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 26171.45162837 .00000636 00000-0 64597-4 0 9990
2 62715 97.7083 250.1532 0002051 134.2221 225.9168 14.94185596 77838Epoch: 2026-06-20T10:50Z
TLE epoch observation values (Epoch: 2026-06-20T10:50:20.691Z)
Latitude
0°
Longitude
178.90093°
Altitude
588.942 km
Speed
7.565 km/s
True Right ascension
16h 40m 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
07:23:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.343 km
Perigee altitude
580.488 km
Semi-major axis
6,960.052 km
Eccentricity
0.00021
Inclination
97.7083°
RAAN
250.1532°
Arg. of periapsis
134.2221°
True anomaly
225.89992°
Mean anomaly
225.9168°
Eccentric anomaly
225.90836°
Mean motion
3.73787 °/min
Orbital period
96.31 mins
BSTAR
0.000064597
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 04:39:11.603Z | 130.775° SE | 2026-06-21 04:42:11.603Z | 78.042° E | 27.57° | 2026-06-21 04:45:11.603Z | 15.167° NNE |
| 4 mins | 2026-06-21 06:16:11.603Z | 235.517° WSW | 2026-06-21 06:18:11.603Z | 272.12° WNW | 17.999° | 2026-06-21 06:20:11.603Z | 305.032° NW |
| 6 mins | 2026-06-21 17:57:11.603Z | 22.449° NNE | 2026-06-21 18:00:11.603Z | 111.708° ESE | 41.844° | 2026-06-21 18:03:11.603Z | 180.406° SSW |
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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