▸Orbital parameters

Orbit class	SSO
Inclination	97.3230°
Eccentricity	0.0012227
Period	93.7 min
Apogee	465 km
Perigee	449 km
Mean motion	15.36300936 rev/day
RAAN	263.8644°
Arg of perigee	349.4162°
Mean anomaly	10.6823°
B*	2.4905e-4
Rev at epoch	12,073

▸Two-line element set (TLE)

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

1 59680U 24085D 26188.19302154 .00008754 00000-0 24905-3 0 9994

2 59680 97.3230 263.8644 0012227 349.4162 10.6823 15.36300936120739

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2024-085D",
  "OBJECT_ID": "2024-085D",
  "EPOCH": "2026-07-07T04:37:57.061+00:00",
  "MEAN_MOTION": 15.36300936,
  "ECCENTRICITY": 0.0012227,
  "INCLINATION": 97.323,
  "RA_OF_ASC_NODE": 263.8644,
  "ARG_OF_PERICENTER": 349.4162,
  "MEAN_ANOMALY": 10.6823,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59680,
  "REV_AT_EPOCH": 12073,
  "BSTAR": 0.00024905,
  "MEAN_MOTION_DOT": 0.00008754,
  "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	2024-085D
Operator	Harbin Institute of TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 7, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	50HIGHvia 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/59680

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