ASTRA 1P (SES 24), 60086
Orbit data source: Space-Track
ASTRA 1P (SES 24), 60086 is a payload satellite owned by SES (LU) in GEO that was launched on Thu, 20 Jun 2024 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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60086 intel report (Beta)
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Identifier
Orbit
Country
LU / SESRelated business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
SPACEBUS NEO200, XPS/PPS-5000
Mass
~5,000 kg wet, ~4,030 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 22.5 m
Radar Cross Section
62.256 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ASTRA 1P (SES 24)
1 60086U 24115A 26170.84211356 .00000115 00000-0 00000-0 0 9996
2 60086 0.0580 357.1167 0000651 25.1211 208.1930 1.00275004 7222Epoch: 2026-06-19T20:12Z
TLE epoch observation values (Epoch: 2026-06-19T20:12:38.611Z)
Latitude
-0.06217°
Longitude
19.2136°
Altitude
35,787.606 km
Speed
3.075 km/s
True Right ascension
15h 21m 45s
True Declination
0° 03' 44"
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
10:18:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.508 km
Perigee altitude
35,784.018 km
Semi-major axis
42,164.9 km
Eccentricity
0.00007
Inclination
0.058°
RAAN
357.1167°
Arg. of periapsis
25.1211°
True anomaly
208.18948°
Mean anomaly
208.193°
Eccentric anomaly
208.19124°
Mean motion
0.25068 °/min
Orbital period
1,436.1 mins
BSTAR
0
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Other satellites on launch #115 in the year 2024 (2024-06-20 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.ASTRA 1P (SES 24) 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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| ASTRA 1P (SES 24) is likely not visible in the next few days. |
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60086 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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