▸Orbital parameters

Orbit class	LEO
Inclination	49.9896°
Eccentricity	0.0010048
Period	97.1 min
Apogee	626 km
Perigee	612 km
Mean motion	14.83418938 rev/day
RAAN	216.1397°
Arg of perigee	290.2076°
Mean anomaly	69.7781°
B*	1.6175e-4
Rev at epoch	4,246

▸Two-line element set (TLE)

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

1 65720U 25214J 26188.10706853 .00001115 00000-0 16175-3 0 9990

2 65720 49.9896 216.1397 0010048 290.2076 69.7781 14.83418938 42468

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-6 08",
  "OBJECT_ID": "2025-214J",
  "EPOCH": "2026-07-07T02:34:10.721+00:00",
  "MEAN_MOTION": 14.83418938,
  "ECCENTRICITY": 0.0010048,
  "INCLINATION": 49.9896,
  "RA_OF_ASC_NODE": 216.1397,
  "ARG_OF_PERICENTER": 290.2076,
  "MEAN_ANOMALY": 69.7781,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65720,
  "REV_AT_EPOCH": 4246,
  "BSTAR": 0.00016175,
  "MEAN_MOTION_DOT": 0.00001115,
  "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 08
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/65720

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