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: 1 day ago
TLE from 1 day ago
0 CONNECTA IOT-10
1 64555U 25135AD 25312.77352661 .00009165 00000-0 43684-3 0 9990
2 64555 97.4547 65.2648 0001798 59.8108 300.3304 15.19329357 21371Epoch: 2025-11-08T18:33Z
TLE epoch observation values (Epoch: 2025-11-08T18:33:52.699Z)
Latitude
-0.00005°
Longitude
98.5969°
Altitude
510.329 km
Speed
7.609 km/s
True Right ascension
04h 21m 03s
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
19:05:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.073 km
Perigee altitude
503.597 km
Semi-major axis
6,882.972 km
Eccentricity
0.00018
Inclination
97.4547°
RAAN
65.2648°
Arg. of periapsis
59.8108°
True anomaly
300.31261°
Mean anomaly
300.3304°
Eccentric anomaly
300.32151°
Mean motion
3.80084 °/min
Orbital period
94.72 mins
BSTAR
0.00043684
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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 | 2025-11-10 07:03:15.856Z | 130.05° SE | 2025-11-10 07:06:15.856Z | 71.042° E | 25.529° | 2025-11-10 07:09:15.856Z | 12.618° NNE |
| 5 mins | 2025-11-10 20:09:15.856Z | 44.801° NE | 2025-11-10 20:11:15.856Z | 120.012° SE | 33.171° | 2025-11-10 20:14:15.856Z | 171.348° S |
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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