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: 12 hours ago
TLE from 12 hours ago
0 CONNECTA IOT-1
1 60472U 24149E 26080.46075174 .00005568 00000-0 23957-3 0 9992
2 60472 97.3802 158.2631 0001597 172.5393 187.5868 15.23027004 88449Epoch: 2026-03-21T11:03Z
TLE epoch observation values (Epoch: 2026-03-21T11:03:28.950Z)
Latitude
-0°
Longitude
173.41134°
Altitude
500.9 km
Speed
7.613 km/s
True Right ascension
10h 33m 03s
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
04:26:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.774 km
Perigee altitude
492.58 km
Semi-major axis
6,871.814 km
Eccentricity
0.00016
Inclination
97.3802°
RAAN
158.2631°
Arg. of periapsis
172.5393°
True anomaly
187.58438°
Mean anomaly
187.5868°
Eccentric anomaly
187.58559°
Mean motion
3.8101 °/min
Orbital period
94.49 mins
BSTAR
0.00023957
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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 | 2026-03-22 04:32:34.830Z | 127.166° SE | 2026-03-22 04:35:34.830Z | 61.253° ENE | 24.803° | 2026-03-22 04:37:34.830Z | 19.574° NNE |
| 5 mins | 2026-03-22 17:35:34.830Z | 35.099° NE | 2026-03-22 17:37:34.830Z | 81.48° E | 32.177° | 2026-03-22 17:40:34.830Z | 164.441° S |
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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