CONNECTA IOT-10, 64555
Orbit data source: Space-Track
CONNECTA IOT-10, 64555 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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64555 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: 12 hours ago
TLE from 12 hours ago
0 CONNECTA IOT-10
1 64555U 25135AD 26224.88523635 .00001424 00000-0 67921-4 0 9997
2 64555 97.4727 339.4012 0002482 104.1559 255.9952 15.20702331 63477Epoch: 2026-08-12T21:14Z
TLE epoch observation values (Epoch: 2026-08-12T21:14:44.420Z)
Latitude
-0.00006°
Longitude
59.38337°
Altitude
507.224 km
Speed
7.61 km/s
True Right ascension
22h 37m 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
23:40:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.396 km
Perigee altitude
498.981 km
Semi-major axis
6,878.826 km
Eccentricity
0.00025
Inclination
97.4727°
RAAN
339.4012°
Arg. of periapsis
104.1559°
True anomaly
255.96761°
Mean anomaly
255.9952°
Eccentric anomaly
255.9814°
Mean motion
3.80427 °/min
Orbital period
94.63 mins
BSTAR
0.000067921
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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-10 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 19:55:49.850Z | 43.859° NE | 2026-08-13 19:58:49.850Z | 110.514° ESE | 23.145° | 2026-08-13 20:00:49.850Z | 148.69° SSE |
| 5 mins | 2026-08-14 08:07:49.850Z | 201.002° SSW | 2026-08-14 08:09:49.850Z | 268.412° W | 34.652° | 2026-08-14 08:12:49.850Z | 332.5° NNW |
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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