▸Orbital parameters

Orbit class	SSO
Inclination	98.1291°
Eccentricity	0.0006048
Period	97.7 min
Apogee	654 km
Perigee	646 km
Mean motion	14.73436466 rev/day
RAAN	243.5439°
Arg of perigee	103.0610°
Mean anomaly	257.1273°
B*	2.0101e-4
Rev at epoch	7,554

▸Two-line element set (TLE)

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

1 62932U 25028E 26188.12865763 .00001253 00000-0 20101-3 0 9990

2 62932 98.1291 243.5439 0006048 103.0610 257.1273 14.73436466 75545

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-2A",
  "OBJECT_ID": "2025-028E",
  "EPOCH": "2026-07-07T03:05:16.019+00:00",
  "MEAN_MOTION": 14.73436466,
  "ECCENTRICITY": 0.0006048,
  "INCLINATION": 98.1291,
  "RA_OF_ASC_NODE": 243.5439,
  "ARG_OF_PERICENTER": 103.061,
  "MEAN_ANOMALY": 257.1273,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62932,
  "REV_AT_EPOCH": 7554,
  "BSTAR": 0.00020101,
  "MEAN_MOTION_DOT": 0.00001253,
  "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-2A
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/62932

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