▸Orbital parameters

Orbit class	GEO
Inclination	0.0523°
Eccentricity	0.0004309
Period	1436.1 min
Apogee	35,805 km
Perigee	35,768 km
Mean motion	1.00272626 rev/day
RAAN	331.5103°
Arg of perigee	89.9482°
Mean anomaly	242.6895°
B*	0.0000e+0
Rev at epoch	1,493

▸Two-line element set (TLE)

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

1 52817U 22061A 26188.07240381 -.00000042 00000-0 00000-0 0 9991

2 52817 0.0523 331.5103 0004309 89.9482 242.6895 1.00272626 14936

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NILESAT 301",
  "OBJECT_ID": "2022-061A",
  "EPOCH": "2026-07-07T01:44:15.689+00:00",
  "MEAN_MOTION": 1.00272626,
  "ECCENTRICITY": 0.0004309,
  "INCLINATION": 0.0523,
  "RA_OF_ASC_NODE": 331.5103,
  "ARG_OF_PERICENTER": 89.9482,
  "MEAN_ANOMALY": 242.6895,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52817,
  "REV_AT_EPOCH": 1493,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -4.2e-7,
  "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	NILESAT 301
Operator	Nilesat IncHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree NilesatMEDIUMvia Wikidata
Country	EgyptMEDIUMvia Wikidata
Launch date	Jun 8, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3938HIGH

▸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/52817

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