▸Orbital parameters

Orbit class	LEO
Inclination	49.9833°
Eccentricity	0.0018623
Period	97.0 min
Apogee	630 km
Perigee	603 km
Mean motion	14.84086248 rev/day
RAAN	81.2354°
Arg of perigee	116.9529°
Mean anomaly	243.3314°
B*	2.0189e-4
Rev at epoch	4,940

▸Two-line element set (TLE)

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

1 65124U 25170F 26188.20838990 .00001475 00000-0 20189-3 0 9997

2 65124 49.9833 81.2354 0018623 116.9529 243.3314 14.84086248 49404

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 06",
  "OBJECT_ID": "2025-170F",
  "EPOCH": "2026-07-07T05:00:04.887+00:00",
  "MEAN_MOTION": 14.84086248,
  "ECCENTRICITY": 0.0018623,
  "INCLINATION": 49.9833,
  "RA_OF_ASC_NODE": 81.2354,
  "ARG_OF_PERICENTER": 116.9529,
  "MEAN_ANOMALY": 243.3314,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65124,
  "REV_AT_EPOCH": 4940,
  "BSTAR": 0.00020189,
  "MEAN_MOTION_DOT": 0.00001475,
  "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 06
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/65124

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