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: 8 hours ago
TLE from 8 hours ago
0 CONNECTA IOT-8
1 62695U 25009CQ 26262.45206308 .00001138 00000-0 11368-3 0 9995
2 62695 97.7010 338.4020 0003902 62.9573 297.2045 14.93395170 91360Epoch: 2026-09-19T10:50Z
TLE epoch observation values (Epoch: 2026-09-19T10:50:58.250Z)
Latitude
0.00003°
Longitude
177.29889°
Altitude
589.162 km
Speed
7.566 km/s
True Right ascension
22h 33m 36s
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
11:24:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.089 km
Perigee altitude
581.656 km
Semi-major axis
6,962.51 km
Eccentricity
0.00039
Inclination
97.701°
RAAN
338.402°
Arg. of periapsis
62.9573°
True anomaly
297.16472°
Mean anomaly
297.2045°
Eccentric anomaly
297.18461°
Mean motion
3.73589 °/min
Orbital period
96.36 mins
BSTAR
0.00011368
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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 | 2026-09-20 04:41:08.794Z | 128.339° SE | 2026-09-20 04:43:08.794Z | 84.107° E | 37.162° | 2026-09-20 04:47:08.794Z | 5.168° NNE |
| 6 mins | 2026-09-20 17:59:08.794Z | 17.288° NNE | 2026-09-20 18:01:08.794Z | 39.169° NE | 67.469° | 2026-09-20 18:05:08.794Z | 188.8° SSW |
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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