CONNECTA IOT-9, 64534
Orbit data source: Space-Track
CONNECTA IOT-9, 64534 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Mon, 23 Jun 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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64534 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: 1 day ago
TLE from 1 day ago
0 CONNECTA IOT-9
1 64534U 25135G 26283.62594019 .00007242 00000-0 32987-3 0 9992
2 64534 97.4864 37.5795 0006356 123.0446 237.1401 15.20960191 72368Epoch: 2026-10-10T15:01Z
TLE epoch observation values (Epoch: 2026-10-10T15:01:21.232Z)
Latitude
0.00001°
Longitude
153.01066°
Altitude
508.408 km
Speed
7.608 km/s
True Right ascension
02h 30m 19s
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
19:11:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.283 km
Perigee altitude
495.539 km
Semi-major axis
6,878.048 km
Eccentricity
0.00064
Inclination
97.4864°
RAAN
37.5795°
Arg. of periapsis
123.0446°
True anomaly
237.07895°
Mean anomaly
237.1401°
Eccentric anomaly
237.10952°
Mean motion
3.80492 °/min
Orbital period
94.61 mins
BSTAR
0.00032987
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-9 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-12 08:12:22.764Z | 198.781° SSW | 2026-10-12 08:14:22.764Z | 242.349° WSW | 37.266° | 2026-10-12 08:17:22.764Z | 325.283° NNW |
| 4 mins | 2026-10-12 21:17:22.764Z | 320.851° NNW | 2026-10-12 21:18:22.764Z | 294.76° NW | 26.657° | 2026-10-12 21:21:22.764Z | 233.347° WSW |
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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