▸Orbital parameters

Orbit class	SSO
Inclination	97.9171°
Eccentricity	0.0004612
Period	97.8 min
Apogee	656 km
Perigee	650 km
Mean motion	14.72483364 rev/day
RAAN	346.5569°
Arg of perigee	192.2241°
Mean anomaly	167.8856°
B*	1.3340e-4
Rev at epoch	8,670

▸Two-line element set (TLE)

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

1 62082U 24219B 26188.20412279 .00000798 00000-0 13340-3 0 9996

2 62082 97.9171 346.5569 0004612 192.2241 167.8856 14.72483364 86700

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-5D",
  "OBJECT_ID": "2024-219B",
  "EPOCH": "2026-07-07T04:53:56.209+00:00",
  "MEAN_MOTION": 14.72483364,
  "ECCENTRICITY": 0.0004612,
  "INCLINATION": 97.9171,
  "RA_OF_ASC_NODE": 346.5569,
  "ARG_OF_PERICENTER": 192.2241,
  "MEAN_ANOMALY": 167.8856,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62082,
  "REV_AT_EPOCH": 8670,
  "BSTAR": 0.0001334,
  "MEAN_MOTION_DOT": 0.00000798,
  "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	KINEIS-5D
Operator	KineisHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	Nov 25, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	28HIGHvia 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/62082

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