▸Orbital parameters

Orbit class	LEO
Inclination	49.9848°
Eccentricity	0.0009582
Period	97.0 min
Apogee	623 km
Perigee	610 km
Mean motion	14.84047543 rev/day
RAAN	81.6712°
Arg of perigee	164.1552°
Mean anomaly	195.9688°
B*	1.8686e-4
Rev at epoch	4,942

▸Two-line element set (TLE)

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

1 65120U 25170B 26188.15238457 .00001346 00000-0 18686-3 0 9995

2 65120 49.9848 81.6712 0009582 164.1552 195.9688 14.84047543 49426

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 02",
  "OBJECT_ID": "2025-170B",
  "EPOCH": "2026-07-07T03:39:26.027+00:00",
  "MEAN_MOTION": 14.84047543,
  "ECCENTRICITY": 0.0009582,
  "INCLINATION": 49.9848,
  "RA_OF_ASC_NODE": 81.6712,
  "ARG_OF_PERICENTER": 164.1552,
  "MEAN_ANOMALY": 195.9688,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65120,
  "REV_AT_EPOCH": 4942,
  "BSTAR": 0.00018686,
  "MEAN_MOTION_DOT": 0.00001346,
  "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-4 02
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Aug 8, 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/65120

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