▸Orbital parameters

Orbit class	LEO
Inclination	50.0006°
Eccentricity	0.0005689
Period	96.2 min
Apogee	580 km
Perigee	572 km
Mean motion	14.97174604 rev/day
RAAN	229.5331°
Arg of perigee	115.4314°
Mean anomaly	244.7219°
B*	1.2000e-4
Rev at epoch	13,232

▸Two-line element set (TLE)

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

1 58907U 24023C 26188.20378299 .00001147 00000-0 12000-3 0 9994

2 58907 50.0006 229.5331 0005689 115.4314 244.7219 14.97174604132327

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 03",
  "OBJECT_ID": "2024-023C",
  "EPOCH": "2026-07-07T04:53:26.85+00:00",
  "MEAN_MOTION": 14.97174604,
  "ECCENTRICITY": 0.0005689,
  "INCLINATION": 50.0006,
  "RA_OF_ASC_NODE": 229.5331,
  "ARG_OF_PERICENTER": 115.4314,
  "MEAN_ANOMALY": 244.7219,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58907,
  "REV_AT_EPOCH": 13232,
  "BSTAR": 0.00012,
  "MEAN_MOTION_DOT": 0.00001147,
  "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 03
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/58907

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