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: 11 hours ago
TLE from 11 hours ago
0 CONNECTA IOT-6
1 62709U 25009DE 26081.13313596 .00000933 00000-0 92806-4 0 9992
2 62709 97.7059 161.1592 0002929 80.5209 279.6342 14.94012656 64364Epoch: 2026-03-22T03:11Z
TLE epoch observation values (Epoch: 2026-03-22T03:11:42.946Z)
Latitude
-0.00006°
Longitude
-66.41361°
Altitude
588.145 km
Speed
7.566 km/s
True Right ascension
10h 44m 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
18:54:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.491 km
Perigee altitude
580.414 km
Semi-major axis
6,960.59 km
Eccentricity
0.00029
Inclination
97.7059°
RAAN
161.1592°
Arg. of periapsis
80.5209°
True anomaly
279.60111°
Mean anomaly
279.6342°
Eccentric anomaly
279.61765°
Mean motion
3.73744 °/min
Orbital period
96.32 mins
BSTAR
0.000092806
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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 | 2026-03-22 18:13:03.747Z | 9.731° NNE | 2026-03-22 18:17:03.747Z | 274.095° WNW | 44.535° | 2026-03-22 18:21:03.747Z | 197.397° SSW |
| 6 mins | 2026-03-23 05:03:03.747Z | 149.33° SSE | 2026-03-23 05:06:03.747Z | 54.197° ENE | 40.263° | 2026-03-23 05:09:03.747Z | 357.759° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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