▸Orbital parameters

Orbit class	GEO
Inclination	0.0026°
Eccentricity	0.0005440
Period	1436.1 min
Apogee	35,810 km
Perigee	35,764 km
Mean motion	1.00271785 rev/day
RAAN	95.3038°
Arg of perigee	37.9515°
Mean anomaly	170.8645°
B*	0.0000e+0
Rev at epoch	5,857

▸Two-line element set (TLE)

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

1 36830U 10037A 26188.07240381 -.00000043 00000-0 00000-0 0 9999

2 36830 0.0026 95.3038 0005440 37.9515 170.8645 1.00271785 58578

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NILESAT 201",
  "OBJECT_ID": "2010-037A",
  "EPOCH": "2026-07-07T01:44:15.689+00:00",
  "MEAN_MOTION": 1.00271785,
  "ECCENTRICITY": 0.000544,
  "INCLINATION": 0.0026,
  "RA_OF_ASC_NODE": 95.3038,
  "ARG_OF_PERICENTER": 37.9515,
  "MEAN_ANOMALY": 170.8645,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 36830,
  "REV_AT_EPOCH": 5857,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -4.3e-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 201
Operator	Nilesat IncHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree NilesatMEDIUMvia Wikidata
Country	EgyptMEDIUMvia Wikidata
Launch date	Aug 4, 2010HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3200HIGH

▸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/36830

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