▸Orbital parameters

Orbit class	LEO
Inclination	49.9875°
Eccentricity	0.0010200
Period	97.0 min
Apogee	624 km
Perigee	609 km
Mean motion	14.84057118 rev/day
RAAN	81.8171°
Arg of perigee	125.9813°
Mean anomaly	234.2072°
B*	2.0264e-4
Rev at epoch	4,940

▸Two-line element set (TLE)

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

1 65119U 25170A 26188.16326399 .00001480 00000-0 20264-3 0 9991

2 65119 49.9875 81.8171 0010200 125.9813 234.2072 14.84057118 49400

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 01",
  "OBJECT_ID": "2025-170A",
  "EPOCH": "2026-07-07T03:55:06.009+00:00",
  "MEAN_MOTION": 14.84057118,
  "ECCENTRICITY": 0.00102,
  "INCLINATION": 49.9875,
  "RA_OF_ASC_NODE": 81.8171,
  "ARG_OF_PERICENTER": 125.9813,
  "MEAN_ANOMALY": 234.2072,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65119,
  "REV_AT_EPOCH": 4940,
  "BSTAR": 0.00020264,
  "MEAN_MOTION_DOT": 0.0000148,
  "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 01
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/65119

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