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: 16 hours ago
TLE from 16 hours ago
0 CONNECTA IOT-7
1 62715U 25009DL 26035.15924160 .00001675 00000-0 16296-3 0 9997
2 62715 97.7186 116.3459 0000083 55.7084 304.4143 14.93860933 57489Epoch: 2026-02-04T03:49Z
TLE epoch observation values (Epoch: 2026-02-04T03:49:18.474Z)
Latitude
-0.0001°
Longitude
-75.31089°
Altitude
588.924 km
Speed
7.566 km/s
True Right ascension
07h 45m 23s
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
21:41:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.983 km
Perigee altitude
582.867 km
Semi-major axis
6,961.062 km
Eccentricity
0.00001
Inclination
97.7186°
RAAN
116.3459°
Arg. of periapsis
55.7084°
True anomaly
304.41352°
Mean anomaly
304.4143°
Eccentric anomaly
304.41391°
Mean motion
3.73706 °/min
Orbital period
96.33 mins
BSTAR
0.00016296
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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 | 2026-02-05 05:40:45.901Z | 193.36° SSW | 2026-02-05 05:42:45.901Z | 240.145° WSW | 36.758° | 2026-02-05 05:46:45.901Z | 335.18° NNW |
| 5 mins | 2026-02-05 17:23:45.901Z | 59.382° ENE | 2026-02-05 17:25:45.901Z | 100.613° ESE | 21.745° | 2026-02-05 17:28:45.901Z | 148.632° SSE |
| 5 mins | 2026-02-05 18:58:45.901Z | 333.605° NNW | 2026-02-05 19:00:45.901Z | 293.932° NW | 23.541° | 2026-02-05 19:03:45.901Z | 239.003° WSW |
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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