CONNECTA IOT-11, 64557
Orbit data source: Space-Track
CONNECTA IOT-11, 64557 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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64557 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: 2 days ago
TLE from 2 days ago
0 CONNECTA IOT-11
1 64557U 25135AF 26297.05514800 .00008020 00000-0 35687-3 0 9994
2 64557 97.4834 51.3804 0000394 181.1218 179.0017 15.21744883 74451Epoch: 2026-10-24T01:19Z
TLE epoch observation values (Epoch: 2026-10-24T01:19:24.787Z)
Latitude
-0.00001°
Longitude
-0.93971°
Altitude
503.939 km
Speed
7.612 km/s
True Right ascension
03h 25m 31s
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
11:14:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.815 km
Perigee altitude
497.273 km
Semi-major axis
6,875.681 km
Eccentricity
0.00004
Inclination
97.4834°
RAAN
51.3804°
Arg. of periapsis
181.1218°
True anomaly
179.00178°
Mean anomaly
179.0017°
Eccentric anomaly
179.00174°
Mean motion
3.80688 °/min
Orbital period
94.57 mins
BSTAR
0.00035687
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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-11 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 | 2026-10-25 20:29:42.367Z | 18.331° NNE | 2026-10-25 20:32:42.367Z | 88.616° E | 68.488° | 2026-10-25 20:35:42.367Z | 183.55° SSW |
| 4 mins | 2026-10-26 07:08:42.367Z | 101.831° ESE | 2026-10-26 07:09:42.367Z | 76.635° E | 25.558° | 2026-10-26 07:12:42.367Z | 16.39° NNE |
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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