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: 3 hours ago
TLE from 3 hours ago
0 CONNECTA IOT-10
1 64555U 25135AD 26133.53875655 .00002077 00000-0 99099-4 0 9996
2 64555 97.4643 248.9100 0002523 90.2658 269.8866 15.20190371 49597Epoch: 2026-05-13T12:55Z
TLE epoch observation values (Epoch: 2026-05-13T12:55:48.565Z)
Latitude
-0.00007°
Longitude
-176.33968°
Altitude
508.359 km
Speed
7.61 km/s
True Right ascension
16h 35m 38s
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
00:50:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.97 km
Perigee altitude
500.498 km
Semi-major axis
6,880.371 km
Eccentricity
0.00025
Inclination
97.4643°
RAAN
248.91°
Arg. of periapsis
90.2658°
True anomaly
269.85769°
Mean anomaly
269.8866°
Eccentric anomaly
269.87214°
Mean motion
3.80299 °/min
Orbital period
94.66 mins
BSTAR
0.000099099
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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 | 2026-05-13 19:49:21.333Z | 44.225° NE | 2026-05-13 19:52:21.333Z | 104.054° ESE | 21.301° | 2026-05-13 19:54:21.333Z | 142.877° SSE |
| 4 mins | 2026-05-13 21:24:21.333Z | 320.781° NNW | 2026-05-13 21:25:21.333Z | 299.961° NW | 19.06° | 2026-05-13 21:28:21.333Z | 243.261° WSW |
| 6 mins | 2026-05-14 08:00:21.333Z | 184.578° SSW | 2026-05-14 08:03:21.333Z | 242.218° WSW | 37.054° | 2026-05-14 08:06:21.333Z | 332.844° 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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