▸Orbital parameters

Orbit class	SSO
Inclination	98.0419°
Eccentricity	0.0002701
Period	97.8 min
Apogee	656 km
Perigee	652 km
Mean motion	14.72292370 rev/day
RAAN	277.9270°
Arg of perigee	58.7701°
Mean anomaly	301.3770°
B*	2.4758e-4
Rev at epoch	9,571

▸Two-line element set (TLE)

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

1 61223U 24172D 26188.14881822 .00001515 00000-0 24758-3 0 9990

2 61223 98.0419 277.9270 0002701 58.7701 301.3770 14.72292370 95719

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-3A",
  "OBJECT_ID": "2024-172D",
  "EPOCH": "2026-07-07T03:34:17.894+00:00",
  "MEAN_MOTION": 14.7229237,
  "ECCENTRICITY": 0.0002701,
  "INCLINATION": 98.0419,
  "RA_OF_ASC_NODE": 277.927,
  "ARG_OF_PERICENTER": 58.7701,
  "MEAN_ANOMALY": 301.377,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61223,
  "REV_AT_EPOCH": 9571,
  "BSTAR": 0.00024758,
  "MEAN_MOTION_DOT": 0.00001515,
  "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-3A
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/61223

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