▸Orbital parameters

Orbit class	SSO
Inclination	97.8916°
Eccentricity	0.0005658
Period	97.3 min
Apogee	631 km
Perigee	623 km
Mean motion	14.80673535 rev/day
RAAN	211.4057°
Arg of perigee	81.4069°
Mean anomaly	278.7784°
B*	1.0401e-4
Rev at epoch	11,035

▸Two-line element set (TLE)

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

1 60084U 24114F 26188.20805421 .00000748 00000-0 10401-3 0 9995

2 60084 97.8916 211.4057 0005658 81.4069 278.7784 14.80673535110357

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-1A",
  "OBJECT_ID": "2024-114F",
  "EPOCH": "2026-07-07T04:59:35.884+00:00",
  "MEAN_MOTION": 14.80673535,
  "ECCENTRICITY": 0.0005658,
  "INCLINATION": 97.8916,
  "RA_OF_ASC_NODE": 211.4057,
  "ARG_OF_PERICENTER": 81.4069,
  "MEAN_ANOMALY": 278.7784,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60084,
  "REV_AT_EPOCH": 11035,
  "BSTAR": 0.00010401,
  "MEAN_MOTION_DOT": 0.00000748,
  "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-1A
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/60084

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