SPAINSAT NG1, 62852
Orbit data source: Space-Track
SPAINSAT NG1, 62852 is a payload satellite owned by Hisdesat (ES) in GEO that was launched on Thu, 30 Jan 2025 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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62852 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
ADST/ADSUK
Mission
Operational Defense Communications
Bus & Motor
EUROSTAR NEO, PPS-5000
Mass
6,100 kg wet, ~5,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 21.4 m
Radar Cross Section
50.755 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SPAINSAT NG1
1 62852U 25021A 26075.85619789 .00000000 00000-0 00000+0 0 9995
2 62852 0.0257 176.0139 0000391 107.2928 228.3631 1.00275083 3068Epoch: 2026-03-16T20:32Z
TLE epoch observation values (Epoch: 2026-03-16T20:32:55.497Z)
Latitude
-0.01741°
Longitude
29.00673°
Altitude
35,786.258 km
Speed
3.075 km/s
True Right ascension
10h 06m 43s
True Declination
0° 01' 03"
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
01:46:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,788.389 km
Perigee altitude
35,785.092 km
Semi-major axis
42,164.878 km
Eccentricity
0.00004
Inclination
0.0257°
RAAN
176.0139°
Arg. of periapsis
107.2928°
True anomaly
228.35975°
Mean anomaly
228.3631°
Eccentric anomaly
228.36143°
Mean motion
0.25068 °/min
Orbital period
1,436.1 mins
BSTAR
0
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Other satellites on launch #21 in the year 2025 (2025-01-30 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.SPAINSAT NG1 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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| SPAINSAT NG1 is likely not visible in the next few days. |
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62852 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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