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: 1 day ago
TLE from 1 day ago
0 CONNECTA IOT-7
1 62715U 25009DL 26215.91695323 .00000737 00000-0 73918-4 0 9990
2 62715 97.7063 293.7988 0002552 66.6032 293.5456 14.94264311 84470Epoch: 2026-08-03T22:00Z
TLE epoch observation values (Epoch: 2026-08-03T22:00:24.759Z)
Latitude
-0.00004°
Longitude
11.20245°
Altitude
586.994 km
Speed
7.567 km/s
True Right ascension
19h 35m 11s
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
20:58:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.447 km
Perigee altitude
579.894 km
Semi-major axis
6,959.807 km
Eccentricity
0.00026
Inclination
97.7063°
RAAN
293.7988°
Arg. of periapsis
66.6032°
True anomaly
293.51879°
Mean anomaly
293.5456°
Eccentric anomaly
293.53219°
Mean motion
3.73807 °/min
Orbital period
96.31 mins
BSTAR
0.000073918
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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 | 2026-08-05 17:58:18.927Z | 19.949° NNE | 2026-08-05 18:01:18.927Z | 87.527° E | 42.731° | 2026-08-05 18:05:18.927Z | 184.531° SSW |
| 5 mins | 2026-08-06 04:48:18.927Z | 123.52° SE | 2026-08-06 04:50:18.927Z | 65.57° ENE | 32.258° | 2026-08-06 04:53:18.927Z | 7.265° 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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