▸Orbital parameters

Orbit class	SSO
Inclination	98.0423°
Eccentricity	0.0001890
Period	97.8 min
Apogee	655 km
Perigee	652 km
Mean motion	14.72322288 rev/day
RAAN	277.7105°
Arg of perigee	95.1992°
Mean anomaly	264.9431°
B*	2.5838e-4
Rev at epoch	9,627

▸Two-line element set (TLE)

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

1 61222U 24172C 26188.02948243 .00001584 00000-0 25838-3 0 9993

2 61222 98.0423 277.7105 0001890 95.1992 264.9431 14.72322288 96275

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-3E",
  "OBJECT_ID": "2024-172C",
  "EPOCH": "2026-07-07T00:42:27.282+00:00",
  "MEAN_MOTION": 14.72322288,
  "ECCENTRICITY": 0.000189,
  "INCLINATION": 98.0423,
  "RA_OF_ASC_NODE": 277.7105,
  "ARG_OF_PERICENTER": 95.1992,
  "MEAN_ANOMALY": 264.9431,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 61222,
  "REV_AT_EPOCH": 9627,
  "BSTAR": 0.00025838,
  "MEAN_MOTION_DOT": 0.00001584,
  "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-3E
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/61222

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