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: 7 hours ago
TLE from 7 hours ago
0 CONNECTA IOT-9
1 64534U 25135G 26120.13012969 .00003757 00000-0 17699-3 0 9997
2 64534 97.4702 235.4620 0004845 355.8302 4.2891 15.20119808 47529Epoch: 2026-04-30T03:07Z
TLE epoch observation values (Epoch: 2026-04-30T03:07:23.205Z)
Latitude
-0.00009°
Longitude
-29.46583°
Altitude
505.241 km
Speed
7.613 km/s
True Right ascension
15h 41m 50s
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
17:28:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.781 km
Perigee altitude
499.114 km
Semi-major axis
6,880.584 km
Eccentricity
0.00048
Inclination
97.4702°
RAAN
235.462°
Arg. of periapsis
355.8302°
True anomaly
4.29325°
Mean anomaly
4.2891°
Eccentric anomaly
4.29118°
Mean motion
3.80281 °/min
Orbital period
94.67 mins
BSTAR
0.00017699
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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 | 2026-04-30 21:04:09.490Z | 343.274° N | 2026-04-30 21:06:09.490Z | 296.578° NW | 28.934° | 2026-04-30 21:09:09.490Z | 226.614° WSW |
| 5 mins | 2026-05-01 07:42:09.490Z | 166.029° S | 2026-05-01 07:44:09.490Z | 112.422° ESE | 44.978° | 2026-05-01 07:47:09.490Z | 348.486° 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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