▸Orbital parameters

Orbit class	LEO
Inclination	49.9656°
Eccentricity	0.0020870
Period	97.2 min
Apogee	637 km
Perigee	608 km
Mean motion	14.82194884 rev/day
RAAN	35.0232°
Arg of perigee	58.6188°
Mean anomaly	301.6787°
B*	1.9534e-4
Rev at epoch	5,001

▸Two-line element set (TLE)

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

1 65126U 25170H 26188.14563730 .00001351 00000-0 19534-3 0 9994

2 65126 49.9656 35.0232 0020870 58.6188 301.6787 14.82194884 50016

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 08",
  "OBJECT_ID": "2025-170H",
  "EPOCH": "2026-07-07T03:29:43.063+00:00",
  "MEAN_MOTION": 14.82194884,
  "ECCENTRICITY": 0.002087,
  "INCLINATION": 49.9656,
  "RA_OF_ASC_NODE": 35.0232,
  "ARG_OF_PERICENTER": 58.6188,
  "MEAN_ANOMALY": 301.6787,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65126,
  "REV_AT_EPOCH": 5001,
  "BSTAR": 0.00019534,
  "MEAN_MOTION_DOT": 0.00001351,
  "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 08
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/65126

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