CONNECTA IOT-6, 62709
Orbit data source: Space-Track
CONNECTA IOT-6, 62709 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Tue, 14 Jan 2025 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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62709 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: 9 hours ago
TLE from 9 hours ago
0 CONNECTA IOT-6
1 62709U 25009DE 26171.47630977 .00000613 00000-0 62414-4 0 9991
2 62709 97.7028 249.7825 0002927 110.4543 249.6991 14.94216100 77859Epoch: 2026-06-20T11:25Z
TLE epoch observation values (Epoch: 2026-06-20T11:25:53.164Z)
Latitude
-0.00007°
Longitude
169.62061°
Altitude
588.561 km
Speed
7.565 km/s
True Right ascension
16h 39m 07s
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
07:20:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.857 km
Perigee altitude
579.783 km
Semi-major axis
6,959.957 km
Eccentricity
0.00029
Inclination
97.7028°
RAAN
249.7825°
Arg. of periapsis
110.4543°
True anomaly
249.66765°
Mean anomaly
249.6991°
Eccentric anomaly
249.68337°
Mean motion
3.73795 °/min
Orbital period
96.31 mins
BSTAR
0.000062414
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Other satellites on launch #9 in the year 2025 (2025-01-14 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-6 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 05:13:28.495Z | 165.223° S | 2026-06-21 05:17:28.495Z | 42.528° NE | 44.93° | 2026-06-21 05:21:28.495Z | 348.576° N |
| 6 mins | 2026-06-21 18:32:28.495Z | 352.065° N | 2026-06-21 18:35:28.495Z | 270.523° WNW | 34.811° | 2026-06-21 18:38:28.495Z | 216.834° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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