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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 CONNECTA IOT-12
1 64553U 25135AB 26083.06963532 .00004990 00000-0 22595-3 0 9990
2 64553 97.4632 199.3150 0001410 59.4741 300.6634 15.21332956 41936Epoch: 2026-03-24T01:40Z
TLE epoch observation values (Epoch: 2026-03-24T01:40:16.491Z)
Latitude
-0.00001°
Longitude
-7.30629°
Altitude
504.415 km
Speed
7.612 km/s
True Right ascension
13h 17m 15s
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
00:43:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.755 km
Perigee altitude
497.816 km
Semi-major axis
6,876.922 km
Eccentricity
0.00014
Inclination
97.4632°
RAAN
199.315°
Arg. of periapsis
59.4741°
True anomaly
300.6495°
Mean anomaly
300.6634°
Eccentric anomaly
300.65645°
Mean motion
3.80585 °/min
Orbital period
94.59 mins
BSTAR
0.00022595
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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 | 2026-03-24 19:37:28.541Z | 61.401° ENE | 2026-03-24 19:39:28.541Z | 98.178° ESE | 15.406° | 2026-03-24 19:41:28.541Z | 132.032° SE |
| 4 mins | 2026-03-24 21:11:28.541Z | 330.238° NNW | 2026-03-24 21:13:28.541Z | 275.245° WNW | 25.358° | 2026-03-24 21:15:28.541Z | 234.703° WSW |
| 5 mins | 2026-03-25 07:48:28.541Z | 173.575° S | 2026-03-25 07:50:28.541Z | 286.184° WNW | 44.426° | 2026-03-25 07:53:28.541Z | 345.068° 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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