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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 CONNECTA IOT-11
1 64557U 25135AF 25269.29149425 .00008395 00000-0 40597-3 0 9996
2 64557 97.4535 22.4387 0001614 151.1485 208.9839 15.18852783 14771Epoch: 2025-09-26T06:59Z
TLE epoch observation values (Epoch: 2025-09-26T06:59:45.103Z)
Latitude
0.00001°
Longitude
-87.8396°
Altitude
513.367 km
Speed
7.607 km/s
True Right ascension
01h 29m 45s
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
15:08:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.387 km
Perigee altitude
505.165 km
Semi-major axis
6,884.413 km
Eccentricity
0.00016
Inclination
97.4535°
RAAN
22.4387°
Arg. of periapsis
151.1485°
True anomaly
208.97494°
Mean anomaly
208.9839°
Eccentric anomaly
208.97942°
Mean motion
3.79964 °/min
Orbital period
94.75 mins
BSTAR
0.00040597
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-27 06:52:48.456Z | 97.429° ESE | 2025-09-27 06:53:48.456Z | 76.053° E | 19.392° | 2025-09-27 06:56:48.456Z | 20.834° NNE |
| 4 mins | 2025-09-27 08:26:48.456Z | 238.025° WSW | 2025-09-27 08:27:48.456Z | 262.288° W | 21.665° | 2025-09-27 08:30:48.456Z | 318.208° NNW |
| 5 mins | 2025-09-27 19:56:48.456Z | 47.946° ENE | 2025-09-27 19:58:48.456Z | 97.488° ESE | 26.507° | 2025-09-27 20:01:48.456Z | 157.66° 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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