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: 1 day ago
TLE from 1 day ago
0 CONNECTA IOT-11
1 64557U 25135AF 26259.30382382 .00003842 00000-0 17541-3 0 9994
2 64557 97.4797 13.8671 0002075 62.8407 297.3040 15.21194044 68717Epoch: 2026-09-16T07:17Z
TLE epoch observation values (Epoch: 2026-09-16T07:17:30.378Z)
Latitude
0.00001°
Longitude
-90.76682°
Altitude
504.673 km
Speed
7.612 km/s
True Right ascension
00h 55m 28s
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
03:01:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.632 km
Perigee altitude
497.778 km
Semi-major axis
6,877.342 km
Eccentricity
0.00021
Inclination
97.4797°
RAAN
13.8671°
Arg. of periapsis
62.8407°
True anomaly
297.28287°
Mean anomaly
297.304°
Eccentric anomaly
297.29343°
Mean motion
3.8055 °/min
Orbital period
94.6 mins
BSTAR
0.00017541
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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 | 2026-09-17 20:09:52.766Z | 30.056° NE | 2026-09-17 20:12:52.766Z | 88.839° E | 37.519° | 2026-09-17 20:15:52.766Z | 163.251° S |
| 5 mins | 2026-09-18 08:21:52.766Z | 209.105° SW | 2026-09-18 08:23:52.766Z | 253.578° W | 30.113° | 2026-09-18 08:26:52.766Z | 321.481° 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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