Showing default

CONNECTA IOT-12, 64553

Orbit data source: Space-Track

CONNECTA IOT-12, 64553 is a payload satellite owned by Plan-S (TR) 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
64553, 2025-135AB
Orbit
SSO
Country
Flag of UnknownUnknown / TURK
Related business
Manufacturer
Plan-S
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
2025-06-23 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 CONNECTA IOT-12
1 64553U 25135AB  25340.81667693  .00007819  00000-0  36483-3 0  9991
2 64553  97.4616  93.1158 0001635  55.6956 304.4433 15.20120932 25638
Epoch: 2025-12-06T19:36Z
TLE epoch observation values (Epoch: 2025-12-06T19:36:00.886Z)
Latitude
-0.0001°
Longitude
83.27314°
Altitude
507.928 km
Speed
7.61 km/s
True Right ascension
06h 12m 27s
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
08:17:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.569 km
Perigee altitude
501.319 km
Semi-major axis
6,880.581 km
Eccentricity
0.00016
Inclination
97.4616°
RAAN
93.1158°
Arg. of periapsis
55.6956°
True anomaly
304.42785°
Mean anomaly
304.4433°
Eccentric anomaly
304.43557°
Mean motion
3.80282 °/min
Orbital period
94.67 mins
BSTAR
0.00036483
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
|