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: 13 hours ago
TLE from 13 hours ago
0 CONNECTA IOT-11
1 64557U 25135AF 26224.56700579 .00001594 00000-0 75504-4 0 9992
2 64557 97.4759 339.3924 0002586 123.8925 236.2557 15.20774393 63431Epoch: 2026-08-12T13:36Z
TLE epoch observation values (Epoch: 2026-08-12T13:36:29.300Z)
Latitude
0.00003°
Longitude
174.25122°
Altitude
507.582 km
Speed
7.61 km/s
True Right ascension
22h 37m 34s
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
16:55:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.25 km
Perigee altitude
498.692 km
Semi-major axis
6,878.608 km
Eccentricity
0.00026
Inclination
97.4759°
RAAN
339.3924°
Arg. of periapsis
123.8925°
True anomaly
236.23106°
Mean anomaly
236.2557°
Eccentric anomaly
236.24338°
Mean motion
3.80445 °/min
Orbital period
94.63 mins
BSTAR
0.000075504
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-13 07:07:09.493Z | 125.914° SE | 2026-08-13 07:10:09.493Z | 61.67° ENE | 24.261° | 2026-08-13 07:12:09.493Z | 20.435° NNE |
| 4 mins | 2026-08-13 20:12:09.493Z | 48.081° ENE | 2026-08-13 20:14:09.493Z | 119.61° SE | 31.24° | 2026-08-13 20:16:09.493Z | 162.175° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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