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: 18 hours ago
TLE from 18 hours ago
0 CONNECTA IOT-2
1 60522U 24149BG 25338.64812181 .00012266 00000-0 53031-3 0 9999
2 60522 97.4040 54.8247 0005435 293.2485 66.8179 15.22591669 72283Epoch: 2025-12-04T15:33Z
TLE epoch observation values (Epoch: 2025-12-04T15:33:17.724Z)
Latitude
-0.00002°
Longitude
107.7993°
Altitude
499.651 km
Speed
7.615 km/s
True Right ascension
03h 39m 17s
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
07:17:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.725 km
Perigee altitude
491.253 km
Semi-major axis
6,873.126 km
Eccentricity
0.00054
Inclination
97.404°
RAAN
54.8247°
Arg. of periapsis
293.2485°
True anomaly
66.87517°
Mean anomaly
66.8179°
Eccentric anomaly
66.84653°
Mean motion
3.80901 °/min
Orbital period
94.51 mins
BSTAR
0.00053031
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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 | 2025-12-05 17:22:27.330Z | 52.325° ENE | 2025-12-05 17:24:27.330Z | 93.524° ESE | 20.747° | 2025-12-05 17:26:27.330Z | 136.296° SSE |
| 4 mins | 2025-12-05 18:56:27.330Z | 325.806° NNW | 2025-12-05 18:58:27.330Z | 282.113° WNW | 19.666° | 2025-12-05 19:00:27.330Z | 245.246° WSW |
| 6 mins | 2025-12-06 05:32:27.330Z | 185.795° SSW | 2025-12-06 05:34:27.330Z | 225.744° WSW | 37.457° | 2025-12-06 05:38:27.330Z | 338.78° 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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