Showing default

CONNECTA IOT-6, 62709

Orbit data source: Space-Track

CONNECTA IOT-6, 62709 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Tue, 14 Jan 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
62709, 2025-009DE
Orbit
SSO
Country
Flag of TRTR / 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)
2025-01-14 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 2.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 CONNECTA IOT-6
1 62709U 25009DE  26262.00892202  .00000532  00000-0  54560-4 0  9995
2 62709  97.6960 338.5725 0002075 141.5678 218.5690 14.94429812 91377
Epoch: 2026-09-19T00:12Z
TLE epoch observation values (Epoch: 2026-09-19T00:12:50.862Z)
Latitude
-0.00008°
Longitude
-22.56303°
Altitude
588.32 km
Speed
7.565 km/s
True Right ascension
22h 34m 17s
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
05:44:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.6 km
Perigee altitude
579.712 km
Semi-major axis
6,959.293 km
Eccentricity
0.00021
Inclination
97.696°
RAAN
338.5725°
Arg. of periapsis
141.5678°
True anomaly
218.55418°
Mean anomaly
218.569°
Eccentric anomaly
218.56159°
Mean motion
3.73848 °/min
Orbital period
96.3 mins
BSTAR
0.00005456
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
|