▸Orbital parameters

Orbit class	SSO
Inclination	98.0430°
Eccentricity	0.0002812
Period	97.8 min
Apogee	656 km
Perigee	652 km
Mean motion	14.72354106 rev/day
RAAN	277.8766°
Arg of perigee	94.8849°
Mean anomaly	265.2679°
B*	2.5036e-4
Rev at epoch	9,601

▸Two-line element set (TLE)

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

1 61220U 24172A 26188.18915971 .00001535 00000-0 25036-3 0 9996

2 61220 98.0430 277.8766 0002812 94.8849 265.2679 14.72354106 96011

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-3C",
  "OBJECT_ID": "2024-172A",
  "EPOCH": "2026-07-07T04:32:23.399+00:00",
  "MEAN_MOTION": 14.72354106,
  "ECCENTRICITY": 0.0002812,
  "INCLINATION": 98.043,
  "RA_OF_ASC_NODE": 277.8766,
  "ARG_OF_PERICENTER": 94.8849,
  "MEAN_ANOMALY": 265.2679,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61220,
  "REV_AT_EPOCH": 9601,
  "BSTAR": 0.00025036,
  "MEAN_MOTION_DOT": 0.00001535,
  "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-3C
Operator	KineisHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	Sep 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/61220

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