Showing default

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.

Loading next visibility...
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 (7 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: 3 days ago

TLE from 3 days ago
0 SPAINSAT NG II
1 66144U 25239A   26150.20996507 -.00000286  00000-0  00000-0 0  9991
2 66144  13.9549 225.7430 7624408 213.1051  59.5965  0.96245958  2178
Epoch: 2026-05-30T05:02Z
TLE epoch observation values (Epoch: 2026-05-30T05:02:20.982Z)
Latitude
0.00002°
Longitude
-97.21299°
Altitude
44,137.571 km
Speed
2.566 km/s
True Right ascension
15h 04m 24s
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
13:14:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
69,998.87 km
Perigee altitude
3,916.711 km
Semi-major axis
43,335.927 km
Eccentricity
0.76244
Inclination
13.9549°
RAAN
225.743°
Arg. of periapsis
213.1051°
True anomaly
147.04228°
Mean anomaly
59.5965°
Eccentric anomaly
102.2814°
Mean motion
0.24059 °/min
Orbital period
1,496.34 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #239 in the year 2025 (2025-10-24 UTC)

Documentation

Showing up to 5 results
|