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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.

Not visible in the next 10 days
Identifier
55012, 2023-001D
Orbit
SSO
Country
Flag of TRTR / TURK
Related business
Manufacturer
Plan-S
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2023-01-03 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CONNECTA T1.2
1 55012U 23001D   26295.76636986  .00087460  00000-0  97403-3 0  9995
2 55012  97.3104   9.5787 0003786 351.2523   8.8669 15.62552992212389
Epoch: 2026-10-22T18:23Z
TLE epoch observation values (Epoch: 2026-10-22T18:23:34.355Z)
Latitude
-0.00003°
Longitude
62.489°
Altitude
380.907 km
Speed
7.683 km/s
True Right ascension
00h 38m 18s
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
13:30:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
379.748 km
Perigee altitude
374.633 km
Semi-major axis
6,755.328 km
Eccentricity
0.00038
Inclination
97.3104°
RAAN
9.5787°
Arg. of periapsis
351.2523°
True anomaly
8.87359°
Mean anomaly
8.8669°
Eccentric anomaly
8.87024°
Mean motion
3.90907 °/min
Orbital period
92.09 mins
BSTAR
0.00097403
Loading maneuver chart data...
Computing Atmospheric mass density...

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