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
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 CONNECTA IOT-14
1 67401U 26004AQ 26146.52557462 .00003072 00000-0 15258-3 0 9991
2 67401 97.4504 145.8724 0011313 61.3813 298.8558 15.18371151 20472Epoch: 2026-05-26T12:36Z
TLE epoch observation values (Epoch: 2026-05-26T12:36:49.647Z)
Latitude
0.00003°
Longitude
72.56778°
Altitude
510.095 km
Speed
7.611 km/s
True Right ascension
09h 43m 29s
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
07:57:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.523 km
Perigee altitude
499.943 km
Semi-major axis
6,885.87 km
Eccentricity
0.00113
Inclination
97.4504°
RAAN
145.8724°
Arg. of periapsis
61.3813°
True anomaly
298.74218°
Mean anomaly
298.8558°
Eccentric anomaly
298.799°
Mean motion
3.79844 °/min
Orbital period
94.78 mins
BSTAR
0.00015258
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-26 23:48:23.053Z | 156.727° SSE | 2026-05-26 23:51:23.053Z | 115.629° SE | 40.171° | 2026-05-26 23:55:23.053Z | 354.594° N |
| 6 mins | 2026-05-27 12:54:23.053Z | 8.129° NNE | 2026-05-27 12:57:23.053Z | 221.414° SW | 42.743° | 2026-05-27 13:00:23.053Z | 197.29° SSW |
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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