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
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: 12 hours ago
TLE from 12 hours ago
0 CONNECTA IOT-9
1 64534U 25135G 26062.26090477 .00005651 00000-0 26688-3 0 9999
2 64534 97.4633 178.1966 0005839 165.3888 194.7517 15.19810933 38733Epoch: 2026-03-03T06:15Z
TLE epoch observation values (Epoch: 2026-03-03T06:15:42.172Z)
Latitude
0.00003°
Longitude
-76.77163°
Altitude
513.388 km
Speed
7.605 km/s
True Right ascension
11h 52m 47s
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
21:49:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.398 km
Perigee altitude
499.362 km
Semi-major axis
6,881.517 km
Eccentricity
0.00058
Inclination
97.4633°
RAAN
178.1966°
Arg. of periapsis
165.3888°
True anomaly
194.73467°
Mean anomaly
194.7517°
Eccentric anomaly
194.74319°
Mean motion
3.80204 °/min
Orbital period
94.69 mins
BSTAR
0.00026688
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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 | 2026-03-03 21:03:25.608Z | 338.934° N | 2026-03-03 21:05:25.608Z | 283.893° WNW | 29.033° | 2026-03-03 21:08:25.608Z | 223.729° SW |
| 5 mins | 2026-03-04 07:41:25.608Z | 165.881° S | 2026-03-04 07:43:25.608Z | 359.047° N | 44.618° | 2026-03-04 07:46:25.608Z | 348.516° N |
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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