▸Orbital parameters

Orbit class	LEO
Inclination	49.9945°
Eccentricity	0.0009355
Period	97.1 min
Apogee	625 km
Perigee	612 km
Mean motion	14.83308879 rev/day
RAAN	261.2417°
Arg of perigee	74.5323°
Mean anomaly	285.6648°
B*	1.7499e-4
Rev at epoch	13,188

▸Two-line element set (TLE)

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

1 58914U 24023K 26188.21084367 .00001221 00000-0 17499-3 0 9993

2 58914 49.9945 261.2417 0009355 74.5323 285.6648 14.83308879131889

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 10",
  "OBJECT_ID": "2024-023K",
  "EPOCH": "2026-07-07T05:03:36.893+00:00",
  "MEAN_MOTION": 14.83308879,
  "ECCENTRICITY": 0.0009355,
  "INCLINATION": 49.9945,
  "RA_OF_ASC_NODE": 261.2417,
  "ARG_OF_PERICENTER": 74.5323,
  "MEAN_ANOMALY": 285.6648,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58914,
  "REV_AT_EPOCH": 13188,
  "BSTAR": 0.00017499,
  "MEAN_MOTION_DOT": 0.00001221,
  "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 10
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/58914

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