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: 7 hours ago
TLE from 7 hours ago
0 CONNECTA IOT-2
1 60522U 24149BG 26126.15243178 .00004946 00000-0 20933-3 0 9996
2 60522 97.3838 204.9462 0008126 109.7516 250.4598 15.23618179 95491Epoch: 2026-05-06T03:39Z
TLE epoch observation values (Epoch: 2026-05-06T03:39:30.105Z)
Latitude
-0.00006°
Longitude
-73.94625°
Altitude
499.906 km
Speed
7.613 km/s
True Right ascension
13h 39m 47s
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
18:23:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.481 km
Perigee altitude
486.315 km
Semi-major axis
6,870.035 km
Eccentricity
0.00081
Inclination
97.3838°
RAAN
204.9462°
Arg. of periapsis
109.7516°
True anomaly
250.37208°
Mean anomaly
250.4598°
Eccentric anomaly
250.41593°
Mean motion
3.81158 °/min
Orbital period
94.45 mins
BSTAR
0.00020933
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-06 18:23:57.591Z | 359.17° N | 2026-05-06 18:26:57.591Z | 291.875° WNW | 37.228° | 2026-05-06 18:29:57.591Z | 212.463° SW |
| 5 mins | 2026-05-07 05:00:57.591Z | 147.102° SSE | 2026-05-07 05:02:57.591Z | 104.697° ESE | 37.141° | 2026-05-07 05:05:57.591Z | 2.241° NNE |
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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