▸Orbital parameters

Orbit class	SSO
Inclination	97.9114°
Eccentricity	0.0002266
Period	97.8 min
Apogee	655 km
Perigee	652 km
Mean motion	14.72308157 rev/day
RAAN	311.7606°
Arg of perigee	247.3914°
Mean anomaly	112.7054°
B*	2.3024e-4
Rev at epoch	7,007

▸Two-line element set (TLE)

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

1 63301U 25056B 26188.17455433 .00001407 00000-0 23024-3 0 9994

2 63301 97.9114 311.7606 0002266 247.3914 112.7054 14.72308157 70078

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-4C",
  "OBJECT_ID": "2025-056B",
  "EPOCH": "2026-07-07T04:11:21.494+00:00",
  "MEAN_MOTION": 14.72308157,
  "ECCENTRICITY": 0.0002266,
  "INCLINATION": 97.9114,
  "RA_OF_ASC_NODE": 311.7606,
  "ARG_OF_PERICENTER": 247.3914,
  "MEAN_ANOMALY": 112.7054,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63301,
  "REV_AT_EPOCH": 7007,
  "BSTAR": 0.00023024,
  "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-4C
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/63301

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