▸Orbital parameters

Orbit class	LEO
Inclination	50.0037°
Eccentricity	0.0010873
Period	97.1 min
Apogee	626 km
Perigee	611 km
Mean motion	14.83327441 rev/day
RAAN	261.8233°
Arg of perigee	142.6224°
Mean anomaly	217.5472°
B*	1.5399e-4
Rev at epoch	13,188

▸Two-line element set (TLE)

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

1 58909U 24023E 26188.16612840 .00001048 00000-0 15399-3 0 9998

2 58909 50.0037 261.8233 0010873 142.6224 217.5472 14.83327441131889

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 05",
  "OBJECT_ID": "2024-023E",
  "EPOCH": "2026-07-07T03:59:13.494+00:00",
  "MEAN_MOTION": 14.83327441,
  "ECCENTRICITY": 0.0010873,
  "INCLINATION": 50.0037,
  "RA_OF_ASC_NODE": 261.8233,
  "ARG_OF_PERICENTER": 142.6224,
  "MEAN_ANOMALY": 217.5472,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58909,
  "REV_AT_EPOCH": 13188,
  "BSTAR": 0.00015399,
  "MEAN_MOTION_DOT": 0.00001048,
  "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-2 05
Operator	GeeSpaceHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Feb 2, 2024HIGHvia 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/58909

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