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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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: 7 hours ago
TLE from 7 hours ago
0 CONNECTA IOT-4
1 60524U 24149BJ 26265.23034702 .00022006 00000-0 45253-3 0 9991
2 60524 97.3745 350.9717 0003905 296.4987 63.5862 15.45979531117309Epoch: 2026-09-22T05:31Z
TLE epoch observation values (Epoch: 2026-09-22T05:31:41.982Z)
Latitude
0.00002°
Longitude
-93.05203°
Altitude
430.446 km
Speed
7.654 km/s
True Right ascension
23h 23m 53s
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
06:03:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.088 km
Perigee altitude
422.775 km
Semi-major axis
6,803.568 km
Eccentricity
0.00039
Inclination
97.3745°
RAAN
350.9717°
Arg. of periapsis
296.4987°
True anomaly
63.62629°
Mean anomaly
63.5862°
Eccentric anomaly
63.60624°
Mean motion
3.86757 °/min
Orbital period
93.08 mins
BSTAR
0.00045253
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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 | 2026-09-22 18:31:12.132Z | 22.786° NE | 2026-09-22 18:33:12.132Z | 62.905° ENE | 53.509° | 2026-09-22 18:36:12.132Z | 179.249° S |
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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