▸Orbital parameters

Orbit class	LEO
Inclination	49.9847°
Eccentricity	0.0012310
Period	97.1 min
Apogee	627 km
Perigee	610 km
Mean motion	14.83391161 rev/day
RAAN	216.4918°
Arg of perigee	303.1080°
Mean anomaly	56.8676°
B*	1.5914e-4
Rev at epoch	4,245

▸Two-line element set (TLE)

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

1 65713U 25214B 26188.06602426 .00001093 00000-0 15914-3 0 9993

2 65713 49.9847 216.4918 0012310 303.1080 56.8676 14.83391161 42458

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-6 01",
  "OBJECT_ID": "2025-214B",
  "EPOCH": "2026-07-07T01:35:04.496+00:00",
  "MEAN_MOTION": 14.83391161,
  "ECCENTRICITY": 0.001231,
  "INCLINATION": 49.9847,
  "RA_OF_ASC_NODE": 216.4918,
  "ARG_OF_PERICENTER": 303.108,
  "MEAN_ANOMALY": 56.8676,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65713,
  "REV_AT_EPOCH": 4245,
  "BSTAR": 0.00015914,
  "MEAN_MOTION_DOT": 0.00001093,
  "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-6 01
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Sep 24, 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/65713

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