▸Orbital parameters

Orbit class	LEO
Inclination	49.9832°
Eccentricity	0.0008908
Period	97.1 min
Apogee	625 km
Perigee	612 km
Mean motion	14.83432097 rev/day
RAAN	219.4399°
Arg of perigee	282.8091°
Mean anomaly	77.1851°
B*	1.9926e-4
Rev at epoch	4,235

▸Two-line element set (TLE)

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

1 65721U 25214K 26187.37338341 .00001428 00000-0 19926-3 0 9996

2 65721 49.9832 219.4399 0008908 282.8091 77.1851 14.83432097 42354

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-6 09",
  "OBJECT_ID": "2025-214K",
  "EPOCH": "2026-07-06T08:57:40.327+00:00",
  "MEAN_MOTION": 14.83432097,
  "ECCENTRICITY": 0.00089083,
  "INCLINATION": 49.9832,
  "RA_OF_ASC_NODE": 219.4399,
  "ARG_OF_PERICENTER": 282.8091,
  "MEAN_ANOMALY": 77.1851,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65721,
  "REV_AT_EPOCH": 4235,
  "BSTAR": 0.00019926489,
  "MEAN_MOTION_DOT": 0.00001428,
  "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 09
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/65721

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