▸Orbital parameters

Orbit class	SSO
Inclination	97.9130°
Eccentricity	0.0001486
Period	97.8 min
Apogee	655 km
Perigee	653 km
Mean motion	14.72317919 rev/day
RAAN	311.7211°
Arg of perigee	167.5396°
Mean anomaly	192.5848°
B*	2.2653e-4
Rev at epoch	7,007

▸Two-line element set (TLE)

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

1 63303U 25056D 26188.21309183 .00001384 00000-0 22653-3 0 9992

2 63303 97.9130 311.7211 0001486 167.5396 192.5848 14.72317919 70073

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-4A",
  "OBJECT_ID": "2025-056D",
  "EPOCH": "2026-07-07T05:06:51.134+00:00",
  "MEAN_MOTION": 14.72317919,
  "ECCENTRICITY": 0.0001486,
  "INCLINATION": 97.913,
  "RA_OF_ASC_NODE": 311.7211,
  "ARG_OF_PERICENTER": 167.5396,
  "MEAN_ANOMALY": 192.5848,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63303,
  "REV_AT_EPOCH": 7007,
  "BSTAR": 0.00022653,
  "MEAN_MOTION_DOT": 0.00001384,
  "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-4A
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/63303

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