▸Orbital parameters

Orbit class	SSO
Inclination	97.3280°
Eccentricity	0.0025143
Period	93.9 min
Apogee	480 km
Perigee	446 km
Mean motion	15.34250254 rev/day
RAAN	263.9286°
Arg of perigee	330.7459°
Mean anomaly	29.2374°
B*	2.1879e-4
Rev at epoch	12,071

▸Two-line element set (TLE)

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

1 59679U 24085C 26188.20034587 .00007246 00000-0 21879-3 0 9998

2 59679 97.3280 263.9286 0025143 330.7459 29.2374 15.34250254120718

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2024-085C",
  "OBJECT_ID": "2024-085C",
  "EPOCH": "2026-07-07T04:48:29.883+00:00",
  "MEAN_MOTION": 15.34250254,
  "ECCENTRICITY": 0.0025143,
  "INCLINATION": 97.328,
  "RA_OF_ASC_NODE": 263.9286,
  "ARG_OF_PERICENTER": 330.7459,
  "MEAN_ANOMALY": 29.2374,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59679,
  "REV_AT_EPOCH": 12071,
  "BSTAR": 0.00021879,
  "MEAN_MOTION_DOT": 0.00007246,
  "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	2024-085C
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/59679

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