▸Orbital parameters

Orbit class	LEO
Inclination	49.9902°
Eccentricity	0.0021860
Period	97.2 min
Apogee	640 km
Perigee	609 km
Mean motion	14.81449195 rev/day
RAAN	111.5888°
Arg of perigee	106.8009°
Mean anomaly	253.5328°
B*	2.0493e-4
Rev at epoch	4,896

▸Two-line element set (TLE)

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

1 65127U 25170J 26188.18544166 .00001400 00000-0 20493-3 0 9992

2 65127 49.9902 111.5888 0021860 106.8009 253.5328 14.81449195 48960

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-4 09",
  "OBJECT_ID": "2025-170J",
  "EPOCH": "2026-07-07T04:27:02.159+00:00",
  "MEAN_MOTION": 14.81449195,
  "ECCENTRICITY": 0.002186,
  "INCLINATION": 49.9902,
  "RA_OF_ASC_NODE": 111.5888,
  "ARG_OF_PERICENTER": 106.8009,
  "MEAN_ANOMALY": 253.5328,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65127,
  "REV_AT_EPOCH": 4896,
  "BSTAR": 0.00020493,
  "MEAN_MOTION_DOT": 0.000014,
  "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 09
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/65127

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