▸Orbital parameters

Orbit class	LEO
Inclination	49.9947°
Eccentricity	0.0007971
Period	97.2 min
Apogee	628 km
Perigee	617 km
Mean motion	14.82210716 rev/day
RAAN	36.3660°
Arg of perigee	38.0611°
Mean anomaly	322.0889°
B*	1.9130e-4
Rev at epoch	5,000

▸Two-line element set (TLE)

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

1 65123U 25170E 26188.12920594 .00001317 00000-0 19130-3 0 9998

2 65123 49.9947 36.3660 0007971 38.0611 322.0889 14.82210716 50007

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 05",
  "OBJECT_ID": "2025-170E",
  "EPOCH": "2026-07-07T03:06:03.393+00:00",
  "MEAN_MOTION": 14.82210716,
  "ECCENTRICITY": 0.0007971,
  "INCLINATION": 49.9947,
  "RA_OF_ASC_NODE": 36.366,
  "ARG_OF_PERICENTER": 38.0611,
  "MEAN_ANOMALY": 322.0889,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65123,
  "REV_AT_EPOCH": 5000,
  "BSTAR": 0.0001913,
  "MEAN_MOTION_DOT": 0.00001317,
  "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 05
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/65123

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