▸Orbital parameters

Orbit class	LEO
Inclination	49.9837°
Eccentricity	0.0009871
Period	97.1 min
Apogee	625 km
Perigee	612 km
Mean motion	14.83450197 rev/day
RAAN	215.9537°
Arg of perigee	301.1553°
Mean anomaly	58.8417°
B*	1.8144e-4
Rev at epoch	4,246

▸Two-line element set (TLE)

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

1 65716U 25214E 26188.09908963 .00001280 00000-0 18144-3 0 9990

2 65716 49.9837 215.9537 0009871 301.1553 58.8417 14.83450197 42463

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-6 04",
  "OBJECT_ID": "2025-214E",
  "EPOCH": "2026-07-07T02:22:41.344+00:00",
  "MEAN_MOTION": 14.83450197,
  "ECCENTRICITY": 0.0009871,
  "INCLINATION": 49.9837,
  "RA_OF_ASC_NODE": 215.9537,
  "ARG_OF_PERICENTER": 301.1553,
  "MEAN_ANOMALY": 58.8417,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65716,
  "REV_AT_EPOCH": 4246,
  "BSTAR": 0.00018144,
  "MEAN_MOTION_DOT": 0.0000128,
  "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 04
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/65716

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