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: 19 hours ago
TLE from 19 hours ago
0 CONNECTA IOT-2
1 60522U 24149BG 26235.47033236 .00003672 00000-0 15232-3 0 9995
2 60522 97.3802 312.6037 0008157 89.8591 270.3581 15.24462407112149Epoch: 2026-08-23T11:17Z
TLE epoch observation values (Epoch: 2026-08-23T11:17:16.715Z)
Latitude
-0.00008°
Longitude
171.51814°
Altitude
495.467 km
Speed
7.617 km/s
True Right ascension
20h 50m 24s
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
21:35:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.961 km
Perigee altitude
483.757 km
Semi-major axis
6,867.496 km
Eccentricity
0.00082
Inclination
97.3802°
RAAN
312.6037°
Arg. of periapsis
89.8591°
True anomaly
270.26463°
Mean anomaly
270.3581°
Eccentric anomaly
270.31136°
Mean motion
3.81369 °/min
Orbital period
94.4 mins
BSTAR
0.00015232
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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 | 2026-08-24 17:47:08.778Z | 27.192° NE | 2026-08-24 17:50:08.778Z | 112.468° ESE | 36.386° | 2026-08-24 17:53:08.778Z | 174.136° S |
| 4 mins | 2026-08-25 04:24:08.778Z | 106.555° ESE | 2026-08-25 04:26:08.778Z | 67.985° E | 17.422° | 2026-08-25 04:28:08.778Z | 30.142° NE |
| 4 mins | 2026-08-25 05:58:08.778Z | 229.153° WSW | 2026-08-25 05:59:08.778Z | 253.116° W | 22.387° | 2026-08-25 06:02:08.778Z | 317.092° NNW |
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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