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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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: 10 hours ago
TLE from 10 hours ago
0 CONNECTA IOT-8
1 62695U 25009CQ 26171.45539862 .00000480 00000-0 51283-4 0 9998
2 62695 97.7078 249.2431 0002832 22.3988 337.7355 14.93205596 77786Epoch: 2026-06-20T10:55Z
TLE epoch observation values (Epoch: 2026-06-20T10:55:46.440Z)
Latitude
-0.00003°
Longitude
176.62983°
Altitude
589.167 km
Speed
7.567 km/s
True Right ascension
16h 36m 58s
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
07:21:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.935 km
Perigee altitude
582.991 km
Semi-major axis
6,963.1 km
Eccentricity
0.00028
Inclination
97.7078°
RAAN
249.2431°
Arg. of periapsis
22.3988°
True anomaly
337.7232°
Mean anomaly
337.7355°
Eccentric anomaly
337.72935°
Mean motion
3.73542 °/min
Orbital period
96.37 mins
BSTAR
0.000051283
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 04:44:54.602Z | 140.385° SSE | 2026-06-21 04:47:54.602Z | 91.535° ESE | 32.171° | 2026-06-21 04:51:54.602Z | 4.562° NNE |
| 6 mins | 2026-06-21 18:03:54.602Z | 14.31° NNE | 2026-06-21 18:06:54.602Z | 173.049° S | 44.199° | 2026-06-21 18:09:54.602Z | 191.32° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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