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: 11 hours ago
TLE from 11 hours ago
0 CONNECTA IOT-11
1 64557U 25135AF 26133.28927264 .00002057 00000-0 98106-4 0 9990
2 64557 97.4674 248.9237 0002972 106.7260 253.4301 15.20214477 49568Epoch: 2026-05-13T06:56Z
TLE epoch observation values (Epoch: 2026-05-13T06:56:33.156Z)
Latitude
-0.00004°
Longitude
-86.26588°
Altitude
508.866 km
Speed
7.609 km/s
True Right ascension
16h 35m 41s
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
01:57:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.206 km
Perigee altitude
500.116 km
Semi-major axis
6,880.298 km
Eccentricity
0.0003
Inclination
97.4674°
RAAN
248.9237°
Arg. of periapsis
106.726°
True anomaly
253.39746°
Mean anomaly
253.4301°
Eccentric anomaly
253.41378°
Mean motion
3.80305 °/min
Orbital period
94.66 mins
BSTAR
0.000098106
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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 | 2026-05-13 20:08:37.313Z | 29.42° NE | 2026-05-13 20:11:37.313Z | 91.076° ESE | 32.451° | 2026-05-13 20:14:37.313Z | 165.35° S |
| 4 mins | 2026-05-14 08:21:37.313Z | 218.946° SW | 2026-05-14 08:23:37.313Z | 271.219° WNW | 25.38° | 2026-05-14 08:25:37.313Z | 314.886° NW |
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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