▸Orbital parameters

Orbit class	SSO
Inclination	97.9035°
Eccentricity	0.0001068
Period	97.8 min
Apogee	654 km
Perigee	653 km
Mean motion	14.72410544 rev/day
RAAN	311.7439°
Arg of perigee	264.9208°
Mean anomaly	95.1878°
B*	2.2967e-4
Rev at epoch	7,007

▸Two-line element set (TLE)

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

1 63302U 25056C 26188.17823852 .00001407 00000-0 22967-3 0 9994

2 63302 97.9035 311.7439 0001068 264.9208 95.1878 14.72410544 70077

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-4D",
  "OBJECT_ID": "2025-056C",
  "EPOCH": "2026-07-07T04:16:39.808+00:00",
  "MEAN_MOTION": 14.72410544,
  "ECCENTRICITY": 0.0001068,
  "INCLINATION": 97.9035,
  "RA_OF_ASC_NODE": 311.7439,
  "ARG_OF_PERICENTER": 264.9208,
  "MEAN_ANOMALY": 95.1878,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63302,
  "REV_AT_EPOCH": 7007,
  "BSTAR": 0.00022967,
  "MEAN_MOTION_DOT": 0.00001407,
  "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-4D
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/63302

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