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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64553 intel report (Beta)
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Identifier
Orbit
Country
TR / 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, 2.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 CONNECTA IOT-12
1 64553U 25135AB 26224.27430965 .00001500 00000-0 71330-4 0 9995
2 64553 97.4785 339.3222 0001632 133.7228 226.4142 15.20743163 63391Epoch: 2026-08-12T06:35Z
TLE epoch observation values (Epoch: 2026-08-12T06:35:00.353Z)
Latitude
-0.00011°
Longitude
-80.15985°
Altitude
507.462 km
Speed
7.61 km/s
True Right ascension
22h 37m 17s
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
18:26:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.688 km
Perigee altitude
499.443 km
Semi-major axis
6,878.703 km
Eccentricity
0.00016
Inclination
97.4785°
RAAN
339.3222°
Arg. of periapsis
133.7228°
True anomaly
226.40066°
Mean anomaly
226.4142°
Eccentric anomaly
226.40743°
Mean motion
3.80438 °/min
Orbital period
94.63 mins
BSTAR
0.00007133
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-13 07:57:56.064Z | 177.916° S | 2026-08-13 08:01:56.064Z | 297.093° NW | 39.545° | 2026-08-13 08:04:56.064Z | 340.449° N |
| 4 mins | 2026-08-13 21:03:56.064Z | 336.865° NNW | 2026-08-13 21:04:56.064Z | 308.322° NW | 31.452° | 2026-08-13 21:07:56.064Z | 223.089° SW |
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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