▸Orbital parameters

Orbit class	SSO
Inclination	97.8943°
Eccentricity	0.0003816
Period	97.3 min
Apogee	630 km
Perigee	625 km
Mean motion	14.80684356 rev/day
RAAN	211.2763°
Arg of perigee	126.1110°
Mean anomaly	234.0456°
B*	1.4066e-4
Rev at epoch	11,034

▸Two-line element set (TLE)

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

1 60083U 24114E 26188.17467218 .00001030 00000-0 14066-3 0 9994

2 60083 97.8943 211.2763 0003816 126.1110 234.0456 14.80684356110349

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-1E",
  "OBJECT_ID": "2024-114E",
  "EPOCH": "2026-07-07T04:11:31.676+00:00",
  "MEAN_MOTION": 14.80684356,
  "ECCENTRICITY": 0.0003816,
  "INCLINATION": 97.8943,
  "RA_OF_ASC_NODE": 211.2763,
  "ARG_OF_PERICENTER": 126.111,
  "MEAN_ANOMALY": 234.0456,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60083,
  "REV_AT_EPOCH": 11034,
  "BSTAR": 0.00014066,
  "MEAN_MOTION_DOT": 0.0000103,
  "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-1E
Operator	KineisHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	Jun 20, 2024HIGHvia 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/60083

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