▸Orbital parameters

Orbit class	LEO
Inclination	49.9806°
Eccentricity	0.0013542
Period	97.1 min
Apogee	628 km
Perigee	609 km
Mean motion	14.83444667 rev/day
RAAN	215.8225°
Arg of perigee	298.3233°
Mean anomaly	61.6339°
B*	1.8362e-4
Rev at epoch	4,246

▸Two-line element set (TLE)

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

1 65715U 25214D 26188.09211708 .00001298 00000-0 18362-3 0 9994

2 65715 49.9806 215.8225 0013542 298.3233 61.6339 14.83444667 42463

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-6 03",
  "OBJECT_ID": "2025-214D",
  "EPOCH": "2026-07-07T02:12:38.916+00:00",
  "MEAN_MOTION": 14.83444667,
  "ECCENTRICITY": 0.0013542,
  "INCLINATION": 49.9806,
  "RA_OF_ASC_NODE": 215.8225,
  "ARG_OF_PERICENTER": 298.3233,
  "MEAN_ANOMALY": 61.6339,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65715,
  "REV_AT_EPOCH": 4246,
  "BSTAR": 0.00018362,
  "MEAN_MOTION_DOT": 0.00001298,
  "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 03
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/65715

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