CONNECTA IOT-3, 60475
Orbit data source: Space-Track
CONNECTA IOT-3, 60475 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Fri, 16 Aug 2024 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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60475 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: 16 hours ago
TLE from 16 hours ago
0 CONNECTA IOT-3
1 60475U 24149H 26295.75572276 .00009863 00000-0 40114-3 0 9996
2 60475 97.3634 9.6071 0003385 153.4516 206.6896 15.24725718121231Epoch: 2026-10-22T18:08Z
TLE epoch observation values (Epoch: 2026-10-22T18:08:14.446Z)
Latitude
0°
Longitude
66.36085°
Altitude
496.785 km
Speed
7.615 km/s
True Right ascension
00h 38m 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
05:27:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.891 km
Perigee altitude
486.243 km
Semi-major axis
6,866.704 km
Eccentricity
0.00034
Inclination
97.3634°
RAAN
9.6071°
Arg. of periapsis
153.4516°
True anomaly
206.67218°
Mean anomaly
206.6896°
Eccentric anomaly
206.68089°
Mean motion
3.81435 °/min
Orbital period
94.38 mins
BSTAR
0.00040114
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-3 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 | 2026-10-23 18:19:44.386Z | 350.75° N | 2026-10-23 18:21:44.386Z | 306.247° NW | 40.142° | 2026-10-23 18:24:44.386Z | 220.086° SW |
| 5 mins | 2026-10-24 04:55:44.386Z | 151.359° SSE | 2026-10-24 04:57:44.386Z | 98.216° ESE | 60.213° | 2026-10-24 05:00:44.386Z | 357.605° N |
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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