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: 7 hours ago
TLE from 7 hours ago
0 CONNECTA IOT-7
1 62715U 25009DL 26125.71132772 .00001240 00000-0 12131-3 0 9991
2 62715 97.7081 205.2547 0001494 41.6327 318.5006 14.94099101 71000Epoch: 2026-05-05T17:04Z
TLE epoch observation values (Epoch: 2026-05-05T17:04:18.715Z)
Latitude
-0.00006°
Longitude
85.59448°
Altitude
587.438 km
Speed
7.567 km/s
True Right ascension
13h 41m 01s
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
08:06:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.224 km
Perigee altitude
581.144 km
Semi-major axis
6,960.321 km
Eccentricity
0.00015
Inclination
97.7081°
RAAN
205.2547°
Arg. of periapsis
41.6327°
True anomaly
318.48925°
Mean anomaly
318.5006°
Eccentric anomaly
318.49493°
Mean motion
3.73766 °/min
Orbital period
96.32 mins
BSTAR
0.00012131
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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 | 2026-05-06 04:27:49.934Z | 120.279° SE | 2026-05-06 04:30:49.934Z | 70.773° E | 21.744° | 2026-05-06 04:33:49.934Z | 19.064° NNE |
| 5 mins | 2026-05-06 06:03:49.934Z | 217.236° SW | 2026-05-06 06:05:49.934Z | 254.473° W | 23.374° | 2026-05-06 06:08:49.934Z | 313.744° NW |
| 6 mins | 2026-05-06 17:45:49.934Z | 33.312° NE | 2026-05-06 17:48:49.934Z | 113.878° SE | 34.667° | 2026-05-06 17:51:49.934Z | 169.388° S |
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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