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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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: 10 hours ago
TLE from 10 hours ago
0 CONNECTA IOT-7
1 62715U 25009DL 26262.18754368 .00001176 00000-0 11448-3 0 9993
2 62715 97.7017 339.1987 0000761 157.6205 202.5049 14.94384561 91382Epoch: 2026-09-19T04:30Z
TLE epoch observation values (Epoch: 2026-09-19T04:30:03.773Z)
Latitude
-0.00002°
Longitude
-86.41669°
Altitude
587.82 km
Speed
7.566 km/s
True Right ascension
22h 36m 47s
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
07:49:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.826 km
Perigee altitude
580.767 km
Semi-major axis
6,959.434 km
Eccentricity
0.00008
Inclination
97.7017°
RAAN
339.1987°
Arg. of periapsis
157.6205°
True anomaly
202.50156°
Mean anomaly
202.5049°
Eccentric anomaly
202.50323°
Mean motion
3.73837 °/min
Orbital period
96.3 mins
BSTAR
0.00011448
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-19 17:55:02.052Z | 18.802° NNE | 2026-09-19 17:59:02.052Z | 109.607° ESE | 64.839° | 2026-09-19 18:03:02.052Z | 183.602° SSW |
| 6 mins | 2026-09-20 04:45:02.052Z | 130.192° SE | 2026-09-20 04:48:02.052Z | 54.896° ENE | 36.303° | 2026-09-20 04:51:02.052Z | 6.328° NNE |
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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