▸Orbital parameters

Orbit class	LEO
Inclination	49.9885°
Eccentricity	0.0012000
Period	97.1 min
Apogee	627 km
Perigee	610 km
Mean motion	14.83430660 rev/day
RAAN	219.4116°
Arg of perigee	306.8932°
Mean anomaly	53.0906°
B*	1.8522e-4
Rev at epoch	4,236

▸Two-line element set (TLE)

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

1 65722U 25214L 26187.46332416 .00001311 00000-0 18522-3 0 9996

2 65722 49.9885 219.4116 0012000 306.8932 53.0906 14.83430660 42368

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-6 10",
  "OBJECT_ID": "2025-214L",
  "EPOCH": "2026-07-06T11:07:11.207+00:00",
  "MEAN_MOTION": 14.8343066,
  "ECCENTRICITY": 0.00119999,
  "INCLINATION": 49.9885,
  "RA_OF_ASC_NODE": 219.4116,
  "ARG_OF_PERICENTER": 306.8932,
  "MEAN_ANOMALY": 53.0906,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65722,
  "REV_AT_EPOCH": 4236,
  "BSTAR": 0.00018522374,
  "MEAN_MOTION_DOT": 0.00001311,
  "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 10
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/65722

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