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: 10 hours ago
TLE from 10 hours ago
0 CONNECTA IOT-12
1 64553U 25135AB 26260.13164883 .00003373 00000-0 15488-3 0 9994
2 64553 97.4823 14.9187 0002108 74.3877 285.7591 15.21088619 68849Epoch: 2026-09-17T03:09Z
TLE epoch observation values (Epoch: 2026-09-17T03:09:34.458Z)
Latitude
-0.00006°
Longitude
-28.54815°
Altitude
505.252 km
Speed
7.612 km/s
True Right ascension
00h 59m 40s
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
06:19:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.973 km
Perigee altitude
498.074 km
Semi-major axis
6,877.66 km
Eccentricity
0.00021
Inclination
97.4823°
RAAN
14.9187°
Arg. of periapsis
74.3877°
True anomaly
285.73585°
Mean anomaly
285.7591°
Eccentric anomaly
285.74748°
Mean motion
3.80524 °/min
Orbital period
94.61 mins
BSTAR
0.00015488
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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 | 2026-09-17 21:06:10.507Z | 340.661° N | 2026-09-17 21:08:10.507Z | 278.584° WNW | 37.942° | 2026-09-17 21:11:10.507Z | 219.493° SW |
| 5 mins | 2026-09-18 07:43:10.507Z | 159.089° S | 2026-09-18 07:45:10.507Z | 104.15° ESE | 74.456° | 2026-09-18 07:48:10.507Z | 352.37° 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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