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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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 CONNECTA IOT-12
1 64553U 25135AB 25268.83884307 .00006614 00000-0 32126-3 0 9997
2 64553 97.4568 22.0105 0000827 149.1305 210.9978 15.18782980 14701Epoch: 2025-09-25T20:07Z
TLE epoch observation values (Epoch: 2025-09-25T20:07:56.041Z)
Latitude
-0.00002°
Longitude
75.13278°
Altitude
513.093 km
Speed
7.607 km/s
True Right ascension
01h 28m 02s
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
15:11:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.057 km
Perigee altitude
505.918 km
Semi-major axis
6,884.624 km
Eccentricity
0.00008
Inclination
97.4568°
RAAN
22.0105°
Arg. of periapsis
149.1305°
True anomaly
210.99292°
Mean anomaly
210.9978°
Eccentric anomaly
210.99536°
Mean motion
3.79947 °/min
Orbital period
94.75 mins
BSTAR
0.00032126
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-27 07:03:31.017Z | 127.415° SE | 2025-09-27 07:06:31.017Z | 62.717° ENE | 25.282° | 2025-09-27 07:08:31.017Z | 20.195° NNE |
| 5 mins | 2025-09-27 20:09:31.017Z | 44.383° NE | 2025-09-27 20:11:31.017Z | 119.195° SE | 33.342° | 2025-09-27 20:14:31.017Z | 171.307° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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