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: 2 days ago
TLE from 2 days ago
0 CONNECTA IOT-4
1 60524U 24149BJ 26173.20336971 .00015178 00000-0 35423-3 0 9999
2 60524 97.3793 257.6331 0004200 260.6701 99.4072 15.42298517103102Epoch: 2026-06-22T04:52Z
TLE epoch observation values (Epoch: 2026-06-22T04:52:51.142Z)
Latitude
0°
Longitude
-85.97265°
Altitude
442.918 km
Speed
7.646 km/s
True Right ascension
17h 10m 31s
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
13:52:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
439.124 km
Perigee altitude
433.4 km
Semi-major axis
6,814.399 km
Eccentricity
0.00042
Inclination
97.3793°
RAAN
257.6331°
Arg. of periapsis
260.6701°
True anomaly
99.45468°
Mean anomaly
99.4072°
Eccentric anomaly
99.43094°
Mean motion
3.85835 °/min
Orbital period
93.3 mins
BSTAR
0.00035423
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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 | 2026-06-24 05:17:21.740Z | 137.208° SSE | 2026-06-24 05:19:21.740Z | 93.9° ESE | 29.796° | 2026-06-24 05:22:21.740Z | 9.044° NNE |
| 4 mins | 2026-06-24 18:11:21.740Z | 43.298° NE | 2026-06-24 18:13:21.740Z | 122.846° SE | 31.73° | 2026-06-24 18:15:21.740Z | 166.331° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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