CONNECTA IOT-7, 62715
Orbit data source: Space-Track
CONNECTA IOT-7, 62715 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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62715 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: 8 hours ago
TLE from 8 hours ago
0 CONNECTA IOT-7
1 62715U 25009DL 25286.47381845 .00002129 00000-0 20823-3 0 9992
2 62715 97.7304 4.6042 0000519 12.2132 347.9100 14.93384448 40517Epoch: 2025-10-13T11:22Z
TLE epoch observation values (Epoch: 2025-10-13T11:22:17.914Z)
Latitude
-0.00002°
Longitude
171.75347°
Altitude
590.083 km
Speed
7.565 km/s
True Right ascension
00h 18m 25s
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
13:54:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.769 km
Perigee altitude
584.046 km
Semi-major axis
6,962.544 km
Eccentricity
0.00005
Inclination
97.7304°
RAAN
4.6042°
Arg. of periapsis
12.2132°
True anomaly
347.90875°
Mean anomaly
347.91°
Eccentric anomaly
347.90938°
Mean motion
3.73587 °/min
Orbital period
96.36 mins
BSTAR
0.00020823
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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-7 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-14 05:11:02.506Z | 157.653° S | 2025-10-14 05:14:02.506Z | 121.973° SE | 41.482° | 2025-10-14 05:18:02.506Z | 353.523° N |
| 6 mins | 2025-10-14 18:30:02.506Z | 357.743° N | 2025-10-14 18:33:02.506Z | 262.867° W | 38.958° | 2025-10-14 18:36:02.506Z | 210.013° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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