▸Orbital parameters

Orbit class	LEO
Inclination	49.9833°
Eccentricity	0.0006841
Period	97.0 min
Apogee	621 km
Perigee	612 km
Mean motion	14.84065505 rev/day
RAAN	81.3612°
Arg of perigee	166.8157°
Mean anomaly	193.2961°
B*	2.0085e-4
Rev at epoch	4,939

▸Two-line element set (TLE)

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

1 65129U 25170L 26188.10672096 .00001465 00000-0 20085-3 0 9998

2 65129 49.9833 81.3612 0006841 166.8157 193.2961 14.84065505 49399

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 11",
  "OBJECT_ID": "2025-170L",
  "EPOCH": "2026-07-07T02:33:40.691+00:00",
  "MEAN_MOTION": 14.84065505,
  "ECCENTRICITY": 0.0006841,
  "INCLINATION": 49.9833,
  "RA_OF_ASC_NODE": 81.3612,
  "ARG_OF_PERICENTER": 166.8157,
  "MEAN_ANOMALY": 193.2961,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65129,
  "REV_AT_EPOCH": 4939,
  "BSTAR": 0.00020085,
  "MEAN_MOTION_DOT": 0.00001465,
  "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 11
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/65129

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