CONNECTA IOT-4, 60524
Orbit data source: Space-Track
CONNECTA IOT-4, 60524 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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60524 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: 19 hours ago
TLE from 19 hours ago
0 CONNECTA IOT-4
1 60524U 24149BJ 25338.66621053 .00033394 00000-0 99477-3 0 9998
2 60524 97.3978 56.6777 0005036 265.9561 94.1107 15.34605362 72420Epoch: 2025-12-04T15:59Z
TLE epoch observation values (Epoch: 2025-12-04T15:59:20.589Z)
Latitude
0.00001°
Longitude
103.12253°
Altitude
465.452 km
Speed
7.634 km/s
True Right ascension
03h 46m 42s
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
09:18:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.482 km
Perigee altitude
455.596 km
Semi-major axis
6,837.176 km
Eccentricity
0.0005
Inclination
97.3978°
RAAN
56.6777°
Arg. of periapsis
265.9561°
True anomaly
94.16826°
Mean anomaly
94.1107°
Eccentric anomaly
94.13948°
Mean motion
3.83909 °/min
Orbital period
93.77 mins
BSTAR
0.00099477
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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-4 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 | 2025-12-05 17:35:58.623Z | 44.222° NE | 2025-12-05 17:37:58.623Z | 84.154° E | 22.271° | 2025-12-05 17:40:58.623Z | 150.447° SSE |
| 5 mins | 2025-12-06 05:40:58.623Z | 189.337° SSW | 2025-12-06 05:42:58.623Z | 250.43° W | 38.186° | 2025-12-06 05:45:58.623Z | 335.728° NNW |
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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