▸Orbital parameters

Orbit class	LEO
Inclination	49.9780°
Eccentricity	0.0013117
Period	97.1 min
Apogee	628 km
Perigee	609 km
Mean motion	14.83429602 rev/day
RAAN	219.0736°
Arg of perigee	285.4268°
Mean anomaly	74.5220°
B*	1.8628e-4
Rev at epoch	4,236

▸Two-line element set (TLE)

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

1 65717U 25214F 26187.44855544 .00001320 00000-0 18628-3 0 9997

2 65717 49.9780 219.0736 0013117 285.4268 74.5220 14.83429602 42365

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-6 05",
  "OBJECT_ID": "2025-214F",
  "EPOCH": "2026-07-06T10:45:55.19+00:00",
  "MEAN_MOTION": 14.83429602,
  "ECCENTRICITY": 0.00131174,
  "INCLINATION": 49.978,
  "RA_OF_ASC_NODE": 219.0736,
  "ARG_OF_PERICENTER": 285.4268,
  "MEAN_ANOMALY": 74.522,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65717,
  "REV_AT_EPOCH": 4236,
  "BSTAR": 0.00018628418,
  "MEAN_MOTION_DOT": 0.0000132,
  "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 05
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/65717

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