▸Orbital parameters

Orbit class	LEO
Inclination	49.9701°
Eccentricity	0.0029900
Period	97.2 min
Apogee	643 km
Perigee	601 km
Mean motion	14.82210124 rev/day
RAAN	35.3326°
Arg of perigee	29.7587°
Mean anomaly	330.5044°
B*	1.9245e-4
Rev at epoch	5,001

▸Two-line element set (TLE)

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

1 65122U 25170D 26188.16310325 .00001331 00000-0 19245-3 0 9999

2 65122 49.9701 35.3326 0029900 29.7587 330.5044 14.82210124 50018

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 04",
  "OBJECT_ID": "2025-170D",
  "EPOCH": "2026-07-07T03:54:52.121+00:00",
  "MEAN_MOTION": 14.82210124,
  "ECCENTRICITY": 0.00299,
  "INCLINATION": 49.9701,
  "RA_OF_ASC_NODE": 35.3326,
  "ARG_OF_PERICENTER": 29.7587,
  "MEAN_ANOMALY": 330.5044,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65122,
  "REV_AT_EPOCH": 5001,
  "BSTAR": 0.00019245,
  "MEAN_MOTION_DOT": 0.00001331,
  "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 04
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/65122

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