CONNECTA IOT-2, 60522
Orbit data source: Space-Track
CONNECTA IOT-2, 60522 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Fri, 16 Aug 2024 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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60522 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: 2 days ago
TLE from 2 days ago
0 CONNECTA IOT-2
1 60522U 24149BG 26303.18976688 .00005588 00000-0 22392-3 0 9999
2 60522 97.3731 19.3138 0005961 195.7460 164.3594 15.25418282122460Epoch: 2026-10-30T04:33Z
TLE epoch observation values (Epoch: 2026-10-30T04:33:15.858Z)
Latitude
0.00001°
Longitude
-87.51568°
Altitude
496.572 km
Speed
7.614 km/s
True Right ascension
01h 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
03:28:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.579 km
Perigee altitude
482.395 km
Semi-major axis
6,864.624 km
Eccentricity
0.0006
Inclination
97.3731°
RAAN
19.3138°
Arg. of periapsis
195.746°
True anomaly
164.3778°
Mean anomaly
164.3594°
Eccentric anomaly
164.3686°
Mean motion
3.81609 °/min
Orbital period
94.34 mins
BSTAR
0.00022392
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-2 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 | 2026-11-01 18:31:18.453Z | 347.668° N | 2026-11-01 18:33:18.453Z | 297.781° NW | 39.008° | 2026-11-01 18:36:18.453Z | 220.6° SW |
| 5 mins | 2026-11-02 05:07:18.453Z | 150.445° SSE | 2026-11-02 05:09:18.453Z | 50.357° ENE | 63.304° | 2026-11-02 05:12:18.453Z | 354.956° 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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