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: 17 hours ago
TLE from 17 hours ago
0 CONNECTA IOT-11
1 64557U 25135AF 25327.84360454 .00005096 00000-0 24166-3 0 9998
2 64557 97.4584 80.2362 0001933 46.2994 313.8401 15.19729397 23667Epoch: 2025-11-23T20:14Z
TLE epoch observation values (Epoch: 2025-11-23T20:14:47.432Z)
Latitude
0.00002°
Longitude
73.48646°
Altitude
508.824 km
Speed
7.61 km/s
True Right ascension
05h 20m 56s
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
10:46:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.956 km
Perigee altitude
502.296 km
Semi-major axis
6,881.763 km
Eccentricity
0.00019
Inclination
97.4584°
RAAN
80.2362°
Arg. of periapsis
46.2994°
True anomaly
313.82412°
Mean anomaly
313.8401°
Eccentric anomaly
313.83211°
Mean motion
3.80184 °/min
Orbital period
94.69 mins
BSTAR
0.00024166
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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 | 2025-11-24 20:30:37.208Z | 12.432° NNE | 2025-11-24 20:33:37.208Z | 24.627° NE | 44.798° | 2025-11-24 20:36:37.208Z | 192.353° SSW |
| 5 mins | 2025-11-25 07:09:37.208Z | 125.001° SE | 2025-11-25 07:11:37.208Z | 75.276° E | 28.337° | 2025-11-25 07:14:37.208Z | 10.794° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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