▸Orbital parameters

Orbit class	SSO
Inclination	97.9826°
Eccentricity	0.0003474
Period	97.3 min
Apogee	630 km
Perigee	625 km
Mean motion	14.80658320 rev/day
RAAN	212.2806°
Arg of perigee	55.5659°
Mean anomaly	304.5881°
B*	9.8105e-5
Rev at epoch	11,036

▸Two-line element set (TLE)

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

1 60079U 24114A 26188.19066500 .00000701 00000-0 98105-4 0 9991

2 60079 97.9826 212.2806 0003474 55.5659 304.5881 14.80658320110366

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-1B",
  "OBJECT_ID": "2024-114A",
  "EPOCH": "2026-07-07T04:34:33.456+00:00",
  "MEAN_MOTION": 14.8065832,
  "ECCENTRICITY": 0.0003474,
  "INCLINATION": 97.9826,
  "RA_OF_ASC_NODE": 212.2806,
  "ARG_OF_PERICENTER": 55.5659,
  "MEAN_ANOMALY": 304.5881,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60079,
  "REV_AT_EPOCH": 11036,
  "BSTAR": 0.000098105,
  "MEAN_MOTION_DOT": 0.00000701,
  "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-1B
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/60079

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