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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 6 hours ago
TLE from 6 hours ago
0 CONNECTA IOT-1
1 60472U 24149E 26035.18579448 .00005495 00000-0 23984-3 0 9993
2 60472 97.3880 113.7551 0002912 54.7423 305.4085 15.22540635 81555Epoch: 2026-02-04T04:27Z
TLE epoch observation values (Epoch: 2026-02-04T04:27:32.643Z)
Latitude
-0.00007°
Longitude
-87.4869°
Altitude
500.115 km
Speed
7.615 km/s
True Right ascension
07h 35m 01s
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
12:22:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.144 km
Perigee altitude
493.141 km
Semi-major axis
6,873.279 km
Eccentricity
0.00029
Inclination
97.388°
RAAN
113.7551°
Arg. of periapsis
54.7423°
True anomaly
305.3813°
Mean anomaly
305.4085°
Eccentric anomaly
305.3949°
Mean motion
3.80888 °/min
Orbital period
94.52 mins
BSTAR
0.00023984
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-04 17:38:37.594Z | 28.425° NE | 2026-02-04 17:41:37.594Z | 104.211° ESE | 35.047° | 2026-02-04 17:44:37.594Z | 170.888° S |
| 4 mins | 2026-02-05 05:50:37.594Z | 227.737° WSW | 2026-02-05 05:51:37.594Z | 252.388° W | 23.586° | 2026-02-05 05:54:37.594Z | 317.961° NNW |
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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