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: 11 hours ago
TLE from 11 hours ago
0 CONNECTA IOT-10
1 64555U 25135AD 26035.80277983 .00005467 00000-0 25569-3 0 9993
2 64555 97.4549 152.2258 0002335 78.0932 282.0565 15.20175141 34745Epoch: 2026-02-04T19:16Z
TLE epoch observation values (Epoch: 2026-02-04T19:16:00.177Z)
Latitude
0.00001°
Longitude
88.26093°
Altitude
508.066 km
Speed
7.61 km/s
True Right ascension
10h 08m 54s
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
07:52:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.886 km
Perigee altitude
500.673 km
Semi-major axis
6,880.417 km
Eccentricity
0.00023
Inclination
97.4549°
RAAN
152.2258°
Arg. of periapsis
78.0932°
True anomaly
282.03033°
Mean anomaly
282.0565°
Eccentric anomaly
282.04342°
Mean motion
3.80295 °/min
Orbital period
94.66 mins
BSTAR
0.00025569
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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 | 2026-02-05 08:02:40.892Z | 196.865° SSW | 2026-02-05 08:04:40.892Z | 260.702° W | 36.038° | 2026-02-05 08:07:40.892Z | 332.873° NNW |
| 5 mins | 2026-02-05 21:06:40.892Z | 340.494° N | 2026-02-05 21:08:40.892Z | 293.954° NW | 27.158° | 2026-02-05 21:11:40.892Z | 228.639° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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