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.

Not visible in the next 10 days
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 (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: 16 hours ago

TLE from 16 hours ago
0 SPAINSAT NG II
1 66144U 25239A   26212.26158217  .00000006  00000-0  00000-0 0  9993
2 66144  13.3379 219.1559 7637202 223.2747  41.3621  0.96597491  2767
Epoch: 2026-07-31T06:16Z
TLE epoch observation values (Epoch: 2026-07-31T06:16:40.699Z)
Latitude
-0.00001°
Longitude
175.64012°
Altitude
33,689.507 km
Speed
3.267 km/s
True Right ascension
14h 34m 47s
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
11:57:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
69,868.889 km
Perigee altitude
3,836.427 km
Semi-major axis
43,230.795 km
Eccentricity
0.76372
Inclination
13.3379°
RAAN
219.1559°
Arg. of periapsis
223.2747°
True anomaly
136.41856°
Mean anomaly
41.3621°
Eccentric anomaly
84.9502°
Mean motion
0.24146 °/min
Orbital period
1,490.9 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
|