▸Orbital parameters

Orbit class	SSO
Inclination	97.8745°
Eccentricity	0.0008346
Period	93.6 min
Apogee	458 km
Perigee	447 km
Mean motion	15.37820675 rev/day
RAAN	198.8942°
Arg of perigee	201.1800°
Mean anomaly	158.9099°
B*	2.4703e-4
Rev at epoch	31,884

▸Two-line element set (TLE)

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

1 46493U 20068H 26188.18618563 .00009100 00000-0 24703-3 0 9994

2 46493 97.8745 198.8942 0008346 201.1800 158.9099 15.37820675318841

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DEKART",
  "OBJECT_ID": "2020-068H",
  "EPOCH": "2026-07-07T04:28:06.438+00:00",
  "MEAN_MOTION": 15.37820675,
  "ECCENTRICITY": 0.0008346,
  "INCLINATION": 97.8745,
  "RA_OF_ASC_NODE": 198.8942,
  "ARG_OF_PERICENTER": 201.18,
  "MEAN_ANOMALY": 158.9099,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 46493,
  "REV_AT_EPOCH": 31884,
  "BSTAR": 0.00024703,
  "MEAN_MOTION_DOT": 0.000091,
  "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	DEKART
Operator	Moscow State UniversityHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Sep 28, 2020HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4HIGHvia 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/46493

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