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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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, 2.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CONNECTA IOT-2
1 60522U 24149BG 25312.16496877 .00009123 00000-0 39132-3 0 9992
2 60522 97.4052 28.7277 0007581 35.3127 324.8611 15.22931261 68257Epoch: 2025-11-08T03:57Z
TLE epoch observation values (Epoch: 2025-11-08T03:57:33.301Z)
Latitude
0.00001°
Longitude
-78.25956°
Altitude
495.837 km
Speed
7.619 km/s
True Right ascension
01h 54m 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
06:22:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.176 km
Perigee altitude
488.757 km
Semi-major axis
6,872.103 km
Eccentricity
0.00076
Inclination
97.4052°
RAAN
28.7277°
Arg. of periapsis
35.3127°
True anomaly
324.81106°
Mean anomaly
324.8611°
Eccentric anomaly
324.83608°
Mean motion
3.80986 °/min
Orbital period
94.49 mins
BSTAR
0.00039132
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-08 17:09:38.486Z | 59.962° ENE | 2025-11-08 17:11:38.486Z | 95.646° ESE | 14.973° | 2025-11-08 17:13:38.486Z | 129.88° SE |
| 4 mins | 2025-11-08 18:43:38.486Z | 331.413° NNW | 2025-11-08 18:45:38.486Z | 275.68° WNW | 25.899° | 2025-11-08 18:47:38.486Z | 234.05° WSW |
| 5 mins | 2025-11-09 05:19:38.486Z | 169.719° S | 2025-11-09 05:21:38.486Z | 186.016° SSW | 43.99° | 2025-11-09 05:24:38.486Z | 346.399° N |
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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