CONNECTA IOT-14, 67401
Orbit data source: Space-Track
CONNECTA IOT-14, 67401 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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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-14
1 67401U 26004AQ 26205.96169973 .00003193 00000-0 15695-3 0 9990
2 67401 97.4525 204.4566 0008947 197.6911 162.4013 15.18733804 29492Epoch: 2026-07-24T23:04Z
TLE epoch observation values (Epoch: 2026-07-24T23:04:50.856Z)
Latitude
-0.00004°
Longitude
-84.43611°
Altitude
518.629 km
Speed
7.601 km/s
True Right ascension
13h 37m 49s
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
10:25:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.796 km
Perigee altitude
500.476 km
Semi-major axis
6,884.773 km
Eccentricity
0.00089
Inclination
97.4525°
RAAN
204.4566°
Arg. of periapsis
197.6911°
True anomaly
162.43227°
Mean anomaly
162.4013°
Eccentric anomaly
162.41679°
Mean motion
3.79935 °/min
Orbital period
94.75 mins
BSTAR
0.00015695
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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-14 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-26 00:31:20.589Z | 211.269° SW | 2026-07-26 00:33:20.589Z | 267.432° W | 29.376° | 2026-07-26 00:36:20.589Z | 327.111° NNW |
| 4 mins | 2026-07-26 13:36:20.589Z | 327.547° NNW | 2026-07-26 13:38:20.589Z | 282.043° WNW | 21.19° | 2026-07-26 13:40:20.589Z | 243.551° WSW |
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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