▸Orbital parameters

Orbit class	SSO
Inclination	97.9882°
Eccentricity	0.0002817
Period	97.5 min
Apogee	643 km
Perigee	639 km
Mean motion	14.76355381 rev/day
RAAN	208.0903°
Arg of perigee	110.5620°
Mean anomaly	249.5892°
B*	8.1998e-5
Rev at epoch	11,007

▸Two-line element set (TLE)

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

1 60082U 24114D 26188.17352536 .00000518 00000-0 81998-4 0 9998

2 60082 97.9882 208.0903 0002817 110.5620 249.5892 14.76355381110077

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-1D",
  "OBJECT_ID": "2024-114D",
  "EPOCH": "2026-07-07T04:09:52.591+00:00",
  "MEAN_MOTION": 14.76355381,
  "ECCENTRICITY": 0.0002817,
  "INCLINATION": 97.9882,
  "RA_OF_ASC_NODE": 208.0903,
  "ARG_OF_PERICENTER": 110.562,
  "MEAN_ANOMALY": 249.5892,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60082,
  "REV_AT_EPOCH": 11007,
  "BSTAR": 0.000081998,
  "MEAN_MOTION_DOT": 0.00000518,
  "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-1D
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/60082

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