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: 10 hours ago
TLE from 10 hours ago
0 CONNECTA IOT-4
1 60524U 24149BJ 26219.76131025 .00010994 00000-0 24293-3 0 9998
2 60524 97.3777 304.8043 0006633 105.2095 254.9887 15.44002108110281Epoch: 2026-08-07T18:16Z
TLE epoch observation values (Epoch: 2026-08-07T18:16:17.205Z)
Latitude
-0.00004°
Longitude
74.45025°
Altitude
438.609 km
Speed
7.648 km/s
True Right ascension
20h 19m 13s
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
18:31:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.761 km
Perigee altitude
426.728 km
Semi-major axis
6,809.381 km
Eccentricity
0.00066
Inclination
97.3777°
RAAN
304.8043°
Arg. of periapsis
105.2095°
True anomaly
254.9153°
Mean anomaly
254.9887°
Eccentric anomaly
254.952°
Mean motion
3.86262 °/min
Orbital period
93.2 mins
BSTAR
0.00024293
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-08 05:18:18.842Z | 127.997° SE | 2026-08-08 05:20:18.842Z | 74.333° E | 27.562° | 2026-08-08 05:22:18.842Z | 18.718° NNE |
| 4 mins | 2026-08-08 18:11:18.842Z | 54.998° ENE | 2026-08-08 18:12:18.842Z | 88.427° E | 28.689° | 2026-08-08 18:15:18.842Z | 163.426° 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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