CONNECTA IOT-12, 64553
Orbit data source: Space-Track
CONNECTA IOT-12, 64553 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Mon, 23 Jun 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.
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Edit Public Description
Identifier
Orbit
Country
Unknown / TURKRelated business
Manufacturer
Plan-S
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 CONNECTA IOT-12
1 64553U 25135AB 25340.81667693 .00007819 00000-0 36483-3 0 9991
2 64553 97.4616 93.1158 0001635 55.6956 304.4433 15.20120932 25638Epoch: 2025-12-06T19:36Z
TLE epoch observation values (Epoch: 2025-12-06T19:36:00.886Z)
Latitude
-0.0001°
Longitude
83.27314°
Altitude
507.928 km
Speed
7.61 km/s
True Right ascension
06h 12m 27s
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
08:17:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.569 km
Perigee altitude
501.319 km
Semi-major axis
6,880.581 km
Eccentricity
0.00016
Inclination
97.4616°
RAAN
93.1158°
Arg. of periapsis
55.6956°
True anomaly
304.42785°
Mean anomaly
304.4433°
Eccentric anomaly
304.43557°
Mean motion
3.80282 °/min
Orbital period
94.67 mins
BSTAR
0.00036483
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Other satellites on launch #135 in the year 2025 (2025-06-23 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 IOT-12 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-07 19:52:36.260Z | 46.266° ENE | 2025-12-07 19:54:36.260Z | 87.203° E | 23.524° | 2025-12-07 19:57:36.260Z | 150.574° SSE |
| 5 mins | 2025-12-08 08:04:36.260Z | 200.008° SSW | 2025-12-08 08:06:36.260Z | 264.52° W | 34.796° | 2025-12-08 08:09:36.260Z | 332.058° NNW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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