CONNECTA IOT-10, 64555
Orbit data source: Space-Track
CONNECTA IOT-10, 64555 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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64555 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-10
1 64555U 25135AD 26178.29462235 .00003323 00000-0 15539-3 0 9995
2 64555 97.4694 293.2277 0000689 85.3328 274.7986 15.20463261 56396Epoch: 2026-06-27T07:04Z
TLE epoch observation values (Epoch: 2026-06-27T07:04:15.371Z)
Latitude
0.00002°
Longitude
-88.24719°
Altitude
507.492 km
Speed
7.61 km/s
True Right ascension
19h 32m 54s
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
07:44:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.884 km
Perigee altitude
500.936 km
Semi-major axis
6,879.547 km
Eccentricity
0.00007
Inclination
97.4694°
RAAN
293.2277°
Arg. of periapsis
85.3328°
True anomaly
274.79073°
Mean anomaly
274.7986°
Eccentric anomaly
274.79467°
Mean motion
3.80367 °/min
Orbital period
94.65 mins
BSTAR
0.00015539
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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-10 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 | 2026-06-28 06:54:56.565Z | 111.097° ESE | 2026-06-28 06:56:56.565Z | 72.556° E | 19.386° | 2026-06-28 06:58:56.565Z | 31.422° NE |
| 4 mins | 2026-06-28 08:28:56.565Z | 224.126° SW | 2026-06-28 08:30:56.565Z | 268.723° W | 21.398° | 2026-06-28 08:32:56.565Z | 309.477° NW |
| 5 mins | 2026-06-28 19:58:56.565Z | 47.944° ENE | 2026-06-28 20:00:56.565Z | 96.255° ESE | 25.91° | 2026-06-28 20:03:56.565Z | 156.721° SSE |
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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