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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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: 10 hours ago
TLE from 10 hours ago
0 CONNECTA IOT-10
1 64555U 25135AD 25328.31548573 .00004582 00000-0 21889-3 0 9997
2 64555 97.4548 80.6077 0000954 50.6183 309.5136 15.19529971 23734Epoch: 2025-11-24T07:34Z
TLE epoch observation values (Epoch: 2025-11-24T07:34:17.967Z)
Latitude
-0.00001°
Longitude
-96.48438°
Altitude
509.93 km
Speed
7.609 km/s
True Right ascension
05h 22m 25s
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
14:20:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.885 km
Perigee altitude
503.572 km
Semi-major axis
6,882.366 km
Eccentricity
0.0001
Inclination
97.4548°
RAAN
80.6077°
Arg. of periapsis
50.6183°
True anomaly
309.50517°
Mean anomaly
309.5136°
Eccentric anomaly
309.50938°
Mean motion
3.80134 °/min
Orbital period
94.7 mins
BSTAR
0.00021889
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-24 20:46:14.775Z | 1.392° NNE | 2025-11-24 20:49:14.775Z | 301.864° NW | 38.815° | 2025-11-24 20:52:14.775Z | 210.695° SW |
| 5 mins | 2025-11-25 07:25:14.775Z | 144.973° SSE | 2025-11-25 07:27:14.775Z | 91.079° ESE | 38.357° | 2025-11-25 07:30:14.775Z | 1.232° 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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