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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 (9 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 22.5 m
Radar Cross Section
50.755 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 SPAINSAT NG1
1 62852U 25021A   25290.91788391  .00000148  00000-0  00000-0 0  9990
2 62852   0.1446  86.1802 0001656 185.7263 117.3243  1.00301726  1557
Epoch: 2025-10-17T22:01Z
TLE epoch observation values (Epoch: 2025-10-17T22:01:45.169Z)
Latitude
-0.11919°
Longitude
32.13386°
Altitude
35,780.915 km
Speed
3.075 km/s
True Right ascension
01h 56m 54s
True Declination
0° 07' 09"
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
23:47:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,786.255 km
Perigee altitude
35,772.293 km
Semi-major axis
42,157.411 km
Eccentricity
0.00017
Inclination
0.1446°
RAAN
86.1802°
Arg. of periapsis
185.7263°
True anomaly
117.34116°
Mean anomaly
117.3243°
Eccentric anomaly
117.33273°
Mean motion
0.25074 °/min
Orbital period
1,435.72 mins
BSTAR
0
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Other satellites on launch #21 in the year 2025 (2025-01-30 UTC)

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