▸Orbital parameters

Orbit class	SSO
Inclination	97.9141°
Eccentricity	0.0004655
Period	97.8 min
Apogee	657 km
Perigee	650 km
Mean motion	14.72312391 rev/day
RAAN	311.7605°
Arg of perigee	220.7241°
Mean anomaly	139.3619°
B*	2.2370e-4
Rev at epoch	7,006

▸Two-line element set (TLE)

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

1 63304U 25056E 26188.19578411 .00001366 00000-0 22370-3 0 9998

2 63304 97.9141 311.7605 0004655 220.7241 139.3619 14.72312391 70068

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-4B",
  "OBJECT_ID": "2025-056E",
  "EPOCH": "2026-07-07T04:41:55.747+00:00",
  "MEAN_MOTION": 14.72312391,
  "ECCENTRICITY": 0.0004655,
  "INCLINATION": 97.9141,
  "RA_OF_ASC_NODE": 311.7605,
  "ARG_OF_PERICENTER": 220.7241,
  "MEAN_ANOMALY": 139.3619,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63304,
  "REV_AT_EPOCH": 7006,
  "BSTAR": 0.0002237,
  "MEAN_MOTION_DOT": 0.00001366,
  "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-4B
Operator	KineisHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	Mar 18, 2025HIGHvia 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/63304

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