▸Orbital parameters

Orbit class	LEO
Inclination	49.9780°
Eccentricity	0.0024933
Period	97.2 min
Apogee	640 km
Perigee	605 km
Mean motion	14.82237094 rev/day
RAAN	34.8955°
Arg of perigee	7.6696°
Mean anomaly	352.4618°
B*	1.8274e-4
Rev at epoch	5,002

▸Two-line element set (TLE)

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

1 65128U 25170K 26188.18111762 .00001251 00000-0 18274-3 0 9993

2 65128 49.9780 34.8955 0024933 7.6696 352.4618 14.82237094 50026

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 10",
  "OBJECT_ID": "2025-170K",
  "EPOCH": "2026-07-07T04:20:48.562+00:00",
  "MEAN_MOTION": 14.82237094,
  "ECCENTRICITY": 0.0024933,
  "INCLINATION": 49.978,
  "RA_OF_ASC_NODE": 34.8955,
  "ARG_OF_PERICENTER": 7.6696,
  "MEAN_ANOMALY": 352.4618,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65128,
  "REV_AT_EPOCH": 5002,
  "BSTAR": 0.00018274,
  "MEAN_MOTION_DOT": 0.00001251,
  "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 10
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/65128

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