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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 (4 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

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 SPAINSAT NG II
1 66144U 25239A   26061.42255774 -.00000002  00000-0  00000+0 0  9995
2 66144  14.9132 234.0730 7654672 199.7792  94.4345  0.96966050  1318
Epoch: 2026-03-02T10:08Z
TLE epoch observation values (Epoch: 2026-03-02T10:08:28.988Z)
Latitude
-0.00004°
Longitude
-78.48758°
Altitude
57,268.054 km
Speed
1.811 km/s
True Right ascension
15h 35m 23s
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
05:25:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
69,750.853 km
Perigee altitude
3,735.189 km
Semi-major axis
43,121.158 km
Eccentricity
0.76547
Inclination
14.9132°
RAAN
234.073°
Arg. of periapsis
199.7792°
True anomaly
160.13428°
Mean anomaly
94.4345°
Eccentric anomaly
128.67474°
Mean motion
0.24239 °/min
Orbital period
1,485.23 mins
BSTAR
0
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Other satellites on launch #239 in the year 2025 (2025-10-24 UTC)

Documentation

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