▸Orbital parameters

Orbit class	LEO
Inclination	49.9988°
Eccentricity	0.0019480
Period	97.1 min
Apogee	633 km
Perigee	605 km
Mean motion	14.83326919 rev/day
RAAN	261.4214°
Arg of perigee	190.7702°
Mean anomaly	169.2822°
B*	1.7762e-4
Rev at epoch	13,188

▸Two-line element set (TLE)

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

1 58915U 24023L 26188.17334426 .00001245 00000-0 17762-3 0 9992

2 58915 49.9988 261.4214 0019480 190.7702 169.2822 14.83326919131882

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 11",
  "OBJECT_ID": "2024-023L",
  "EPOCH": "2026-07-07T04:09:36.944+00:00",
  "MEAN_MOTION": 14.83326919,
  "ECCENTRICITY": 0.001948,
  "INCLINATION": 49.9988,
  "RA_OF_ASC_NODE": 261.4214,
  "ARG_OF_PERICENTER": 190.7702,
  "MEAN_ANOMALY": 169.2822,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58915,
  "REV_AT_EPOCH": 13188,
  "BSTAR": 0.00017762,
  "MEAN_MOTION_DOT": 0.00001245,
  "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 11
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/58915

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