CONNECTA IOT-8, 62695
Orbit data source: Space-Track
CONNECTA IOT-8, 62695 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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62695 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: 10 hours ago
TLE from 10 hours ago
0 CONNECTA IOT-8
1 62695U 25009CQ 25335.16402888 .00001646 00000-0 16718-3 0 9992
2 62695 97.7273 51.9102 0001665 329.4635 30.6487 14.92170648 47756Epoch: 2025-12-01T03:56Z
TLE epoch observation values (Epoch: 2025-12-01T03:56:12.095Z)
Latitude
0°
Longitude
-77.40766°
Altitude
593.213 km
Speed
7.564 km/s
True Right ascension
03h 27m 38s
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
11:44:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.345 km
Perigee altitude
587.026 km
Semi-major axis
6,966.323 km
Eccentricity
0.00017
Inclination
97.7273°
RAAN
51.9102°
Arg. of periapsis
329.4635°
True anomaly
30.65843°
Mean anomaly
30.6487°
Eccentric anomaly
30.65356°
Mean motion
3.73283 °/min
Orbital period
96.44 mins
BSTAR
0.00016718
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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-8 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 | 2025-12-01 17:23:41.129Z | 44.628° NE | 2025-12-01 17:26:41.129Z | 99.597° ESE | 23.145° | 2025-12-01 17:29:41.129Z | 149.777° SSE |
| 5 mins | 2025-12-01 18:59:41.129Z | 334.385° NNW | 2025-12-01 19:01:41.129Z | 297.551° NW | 22.471° | 2025-12-01 19:04:41.129Z | 242.361° WSW |
| 5 mins | 2025-12-02 05:49:41.129Z | 208.846° SW | 2025-12-02 05:51:41.129Z | 260.809° W | 31.657° | 2025-12-02 05:54:41.129Z | 325.044° NNW |
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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