▸Orbital parameters

Orbit class	SSO
Inclination	97.9016°
Eccentricity	0.0006109
Period	97.8 min
Apogee	658 km
Perigee	650 km
Mean motion	14.72292635 rev/day
RAAN	346.6172°
Arg of perigee	189.2069°
Mean anomaly	170.9028°
B*	9.6193e-5
Rev at epoch	8,671

▸Two-line element set (TLE)

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

1 62083U 24219C 26188.22089955 .00000560 00000-0 96193-4 0 9995

2 62083 97.9016 346.6172 0006109 189.2069 170.9028 14.72292635 86713

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-5E",
  "OBJECT_ID": "2024-219C",
  "EPOCH": "2026-07-07T05:18:05.721+00:00",
  "MEAN_MOTION": 14.72292635,
  "ECCENTRICITY": 0.0006109,
  "INCLINATION": 97.9016,
  "RA_OF_ASC_NODE": 346.6172,
  "ARG_OF_PERICENTER": 189.2069,
  "MEAN_ANOMALY": 170.9028,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62083,
  "REV_AT_EPOCH": 8671,
  "BSTAR": 0.000096193,
  "MEAN_MOTION_DOT": 0.0000056,
  "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-5E
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/62083

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