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CONNECTA T3.1, 58256

Orbit data source: Space-Track

CONNECTA T3.1, 58256 is a payload satellite owned by Plan-S (TR) in LEO that was launched on Sat, 11 Nov 2023 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.

Not visible in the next 10 days
Identifier
58256, 2023-174A
Orbit
LEO
Country
Flag of UnknownUnknown / TURK
Related business
Manufacturer
Plan-S
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2023-11-11 (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 Pan, 1.7 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 4 weeks ago

TLE from 4 weeks ago
0 CONNECTA T3.1
1 58256U 23174A   25320.29069665  .11407706  25153-5  10568-2 0  9997
2 58256  97.3613  50.0486 0009475 269.0704  90.9510 16.38733451113418
Epoch: 2025-11-16T06:58Z
TLE epoch observation values (Epoch: 2025-11-16T06:58:36.190Z)
Latitude
0.00005°
Longitude
-110.2098°
Altitude
172.533 km
Speed
7.803 km/s
True Right ascension
03h 20m 11s
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
18:31:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
172.182 km
Perigee altitude
159.781 km
Semi-major axis
6,544.118 km
Eccentricity
0.00095
Inclination
97.3613°
RAAN
50.0486°
Arg. of periapsis
269.0704°
True anomaly
91.05956°
Mean anomaly
90.951°
Eccentric anomaly
91.00528°
Mean motion
4.09984 °/min
Orbital period
87.81 mins
BSTAR
0.0010568
Loading maneuver chart data...
Computing Atmospheric mass density...

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