▸Orbital parameters

Orbit class	GEO
Inclination	0.0184°
Eccentricity	0.0002666
Period	1436.1 min
Apogee	35,798 km
Perigee	35,775 km
Mean motion	1.00272994 rev/day
RAAN	52.2368°
Arg of perigee	52.7034°
Mean anomaly	288.1460°
B*	0.0000e+0
Rev at epoch	4,104

▸Two-line element set (TLE)

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

1 40617U 15023A 26188.15537461 .00000119 00000-0 00000-0 0 9997

2 40617 0.0184 52.2368 0002666 52.7034 288.1460 1.00272994 41042

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TURKMENALEM52E/MONACOSAT",
  "OBJECT_ID": "2015-023A",
  "EPOCH": "2026-07-07T03:43:44.366+00:00",
  "MEAN_MOTION": 1.00272994,
  "ECCENTRICITY": 0.0002666,
  "INCLINATION": 0.0184,
  "RA_OF_ASC_NODE": 52.2368,
  "ARG_OF_PERICENTER": 52.7034,
  "MEAN_ANOMALY": 288.146,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40617,
  "REV_AT_EPOCH": 4104,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000119,
  "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	TURKMENALEM52E/MONACOSAT
Operator	Space Systems International - Monaco S.A.M. / Ministry of Communications of TurkmenistanHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Turkmenistan National Space AgencyMEDIUMvia Wikidata
Country	MonacoMEDIUMvia Wikidata
Launch date	Apr 27, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/40617

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