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: 1 day ago
TLE from 1 day ago
0 CONNECTA IOT-3
1 60475U 24149H 25312.66639634 .00013203 00000-0 57776-3 0 9992
2 60475 97.3961 27.4643 0002359 354.0139 6.1068 15.22173663 68246Epoch: 2025-11-08T15:59Z
TLE epoch observation values (Epoch: 2025-11-08T15:59:36.643Z)
Latitude
-0.00011°
Longitude
99.4689°
Altitude
500.766 km
Speed
7.615 km/s
True Right ascension
01h 49m 51s
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
19:00:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.87 km
Perigee altitude
494.626 km
Semi-major axis
6,874.385 km
Eccentricity
0.00024
Inclination
97.3961°
RAAN
27.4643°
Arg. of periapsis
354.0139°
True anomaly
6.10968°
Mean anomaly
6.1068°
Eccentric anomaly
6.10824°
Mean motion
3.80796 °/min
Orbital period
94.54 mins
BSTAR
0.00057776
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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 | 2025-11-10 04:25:49.658Z | 115.207° SE | 2025-11-10 04:27:49.658Z | 74.9° E | 21.201° | 2025-11-10 04:30:49.658Z | 17.921° NNE |
| 5 mins | 2025-11-10 17:28:49.658Z | 42.229° NE | 2025-11-10 17:30:49.658Z | 89.162° E | 28.097° | 2025-11-10 17:33:49.658Z | 158.486° 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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