▸Orbital parameters

Orbit class	SSO
Inclination	97.9846°
Eccentricity	0.0002496
Period	97.3 min
Apogee	629 km
Perigee	626 km
Mean motion	14.80660440 rev/day
RAAN	212.1003°
Arg of perigee	104.7852°
Mean anomaly	255.3637°
B*	9.4422e-5
Rev at epoch	11,033

▸Two-line element set (TLE)

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

1 60081U 24114C 26188.15672825 .00000673 00000-0 94422-4 0 9999

2 60081 97.9846 212.1003 0002496 104.7852 255.3637 14.80660440110339

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-1C",
  "OBJECT_ID": "2024-114C",
  "EPOCH": "2026-07-07T03:45:41.321+00:00",
  "MEAN_MOTION": 14.8066044,
  "ECCENTRICITY": 0.0002496,
  "INCLINATION": 97.9846,
  "RA_OF_ASC_NODE": 212.1003,
  "ARG_OF_PERICENTER": 104.7852,
  "MEAN_ANOMALY": 255.3637,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60081,
  "REV_AT_EPOCH": 11033,
  "BSTAR": 0.000094422,
  "MEAN_MOTION_DOT": 0.00000673,
  "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-1C
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/60081

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