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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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, 2.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 CONNECTA IOT-3
1 60475U 24149H 25286.17382945 .00006605 00000-0 28760-3 0 9997
2 60475 97.3959 1.4069 0005088 57.1955 302.9771 15.22539773 64215Epoch: 2025-10-13T04:10Z
TLE epoch observation values (Epoch: 2025-10-13T04:10:18.864Z)
Latitude
-0.00002°
Longitude
-83.1521°
Altitude
499.374 km
Speed
7.616 km/s
True Right ascension
00h 05m 37s
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
14:42:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.642 km
Perigee altitude
491.648 km
Semi-major axis
6,873.282 km
Eccentricity
0.00051
Inclination
97.3959°
RAAN
1.4069°
Arg. of periapsis
57.1955°
True anomaly
302.92817°
Mean anomaly
302.9771°
Eccentric anomaly
302.95264°
Mean motion
3.80888 °/min
Orbital period
94.52 mins
BSTAR
0.0002876
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-15 05:11:46.933Z | 168.641° S | 2025-10-15 05:14:46.933Z | 320.496° NNW | 44.736° | 2025-10-15 05:17:46.933Z | 347.073° N |
| 5 mins | 2025-10-15 18:15:46.933Z | 354.032° N | 2025-10-15 18:17:46.933Z | 277.908° WNW | 39.588° | 2025-10-15 18:20:46.933Z | 208.182° SW |
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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