▸Orbital parameters

Orbit class	SSO
Inclination	98.0427°
Eccentricity	0.0002624
Period	97.8 min
Apogee	655 km
Perigee	652 km
Mean motion	14.72355741 rev/day
RAAN	277.8129°
Arg of perigee	94.4977°
Mean anomaly	265.6530°
B*	2.5341e-4
Rev at epoch	9,628

▸Two-line element set (TLE)

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

1 61221U 24172B 26188.11446300 .00001554 00000-0 25341-3 0 9995

2 61221 98.0427 277.8129 0002624 94.4977 265.6530 14.72355741 96285

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-3D",
  "OBJECT_ID": "2024-172B",
  "EPOCH": "2026-07-07T02:44:49.603+00:00",
  "MEAN_MOTION": 14.72355741,
  "ECCENTRICITY": 0.0002624,
  "INCLINATION": 98.0427,
  "RA_OF_ASC_NODE": 277.8129,
  "ARG_OF_PERICENTER": 94.4977,
  "MEAN_ANOMALY": 265.653,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61221,
  "REV_AT_EPOCH": 9628,
  "BSTAR": 0.00025341,
  "MEAN_MOTION_DOT": 0.00001554,
  "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-3D
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/61221

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