CONNECTA IOT-16, 67390
Orbit data source: Space-Track
CONNECTA IOT-16, 67390 is a payload satellite owned by Plan-S (TR) in SSO that was launched on Sun, 11 Jan 2026 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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67390 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: 22 hours ago
TLE from 22 hours ago
0 CONNECTA IOT-16
1 67390U 26004AD 26263.88355312 .00005257 00000-0 25740-3 0 9991
2 67390 97.4654 261.5292 0004475 38.3349 321.8202 15.18597037 38262Epoch: 2026-09-20T21:12Z
TLE epoch observation values (Epoch: 2026-09-20T21:12:18.989Z)
Latitude
-0.00008°
Longitude
-56.32125°
Altitude
510.743 km
Speed
7.61 km/s
True Right ascension
17h 26m 07s
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
12:35:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.131 km
Perigee altitude
503.969 km
Semi-major axis
6,885.187 km
Eccentricity
0.00045
Inclination
97.4654°
RAAN
261.5292°
Arg. of periapsis
38.3349°
True anomaly
321.78849°
Mean anomaly
321.8202°
Eccentric anomaly
321.80435°
Mean motion
3.799 °/min
Orbital period
94.76 mins
BSTAR
0.0002574
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Other satellites on launch #4 in the year 2026 (2026-01-11 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-16 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 | 2026-09-22 00:13:00.159Z | 182.344° SSW | 2026-09-22 00:16:00.159Z | 278.152° WNW | 57.604° | 2026-09-22 00:19:00.159Z | 338.682° N |
| 5 mins | 2026-09-22 13:19:00.159Z | 340.009° N | 2026-09-22 13:21:00.159Z | 280.405° WNW | 37.115° | 2026-09-22 13:24:00.159Z | 220.856° SW |
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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