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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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: 7 hours ago
TLE from 7 hours ago
0 CONNECTA IOT-6
1 62709U 25009DE 25286.49988575 .00003468 00000-0 33630-3 0 9997
2 62709 97.7251 4.4004 0001032 170.6948 189.4291 14.93322362 40531Epoch: 2025-10-13T11:59Z
TLE epoch observation values (Epoch: 2025-10-13T11:59:50.128Z)
Latitude
-0.00004°
Longitude
162.13976°
Altitude
591.339 km
Speed
7.564 km/s
True Right ascension
00h 17m 36s
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
13:48:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.319 km
Perigee altitude
583.882 km
Semi-major axis
6,962.737 km
Eccentricity
0.0001
Inclination
97.7251°
RAAN
4.4004°
Arg. of periapsis
170.6948°
True anomaly
189.42716°
Mean anomaly
189.4291°
Eccentric anomaly
189.42813°
Mean motion
3.73571 °/min
Orbital period
96.37 mins
BSTAR
0.0003363
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-14 04:14:54.835Z | 93.56° ESE | 2025-10-14 04:16:54.835Z | 60.283° ENE | 15.52° | 2025-10-14 04:18:54.835Z | 30.192° NE |
| 6 mins | 2025-10-14 05:48:54.835Z | 198.365° SSW | 2025-10-14 05:51:54.835Z | 269.093° W | 32.524° | 2025-10-14 05:54:54.835Z | 327.852° NNW |
| 6 mins | 2025-10-14 17:31:54.835Z | 45.649° ENE | 2025-10-14 17:33:54.835Z | 83.611° E | 25.55° | 2025-10-14 17:37:54.835Z | 157.424° SSE |
| 4 mins | 2025-10-14 19:07:54.835Z | 325.19° NNW | 2025-10-14 19:09:54.835Z | 286.816° WNW | 19.825° | 2025-10-14 19:11:54.835Z | 252.019° W |
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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