▸Orbital parameters

Orbit class	LEO
Inclination	49.9809°
Eccentricity	0.0008444
Period	97.0 min
Apogee	622 km
Perigee	610 km
Mean motion	14.84246587 rev/day
RAAN	309.9915°
Arg of perigee	340.2207°
Mean anomaly	19.8403°
B*	2.5759e-4
Rev at epoch	4,464

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 65558U 25201J 26187.34181016 .00001953 00000-0 25759-3 0 9996

2 65558 49.9809 309.9915 0008444 340.2207 19.8403 14.84246587 44646

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-5 09",
  "OBJECT_ID": "2025-201J",
  "EPOCH": "2026-07-06T08:12:12.398+00:00",
  "MEAN_MOTION": 14.84246587,
  "ECCENTRICITY": 0.00084438,
  "INCLINATION": 49.9809,
  "RA_OF_ASC_NODE": 309.9915,
  "ARG_OF_PERICENTER": 340.2207,
  "MEAN_ANOMALY": 19.8403,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65558,
  "REV_AT_EPOCH": 4464,
  "BSTAR": 0.00025759223,
  "MEAN_MOTION_DOT": 0.00001953,
  "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-5 09
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 8, 2025HIGHvia 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/65558

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