Showing default

IOD2_STARTICAL, 64538

Orbit data source: Space-Track

IOD2_STARTICAL, 64538 is a Spanish payload satellite in SSO that was launched on Mon, 23 Jun 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
64538, 2025-135L
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
NanoAvionics
Mission
Operational Commercial Communications
Bus & Motor
MP42, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
2025-06-23 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.146 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 IOD2_STARTICAL
1 64538U 25135L   25328.36362455  .00004912  00000-0  24366-3 0  9996
2 64538  97.4570  80.4286 0005346 156.6878 203.4600 15.18168004 23720
Epoch: 2025-11-24T08:43Z
TLE epoch observation values (Epoch: 2025-11-24T08:43:37.161Z)
Latitude
0.00006°
Longitude
-114.04091°
Altitude
517.844 km
Speed
7.603 km/s
True Right ascension
05h 21m 42s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
14:19:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.029 km
Perigee altitude
504.666 km
Semi-major axis
6,886.485 km
Eccentricity
0.00053
Inclination
97.457°
RAAN
80.4286°
Arg. of periapsis
156.6878°
True anomaly
203.43563°
Mean anomaly
203.46°
Eccentric anomaly
203.44781°
Mean motion
3.79793 °/min
Orbital period
94.79 mins
BSTAR
0.00024366
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...

Documentation

Showing up to 5 results
|