▸Orbital parameters

Orbit class	SSO
Inclination	97.5397°
Eccentricity	0.0007061
Period	96.9 min
Apogee	617 km
Perigee	607 km
Mean motion	14.85494226 rev/day
RAAN	26.7235°
Arg of perigee	251.5924°
Mean anomaly	108.4524°
B*	9.8131e-5
Rev at epoch	65,192

▸Two-line element set (TLE)

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

1 40010U 14033A 26188.16854698 .00000797 00000-0 98131-4 0 9997

2 40010 97.5397 26.7235 0007061 251.5924 108.4524 14.85494226651926

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KAZEOSAT 2",
  "OBJECT_ID": "2014-033A",
  "EPOCH": "2026-07-07T04:02:42.459+00:00",
  "MEAN_MOTION": 14.85494226,
  "ECCENTRICITY": 0.0007061,
  "INCLINATION": 97.5397,
  "RA_OF_ASC_NODE": 26.7235,
  "ARG_OF_PERICENTER": 251.5924,
  "MEAN_ANOMALY": 108.4524,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40010,
  "REV_AT_EPOCH": 65192,
  "BSTAR": 0.000098131,
  "MEAN_MOTION_DOT": 0.00000797,
  "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	KAZEOSAT 2
Operator	Kazakh National Space AgnecyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Kazakhstan
Launch date	Jun 19, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	177HIGHvia 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/40010

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