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: 5 hours ago
TLE from 5 hours ago
0 CONNECTA IOT-1
1 60472U 24149E 25312.18918936 .00008889 00000-0 38123-3 0 9990
2 60472 97.3992 27.1600 0001679 21.4214 338.7093 15.22964547 68162Epoch: 2025-11-08T04:32Z
TLE epoch observation values (Epoch: 2025-11-08T04:32:25.960Z)
Latitude
-0.00001°
Longitude
-88.57054°
Altitude
498.923 km
Speed
7.616 km/s
True Right ascension
01h 48m 38s
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
05:32:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.02 km
Perigee altitude
492.712 km
Semi-major axis
6,872.003 km
Eccentricity
0.00017
Inclination
97.3992°
RAAN
27.16°
Arg. of periapsis
21.4214°
True anomaly
338.70231°
Mean anomaly
338.7093°
Eccentric anomaly
338.70581°
Mean motion
3.80994 °/min
Orbital period
94.49 mins
BSTAR
0.00038123
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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 | 2025-11-08 17:43:36.967Z | 27.702° NE | 2025-11-08 17:46:36.967Z | 127.028° SE | 36.389° | 2025-11-08 17:49:36.967Z | 176.473° S |
| 4 mins | 2025-11-09 05:54:36.967Z | 223.025° SW | 2025-11-09 05:56:36.967Z | 268.756° W | 21.82° | 2025-11-09 05:58:36.967Z | 310.346° NW |
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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