▸Orbital parameters

Orbit class	LEO
Inclination	49.9949°
Eccentricity	0.0004881
Period	97.1 min
Apogee	622 km
Perigee	615 km
Mean motion	14.83319856 rev/day
RAAN	261.3098°
Arg of perigee	110.0839°
Mean anomaly	250.0624°
B*	1.7663e-4
Rev at epoch	13,188

▸Two-line element set (TLE)

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

1 58905U 24023A 26188.21867119 .00001236 00000-0 17663-3 0 9996

2 58905 49.9949 261.3098 0004881 110.0839 250.0624 14.83319856131883

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 01",
  "OBJECT_ID": "2024-023A",
  "EPOCH": "2026-07-07T05:14:53.191+00:00",
  "MEAN_MOTION": 14.83319856,
  "ECCENTRICITY": 0.0004881,
  "INCLINATION": 49.9949,
  "RA_OF_ASC_NODE": 261.3098,
  "ARG_OF_PERICENTER": 110.0839,
  "MEAN_ANOMALY": 250.0624,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58905,
  "REV_AT_EPOCH": 13188,
  "BSTAR": 0.00017663,
  "MEAN_MOTION_DOT": 0.00001236,
  "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 01
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/58905

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