▸Orbital parameters

Orbit class	SSO
Inclination	98.0082°
Eccentricity	0.0001912
Period	97.4 min
Apogee	636 km
Perigee	633 km
Mean motion	14.78373579 rev/day
RAAN	351.8700°
Arg of perigee	161.7191°
Mean anomaly	198.4089°
B*	1.3513e-4
Rev at epoch	8,695

▸Two-line element set (TLE)

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

1 62085U 24219E 26188.14974383 .00000932 00000-0 13513-3 0 9993

2 62085 98.0082 351.8700 0001912 161.7191 198.4089 14.78373579 86954

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-5B",
  "OBJECT_ID": "2024-219E",
  "EPOCH": "2026-07-07T03:35:37.867+00:00",
  "MEAN_MOTION": 14.78373579,
  "ECCENTRICITY": 0.0001912,
  "INCLINATION": 98.0082,
  "RA_OF_ASC_NODE": 351.87,
  "ARG_OF_PERICENTER": 161.7191,
  "MEAN_ANOMALY": 198.4089,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62085,
  "REV_AT_EPOCH": 8695,
  "BSTAR": 0.00013513,
  "MEAN_MOTION_DOT": 0.00000932,
  "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-5B
Operator	KineisHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	Nov 25, 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/62085

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