CONNECTA IOT-1, 60472
Orbit data source: Space-Track
CONNECTA IOT-1, 60472 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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60472 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-1
1 60472U 24149E 26171.44543448 .00003210 00000-0 13722-3 0 9996
2 60472 97.3755 247.6820 0000465 222.4815 137.6386 15.23561077102290Epoch: 2026-06-20T10:41Z
TLE epoch observation values (Epoch: 2026-06-20T10:41:25.539Z)
Latitude
-0.00002°
Longitude
178.66564°
Altitude
498.442 km
Speed
7.615 km/s
True Right ascension
16h 30m 43s
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
07:21:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.389 km
Perigee altitude
491.75 km
Semi-major axis
6,870.206 km
Eccentricity
0.00005
Inclination
97.3755°
RAAN
247.682°
Arg. of periapsis
222.4815°
True anomaly
137.64219°
Mean anomaly
137.6386°
Eccentric anomaly
137.6404°
Mean motion
3.81143 °/min
Orbital period
94.45 mins
BSTAR
0.00013722
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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-1 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 | 2026-06-21 05:44:30.568Z | 212.185° SW | 2026-06-21 05:46:30.568Z | 260.053° W | 26.207° | 2026-06-21 05:49:30.568Z | 323.072° NNW |
| 4 mins | 2026-06-21 18:47:30.568Z | 321.986° NNW | 2026-06-21 18:48:30.568Z | 300.669° NW | 19.607° | 2026-06-21 18:51:30.568Z | 241.895° WSW |
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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