CONNECTA T3.1, 58256
Orbit data source: Space-Track
CONNECTA T3.1, 58256 is a payload satellite owned by Plan-S (TR) in SSO 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.
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58256 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / TURKRelated business
Manufacturer
Plan-S
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.7 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CONNECTA T3.1
1 58256U 23174A 25300.49334741 .00359934 00000-0 16151-2 0 9997
2 58256 97.3871 28.3128 0006685 268.7692 91.2811 15.83189938110258Epoch: 2025-10-27T11:50Z
TLE epoch observation values (Epoch: 2025-10-27T11:50:25.216Z)
Latitude
-0.00004°
Longitude
174.61334°
Altitude
324.705 km
Speed
7.713 km/s
True Right ascension
01h 53m 15s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:04:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
322.784 km
Perigee altitude
313.831 km
Semi-major axis
6,696.445 km
Eccentricity
0.00067
Inclination
97.3871°
RAAN
28.3128°
Arg. of periapsis
268.7692°
True anomaly
91.35768°
Mean anomaly
91.2811°
Eccentric anomaly
91.31939°
Mean motion
3.96074 °/min
Orbital period
90.89 mins
BSTAR
0.0016151
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Other satellites on launch #174 in the year 2023 (2023-11-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CONNECTA T3.1 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-28 18:44:04.086Z | 25.901° NE | 2025-10-28 18:46:04.086Z | 146.023° SSE | 36.7° | 2025-10-28 18:48:04.086Z | 181.368° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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