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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 (8 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, 21.4 m
Radar Cross Section
50.755 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 SPAINSAT NG1
1 62852U 25021A   25260.94558296  .00000133  00000-0  00000-0 0  9993
2 62852   0.0672  89.5528 0000811 170.3585 107.3294  1.00286615  1259
Epoch: 2025-09-17T22:41Z
TLE epoch observation values (Epoch: 2025-09-17T22:41:38.367Z)
Latitude
-0.07547°
Longitude
29.72718°
Altitude
35,782.952 km
Speed
3.075 km/s
True Right ascension
00h 29m 00s
True Declination
0° 04' 31"
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
01:35:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,786.928 km
Perigee altitude
35,780.089 km
Semi-major axis
42,161.646 km
Eccentricity
0.00008
Inclination
0.0672°
RAAN
89.5528°
Arg. of periapsis
170.3585°
True anomaly
107.33827°
Mean anomaly
107.3294°
Eccentric anomaly
107.33384°
Mean motion
0.25071 °/min
Orbital period
1,435.94 mins
BSTAR
0
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Other satellites on launch #21 in the year 2025 (2025-01-30 UTC)

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