▸Orbital parameters

Orbit class	SSO
Inclination	97.9658°
Eccentricity	0.0005030
Period	97.7 min
Apogee	654 km
Perigee	647 km
Mean motion	14.73437491 rev/day
RAAN	240.6061°
Arg of perigee	91.8196°
Mean anomaly	268.3588°
B*	1.9363e-4
Rev at epoch	7,559

▸Two-line element set (TLE)

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

1 62934U 25028G 26188.10601684 .00001207 00000-0 19363-3 0 9997

2 62934 97.9658 240.6061 0005030 91.8196 268.3588 14.73437491 75590

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-2B",
  "OBJECT_ID": "2025-028G",
  "EPOCH": "2026-07-07T02:32:39.855+00:00",
  "MEAN_MOTION": 14.73437491,
  "ECCENTRICITY": 0.000503,
  "INCLINATION": 97.9658,
  "RA_OF_ASC_NODE": 240.6061,
  "ARG_OF_PERICENTER": 91.8196,
  "MEAN_ANOMALY": 268.3588,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62934,
  "REV_AT_EPOCH": 7559,
  "BSTAR": 0.00019363,
  "MEAN_MOTION_DOT": 0.00001207,
  "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-2B
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/62934

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