CONNECTA T1.2, 55012
Orbit data source: Space-Track
CONNECTA T1.2, 55012 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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55012 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
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 CONNECTA T1.2
1 55012U 23001D 25286.64628474 .00018073 00000-0 48346-3 0 9990
2 55012 97.3637 350.0668 0005992 266.0656 93.9905 15.38089221154514Epoch: 2025-10-13T15:30Z
TLE epoch observation values (Epoch: 2025-10-13T15:30:39.001Z)
Latitude
0.00007°
Longitude
94.95821°
Altitude
455.163 km
Speed
7.639 km/s
True Right ascension
23h 20m 16s
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
02:30:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452.791 km
Perigee altitude
444.609 km
Semi-major axis
6,826.837 km
Eccentricity
0.0006
Inclination
97.3637°
RAAN
350.0668°
Arg. of periapsis
266.0656°
True anomaly
94.05899°
Mean anomaly
93.9905°
Eccentric anomaly
94.02475°
Mean motion
3.84781 °/min
Orbital period
93.56 mins
BSTAR
0.00048346
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Other satellites on launch #1 in the year 2023 (2023-01-03 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 T1.2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-14 17:03:13.393Z | 20.005° NNE | 2025-10-14 17:06:13.393Z | 124.213° SE | 41.408° | 2025-10-14 17:09:13.393Z | 182.965° 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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