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 26259.28136354 .00007328 00000-0 33656-3 0 9990
2 64534 97.4835 13.4012 0004583 199.5456 160.5604 15.20679867 68669Epoch: 2026-09-16T06:45Z
TLE epoch observation values (Epoch: 2026-09-16T06:45:09.809Z)
Latitude
-0.00007°
Longitude
-83.12487°
Altitude
509.853 km
Speed
7.607 km/s
True Right ascension
00h 53m 36s
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
03:01:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.91 km
Perigee altitude
497.604 km
Semi-major axis
6,878.894 km
Eccentricity
0.00046
Inclination
97.4835°
RAAN
13.4012°
Arg. of periapsis
199.5456°
True anomaly
160.57787°
Mean anomaly
160.5604°
Eccentric anomaly
160.56914°
Mean motion
3.80422 °/min
Orbital period
94.63 mins
BSTAR
0.00033656
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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 | 2026-09-17 19:39:19.297Z | 53.123° ENE | 2026-09-17 19:41:19.297Z | 86.248° E | 16.388° | 2026-09-17 19:43:19.297Z | 124.108° SE |
| 5 mins | 2026-09-17 21:13:19.297Z | 339.15° N | 2026-09-17 21:15:19.297Z | 295.103° NW | 28.471° | 2026-09-17 21:18:19.297Z | 231.582° WSW |
| 5 mins | 2026-09-18 07:51:19.297Z | 175.955° S | 2026-09-18 07:53:19.297Z | 305.672° NW | 71.872° | 2026-09-18 07:56:19.297Z | 344.536° 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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