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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.

Not visible in the next 10 days
Identifier
62852, 2025-021A
Orbit
GEO
Country
Flag of ESES / SPN
Related 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)
2025-01-30 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 21.4 m
Radar Cross Section
50.755 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 SPAINSAT NG1
1 62852U 25021A   26256.08400328  .00000000  00000-0  00000-0 0  9999
2 62852   0.0187 152.6954 0000274 287.2911 331.3150  1.00270207  4869
Epoch: 2026-09-13T02:00Z
TLE epoch observation values (Epoch: 2026-09-13T02:00:57.883Z)
Latitude
-0.04213°
Longitude
28.9733°
Altitude
35,785.525 km
Speed
3.075 km/s
True Right ascension
03h 25m 11s
True Declination
0° 02' 32"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:40:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.263 km
Perigee altitude
35,786.952 km
Semi-major axis
42,166.245 km
Eccentricity
0.00003
Inclination
0.0187°
RAAN
152.6954°
Arg. of periapsis
287.2911°
True anomaly
331.31349°
Mean anomaly
331.315°
Eccentric anomaly
331.31425°
Mean motion
0.25067 °/min
Orbital period
1,436.17 mins
BSTAR
0
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Other satellites on launch #21 in the year 2025 (2025-01-30 UTC)

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