U 24023G 26188.19600551 .00001056 00000-0 15495-3 0 9996

2 58911 50.0047 262.0908 0010130 138.4775 221.6934 14.83322636131885

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 07",
  "OBJECT_ID": "2024-023G",
  "EPOCH": "2026-07-07T04:42:14.876+00:00",
  "MEAN_MOTION": 14.83322636,
  "ECCENTRICITY": 0.001013,
  "INCLINATION": 50.0047,
  "RA_OF_ASC_NODE": 262.0908,
  "ARG_OF_PERICENTER": 138.4775,
  "MEAN_ANOMALY": 221.6934,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58911,
  "REV_AT_EPOCH": 13188,
  "BSTAR": 0.00015495,
  "MEAN_MOTION_DOT": 0.00001056,
  "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 07
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/58911

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