▸Orbital parameters

Orbit class	SSO
Inclination	97.9059°
Eccentricity	0.0003481
Period	97.8 min
Apogee	656 km
Perigee	651 km
Mean motion	14.72307367 rev/day
RAAN	346.4755°
Arg of perigee	198.8346°
Mean anomaly	161.2733°
B*	9.4961e-5
Rev at epoch	8,669

▸Two-line element set (TLE)

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

1 62081U 24219A 26188.17664226 .00000552 00000-0 94961-4 0 9999

2 62081 97.9059 346.4755 0003481 198.8346 161.2733 14.72307367 86699

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-5C",
  "OBJECT_ID": "2024-219A",
  "EPOCH": "2026-07-07T04:14:21.891+00:00",
  "MEAN_MOTION": 14.72307367,
  "ECCENTRICITY": 0.0003481,
  "INCLINATION": 97.9059,
  "RA_OF_ASC_NODE": 346.4755,
  "ARG_OF_PERICENTER": 198.8346,
  "MEAN_ANOMALY": 161.2733,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62081,
  "REV_AT_EPOCH": 8669,
  "BSTAR": 0.000094961,
  "MEAN_MOTION_DOT": 0.00000552,
  "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-5C
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/62081

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