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SPAINSAT NG II, 66144

Orbit data source: Space-Track

SPAINSAT NG II, 66144 is a payload satellite owned by Hisdesat (ES) in HEO that was launched on Fri, 24 Oct 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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Identifier
66144, 2025-239A
Orbit
HEO
Country
Flag of ESES / SPN
Related business
Manufacturer
ADST/ADSUK
Mission
Non-operational Defense Communications
Bus & Motor
EUROSTAR NEO, PPS-5000
Mass
6,100 kg wet, ~5,500 kg dry
Launch date (UTC)
2025-10-24 (11 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: 2 days ago

TLE from 2 days ago
0 SPAINSAT NG II
1 66144U 25239A   26256.75069373 -.00000016  00000-0  00000-0 0  9991
2 66144  12.8716 213.8243 7646866 231.2681  32.4661  0.96596926  3194
Epoch: 2026-09-13T18:00Z
TLE epoch observation values (Epoch: 2026-09-13T18:00:59.938Z)
Latitude
0.00003°
Longitude
-49.41511°
Altitude
28,063.519 km
Speed
3.732 km/s
True Right ascension
14h 14m 18s
True Declination
0° 00' 00"
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
20:43:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
69,911.034 km
Perigee altitude
3,794.697 km
Semi-major axis
43,231.003 km
Eccentricity
0.76469
Inclination
12.8716°
RAAN
213.8243°
Arg. of periapsis
231.2681°
True anomaly
128.88637°
Mean anomaly
32.4661°
Eccentric anomaly
74.73326°
Mean motion
0.24146 °/min
Orbital period
1,490.91 mins
BSTAR
0
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Other satellites on launch #239 in the year 2025 (2025-10-24 UTC)

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