▸Orbital parameters

Orbit class	SSO
Inclination	97.9271°
Eccentricity	0.0004503
Period	97.6 min
Apogee	646 km
Perigee	640 km
Mean motion	14.75752629 rev/day
RAAN	240.1176°
Arg of perigee	127.3515°
Mean anomaly	232.8106°
B*	2.1336e-4
Rev at epoch	7,564

▸Two-line element set (TLE)

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

1 62930U 25028C 26188.05466654 .00001411 00000-0 21336-3 0 9993

2 62930 97.9271 240.1176 0004503 127.3515 232.8106 14.75752629 75646

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-2D",
  "OBJECT_ID": "2025-028C",
  "EPOCH": "2026-07-07T01:18:43.189+00:00",
  "MEAN_MOTION": 14.75752629,
  "ECCENTRICITY": 0.0004503,
  "INCLINATION": 97.9271,
  "RA_OF_ASC_NODE": 240.1176,
  "ARG_OF_PERICENTER": 127.3515,
  "MEAN_ANOMALY": 232.8106,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62930,
  "REV_AT_EPOCH": 7564,
  "BSTAR": 0.00021336,
  "MEAN_MOTION_DOT": 0.00001411,
  "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-2D
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/62930

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