▸Orbital parameters

Orbit class	SSO
Inclination	97.8957°
Eccentricity	0.0003141
Period	97.8 min
Apogee	656 km
Perigee	652 km
Mean motion	14.72289083 rev/day
RAAN	346.1558°
Arg of perigee	233.6875°
Mean anomaly	126.4043°
B*	1.9839e-4
Rev at epoch	8,660

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 62084U 24219D 26187.45123198 .00001205 00000-0 19839-3 0 9996

2 62084 97.8957 346.1558 0003141 233.6875 126.4043 14.72289083 86606

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-5A",
  "OBJECT_ID": "2024-219D",
  "EPOCH": "2026-07-06T10:49:46.443+00:00",
  "MEAN_MOTION": 14.72289083,
  "ECCENTRICITY": 0.00031406,
  "INCLINATION": 97.8957,
  "RA_OF_ASC_NODE": 346.1558,
  "ARG_OF_PERICENTER": 233.6875,
  "MEAN_ANOMALY": 126.4043,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62084,
  "REV_AT_EPOCH": 8660,
  "BSTAR": 0.00019838985,
  "MEAN_MOTION_DOT": 0.00001205,
  "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-5A
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/62084

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