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: 11 hours ago
TLE from 11 hours ago
0 CONNECTA IOT-7
1 62715U 25009DL 26080.50409731 .00001456 00000-0 14187-3 0 9992
2 62715 97.7114 160.8783 0002768 110.0601 250.0917 14.93992523 64255Epoch: 2026-03-21T12:05Z
TLE epoch observation values (Epoch: 2026-03-21T12:05:54.007Z)
Latitude
-0.00005°
Longitude
160.37941°
Altitude
589.205 km
Speed
7.565 km/s
True Right ascension
10h 43m 30s
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
03:53:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.442 km
Perigee altitude
580.589 km
Semi-major axis
6,960.652 km
Eccentricity
0.00028
Inclination
97.7114°
RAAN
160.8783°
Arg. of periapsis
110.0601°
True anomaly
250.06188°
Mean anomaly
250.0917°
Eccentric anomaly
250.07679°
Mean motion
3.73739 °/min
Orbital period
96.32 mins
BSTAR
0.00014187
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-22 04:20:11.578Z | 100.11° ESE | 2026-03-22 04:22:11.578Z | 64.959° ENE | 17.843° | 2026-03-22 04:24:11.578Z | 31.27° NE |
| 5 mins | 2026-03-22 05:55:11.578Z | 212.988° SW | 2026-03-22 05:57:11.578Z | 260.469° W | 28.812° | 2026-03-22 06:00:11.578Z | 322.049° NNW |
| 6 mins | 2026-03-22 17:37:11.578Z | 42.633° NE | 2026-03-22 17:39:11.578Z | 84.18° E | 28.904° | 2026-03-22 17:43:11.578Z | 162.763° S |
| 4 mins | 2026-03-22 19:13:11.578Z | 320.942° NNW | 2026-03-22 19:15:11.578Z | 284.866° WNW | 17.192° | 2026-03-22 19:17:11.578Z | 253.676° W |
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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