▸Orbital parameters

Orbit class	LEO
Inclination	49.9828°
Eccentricity	0.0010554
Period	97.1 min
Apogee	626 km
Perigee	611 km
Mean motion	14.83432422 rev/day
RAAN	219.8510°
Arg of perigee	286.9026°
Mean anomaly	73.0755°
B*	2.2019e-4
Rev at epoch	4,234

▸Two-line element set (TLE)

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

1 65714U 25214C 26187.32097903 .00001601 00000-0 22019-3 0 9999

2 65714 49.9828 219.8510 0010554 286.9026 73.0755 14.83432422 42342

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-6 02",
  "OBJECT_ID": "2025-214C",
  "EPOCH": "2026-07-06T07:42:12.588+00:00",
  "MEAN_MOTION": 14.83432422,
  "ECCENTRICITY": 0.00105538,
  "INCLINATION": 49.9828,
  "RA_OF_ASC_NODE": 219.851,
  "ARG_OF_PERICENTER": 286.9026,
  "MEAN_ANOMALY": 73.0755,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65714,
  "REV_AT_EPOCH": 4234,
  "BSTAR": 0.00022019199,
  "MEAN_MOTION_DOT": 0.00001601,
  "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 02
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/65714

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