CONNECTA IOT-12, 64553
Orbit data source: Space-Track
CONNECTA IOT-12, 64553 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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64553 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: 13 hours ago
TLE from 13 hours ago
0 CONNECTA IOT-12
1 64553U 25135AB 26133.07191883 .00002305 00000-0 10802-3 0 9995
2 64553 97.4702 248.8739 0002264 122.4573 237.6881 15.20705168 49534Epoch: 2026-05-13T01:43Z
TLE epoch observation values (Epoch: 2026-05-13T01:43:33.786Z)
Latitude
-0.0001°
Longitude
-7.85406°
Altitude
507.635 km
Speed
7.61 km/s
True Right ascension
16h 35m 29s
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
22:52:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.237 km
Perigee altitude
499.123 km
Semi-major axis
6,878.817 km
Eccentricity
0.00023
Inclination
97.4702°
RAAN
248.8739°
Arg. of periapsis
122.4573°
True anomaly
237.66618°
Mean anomaly
237.6881°
Eccentric anomaly
237.67714°
Mean motion
3.80428 °/min
Orbital period
94.63 mins
BSTAR
0.00010802
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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-12 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 | 2026-05-13 19:40:35.472Z | 52.27° ENE | 2026-05-13 19:42:35.472Z | 85.978° E | 16.335° | 2026-05-13 19:44:35.472Z | 124.991° SE |
| 4 mins | 2026-05-13 21:15:35.472Z | 321.204° NNW | 2026-05-13 21:16:35.472Z | 294.899° NW | 24.384° | 2026-05-13 21:19:35.472Z | 232.967° WSW |
| 5 mins | 2026-05-14 07:52:35.472Z | 178.907° S | 2026-05-14 07:54:35.472Z | 289.909° WNW | 43.212° | 2026-05-14 07:57:35.472Z | 343.113° 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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