▸Orbital parameters

Orbit class	GEO
Inclination	0.0177°
Eccentricity	0.0001813
Period	1436.1 min
Apogee	35,794 km
Perigee	35,779 km
Mean motion	1.00271234 rev/day
RAAN	89.4952°
Arg of perigee	340.3536°
Mean anomaly	322.6289°
B*	0.0000e+0
Rev at epoch	3,843

▸Two-line element set (TLE)

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

1 41238U 16001A 26188.15520125 .00000122 00000-0 00000-0 0 9997

2 41238 0.0177 89.4952 0001813 340.3536 322.6289 1.00271234 38439

▸ source OMM (JSON)

{
  "OBJECT_NAME": "BELINTERSAT-1",
  "OBJECT_ID": "2016-001A",
  "EPOCH": "2026-07-07T03:43:29.388+00:00",
  "MEAN_MOTION": 1.00271234,
  "ECCENTRICITY": 0.0001813,
  "INCLINATION": 0.0177,
  "RA_OF_ASC_NODE": 89.4952,
  "ARG_OF_PERICENTER": 340.3536,
  "MEAN_ANOMALY": 322.6289,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41238,
  "REV_AT_EPOCH": 3843,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000122,
  "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	BELINTERSAT-1
Operator	Precision Electromechanics FactoryHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Belarus
Launch date	Jan 15, 2016HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5200HIGHvia 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/41238

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