▸Orbital parameters

Orbit class	LEO
Inclination	49.9885°
Eccentricity	0.0003510
Period	97.1 min
Apogee	621 km
Perigee	616 km
Mean motion	14.83321664 rev/day
RAAN	260.6125°
Arg of perigee	63.6294°
Mean anomaly	296.5004°
B*	1.6858e-4
Rev at epoch	13,188

▸Two-line element set (TLE)

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

1 58912U 24023H 26188.18094366 .00001170 00000-0 16858-3 0 9998

2 58912 49.9885 260.6125 0003510 63.6294 296.5004 14.83321664131886

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GEESAT-2 08",
  "OBJECT_ID": "2024-023H",
  "EPOCH": "2026-07-07T04:20:33.532+00:00",
  "MEAN_MOTION": 14.83321664,
  "ECCENTRICITY": 0.000351,
  "INCLINATION": 49.9885,
  "RA_OF_ASC_NODE": 260.6125,
  "ARG_OF_PERICENTER": 63.6294,
  "MEAN_ANOMALY": 296.5004,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58912,
  "REV_AT_EPOCH": 13188,
  "BSTAR": 0.00016858,
  "MEAN_MOTION_DOT": 0.0000117,
  "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 08
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/58912

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