▸Orbital parameters

Orbit class	SSO
Inclination	97.9061°
Eccentricity	0.0003065
Period	97.8 min
Apogee	656 km
Perigee	652 km
Mean motion	14.72286647 rev/day
RAAN	311.5051°
Arg of perigee	99.0013°
Mean anomaly	261.1541°
B*	2.3055e-4
Rev at epoch	7,006

▸Two-line element set (TLE)

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

1 63300U 25056A 26188.16205699 .00001408 00000-0 23055-3 0 9994

2 63300 97.9061 311.5051 0003065 99.0013 261.1541 14.72286647 70068

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-4E",
  "OBJECT_ID": "2025-056A",
  "EPOCH": "2026-07-07T03:53:21.724+00:00",
  "MEAN_MOTION": 14.72286647,
  "ECCENTRICITY": 0.0003065,
  "INCLINATION": 97.9061,
  "RA_OF_ASC_NODE": 311.5051,
  "ARG_OF_PERICENTER": 99.0013,
  "MEAN_ANOMALY": 261.1541,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63300,
  "REV_AT_EPOCH": 7006,
  "BSTAR": 0.00023055,
  "MEAN_MOTION_DOT": 0.00001408,
  "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-4E
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/63300

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