▸Orbital parameters

Orbit class	LEO
Inclination	49.9917°
Eccentricity	0.0020144
Period	97.0 min
Apogee	631 km
Perigee	602 km
Mean motion	14.84063185 rev/day
RAAN	81.3544°
Arg of perigee	137.4006°
Mean anomaly	222.8499°
B*	2.0123e-4
Rev at epoch	4,940

▸Two-line element set (TLE)

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

1 65121U 25170C 26188.18511139 .00001469 00000-0 20123-3 0 9995

2 65121 49.9917 81.3544 0020144 137.4006 222.8499 14.84063185 49406

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 03",
  "OBJECT_ID": "2025-170C",
  "EPOCH": "2026-07-07T04:26:33.624+00:00",
  "MEAN_MOTION": 14.84063185,
  "ECCENTRICITY": 0.0020144,
  "INCLINATION": 49.9917,
  "RA_OF_ASC_NODE": 81.3544,
  "ARG_OF_PERICENTER": 137.4006,
  "MEAN_ANOMALY": 222.8499,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65121,
  "REV_AT_EPOCH": 4940,
  "BSTAR": 0.00020123,
  "MEAN_MOTION_DOT": 0.00001469,
  "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 03
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/65121

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