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: 22 hours ago
TLE from 22 hours ago
0 CONNECTA IOT-11
1 64557U 25135AF 26035.31634235 .00005482 00000-0 25324-3 0 9994
2 64557 97.4583 151.9037 0002729 101.0440 259.1102 15.20599203 34677Epoch: 2026-02-04T07:35Z
TLE epoch observation values (Epoch: 2026-02-04T07:35:31.979Z)
Latitude
-0.00003°
Longitude
-96.46421°
Altitude
507.477 km
Speed
7.61 km/s
True Right ascension
10h 07m 36s
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
07:52:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.877 km
Perigee altitude
499.122 km
Semi-major axis
6,879.136 km
Eccentricity
0.00027
Inclination
97.4583°
RAAN
151.9037°
Arg. of periapsis
101.044°
True anomaly
259.07949°
Mean anomaly
259.1102°
Eccentric anomaly
259.09485°
Mean motion
3.80402 °/min
Orbital period
94.64 mins
BSTAR
0.00025324
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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 | 2026-02-05 07:24:39.987Z | 148.875° SSE | 2026-02-05 07:27:39.987Z | 78.26° E | 38.015° | 2026-02-05 07:30:39.987Z | 1.058° NNE |
| 5 mins | 2026-02-05 20:29:39.987Z | 16.352° NNE | 2026-02-05 20:31:39.987Z | 74.241° E | 44.548° | 2026-02-05 20:34:39.987Z | 189.074° SSW |
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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