▸Orbital parameters

Orbit class	SSO
Inclination	98.0412°
Eccentricity	0.0002209
Period	97.8 min
Apogee	655 km
Perigee	652 km
Mean motion	14.72278926 rev/day
RAAN	278.0002°
Arg of perigee	46.7741°
Mean anomaly	313.3650°
B*	2.3614e-4
Rev at epoch	9,629

▸Two-line element set (TLE)

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

1 61224U 24172E 26188.19933163 .00001442 00000-0 23614-3 0 9991

2 61224 98.0412 278.0002 0002209 46.7741 313.3650 14.72278926 96297

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-3B",
  "OBJECT_ID": "2024-172E",
  "EPOCH": "2026-07-07T04:47:02.253+00:00",
  "MEAN_MOTION": 14.72278926,
  "ECCENTRICITY": 0.0002209,
  "INCLINATION": 98.0412,
  "RA_OF_ASC_NODE": 278.0002,
  "ARG_OF_PERICENTER": 46.7741,
  "MEAN_ANOMALY": 313.365,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61224,
  "REV_AT_EPOCH": 9629,
  "BSTAR": 0.00023614,
  "MEAN_MOTION_DOT": 0.00001442,
  "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-3B
Operator	KineisHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	Sep 20, 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/61224

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