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: 21 hours ago
TLE from 21 hours ago
0 CONNECTA IOT-7
1 62715U 25009DL 26067.77847435 .00001835 00000-0 17762-3 0 9996
2 62715 97.7132 148.3836 0002264 129.2445 230.8977 14.93959791 62355Epoch: 2026-03-08T18:41Z
TLE epoch observation values (Epoch: 2026-03-08T18:41:00.183Z)
Latitude
0.00003°
Longitude
61.65195°
Altitude
589.644 km
Speed
7.565 km/s
True Right ascension
09h 53m 32s
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
19:48:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.193 km
Perigee altitude
581.041 km
Semi-major axis
6,960.754 km
Eccentricity
0.00023
Inclination
97.7132°
RAAN
148.3836°
Arg. of periapsis
129.2445°
True anomaly
230.87757°
Mean anomaly
230.8977°
Eccentric anomaly
230.88764°
Mean motion
3.73731 °/min
Orbital period
96.33 mins
BSTAR
0.00017762
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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 | 2026-03-09 17:45:31.050Z | 28.722° NE | 2026-03-09 17:48:31.050Z | 82.523° E | 34.17° | 2026-03-09 17:52:31.050Z | 170.56° S |
| 5 mins | 2026-03-10 04:35:31.050Z | 116.615° SE | 2026-03-10 04:37:31.050Z | 78.081° E | 24.359° | 2026-03-10 04:40:31.050Z | 18.95° NNE |
| 4 mins | 2026-03-10 06:11:31.050Z | 231.365° WSW | 2026-03-10 06:13:31.050Z | 271.618° WNW | 20.695° | 2026-03-10 06:15:31.050Z | 307.185° NW |
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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