▸Orbital parameters

Orbit class	SSO
Inclination	97.8944°
Eccentricity	0.0002127
Period	97.5 min
Apogee	640 km
Perigee	637 km
Mean motion	14.77072473 rev/day
RAAN	239.3498°
Arg of perigee	101.1848°
Mean anomaly	258.9602°
B*	1.9502e-4
Rev at epoch	7,572

▸Two-line element set (TLE)

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

1 62931U 25028D 26188.14176566 .00001327 00000-0 19502-3 0 9992

2 62931 97.8944 239.3498 0002127 101.1848 258.9602 14.77072473 75722

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-2E",
  "OBJECT_ID": "2025-028D",
  "EPOCH": "2026-07-07T03:24:08.553+00:00",
  "MEAN_MOTION": 14.77072473,
  "ECCENTRICITY": 0.0002127,
  "INCLINATION": 97.8944,
  "RA_OF_ASC_NODE": 239.3498,
  "ARG_OF_PERICENTER": 101.1848,
  "MEAN_ANOMALY": 258.9602,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62931,
  "REV_AT_EPOCH": 7572,
  "BSTAR": 0.00019502,
  "MEAN_MOTION_DOT": 0.00001327,
  "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-2E
Operator	KineisHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	France
Launch date	Feb 8, 2025HIGHvia 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/62931

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