NILESAT 301, 52817
Orbit data source: Space-Track
NILESAT 301, 52817 is a payload satellite owned by Nilesat (EG) in GEO that was launched on Wed, 08 Jun 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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52817 intel report (Beta)
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Identifier
Orbit
Country
EG / EGYPRelated business
Manufacturer
Thales Alenia
Mission
Operational Civil Communications
Bus & Motor
SPACEBUS 4000B2, S400
Mass
3,938 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.8 m
Radar Cross Section
20.286 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 NILESAT 301
1 52817U 22061A 26171.39059714 -.00000062 00000-0 00000+0 0 9997
2 52817 0.0507 20.7867 0004675 36.9855 344.4364 1.00271181 14762Epoch: 2026-06-20T09:22Z
TLE epoch observation values (Epoch: 2026-06-20T09:22:27.592Z)
Latitude
0.03018°
Longitude
-7.01458°
Altitude
35,767.246 km
Speed
3.076 km/s
True Right ascension
02h 48m 49s
True Declination
0° 01' 49"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:36:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,807.547 km
Perigee altitude
35,768.122 km
Semi-major axis
42,165.972 km
Eccentricity
0.00047
Inclination
0.0507°
RAAN
20.7867°
Arg. of periapsis
36.9855°
True anomaly
344.42202°
Mean anomaly
344.4364°
Eccentric anomaly
344.42921°
Mean motion
0.25067 °/min
Orbital period
1,436.16 mins
BSTAR
0
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Other satellites on launch #61 in the year 2022 (2022-06-08 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NILESAT 301 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| NILESAT 301 is likely not visible in the next few days. |
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52817 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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