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: 17 hours ago
TLE from 17 hours ago
0 CONNECTA IOT-1
1 60472U 24149E 25286.95562690 .00007961 00000-0 34579-3 0 9998
2 60472 97.4010 2.3053 0003325 75.3911 284.7694 15.22566329 64320Epoch: 2025-10-13T22:56Z
TLE epoch observation values (Epoch: 2025-10-13T22:56:06.164Z)
Latitude
-0.00001°
Longitude
-4.47136°
Altitude
500.615 km
Speed
7.614 km/s
True Right ascension
00h 09m 13s
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
10:35:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.351 km
Perigee altitude
492.78 km
Semi-major axis
6,873.202 km
Eccentricity
0.00033
Inclination
97.401°
RAAN
2.3053°
Arg. of periapsis
75.3911°
True anomaly
284.73255°
Mean anomaly
284.7694°
Eccentric anomaly
284.75098°
Mean motion
3.80894 °/min
Orbital period
94.51 mins
BSTAR
0.00034579
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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 | 2025-10-14 18:25:48.800Z | 348.732° N | 2025-10-14 18:27:48.800Z | 300.35° NW | 32.624° | 2025-10-14 18:30:48.800Z | 220.446° SW |
| 5 mins | 2025-10-15 05:02:48.800Z | 153.866° SSE | 2025-10-15 05:04:48.800Z | 83.87° E | 42.749° | 2025-10-15 05:07:48.800Z | 354.965° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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