▸Orbital parameters

Orbit class	LEO
Inclination	49.9987°
Eccentricity	0.0014400
Period	97.1 min
Apogee	629 km
Perigee	609 km
Mean motion	14.83306768 rev/day
RAAN	261.5394°
Arg of perigee	76.2394°
Mean anomaly	284.0145°
B*	1.7330e-4
Rev at epoch	13,188

▸Two-line element set (TLE)

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

1 58906U 24023B 26188.20364323 .00001207 00000-0 17330-3 0 9994

2 58906 49.9987 261.5394 0014400 76.2394 284.0145 14.83306768131887

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 02",
  "OBJECT_ID": "2024-023B",
  "EPOCH": "2026-07-07T04:53:14.775+00:00",
  "MEAN_MOTION": 14.83306768,
  "ECCENTRICITY": 0.00144,
  "INCLINATION": 49.9987,
  "RA_OF_ASC_NODE": 261.5394,
  "ARG_OF_PERICENTER": 76.2394,
  "MEAN_ANOMALY": 284.0145,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58906,
  "REV_AT_EPOCH": 13188,
  "BSTAR": 0.0001733,
  "MEAN_MOTION_DOT": 0.00001207,
  "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 02
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/58906

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