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: 12 hours ago
TLE from 12 hours ago
0 CONNECTA IOT-7
1 62715U 25009DL 25335.18142256 .00001835 00000-0 17913-3 0 9995
2 62715 97.7272 52.4859 0002620 111.7932 248.3567 14.93617316 47786Epoch: 2025-12-01T04:21Z
TLE epoch observation values (Epoch: 2025-12-01T04:21:14.909Z)
Latitude
0.00001°
Longitude
-83.11083°
Altitude
590.387 km
Speed
7.564 km/s
True Right ascension
03h 29m 56s
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
13:50:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.507 km
Perigee altitude
581.859 km
Semi-major axis
6,961.82 km
Eccentricity
0.00026
Inclination
97.7272°
RAAN
52.4859°
Arg. of periapsis
111.7932°
True anomaly
248.3288°
Mean anomaly
248.3567°
Eccentric anomaly
248.34275°
Mean motion
3.73645 °/min
Orbital period
96.35 mins
BSTAR
0.00017913
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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 | 2025-12-01 17:46:57.090Z | 26.822° NE | 2025-12-01 17:50:57.090Z | 113.742° SE | 34.628° | 2025-12-01 17:53:57.090Z | 169.338° S |
| 5 mins | 2025-12-02 04:37:57.090Z | 109.365° ESE | 2025-12-02 04:39:57.090Z | 63.614° ENE | 24.82° | 2025-12-02 04:42:57.090Z | 13.507° NNE |
| 5 mins | 2025-12-02 06:12:57.090Z | 224.98° SW | 2025-12-02 06:14:57.090Z | 261.206° W | 20.467° | 2025-12-02 06:17:57.090Z | 312.944° 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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