Showing default

IOD1_STARTICAL, 63212

Orbit data source: Space-Track

IOD1_STARTICAL, 63212 is a Spanish payload satellite in SSO that was launched on Sat, 15 Mar 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
63212, 2025-052C
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
GOMSpace
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
2025-03-15 (11 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 + 1 Ant, 0.3 m
Radar Cross Section
0.152 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 IOD1_STARTICAL
1 63212U 25052C   26032.23506210  .00032817  00000-0  81441-3 0  9992
2 63212  97.4017 291.1965 0000726 156.5920 203.5359 15.40288645 49474
Epoch: 2026-02-01T05:38Z
TLE epoch observation values (Epoch: 2026-02-01T05:38:29.365Z)
Latitude
-0.00005°
Longitude
75.12654°
Altitude
448.829 km
Speed
7.643 km/s
True Right ascension
19h 24m 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
05:41:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.691 km
Perigee altitude
441.7 km
Semi-major axis
6,820.332 km
Eccentricity
0.00007
Inclination
97.4017°
RAAN
291.1965°
Arg. of periapsis
156.592°
True anomaly
203.53258°
Mean anomaly
203.5359°
Eccentric anomaly
203.53424°
Mean motion
3.85332 °/min
Orbital period
93.43 mins
BSTAR
0.00081441
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
|