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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Edit Public Description
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: 11 hours ago
TLE from 11 hours ago
0 SPAINSAT NG1
1 62852U 25021A 25241.24728806 .00000154 00000-0 00000-0 0 9994
2 62852 0.0126 107.7991 0000078 16.6300 331.2955 1.00277514 1050Epoch: 2025-08-29T05:56Z
TLE epoch observation values (Epoch: 2025-08-29T05:56:05.688Z)
Latitude
-0.0119°
Longitude
29°
Altitude
35,784.193 km
Speed
3.075 km/s
True Right ascension
06h 22m 53s
True Declination
0° 00' 43"
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
08:22:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,786.388 km
Perigee altitude
35,785.731 km
Semi-major axis
42,164.196 km
Eccentricity
0.00001
Inclination
0.0126°
RAAN
107.7991°
Arg. of periapsis
16.63°
True anomaly
331.29507°
Mean anomaly
331.2955°
Eccentric anomaly
331.29529°
Mean motion
0.25068 °/min
Orbital period
1,436.07 mins
BSTAR
0
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Other satellites on launch #21 in the year 2025 (2025-01-30 UTC)
SPAINSAT NG1 Visibility
Observer location: undefined°, undefined°
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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62852 neighbors
Authenticating...
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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