▸Orbital parameters

Orbit class	SSO
Inclination	98.1233°
Eccentricity	0.0003576
Period	97.7 min
Apogee	653 km
Perigee	648 km
Mean motion	14.73413024 rev/day
RAAN	242.5660°
Arg of perigee	181.8671°
Mean anomaly	178.2524°
B*	2.2406e-4
Rev at epoch	7,555

▸Two-line element set (TLE)

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

1 62929U 25028B 26188.15101484 .00001402 00000-0 22406-3 0 9998

2 62929 98.1233 242.5660 0003576 181.8671 178.2524 14.73413024 75554

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KINEIS-2C",
  "OBJECT_ID": "2025-028B",
  "EPOCH": "2026-07-07T03:37:27.682+00:00",
  "MEAN_MOTION": 14.73413024,
  "ECCENTRICITY": 0.0003576,
  "INCLINATION": 98.1233,
  "RA_OF_ASC_NODE": 242.566,
  "ARG_OF_PERICENTER": 181.8671,
  "MEAN_ANOMALY": 178.2524,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62929,
  "REV_AT_EPOCH": 7555,
  "BSTAR": 0.00022406,
  "MEAN_MOTION_DOT": 0.00001402,
  "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-2C
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/62929

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