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: 22 hours ago
TLE from 22 hours ago
0 CONNECTA IOT-1
1 60472U 24149E 26264.75276685 .00005480 00000-0 22698-3 0 9992
2 60472 97.3686 339.4171 0000868 343.7808 16.3402 15.24323403116509Epoch: 2026-09-21T18:03Z
TLE epoch observation values (Epoch: 2026-09-21T18:03:59.055Z)
Latitude
-0.00001°
Longitude
67.79296°
Altitude
495.343 km
Speed
7.617 km/s
True Right ascension
22h 37m 40s
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
09:22:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.372 km
Perigee altitude
489.18 km
Semi-major axis
6,867.913 km
Eccentricity
0.00009
Inclination
97.3686°
RAAN
339.4171°
Arg. of periapsis
343.7808°
True anomaly
16.343°
Mean anomaly
16.3402°
Eccentric anomaly
16.3416°
Mean motion
3.81334 °/min
Orbital period
94.41 mins
BSTAR
0.00022698
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-22 18:14:51.732Z | 0.793° NNE | 2026-09-22 18:17:51.732Z | 314.779° NW | 45.887° | 2026-09-22 18:21:51.732Z | 209.726° SW |
| 6 mins | 2026-09-23 04:51:51.732Z | 146.546° SSE | 2026-09-23 04:53:51.732Z | 105.081° ESE | 48.138° | 2026-09-23 04:57:51.732Z | 358.264° 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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