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: 19 hours ago
TLE from 19 hours ago
0 CONNECTA IOT-4
1 60524U 24149BJ 26080.19348085 .00021493 00000-0 56024-3 0 9990
2 60524 97.3825 163.7337 0004905 237.2632 122.8141 15.38860412 88784Epoch: 2026-03-21T04:38Z
TLE epoch observation values (Epoch: 2026-03-21T04:38:36.745Z)
Latitude
-0.00002°
Longitude
-84.63711°
Altitude
454.411 km
Speed
7.639 km/s
True Right ascension
10h 54m 56s
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
04:26:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.765 km
Perigee altitude
443.07 km
Semi-major axis
6,824.555 km
Eccentricity
0.00049
Inclination
97.3825°
RAAN
163.7337°
Arg. of periapsis
237.2632°
True anomaly
122.86132°
Mean anomaly
122.8141°
Eccentric anomaly
122.83771°
Mean motion
3.84974 °/min
Orbital period
93.51 mins
BSTAR
0.00056024
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-22 05:44:07.213Z | 179.239° S | 2026-03-22 05:47:07.213Z | 258.806° W | 40.971° | 2026-03-22 05:50:07.213Z | 339.51° N |
| 5 mins | 2026-03-22 18:40:07.213Z | 351.549° N | 2026-03-22 18:42:07.213Z | 274.483° WNW | 37.244° | 2026-03-22 18:45:07.213Z | 209.526° SW |
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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