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: 9 hours ago
TLE from 9 hours ago
0 CONNECTA IOT-8
1 62695U 25009CQ 26038.15193734 .00001812 00000-0 18149-3 0 9994
2 62695 97.7184 118.5855 0003885 82.1927 277.9733 14.92609387 57898Epoch: 2026-02-07T03:38Z
TLE epoch observation values (Epoch: 2026-02-07T03:38:47.386Z)
Latitude
-0.00003°
Longitude
-73.39151°
Altitude
592.472 km
Speed
7.564 km/s
True Right ascension
07h 54m 20s
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
14:23:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.525 km
Perigee altitude
584.113 km
Semi-major axis
6,964.956 km
Eccentricity
0.00039
Inclination
97.7184°
RAAN
118.5855°
Arg. of periapsis
82.1927°
True anomaly
277.92921°
Mean anomaly
277.9733°
Eccentric anomaly
277.95125°
Mean motion
3.73393 °/min
Orbital period
96.41 mins
BSTAR
0.00018149
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-07 17:06:59.104Z | 61.433° ENE | 2026-02-07 17:08:59.104Z | 94.368° ESE | 16.136° | 2026-02-07 17:10:59.104Z | 126.611° SE |
| 6 mins | 2026-02-07 18:41:59.104Z | 345.659° N | 2026-02-07 18:44:59.104Z | 273.038° WNW | 29.968° | 2026-02-07 18:47:59.104Z | 223.616° SW |
| 7 mins | 2026-02-08 05:30:59.104Z | 182.201° SSW | 2026-02-08 05:33:59.104Z | 259.525° W | 41.019° | 2026-02-08 05:37:59.104Z | 340.038° N |
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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