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: 5 hours ago
TLE from 5 hours ago
0 CONNECTA IOT-1
1 60472U 24149E 26126.18807280 .00004033 00000-0 17336-3 0 9993
2 60472 97.3759 203.1978 0003510 79.8661 280.2972 15.23220246 95402Epoch: 2026-05-06T04:30Z
TLE epoch observation values (Epoch: 2026-05-06T04:30:49.489Z)
Latitude
-0.00003°
Longitude
-88.56055°
Altitude
498.8 km
Speed
7.615 km/s
True Right ascension
13h 32m 47s
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
17:31:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.507 km
Perigee altitude
490.683 km
Semi-major axis
6,871.232 km
Eccentricity
0.00035
Inclination
97.3759°
RAAN
203.1978°
Arg. of periapsis
79.8661°
True anomaly
280.25762°
Mean anomaly
280.2972°
Eccentric anomaly
280.27741°
Mean motion
3.81058 °/min
Orbital period
94.47 mins
BSTAR
0.00017336
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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 | 2026-05-06 17:41:00.063Z | 23.03° NE | 2026-05-06 17:44:00.063Z | 73.584° E | 36.389° | 2026-05-06 17:47:00.063Z | 171.744° S |
| 4 mins | 2026-05-07 05:53:00.063Z | 226.771° WSW | 2026-05-07 05:55:00.063Z | 275.233° WNW | 21.614° | 2026-05-07 05:57:00.063Z | 313.666° NW |
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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