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: 1 day ago
TLE from 1 day ago
0 CONNECTA IOT-1
1 60472U 24149E 26259.17283180 .00007648 00000-0 31613-3 0 9995
2 60472 97.3685 333.9319 0001385 9.6617 350.4647 15.24262392115659Epoch: 2026-09-16T04:08Z
TLE epoch observation values (Epoch: 2026-09-16T04:08:52.667Z)
Latitude
-0.00002°
Longitude
-83.41577°
Altitude
495.16 km
Speed
7.618 km/s
True Right ascension
22h 15m 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
03:01:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.911 km
Perigee altitude
489.009 km
Semi-major axis
6,868.097 km
Eccentricity
0.00014
Inclination
97.3685°
RAAN
333.9319°
Arg. of periapsis
9.6617°
True anomaly
350.46207°
Mean anomaly
350.4647°
Eccentric anomaly
350.46339°
Mean motion
3.81319 °/min
Orbital period
94.41 mins
BSTAR
0.00031613
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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 | 2026-09-17 18:32:01.288Z | 336.317° NNW | 2026-09-17 18:34:01.288Z | 282.458° WNW | 31.188° | 2026-09-17 18:37:01.288Z | 225.213° WSW |
| 5 mins | 2026-09-18 05:08:01.288Z | 165.526° S | 2026-09-18 05:10:01.288Z | 10.26° NNE | 82.868° | 2026-09-18 05:13:01.288Z | 348.891° N |
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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