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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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, 0.1 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 25312.56606181 .00007093 00000-0 35118-3 0 9994
2 64534 97.4626 64.9243 0004509 199.1643 160.9422 15.18082326 21325Epoch: 2025-11-08T13:35Z
TLE epoch observation values (Epoch: 2025-11-08T13:35:07.740Z)
Latitude
-0.00002°
Longitude
173.14821°
Altitude
517.66 km
Speed
7.603 km/s
True Right ascension
04h 19m 41s
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
18:13:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.713 km
Perigee altitude
505.502 km
Semi-major axis
6,886.745 km
Eccentricity
0.00045
Inclination
97.4626°
RAAN
64.9243°
Arg. of periapsis
199.1643°
True anomaly
160.95906°
Mean anomaly
160.9422°
Eccentric anomaly
160.95063°
Mean motion
3.79771 °/min
Orbital period
94.79 mins
BSTAR
0.00035118
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-10 06:52:20.249Z | 108.646° ESE | 2025-11-10 06:54:20.249Z | 67.69° E | 20.088° | 2025-11-10 06:56:20.249Z | 28.24° NE |
| 4 mins | 2025-11-10 08:26:20.249Z | 225.754° WSW | 2025-11-10 08:28:20.249Z | 270.151° WNW | 21.277° | 2025-11-10 08:30:20.249Z | 309.707° NW |
| 5 mins | 2025-11-10 19:57:20.249Z | 46.397° ENE | 2025-11-10 19:59:20.249Z | 95.921° ESE | 27.279° | 2025-11-10 20:02:20.249Z | 158.283° S |
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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